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Document Information 

Document # RPP-24544 Revision 1D 

Title 

DEMONSTRATION BULK VITRIFICATION SYS 

INDEPENDENT QUALIFIED REGISTERED 

PROFESSIONAL ENGINEER (IQRPE & RCRA DESIGN 

REVIEW PACKAGE 

Date 05/11/2006 

Originator SHUFORD DH ORG CO CH2M 

Recipient Recipient Co. 

References ECN-723118-R5, RPP-24544-R0, RPP-24544-R1, RPP- 

24544-R1A, RPP-24544-RIB, RPP-24544-RIC, EDT- 

821657, ECN-723118-R0, ECN-723118-RI, ECN- 

723118-R3, ECN-723118-R4 

Keywords SUPPL TREATMENT 

Projects

to 

4 a 

S> 

0 

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v

DMJM H&N AECQM 

RPP-24544 REV Id 

Page I of 12 

• CALCULATION COVER SHEET Date: 03-25-2006 

0 

• 

Calculation No: 145579-D-CA-056 

Calculation Title: DBVS OGTS Bypass System Thermal Hydraulics Analysis 

Project No. & Title: 145579 - Demonstration Bulk Vitrification System 

Design Verification Required: ® Yes q No 

Calculation Type: q Scoping q Preliminary ® Final 

q Superseded by Calculation No: q Voided 

ORIGINAL AND REVISED CALCULATION/ANALYSIS APPROVAL 

Rev. A Rev. 0 Rev. 1 

Printed Printed Printed 

Name/Signature/Initials/Date Name/Signature/Initials/Date Name/$'gnat re/I tials/Date 

r 

Originator: John Irwin John Irwin 3 a5 

Checked By: Jack McConwell Jack McConwelI ckZK Conwe Z 

Approved By: Kurt McCracken 

Other: Kurt McCracken Kurt McCracken 

Document 

Number 

AFFECTED DOCUMENTS 

Document Title Rev. 

Number 

RECORD OF REVISION 

Rev. Reason for Revision 

A Initial Release 

0 Comment Incorporation 

1 Comment Incorporation 

Responsible Discipline 

Lead Initials 

ATTACHMENTS 

Attachment # Title Total Pages 

1 DBVS OGTS Bypass System Drawings 17 

2 AFT Arrow Model Input and Output Files 46 

3 OGTS Bypass System Fluid Flow Model Input Data 22 

4 Equipment Data Sheets 8 

5 ASHRAE Fundamentals Duct Fitting Loss Coefficients 32 

Total Calculation Page Count 138 

Form EP 3.3-2F. April 2005 

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AEC®M 

Calculation No 145579-D-CA-056 

Rev. No.: I 


ORIGINATOR: John 

Project Number: 145579 

Page 2 of 12 

irwin //,,^^ 

Calculation Title: DBVS OGTS Bypass System CHECKER: J kMcConwel `3-2G 

Thermal Hydraulics Analysis 


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Page 3 of 12 

ORIGINATOR: John Irwin'1% 03-25-2006 

Calculation Title: DBVS OGTS Bypass System CHECKER: y ack McConwell 


3--eC vC 

1.0 INTRODUCTION 

The Demonstration Bulk Vitrification System (DBVS) will be used to demonstrate the 

bulk verification process on low activity tank waste. Waste is retrieved by a Single-Shell 

Tank Waste Retrieval System and then delivered in batches to the DBVS Waste Staging 

Tanks. The liquid waste is dried and then transferred into a process system including an 

in container vitrification station (ICV box). The ICV box is ventilated by an Off Gas 

Treatment system (OGTS). The OGTS has an emergency backup exhaust system, the 

OGTS Bypass system, which is connected to the ICV box through a piping connection on 

the main OGTS ductwork. The OGTS bypass system consists of HEPA filters, fans, air 

bypass filters, valves, heaters and piping. When required following a loss of normal flow 

to the ICV Box, the OGTS bypass system is automatically valved in, to provide a 

negative pressure at the ICV box and transfers the process gas to a HEPA filter and 

• finally into the main OGTS exhaust stack. 

1.1 Purpose 

1.2 Scope 

2.0 Basis 

This calculation provides a thennal hydraulic assessment of the OGTS Bypass System. 

The OGTS bypass system air flow rates, system pressure losses and temperatures are 

determined during its expected normal operating conditions. 

The scope of the calculation is limited to the determination of the system flow rates, 

pressure losses and temperature in the piping and components from the ICV box to the 

OGTS exhaust stack. This analysis will determine the fan/system operating point; assess 

the operating pressure in the ICV box (insuring a negative pressure is maintained in the 

ICV Box) and predict the temperature of the piping from the ICV box to the OGTS 

exhaust stack for normal flow conditions as specified in Section 2.1. 

2.1 Design Inputs 

1. Component and pipe lengths are derived from the project drawings listed in the 

reference section and contained in Attachment I of this report. The Bypass 

• system ducting is schedule I OS (8 inch and larger) and schedule 40S (6 inch and 

smaller), stainless steel pipe, A312 type 316L with surface roughness as specified 

in Crane 1988. 

1-'om EP 3.3-21'. April 2005 

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Calculation Title: DBVS OGTS Bypass CHECKER: 


Page 4 of 12 

ORIGINATOR: John Irwin 03-25-2006 

2. The process conditions for the ICV box are as defined on the DBVS process flow 

diagram, F-145579-00-A-0021. The ICV Off-gas Exit Temperature is listed as 

875 °F. 

3. The maximum ambient temperature 115°F, HNF-SD-GN-ER-501. 

4. A nominal air flow of 750 acfin was specified based upon a preliminary 

engineering assessment of commercially available fans suitable for the OGTS 

Bypass system 

5. All isolation and control valves were assumed to be Keystone butterfly valves, 

with the Cv flow parameter as provided by the manufacturer (See Attachment 4) 

for each size of valve and its relative open position percentage. 

6. The HEPA filters were assumed to be Flanders filters with pressure drops 

provided by the manufacturer for similar applications (See Attachment 4). Clean 

and dirty filter pressure drops were utilized for the various parametric models. 

7. The fan characteristics were as provided by the manufacturer for a New York 

Blower Company Model 1508 (See Attachment 4). 

8. The pressure drop characteristics of the Back draft damper were as provided by 

industry test data (See Attachment 4). 

The flow loss coefficients for the standard piping components of the system were 

determined using the ASHRAE Fundamentals (Attachment 5). The ASHRAE 

duct fitting flow loss tables were utilized to calculate these loss coefficients for 

standard fittings, including elbows, wyes, transitions and miscellaneous fittings. 

10. The site elevation at the 20OW area location for the DBVS of 662 feet was 

utilized to determine the local atmospheric pressure. 

11. The flow loss coefficients were added to the pipe loss model within the AFT 

Arrow model for each pipe segment as required by the physical layout. 

12. A main input to the flow model was the heat transfer boundary conditions. The 

AFT Arrow model requires an input for the external heat transfer coefficient for 

• the pipe system being analyzed. The external heat transfer coefficients were 

calculated from standard correlations found in the Holman, 1990. The simplified 

McAdams air correlations, found in Holman, for natural convection from a 

Form EP 3.3-2F ; April 2005 

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Calculation Title: DBVS OGTS Bypass System 




Page 5 of 12 


CHECKER: ckMcConwe 3-2C -ce 

horizontal cylinder was used. In addition, heat transfer by thermal radiation from 

the pipe external surface was accounted for by using methods defined by Holman, 

1990. A combined convection and thermal radiation heat transfer coefficient was 

an input parameter for the AFT Arrow flow model. The calculation of the 

external heat transfer coefficient is contained in Attachment 3. 

13. The pipe internal convection coefficient was calculated by AFT Arrow using the 

standard Dittus-Boelter correlation for forced flow. The thermal properties of 

stainless steel were provided for by the AFT Arrow database to calculate the 

conductive heat transfer through the pipe wall. 

14. The ICV box and the OGTS bypass system were given an arbitrary elevation of 0 

feet relative to the project site elevation. Elevation changes and thus air density 

• changes have third order effects on the results of the analysis, and therefore were 

neglected. 

2.2 Assumptions 

1. The process fluid was assumed to be dry air with temperature dependent 

properties that are accounted for by the fluid flow modeling software database of 

properties, including non-ideal gas behavior. 

2. For the condition where flow from the ICV box is through the Bypass system, a 

nominal mass flow split of 60% through the air inlet bleed path and 40% through 

the ICV box is to be utilized in the flow model. This will configuration will 

match the normal OGTS flow through the ICV and is anticipated to produce a 

vacuum at the ICV box within its normal operating range. 

3. Worst case ambient conditions were assumed for conservative prediction of the 

heat loss from the bypass piping. An ambient temperature of 115 °F with no wind 

was assumed for all external heat transfer effects. 

4. The thennal emissivity of 0.6 was assumed for the stainless steel piping, no 

piping insulation was assumed. The emissivity chosen is conservative with 

respect to "as received" or oxidized stainless steel piping typically used in 

construction (Irwin 2000). 

• 5. The HEPA filter pressure drops for dirty filters was assumed to be twice the value 

of clean filters, for example, the main HEPA filter element has a clean filter 

Form EP 3.3-2F ; April 2005 

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•- ORIGINATOR: John/ 

Rev. No.: 1 ' 


Page 6 of 12 

03-25-2006 

Calculation Title: DBVS OGTS Bypass System CHECKER: ckMc 


onwell 3- Z.- v c, 

pressure drop of I inch w.c„ the dir ty filter pressure drop was assumed to be 2 

inches w.c. 

6. The ICV air inlet was assumed to be 60% open screen with a rectangular right 

angle rain cap. The flow loss of this component was modeled using ASHRAE 

flow loss tables. 

3.0 References 

I AFT Arrow Compressible Pipe Flow Modeling, Users Guide, Version 3.0, 

Applied Flow Technology, 2005. 

2. ASHRAE Fundamentals, 2005, Ame rican Society of Heating, Refrigerating and 

Air conditioning Engineers, Inc. Atlanta, GA. 

3. DBVS Drawing F-145579-00-A-0021, Rev. OJ, "Full DBVS Feed Preparation & 

Melt Process Flow Diagram." 

4. DBVS Drawing F-145579-00-D-0002, Rev. J, "Bulk Vitrification Site Layout 

Plan." 

5. DBVS Drawing F-145579-00-D-0008, Rev. D, "Bulk Vitrification Off-Gas and 

Elec. Trailers GA." 

6. DBVS Drawing F-145579-35-A-0100, Rev. P, `Bulk Vit rification ICV Box 

P&ID." 

7. DBVS Drawing F-145579-36-A-0108, Rev. F, "Bulk Vitrification OGTS Bypass 

P&ID." 

8. DBVS Drawing F-145579-36-V-0001, Rev. H, "Bulk Vit rification Off-Gas 

Treatment Plot Plan." 

9. 

DBVS Drawing F-145579-36-V-0003, Rev. K, "Bulk Vitrification Off-Gas 

Treatment Melt & D ryer Lower Plan" 

10. DBVS Drawing F-145579-36-V-0006, Rev. H, `Bulk Vit rification Off-Gas 

Treatment Wet Scrubber Skid Plan." 


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Calculation No 1 45579-D-CA-056 

Rev. No.: 1 

Calculation Title: DBVS OGTS Bypass 




Page 7 of 12 

ORIGINATOR: John Irwinn/ 

203-25-2006 

/ 

3 ?C-r-:6 

CHECKER: cJ6kMCCo ell 

11. DBVS Drawing F-145579-36-V-0007, Rev. H, "Bulk Vitrification Off-Gas 

Treatment Scrub & Stack Plan." 

12. 

13. 

14. 

DBVS Drawing F-145579-36-V-0028, Rev. K, "Bulk Vitrification Off-Gas 

Treatment Melt & Dryer Section `C'." 

DBVS Drawing F-145579-36-V-0029, Rev. J, `Bulk Vitrification Off-Gas 

Treatment Melt & Dryer Section 'U." 

DBVS Drawing F-145579-36-V-0030, Rev. J, "Bulk Vitrification Off-Gas 

Treatment Melt & Dryer Section È'." 

15. DBVS DrawingF-145579-36-V-0031, Rev. G, "Bulk Vitrification Off-Gas 

• Treatment Wet Scrubber Skid Sections." 

16. 

17. 

18. 

19. 

20. 

DBVS Drawing F-145579-36-V-0033, Rev. H, "Bulk Vitrification Off-Gas 

Treatment Scrub & Stack Section." 

DBVS Drawing F-145579-36-V-0034, Rev. H, "Bulk Vitrification Off-Gas 

Treatment Scrub & Stack Sections." 

Crane, Flow of Fluids Through Valves, Fittings, and Pipe, Technical Paper No. 

410, 1988, Crane. 

HNF-SD-GN-ER-501, Natural Phenomena Hazards Hanford Site Washington, 

Rev. 1 B, Fluor Hanford. 

Holman, J. P., Heat Transfer, 1990, McGraw Hill 

21. Idelchik, I. E., Handbook of Hydraulic Resistance, 1996, Begell House 

Publishing. 

22. Irwin, J.J., Thermal Analysis Methods for Safety Analysis Reports for Packaging, 

WHC-SD-TP-RPT-005, Rev. 1, 2000, Fluor Hanford Inc. 

4.0 Methods 

The OGTS bypass system thennal-hydraulic calculations are performed using AFT 

Arrow Version 3.0, with inputs provided from the MS Excel spreadsheets 

Form EP 3.3-217 ; April 2005 

A5-469

DM)M H&N, AECOM 


Rev. No.: 1 



Page 8 of 12 

ORIGINATOR: John 03-25-2006 

Calculation Title: DBVS OGTS Bypass System CHECKER: J Mc -W-e^ 

Thermal Hydraulics Analysis_ 

(Attachment 3), manufacturer's data (Attachment 4) and selected ASHRAE 

Fundamentals duct fitting flow loss tables (A ttachment 5). 

The AFT Arrow program was utilized for analyzing the one-dimensional compressible 

flow in the OGTS Bypass system piping network. Temperature dependent thermophysical 

properties of prescribed fluids are accounted for in the AFT Arrow program's 

database. Non-ideal g as effects can be accounted for in AFT Arrow by the use of a 

suitable thermodynamic equation of state. AFT Arrow utilizes the Redlich-Kwong 

equation of state to account for compressibility effects. The AFT Arrow pro gram only 

models steady state conditions. 

The cases analyzed by the AFT Arrow model are listed in Table 1 for the selected fan 

case. The major consideration is the operating pressure drops of the clean and di rty 

• filters. Clean filter pressure drops are as specified by the filter vendor per data in 

Attachment 4. The di rty filter pressure drops are based upon past Hanford expe rience at 

twice the as received filter pressure drop. 

Table 1. Bypass System Selected Fan Cases. 

`^ r 

Gase 

No 

ICV Boz IIEPA &rass;IIDPA BYliass Inlet 

'y Fylfer TrilY^r„f3^r,^0^, , Bleed FilteF, € 

(35 N4Z 010) g23111IIj ^, (6 702134) 

,Coe niiron ' ,: Gogdition; , , s' Co nditror( 'rff--; . 

TGV/)nlet 

Bleed-Mass 

Floyv Ratro 

" 

Iso Value, 

Posrhon (^V ,' 

^ 9011902)^^ i 

° ; 

1 Clean Clean Clean 40/60 100 

2 Clean Clean Clean 0/100 0 

3 Dirty Dirty Di rt 40/60 100 

4 Dirt Dirt Dirt 0/100 0 

The second consideration for the paramet ric cases was whether the system was in 

standby, i.e. no flow from the ICV box to the Bypass system but flow through the Bypass 

inlet bleed filter. The initial case was for flow both through the ICV Box, with the main 

OGTS isolated, and flow through the Bypass inlet bleed filter with all HEPA filters 

having their clean pressure drops. The Bypass inlet bleed filter flow w as set to achieve a 

nominal 60/40 mass flow split between the inlet bleed flow and the ICV box flow. 

AFT A rrow has been previously verified and validated on computer #DMJMH+N 

• 102514. MS Excel is a general purpose spreadsheet program. 


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Calculation Title: DBVS OGTS Bypass System CHECKER: A McConwe l C 

5.0 Results and Conclusions 

The AFT flow model results are categorized by the assumptions on the condition of the 

three sets of HEPA filters (ICV inlet HEPA, Bypass system main HEPA and Bypass 

system inlet bleed HEPA) in the system and the assumption on the flow split between the 

main bypass flow from the ICV box and the flow through the inlet bleed filter. The 

HEPA filters are defined by the condition of "clean", i.e. the manufacturer's stated 

pressure drop for new filter elements, or "dirty", the maximum expected pressure drop 

during operation. 

5.1 Results for the Selected Fan Cases 

For a nominal flow of 750 ACFM at the fan and an 8 inch mainbypass line with 875 °F 

ICV outlet temperature, a fan was selected to achieve this flow rate with a static head 

capability of approximately 15 inches w.c. A NYB fan, model number 1508 was 

determined to be acceptable for this application. An evaluation of the selected fan was 

performed. The following results (Tables 2, 3, and 4) were determined by the AFT 

Arrow flow model. 

Table 2. ICV Box Pressure with the Bypass System. 

1) Inlet bleed valve position set to achieve a nominal 60% of full fan flow through the inlet bleed 

filter when the main bypass line is open to the ICV box. 

Form I P 3.3-2F, April 2005 

A5-471

0 

11 

DM)M H&N ( AECOM 


Rev. No.: 1 


Calculation Title: DBVS OGTS Bypass System CHECKER: /^/ 

lr „3s^fir r y a 

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ORIGINATOR: John Irwin i/, 

Table 3. Bypass System Air Flows and Fan Conditions. 

(± < 5. 

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a 


Page 10 of 1 2 

06e 

1 344 517 13.99 3.2 617 

2 0 676 15.76 2.6 807 

3 277 1 428 14.25 3.0 582 

4 0 635 15.79 2.4 758 

Note: 

1) Flow is at the Inlet HEPA filter, 36-NO2-010. 

2) A nominal fan efficiency of 67% was assumed based upon vendor data (attachment 4). 

3) Pipe Flow Velocity is the minimum velocity within the OGTS Bypass line. 

Table 4. Bypass System Temperatures. 

Note: 

1) AHeat Transfer Ratio of I means there are no fins on the pipe for enhanced cooling. 

5.2 Conclusions for the Specified Fan Case 

03-25-2006 

-3 -2c.-c,e 

The selected fan, NYB fan model 1508 (Attachment 4), will be able to achieve the 

required flow rates through and pressure in the OGTS Bypass system. The expected 

temperatures at the OGTS Bypass HEPA filters are less than 250 °F and therefore 

acceptable. The throttled condition at the air inlet bleed valve, with a Cv value of 300 or 

approximately 45% open, is acceptable for this valve. 

Form EP 3.3-2 17, April 2005 

A5-472

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I 

Calculn atioNo 

145579-D-CA-056 

Rev. lati 

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ORIGINATOR: John Irwin 


Page 11 of 12 

V03-25-2006 

Calculation Title: DBVS OGTS Bypass System CHECKER: ackMo nwe êC-0C 


6.0 Calculations and Analyses 

M 

The AFT Arrow model, as shown in the figure, considers the process loop as follows: 

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The drawings used to develop the AFT physical model are contained in Attachment 1. 

The AFT Arrow Input and Output Files for the various cases analyzed are in 

Attachment 2. Attachment 3 contains the flow coefficient and physical configuration 

input data for the AFT Arrow thermal hydraulic model. Attachment 4 contains the 

manufacturer's data for the butterfly valves, HEPA filters and fans that may be used in 

the OGTS Bypass system. Attachment 5 contains p rintouts from the ASHRAE 

Fundamentals, flow loss coefficient tables. 


A5-473 

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Page 12 of 12 

ORIGINATOR: Jobn Irvin 03-25-2006 

Calculation Title: DBVSOGTS Bypass System CHECKER: c Conwe 3 


• Form EP 3.3-2F. Apri12005 


A5-474 

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DMJM H&N ( AECOM 

Calculation No. 145579-D-CA-056 

Rev. No.: I 

Calculation Title: DBVS OGTS Bypass System 

RPP-24544 REV id 

A tt achment 1 

DBVS OGTS Bypass System Drawings 

A5-475 


Page 1 of 17 

ORIGINATOR: John Irwin 1 03-25-2006 

CHECKER: ckMcConwel 3-2G—r'^

• 

• 

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RPP-24544 REV Walculation No. 145579-D-CA-056, Rev.1 

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FWM:Air 

Max FIaH TemperaMre Dab= 1000 deg. K 

Mb Fhld Weight 2 Data=200 tlag.K 

MobconsWeigh1=8. ass l emu 

Gas w PSessure655 son 

Critical Pmssure ^T.25 Z4 

Acerkc Fa m r 3241 deg. K 

Acentri Factor =0.021 

Equation of Slab+ h ralloy 

Specir lo Aomrs 

SpedOC Heat Ralb .=14. 

Ae Heat 

i psia 

Gravbt dc Pressure= 14.3 Aia 

GYavitaidAcc SldaRmh,14.69 1 g 

rd Remh, . 6 ode, F 

Stan eodard JIMAbmre=0deg 

Turbul ent Flow owa ye . NN 

bare-2 -4000 

la minar flow Below elow el ReY^wlds umber--2300 

Roe lop tT ble 

h _ 

Pipe 

.,_ t 

Name PRD¢ LergU Length I y limet Hyd j 

Defined I I Oamel 5 . D am. UAs 

.P pe ... Yes_ " , nches 6065. 

ochIe¢ 

W Se 

D.ata Set 

Unspecified 

Roughne s Roug hness . n 

, Has Us 

_ 0.00151 feet 

Losses (K) IMIIN FlOw 

283.. 

2 PipeI Yes 1 04 • inches! 6.001 iW,esl Unsm,ified O.00D151 

fee 

l_ 0.21 

3 3FFS Yes 163! inches! 4.028 Inches Un dfiedl 0.000151 feet 1.635 

, 

.. _.? Poe Yes 39 Nclgs 6.065! ches (Mmeafietl 0..00015 k_etI 0.16 _ ...... 

, _0 Pipe _ Yes 22t, indês 4025;,., ches _Unsyeafietl ¢00015 feed D32 

6 R Yes T2f IncM1eS 60651 GIs Uns afied' 0.0015 feet! D.15 

R e Yes. 141.5' bd19a 5.047 i ind e. Uns edfed'. 0.00015 feet! 0.47 

-_e "., 

9 

R 

Rp¢ 

_. Yes 

._. Ys 

6.. Indies 

105' Fdgms 

8065' 

6065, 

they Unspedr 0.00015 feet 014 

... 

nches Unspeafod 0.00015 

...__ 

fear 

..__._.. 

D" 

',. 

10 

1t 

12 

Pi el Yes 

RDgI_ ___Yes 

Rpg _ Y 5 

8^-inches 

8 oche I 

12 inctws 

6065 

6065_ 

6.065 

inches 

Gres 

mohas 

Un edfied 

Unspe fed 

Unspeaf d 

0.00015 

_ 0.00015 

O.DDIs 

feat 

feet 

_feet 

0.05 

_005 

t 227961 _ 

13 P' a Yes 251. "aches 8329 aches Uns elect 0.00015 leaf 039. 

j _ib top. 

., Yes 1969 ), cM1es 6329, toes Unspenfetl 0.00015 feet OTII.".,,___ 

IS i Pipe _... Yes 2715'_aches 8329_ _ mches^ Uwpeafied 0.00015 feet 1.32i 

16 Rpe Yes 18 . Ineh¢s 8329' ches! Unspe fetl 0.00015 feet 0,43j, 

17 Roo Yes. 12inrU¢s 8.329 n¢hes^ Vnz 'led D.00D15t feet 0.111 

_ 

_ 18 

19.! 

Rpe _ Yes _ 42... nOos 

Rpe. „, , Yes .12." IrtMa 

8.329;, . ,., 

0.329,;,. 

ndes I ^nso- a ed 

ndues . Wepe ofietl 

O.o9O151 

0.00015 

feet 

/eet, 

0.17 {" 

01 

20 Roo Yes $64 inGms 8.329: indlas Vre efifred 0.00015 feet 2.04: 

,. 21Rye. .____Ye 

22 Rite Yes 

104__ nchss 

6. _nqhes 

1239- 

8065: 

i1l a 

iNes 

Unspevtied- ., 

Unspeafied- 

000015 

0,00015 

feet, 

feet i_ 

1421.. 

004__"" 

23 Rpe _ Yes 260__lnrAes 60&5!, lnNes__UnsDeofied- 000015 ,.feel, 08/I 

A5-494

E 

0 



Attachment 2 

Page 4 of 46 

AFTArrow 3.Otepul (2.fs) 342MODe le,.0 AM 

DWMH 

AFT AIM Modal, OGtS Bypass System T-H Model Case I (Clean FftM NY8 t 50 1 3. 115 TAblett HT) 

Hydmek URIT 

laseOesse 

I R.=. Usses (K^ ) 'n 

0 linlitJOSS Fl. 

-4--- 

30 r 

31 

PipO 

Real 

Yes! OS` 

_w- Yes'_ 05! 

fee d 

fgpj t 

5.041 

4^.^ 291 

unspq5i;d, 

tq4 h&! 

0.. 

O.00DISI 

I 

-1 

Piper Inblal Floss Jubwom GeoneUy matedai size Type Thermal 

Eounda^ 

Aelblera Tang. 

6wb schedweQ AmbbalLci.- 

Z3 CYMWm1 Rpo I -61e^ - wbeddg^_Adabaticl 

3 

4 

__ ,.k11,gyN 

p. 

CyfnqkfgApIpA j!W 

inch . schedule, 40 --- 

6 _Inch. sdl ted.T.40 

5 

6 

516 calm 

6.7. CyNnddcalPive 

Umedfied' 

Sla =Steel ! 61rwh scheckie 40 GenvalHostTransfew 115 

r 8 

------ ------ -- 

a 9 : 0y6rAr^f- 

— -------wl-^ lf 

115 

9 9.10 CAndripi Roo Shch schecula 40 Gaeeral Heal Trange,; 115 

io 10,11,: CyETM ggmpe ,. t qssSteW . 61nW _sMedu1040 --qamral Heal Transfer_.__,_.. .-Al§ 

WNSUIe Q 

_A_Traqufa,, Als 

12,11 CY11nd4calRp. Stainless Steel: 6 in s aduw4o Genend Heat Transfer; 115 

._13 ........_ 

...... . ........ 

lc allp. ___115 

15 _sOedAejO Oweral Heat TramfeI4 115 

16 

1 .7 .... 

18 

__„ IS16- 

AV 

tT 18 

S mlosssle2! 

-22LOmfiteel 

CyfeWnrat Pipe) _Sty( less Steel 

Ain.h . _jqtAdOaIQ .. jpL Ffqaff,..fe,^ 

SL h uNUM l0 , 

Binch schWlajD General Heal Transter 

115 

§ 

19 ClftdulvBM-SA t . - - Go - - ôq I Ho st -I^qare^ -11 5 M 

7 

...... 19 20 

n. 23 

GygndflmdPipe SWOMStoof 

cymimpR^moa stainless 

8iAr 

; 2 iw;l 

=heftfolO Gsnon4lia.tTra^sw 

l&AJ 

Adaeafi 

1 

1151 

— 

i 

23 ' 

_30 

31 

21 13 

830 

CY."WELIP M- -ft L ^tsjnIm_SLW 

Cyl MricN Pipe t , Sbmtess Steel: 

i 

5inch 

ainr l 

schedule 40 

schedul 

.... 

Adiob.fic 

Adiabatic 

Pipe AmdentTemp. Special - 

I. _, Units .. Coalition j 

I 

2 No n. 

3 No e' 

None 

5 

6 deq. F Me. 

deo:Fl Nine 

a ds o . F; Nme 

9 cl.qF' None. 

10 deer F i None- 

1l dm. F : Nwe 

12 dog, F 1 ot 

13 i dog. F uwe 

14 deg: F m"I 

is I d.Q- F None, 

16 dw, F 

17 d". F , t4one 

18 deg. F: 

1__ deer. F 

20 deed qq.,i 

jl . 

Am.. 

2t _ None 

Nona 

23 None 

A5495

• 

RPP-24544 REV 1d Calculation No. 145579-D-CA-056, Rev.1 

Attacbment 2 

Page 5 of 46 

AFTAnSnItU1nput - (3or8) 3/25r2M 10.22 AM 

oww.N 

AFT Arse Model, OGTS Bypass System T-H Model Casa t ( Clean Fkless, NYB 1508, 115'F AmNee, Nn 

. Plpe Amblart Temp. Spe cial 

:..._^._. Urufs......^COn4M4 

Novel 

F LOSS Table 

tripe i. K Tatat SlarMard Mitre Smm1M1 Ar^ya . -Ball. eukelky CyAder Gate Gbbe Piug Poppet I 

j . LOSSe;^ _._._._.BeMS_._. eands__Berds ,_VaNe;_Valv_es Valves _Valves Valves _, Valves Vahxs„,Vale_as_ 

12 1.23 110.1311 

13 0.11 

I_. 15 7:32 

21 1.42 

22 

0.04 

_.. 23..._...._,0,.7/ ..... .. .. .. ^. _. _._ _ . ... . .........._^__..._._. ...._._.. ..._._...^_...._..._^... ._.__ 

Mee Three,my g Disc StoP Check ; Sh Conaacilom Eepambns 

La seas V.W. Valves i Valves Check Valves Valdes Odkce i Or10ee i 

13 

... 15 t. .._.. .... ._;. .. _....__ f _..” _ .......__. _____._.__._. _.. .. _._.. 

_.:.. 21 ._... ......_ ...... .. ...._.. _. _._._._ - 

22 

23 

Fipa Entrances Evitaoiffe ren0al Honeycomb Sveen Tea - Atl01 LOu 

locus Fbwmeler .. 

13 . _ ..... .... .. 10,11) 

15 I 1 1.1 0.22 

._1 

_110.04) 

_ 22..... 

2J 0.11 

. 

Area Cbar!ae Table .__ .._. 

. At¢a CM1ange Name Object 

Defined 

... 3 .. ....... Area Change l Yes 

d - Area Change! Yes 

5 Area Charm. Yes 

.. .. _. _ ._ 

De align Bavarian I Init2lP ressureIm Pressu Pressure reDatabase . Type Geomeby 

Unls Units Source 

_. _P .... feed . ... 

.!: Co wal _COn12Gan_ 

0 feet! ; Con WIC_ Expansion 

_ 0 feet Co '. Conbacdon 

_., T .' Area Chan:_ . _. Yes ...A feet _. Coaifall,COnVacuan- 

A re a Charge' Angle Loss 

Fader 

3 V. i 0.4399 

_ 4 22.0.1562 

S V.1 0.4404 

T 28, i 0.1241 

C.Meresser/P.. Table 

Canpressw/Fan Name00jec[ ! El.-Hea Elevalim Irvlial Pressure Initial Pressure i Da labasa : Speeal 

i OeOnatl _ Units _ 

tMks Saae. Cosliton 

17N31-130' 

_. ..... .. ... 

ComPressorffan Pa P 

Yas B feet 

._ 

"n Fla. Design Plow Cerre t . 

..... 

Indepemte t Ind Variable 

NMe 

_.._... _. 

oeperdent 

T Rat Rat. Unls Conf!oaralon Variable Un'h Variable 

1 7Comp/Fan LL ,. . _ VoI FIOW Rafe' ._h3/min Pressure loss_! 

A5-496

u 

E 

RPP-24544 RFV" a Calculation No_ 145579-D-CA-056, Rev. t 

Attachment 2 

Page 6 of 46 

AFT'Mww3.01npu1 (4of6) 3 25120 0 6 10:22 AM 

DMJMHaN 

AFT Mow ModN, DOTS Bypass System T-H Model Case I ( Clean Fillers, NYS 1508, 116'F AmbiwL Kr) 

ComplesmdFen Dep.Variable ICornpJF.Csys . Complfan Curve j ConVOan Cures OwvJFan Cw l CdnpJFen Curve 

NNts. Constanta _'_ . _ . COnslantb .(_ ConstantD ,.. _. ConatantA _ y_COnstanle 

17 es H2OStd 1246429: 2S71420E-03i 2286714E416 Oj 

__r.__._...__._._...._____ ..___,.__.___._..._........ —__. ..__..._.. 

Compm55or/Fan ; RVnRat Flow R atel Flux : Atld In Press.: Speed 

Go" Men C 

0 

^_.._ t] 

Rate ^ Rat UNh 

__: __........ _......... ... i. 

TvDe ' Disdiar4e 

[' 

. Slak_ . . 180 .___. 

pisih nÛ Ills ' Ez 

pnaee 

dedOhr 

._.... __.Adabak- 

ead End Table 

Dead End Name Object Pietallon i Elevation ' Irdtal Pressure : I nitial Pressure Database 

Dolled i I Drvt4 Units Sowoe 

30 To Main OGT9.. Yes: 01 - fee. 

31 '. To Train B HEPA'. yes; 0' feet` - 

Ggnenat Qom tT 

General Component Name Obled '. Elevation Eleva tion In111a1Pressure IniSal Pressure Database Special 

___ _____._._.._ 

'2 

.__.. ........ ..._. I Defined 

HEPAFdter NO2-010 Yes 

...Units 

0 - feet 

_......_._._...._.....UNIS..._ _Source ... COnd_lon t.. 

Nonet6 

HEPA FBIer1361i37 Yes' 0 feet Nona 

16„.. Backdra6Darrêr Tes: ... 0 feet __...__._ ..__None; 

22 HeaterBHEPAFi!ftn Yee, 0 feat None 

General Component Lois toss IedependeM IM. Variable Dependent Dep. Varwde Loss 

Yell Variable Units ..Variable _Units Constanta 

2 Geneml OMiMi Variable Vd: Flow Rate 93fmin. Preswr6 LOSS In. H2O rid. -1.165517E-17 

^ 16 _, _,_^ GOneral Polynomial Vanable . Vol Flow Rate.._ fl3fmm_ Pressurekp al _. n. H2O dQ 3534699E-I] 

18 1 QeneralPdynomial Variable Vol Flow Rate _ ft3fvan Presaura Loss n; 142O aid 7023.761E-02 

%.. .. 22 _ _^ Ger;e@I PO.lyrgmd Varable_,_ Vd FIOWR Ie__. A3tmn Prcu re lDSSI .0_1120 51d. 1_438568E4_7 , 

' Gerwml Component Loss Loss loss Loss 

- _ __ , 

Condant b constant p , :` GOnslant d Conelanl e 

2 I 0.00224 0; 0 0 

.. 16._ __.......826666E-03. 01 0 0 

18 1.687181E-04 3.4618E-OBi 0. 0 

22 0.001382 01 0 0 

HeatE cha a Table 

Heat E4chan” Name r s 

_ 

EI al on i E valwn r Wlal Pressure Initial Premn, I Da abase Spa al Type 

6CV Pkwm 

WObleed Yes D" 

u 6s I 

feet 

UNIS Source Condition 

None. 

HeatE burger Loss Lo55 Ind pe dent Ind V daWe Dependent Dep. Variable LOSS Loss Loss 

Modal Value. Vanable ,. Unte Varada - Unite Constanta ; Cprelantb Co 5lantc 

6 K Constant 1.5 

Heat EVGarger Ines - Loss 

Cmtslanld Comrante . 

6 

Tank T bl 

Naa t. Object 

..... 

Elevation Elevation 

_ 

Initlat Pressure Ini ti Tan Nan 

al Preswr I Database Preswre Preswre TemDeralure 

1 

20 

'. 21 

Oertned .. tlnle 

AM Preal _ Yes 0 feet 

Atm;R s lYes 0 feel 

AM Press Yes0 led, 

- 

Units Source 

_. iI .. _.. 

_ 

! Units 

143 psm 

1431 a 

143_ psial 

115 

115 

115 

A5-497

0 

• 

DWMH-N 


Calculation No, 145579-D-CA-056, Rev. I 

Attachmicnt 2 

Page. 7 of 46 

Mail) 

AFf Aimeov Masi OGTS Bypass Syslarre T-H hft" Casa 1( dean Mai NNTI ISM, 115 T 

i Tem, I Temxicat Balance Sailwas, 1 

i —T l 

Unh -- 1 Cncentrattere 

(mr,eirl) onpen) (neati i (pip s ") s ( pieam) 

KM, K (^& &I. 

T -ii^F a-----We 

21 I 0 1 No. 

Na' 1P21)0.01 

32580081022 W 

(Pl iem)l 

I I.* i (pipe #?) (Pipe #B) (Plee#10) (PlImAIII) (PIP012) (PIM013) 1 (Fime 014) : (INIMMS) 

I 

Ont . KIn, KQqt . ; ' KInKOut K R& KOW 10Int)(Oul Kh,,KOuI KJ9, K Out , KIA.Kw I 

I - _1.:: 

Tack' (Pipe '7) (P11#18) (Pipe, 01% (Pipe #2Q) 1 (Pipe RI) (Pipe #22) (Isme #M) (M,#24) 

, = .I Kip K'9 Kin K_ A ! '! : pyt t 15 Out KIQKÔql .. _J 0 , Clut K inKOw 

20 

Tank i (PtM#25) 

K M, K OW-D 

, 

21 

TcrW. Table 

T".,Wy.: 

Name 

F —i In 

9 . 

t 

i 30i 

13 45 

Is .135 

VaWe Ti ble 

Object I El.,ndaari ' 

M. San: Initial pireaces. Ini fiall',asans Database TeeMya, Lou 

Valve I Name Object Elevation Ele,mlim Initial Ressure Initial Presswe Database f Special ul Eici 

10 1 HV-901 Yea 

palmed , Uni.t. UnIts Skurce, Condition Valve P...'e, 

reasti I Nim. No 

12 HV-9021. Yes] 

------ - . "e, - No. , - ,. - 

15 YaeO^ Vas oestNo 

- 

No, 

23 V-1781 

ys'l 

Y.1 

a 

0 

0 

feet 

Iset I 

-- Non. 

None 

Me 

N. 

Valle -- iZ' 

CM CIA — Lo- s. Uss$ trajep Ind. Variable VariableDependent - D.p'. 'V LO- 

P'. 

' re ynaa4 . Variable ..LLnit. Variable .......Units , Constants 

1 . 0 

12 

1 

Ce Constant_ 1194 

Cv Oe 

11941 

-is 

Constant. 240 

19 ._ [ 

^qossumt^ 241,10 1 - ------- 

23_ 

Cv Constant.. 

A5-498

L 

1 

RPP-24544 REV Id Calculation No. 145579-D-CA-056; Rev. 1 

Attachment 2 

Page 8 of 46 

AFTM"&OMpW (606) 3I25R00510.L2AM 

DMJMN-N 

AFT Model,OGTS Byp.8ptemTat Model Casai(dear Fiilw4NY8150&115'FAmblwk" 

Va a Loss toss Loss Lass 

!.__. Cgnsfantb ^ Conslzntc, G?tSLte^.^ Constanla 

i 15 

19 

M 

A5-499

• 

• 

• 

RPP=24544 REV lot 

Calculation No 145579-D-CA-056, Rev.1 

Attaclunent 2 

Page 9 of 46 

AFT Anov 3.0OuVul V -M 32512008 

DM)MH01 

AFTArzow Mpdet.OGTS Bypass System T-H Model Case1 (elm FBers. NYB INS. 115' 1' Anbleni, ITO 

Title: AFTArmv MOdN,OGTSBypzss System T.H Mold Casa If Clean Files. NYB 1508,115 T Ambient, HT) 

Analysis run on: 312520 0 8 10:/ 236 AM 

Appgca0on version: AFT Arrow VeRbn 3 .0 (2005.09.14) 

. Inpu t FBe: MiOemons0ialm Bulk V1TIRscal Year 2006 Wer)(T.Wi ta8o resIOGTS Bypam Tlermat HydrauFa AndistsMork FBesSByposs Flow 

Inch Pipe Rav 1 Case tare 

Ezeation Tfo e= 1:46.98 (106.86 secerbs) 

Trial Number 0P,.asure Xeratles=5]3 

Total Nwnber Of Flow lwatfa s=-195 

Test Number a Enthalpy Itemdons= 195 

Number Of Pienn^ 25 

Number Of Juncuor s^ 25 

Mani. Method= Gaussian E knimubn 

LerIgl )i Mosul Solut ion Me0lod whh Mau! Number Umits 

Length Step Size= 12 Inches 

Maur Number lnnemenC 0.01 

Pressure Tole ance=0.0001 relative charge 

Mau Flow Rate Tolerance= 0.0001 relative change 

Enthalpy Tolerenca= 0.0001 realm change 

FHw R.IonationP (AatemaBc) 

Pressure Relaxation= (AUWrreBe) 

Res'stonce Relaxations = (AetanallC) 

Fluid Dalease: AFT Standard 

Field: Air 

Max Fluid Tempefature Data= 1000 deg. K 

Mn Fluid Temperature Dal.= 2000eg. K 

Muleatar WNgM1t=28.9] emu 

Gas Constant =0.061f55 BWObmR 

CritiW Pressure -3725 en 

Critical Tempemlure =132.41 deg. K 

Acentric Feet,=0.021 

EquaOOn of Sale- RediicRKwong 

Enthalpy e Pat Rain Aesuacy 

Specific Heat Ratio Accuracy=is 

Atmospheric ressure=46.3 Asia 

Gra dra d Pr Acceler l it 

Standard Pr lu 14.696 psis 

Stall., ard Fempeb 

W deg. F 

Tmbulenl 

Flow Above Reynolds Number= 4000 

Laminar Fbw Buaw Reynolds Number- 2300 

Total 

To ta Oufflow= 0.0.90 teals 

l outflo 0.9 273.25 

Total En ergy Innbw= 

, 210.4 Bads Blois 

Total Enegy OSfene 210A. S,V 

T xj Neal Transferred Into ystem=ots 

-62:]9 Bl 

Maumumet 

,meane 41[.35 pain at urie ion 

1 7 Outl 

Mininvm Pressure is 13.86 psis at JX dtelf I] Intel 

M aximum TempereNre is 8 75.0 de0- F at Jun dim 6 Oullet 

Minimum Basec iotic TempdaNre is 115.0 deg. F at Junctio.n 23 Outlet 

GenwassorNan Summa, 

Jet Name Mass Vot. OP OP Overall Speed Overall Comp. BEP CEP 

Fl Flow Slag. 51 be Effde 9' I - Power Ratio 0 Mass ^. 

Gm) (X31min),. (q H2O Sfd.) tin. H2O ML_(Perce I) j (Percent)___ LhP2 '^.(Pec, np , (RUsec) . (bWsec) - 

1 7 N31130i ]566 980.2 13.99 1399 6]401. 100.0 3151 :103.6, NIA NIA. 

__. 

Jcl %of 

BEP 

(Percent 

1/ NIA 

V.N. Summery 

A5-500

• 

• 

• 



Attachment 2 

Page 10 of 46 

AFTA1 100etW 

DWM-N 

A" AnO MoM, OGTS Bypass System T-H Model Cases( Clem Fiftein, WH 1508, 115 TArnblent. HT) 

Jet 

No= Valve Mess i OPS" Die Staft : P Staffe K V*n Ov C, 

TYPeI ^ 1 Inlet Slate Est 

1 

12 1N302 

REGULAR 

REGULAR 

(Pold) LO)sbI 

03122.11E.R.P9Z 0.00]043]_;___ 9^007D437 14.06; 

O.MW IXOW4217f 0.0004217 I0.06 : 

0 en 

Open 

1,194.0 

;194.0 

WA 

Fi^ REGULAR 0.96353! 0.00916W D.009IMi 13.96. 0.]]]O; Open 2,440.0 

191 V-167 REGULAR 0.96353! 0.0090172 1 0.0780265: 1433. O.PM; Ow 2.640.0 

23: V-i]B REGULAR WMi 0A 841163 ! 0.18429I8 1426 13.7426 1 Open 300 .0 NA 

JPl Name Mo. I op. !;Ô (41L eOCL. OT pId T9. Fj 

T I Heel 

Flow 

Me% nmDIn 

r0w)- -WO.. P: 

oq : F). L(gLoo-, 

6 ICV PIe_n0n1 1 03 048 .. Q04625 , 002933__-?W.G _114A _874. 2 

Pi Ou LT Me 

pip. 

N... Mass Vd. V.I. Vel. Mach hladl op S". P slaI,. 

Flow F AVq In Ow pin # Out Tool In 

M) -("Tti ...... __ . ..... on H2O std. (91) (in. 

3/2512006 

9)) 

`= 

Pipe M2.28 344.0 28.55i 1.7154 0.024385 0024417: 0.51497 N 0.0000 '.i 

NpA _3022841 ._N4 1.719 O= 

0.0918134 -U859 43n7W4 

3 3 FE. 302.28 M83 65A2 

1 2.0]11608 -1.4500 13.621116M 1 

30228 367.0; 23.82, 1,729.2 ; 0.024613, 0.024616: 0.0480714 4.6533 

6 

0.3658546 -3]]41!... 4.13991828 

6 F.P. 01455076 -S.4202 -5565693661 

7 Pipe 302281 71.1 13.71 5 5^265^61 2._L ''3 0637,, " 3 O":Nj 

0.]859]42 9742 -5.6118 1 -6.37]]8568 8568 

2 .0 60.18 

0.05!54101 

^! '.2 1 "W7 ! I 

11N 34 1 19.5; 49.12 2,9N.W D.0291^ 0.029074 : Q:^01113^1 1 

ZNFIYO 

10 Roe 1 246.241 IiE36.8, 48.N 2.9118A 0029086 0.029024 

6.6205; 6IW8305, 

57031 13T 7.0I IIA2 MOA 0006781 6781 0.008757 0. 0009239 ^-6.63031091. 

13 

7,p, 2_;_ . 5703 ^ 

Roo 302.28' 681.0 

ilA^ ..... ... 

31.72 1,06.8, 

Rqq§]5z. 

0.018944 

P-PORIP, 

0.017873 

-0-MIM 

0 .089807 1 

-q.650.0i 

--6 .63B31 

-.6 6.WV^ 66 

41.728117941 

14 Mool 756.85 l 1.078.0 51 53 2.606.4 0.05125 0.035D55 1.7142507 -6.74961 -8.523839001 

15 Ron 756.85 9793 43.44 2.572 .8 0.035055 0.034856 0.6301 54] 41.52381 -9.1 5399361! 

N P'pe 756.85 973.9: 42.911' 2.5714 0k348 79 0.034 877 0J5311 07 .9.40751 -9.56058025 1 

17 ±jM 756.65 980.5: 4320 2.690.8 0.035128 0.035122 0.0446396 -12.31291 42.357511521 

18 Pipe 756.65 959.8 42.32 2,533.2 0 03610 00311 L9 4a 

,62^ IiI1.56488]141 

19 

20 

211 

P^pm 

Pie 

Pip. 

756-85 ... 

]56.85 

454.56 

W7 

51618 

A2.25-. 2. 2,533,8: 

42.25 _L474 4 

10,29 617-4 

O.W4142 , AW41n 

0041153 0_033782 

0 .000784 I 0.008785 

0 1 !3423421 "-L 1 

0 .0336955 

129211 

342 

i.MW,1061 

-0.00002640 

I 

0.00001 -D.03389547 

22 Pipe 454.56 518.1 43.04_„_25826 0.036755; 0.036758 4)36996034 

23 FIM 454.156 525.2 52 43.W .619.^ O bnzw *^.Oim -6.41318607 

i 30 V." 0.0 000 Omw 0.0 0.00000 D 0.000000 o.wwm ;l .6.37781 EI.37778566 

31 R 0.0 0.0 0.00 

P I, P s tav^ P SI.U. d Step. T Stag- T StaI;. T Stafic fitim. Y"im7 sleI,. A sto-; , I 

In 

IN.1 

In 

fin.Wosw. OD (In. H2O 0" stI. fall Won. F) (deq, F) wu 0 l ! `; ! ) (d: F) Idm. R flhiAml uAb.) Ifthorn) 

__ .,Qj6W4 0.07883, 0.000" 

115.0 114.9 114.9 000000 M6.1 2N.11 

2 .. . .... __ 

I - - -1.!54198 ... 7QOqQ06l0WV "5 115.0 .0 11151 '50 "4 114.9 :9 :114.9^ O.NM 206.1 206.1! 

-3, Z.;;7.451 - - - -4.373101 .0 'ooloem 115.0 1150 114.7 .114.d 0.00000 206.1 2061: 

-3.81 644 3z8" 000000000 115.0 1150 114.9 1114.9 0.00000 2013.1 2013.1 1 

5 

6 

4.627" .4.9%1.2 

5.93728 

AOI 

49.51 

115.0 114.6 - 

874.6. 

1 -- 

825.1 

000000 

. 12.39,724i ... 

206.j 

493,A 

2061; . 

381.4, 

7 ]417__9241 __2068008 381.4 30,5: 

a 73.8.2 741.4* 737.9 A8]2461 360.5 1 359.7; 

A5-501

E 

• 

• 


Calculation No 145579-D-CA-056, Rev. 1 

Attachment 2 

Page I I of 46 

AFT b3.00ulplft Pals) 3126MOS 

D611MHxN 

AFTArrow Model, OGTS Bypass I (Chum Filtens.WM INS. 115"FAmbleid. HT) 

pipe 

P Stalk, 

in 

Is Staft 

Out 

dT Stag. T $Mg. 

east 

T Stag. 

Outlet 

TSbk 

In 

T$taft 

0, 

crH Stag. H Stag. 

In 

H Mag. 

Out 

1120hs el. (g)). 

dqg .,Fl (d Di(de,, _n^@MFL 

_(ElkAbyl)_ _Mhuffles 

.646to Ag^ ___ _ 

.2' 73&Of 731.0 _ .1L73454 .1.73454 - 

.6.8 

.6.11IN196 -52 S!slim7..; 1312 M O; 731.0 : ]25.8 -1.30798 

.9 30.6 

464974 .6.65059 -8.4614298: 73&2 729.7: 738.2 -2.10707 359.7 357.6 

13 

.SAMS 

$.73469 

-UnU 4 6.511691797 

428.618506859: 

m.7 

7239 

k^.2 g^7 7132 

, - 594.8 

-4.1=64 

41.96418 

:157.6 

356.0 

3514 

324m1 

-7.14175 14175 

.123.2612152t; 307.61 184,3i MILL I - 104m2 30.19798 2512 223.0 

16 

! Ô 

A73399 

.9.4 m9626177979; 164.3 

176.0 

1]5.0' 

174.5. 

184.2. 

174.0 

174.9 

1743 

-226422 

-0.13588 

223.0 

220.7 

220.7 

220A 

17 -12M6,1158 .42.68609 4,.36 3611 174mS 1741 174.3'1740 M..61 

Is I.30]35 1m24357 4 ,1818028 I"Li I 62.6 ; I84.0i IlmS -0 .38306 222.9 222.6 

19 

M 

O.wm- 

1),712118 

amift 

4.31385 

-0.4183349: 

.16,99127197 

182.6 

182.2 

1822; 1825 1 

-0.'0228 

165.2i InI "2.' 

222,5 

1 

, 

21 4005515 0.01:036621 115.0 

165.1 -:i.1111 

ismallso îl 5 0 0.00000 

222 

2m-1 

218.3 

mm 

-1.11905 -1.14094 

Its5 

M- : ... ... -6.24226 .- ^ -6.7 -5 

M 

4,37779 

-6.37779 

assostcsi. 

O.D(IG18828t 

0.00000000' 

115.0 

115.0 

741.7 

115.Oi 

115.0 

741.7 

114.8: 

1 14.8 

741.7 

114.8 O-ONOG 206.1 =I 

114.8.,.. _0.00000_ -_ ,_206.1 

_ ----- - 206 -- .1- 

741.7 0.00000 363'5 360.5 

31 .8.52384 -8.523114 0900600M. - I84 .3 184.3 1843 184 .3 0.000001 223.0 

p 

ipe --W^Muic 

âal i' 

In Out 

(BtWb,) (SIL 

s 

MO Rho Stag entat Heat Heat 

stall, In Out Model Flux Rat. 

f1 ornf(13) (lbeL 

(81evs-82) (Bous) 

1 

2 

206.0 

206.0 

206.0 

2DE3.0 

0.06719i 

0.066 

0.06711. Ad 

so 

0.00006 

0.00000 

0.00000. 

3 206.0 2M.0 0.06695: 0,06W Idiall UL al i GWGOO 0.00000 0.00000D. 

4 2()6D 206.0 0.06657 !0.05657 Adiabatic] O.ODWO D.NM 

5 WS.O: 2W.0 0.06655 0.06649 atuatic; D.ODODOJ 0.00000` 

-393.7: 31113 0 .02852 0.02961 Geall- leatTran. 460078; 4.77085 

7 38 I-2 MAL 0.02961 0.03161` GenI Heat Tmn. -0.51574 - 803633 

8 

9 

3605 3596; 0.03161 0.03170 Geal Heat Tran. 

3595357- L",1 

O.WIA NI i^. P^.032 OMJW 03188^, GenlHeatT,.n. 

-0.422911 

--a3 

079 . 1 ^q. -WIS-5 

10 357.9 

GanI Heat Tran. .0.38578 -OAD837 

11 359.7 

O 0.031611: 

Genl Heat Tran. -0.19269 1 -0.15298 

12 357.6 353.4 ; 0.2190 0.03235 1 Ga.1 Heat Tran. -0.1818551 8.29939 

13 356.0 324.01 0.03207. 0.03598 1 Gent IM.t1F., 

14 253.1' Seel Heat Tree. 

15 223.0- . I tT.. 0.04327 -2.1510 

is 

F I-7 

220.7 - 1 . 

220.6 

Go I Iran. 

3 - 

-OA31)92 

.0.08660 - 

-0.09855 

i -0,001]1 

0.00000 

0.09000 , 

0.00000 

._0.9000' 

a W! Hea. I Trae.I 

-0.0AF3j 

O.M9721 

' 18 2229 Geel Heat Tran. 

19 

M 

222.5 222A; 

2183 06. 

U%30 

0.06030 

0.06030 

0.081 5 

Geell-eall'Tan. 

Gent Heet T,.. 

.0,014519' 

D.03905 7 

0.06719 0.06719 Adiabatic 0.00001 

22206.-0 21 -i66-i 

206.0 

M L 3W.5 

206.0 046707 

-206.010.06620 . 

3W.5 0.03161 

0.06706E 

0.06611 

0.03161 

Puflabatic 

Afticalle 

O.Mool 

D.00000 

31 223 .0, 223.01 0.05866 __0.05866_ Atiabatic B.00MO 

AI, unction T.W. 

• Jet No. 

I 

2 

3 

-dPSMg. 

P &as. P Stag. p Static p static 

1 In, Mass J, F17W z. Total In Out In Out 

m H2O Std =9d.L9)) (h.H2Ostd_._(q)L Cm.1120std.fq)) Iin.H20stdjg))- 

i" ^P3 

,as 

( in 

O.Woo... 

- 0.0 09m . Uwe 

HEPARR.NO2-010 

Avon Chan h.e,, 

=281 

3131 

0.7]096s... .0.51490 

0.07=-__ L37776: 

.1.2859 

1.45M 

-067883 

4 .54198 

-1-4901 

A5-502

• 

E 

• 


Calculation No. 145579-D-CA-056, Rev. 1' 

Attachment 2 

Page 12 of 46 

AFTA,nm1OW" (4 015) 

DWMH-N 

AFT Anw Model, 0GTSBYPassSysI..T-H ModelC;ese I (Clesan Filt.M.NYD ISM 116 •FAndieskHT) 

3/2512006 

jet 

Norse Mass^ I PSla% P Stag 

P Stag. s p staft i p Stak 

7144 Jt TOW In ' 

Out In1 Out 

I 

-(.-4m) ("20. see.) . (n H2O dd: (9)) _@m MOsId. A fg)LLLK 1120 tdjq)j 

A 

5 

- TIT-0-m 

Area Change 

_362. 

302.28 . 

p.132U -1-42112: 

0.07273.3.70134 I 

....... 

-In41! amm, 

-4-4274 

6 ICVPI.. 302.28. 1.211028' -4.13992. 5.42023 4.99412; &BNO 

7 1 Area Channe M2.211 I O.MIO! 5.56569' 'Elmn 

8 i TesorlMe 1A;; O-DOOCK); 6Z7179: 6.3778; 4I.89796i 

9 t 1. . VWS NIA! See Losses: 4,43308 6.4331; 6 .611203; -6.6820 

,10 wlliII 245.24; 0.I 94861 -6,42559 6.620: 4.65265t 6.13,177 

ILL Tee. vh. WA I See Losses'. -6.63831; -6.6383. 43.7613117 1 -6.7669 

12 liv-902 57.031 0.01167! -6A3031. -6.6500; 6.650591 -6.6623 

13 TeemW" ^WA I Seel-wses I 

Teoorft, 6851 Ii: Ê.! 

O n 

.6.74958' 

-ti .5m u 

.6.7496 ; 

^M B 

4.05828; 

8.854,10 

-7.M3 

6.8546 w 

15 V-166 

-9.153901 6-4075: -9. -9.48030; -9.7540 

16 HEPAF1bnI3wl37 6.5605o8; -12.31 29. .9.88694, -I26416 

17 

18 

1431-130- 156mi 

BmWmft Damper 7%M1 

-13.98687 

0.27278; 

-1235751 

1 .5648]. 

1.2921 

-12.686091 

1.24357: 

1.3074 

0.970; 

19 

V-187 U 756.85; 024960 

1.28 384) 

I.0302 0.9624 8; 

Ann Pros 756 .851 0.004)(I0 0.00000 1 0.0000 0.00000 0.0000 

131_._,. _.._.-.. AM PM 

7 

454.W 000000 

71421 

„- ._.-0.09060____-.. 

O-DOODI 

.0.0^ 

-0.7481' 

O.DOOOO: 

-0.05515. 

-0- O000 

.1.1191 

123 1 8 12. 421 5.013646 -0.76996 5 I86" -1.14004 

24238: 

.6.3778. -6.37 M :tG 6 37:7: 

31 To Tra;n B HEPA 0001..__0:00000 . -U2384 

B.Sne4 

id dT See,. -i St.g. -- 

I 

T St.g. I T M.k I Sonic OH Hitog.H Sta^. H Stall. 

1.10 T- 1 owlet - In 

In pat In W A 

(deo. F) (dem F) ;' d F) i fdso. F^ I (do.. MIF1 

ffits,filo;n^ &aO fl3ttofflorn) ROW (Shlinn) b feel 

0.0000000 11501 115.0; IISOI 115A O.Wo 206.11 206.1 206.11 208.1 0.008447 

2 

3 

-0.00061061 

0 1004113 

115.01 

115.0 1 

115.0 1 

115.0 1 

14.91 

i14.91 

11411 L ONO 

1 0.000 M 

206.1. 

206.1 1 

206.1 

206. 1 

M.0 

206.0 

206.0 

206.0 

0.008453 

0.008472 

4 00002441 15.0 , 1150! . 114.6 1110 46 1 1^1 1) 

206.0 2060 O.OD8518 

5 -O.DOO48M: ; 1 1&0 1 5.0 114.9 1 1 0.000 206.1 • 206.1 2WO 206.0 0.008522 

6 759.909542: 115b 1 875.01 206.1 1 393.8 206.0 3933 0 .008532 

] 0.00012211 821 *4 125- 7,i 4,:.7 813&1 , 7"0 I ^ 614,7 7,eol 4, 3 O,GEW: "A 1 381,§ 360 _ MIA 3813 NI.2 O.OIM48 

a 0.0000000 741 7419:^ 

3fi0.5 360.4 3604 WA 

9 DOoonwo, 738.21 

M 

359.]1 3599 359.6 359.6 N/A 

10 0.0000000 731.2 ;. MI.2 731.0 . 731.O t 0 .11001 357. 91 357.9 357.9 39 .9 0.010052 

11 

72 3.6 723.61 723.5; 723.5 ; NIA' , . 356-D[_ . 356-D . ^6.0 3%0, NIA, 

12 O.OQOOOODJ 729.7 729.71 729.7' 729] 

nz.-i 357,6 367.6 357.6 0.002337 

13 

14 

0.0000000 307.6 

00000000 ._ . 00 .. .... .. 1114j 

307.61 

U4.3 

307.4 

184.2 

3004 

18^4.21 

WA 

WA 1 

253.2 1 

2n.0 

2532 

223.0 

253.2 

. 223.91 

2532 

Z?q.Qi . 

WA • 

NIA. 

15 

16 

-.001831 

0 .. 0...... 

. 

-0001 7090 

_ . 175.0 . .._ 

174.5 

175.0 

. 

174.6 

174.il a 

174.3 7 

174.91 

I I 

174.31 

0.000 ---- 1 . 

0OW 

22D. 

2206 . 

2N.7 

2206 

226.7 1 

220Ol 

- M.7 

2206 . 

0.022748 

0.022761 

17 10.0006714 174.1 INA 174.01 184 .0 i -2.4431 220.5 222.9 220.5 1 222.9. 0.022921 

is 

4 

-0.0001*31 

:o-vm7m 

" 2^ 

182.2 

. 102.6 

1822 

152,51 

182.1 

102^! 

182.1 

0. 00D ^ 

0 ODO. 

22 -2.6 

2=5 

Z2- 

2.6 

222.5; 222.4 

2M5:_O.On267 

222.4. 0 .022275 

20 

21 

OOOODOOO 

00000600 

11S.^-1 1 5. 0 

1150 

1150 115.0 1 0.000 1 2061. 2061 206.11 2061. 0.022048 

22 -0.0007324 

23 -0.0040894 

. 

1150 1150 

012695, 

lisb l 115.0 116.0 

012696 

116.01 115.0 1141 

0012720- 

30 t O.00OODGO 7417'_ ..- 7417 741.) 741.71 0.660 

00_0,000_0, 

31 0-06666-06 1- W.3 1114.3 184.3 0.000 _ 223.0 223.0. 2230, . 223.0 . 00000 00_ 

JUrcA.n Loss Tade 

A5-503

• 

RPP-24544 REV Id Calcula tion No. 145579-D-CA-056, Rev. 1 

Attachment 2 

Page 13 of 46 

AFTA 3.0 Output (5015) _ 31252008 

OMJMHIH 

AFT Modd, DOTS 0ypass System T-H Mode) Case 1( Ctean Fate NYS 1508, 115-F AmbIW. HT) 

• 

• 

J0 . F1pe Pipe d S1e9.TO ; 

^8_'. pTi In^ 0.000! 

A5-504

• 

• 


Calculation No.145579-D-CA-056, Rev, t 

Attachment2 

Page 14 of 46 

AFT.Anx w3.o utw (1 m6) 3nvzoo6-0:2s AM 

DMJMH.N 

AFT Arose Model,OGTS Bypass System T-H Model Case 2 (Clean F â1ers, NYB 1508.115'FAm bleK HI) 

TAw AFTArmw Mod el, OGTS. Bigness Syslan T-H Model Case 2 (Clean Filters, Ming 1508,115 •FAmbiwa, HT) 

hlplRe: Su bc Y osoa Year 2008 Wodl a lalionslOGTS Bypeax TMlmal . Hydritoks AnalysislWak F'deslBypass F lo w 

etch Hpe Rev 1 Case tam .. .. 

Number of Pipes= 25 

MtaiWol JUnctiom=25 

Len9N Ma rch Sohillon M et hod with Mach Numbw Limas . 

Length Step $ae= l2 inches 

Mach Number Increment- 0.01 

Pressure Toterence=04001 neiaBVe change 

Mass F low Rate Tolemnce= 0.0001 sela8Ye change. 

Enthalpy Toleranoe= 0.0001 re loO,e charge 

Flow Relaxala, = (AUtoma lle) 

Prassure Relaxation= (Automa tic) 

Resistance Relexaton= (Autemafic) 

FluM Database: AFT Standard 

Fluid: Air 

Max Fluid Temperanne Dala,- IOW dog. K 

Min FhAd Temperalure DsM= 200 d ing. K 

Moleadar We ight =28.91 emu 

Gas Constant =0.06855 BNObrrmR 

C ritical Preswre -W.25 alm 

C ritical Tempealore-13241 deg. K 

Ace ntric Factor =0.021 

Equa tion of State= Redli ch4(woog 

EnlMlq Model= Generatixed 

Spe cific Heal Ratio A=mW = High 

Atmospheric Pressure=14.3 live 

Gravitat ional Acceleration= 19 

Standard Pressure=14.696 pSi. 

Standard Temperalwe=60 deg F 

TwWlent Flory Above Reynolds Number= 4000 

Uniiiar Flow Be low Reyn tds Number- 2300 

Hoe lnoVi Table ... 

Hpe Name P pe Length g 

Defnetl 

. 

.. .._. 

Len itih I Hydraulic 

U H uam t r 

_... 

Hydm .11 

O am Units 

.. .. 

F Im 

Dal Sel 

. .. 

Rough ess 

.. .. 

Roughnea 

Units 

losses (K) Inl at Flaw 

(,., ., F` 

2 Plpe 

3 3FEs l 

Yes; 

Yes. 

Yes 

_ 66_ .ches 

104 *inches 

163 in 

6065 

665 :0 

inches 

Unspecified 

ch 

ew U s afed 

. 0;00015 

0.00016 

,.._.__.feet 

feet 021 

ch 

. 

es 4.026. inches) Uns dfied 0.00015( feet) 1.6351 1 

4 

5 

Pipe ^ 

Pipet 

Y s 

Yes 

39_. the 

22_ inthes. 

6.065 

4.025 

inches i_ U speafias 

inches; Unspe cified 

0.00015 1 

0.00015 

feel) 0161._. 

feel 032 

_ 

6 

7 

Fire 

Piee 

Yes 

Yes 

72- 

14151 

aches 

inches 

6.065 

504] 

inches i 

closl 

Unspeafed 

Unspe cified 

0.00015 

0.00015 

feel 

feet) 

0151 

041. 

- 8 Pip. Yes 6: inclhes 8065 nch !_Unspcfied 0.00015 feet 014' 

9 Pipe Yes 105; incites 8065 Ina. Unspecified, 0.00015 (eel 0: --^ 

10 Pipet 

11 .,.,_Pipet., 

Yesyo 

s 

8 inches) 6.065, inches Uozicedfl.d 0.00015 feel 

in 

005 

ch 

. . . 

.12 ,. _ _Pipe Yes. 

es _ 6.065' Inches Unspe cifieg .____O.00015 feel 

12 __ chins 6.065 , _ranches 

,_:0,05_,_.,_._._.; ___ 

. 

13 Hal 

! 1 4 Pipe'_ 

15 Ppe __ 

16 . Pier ^. 

Yes 

Ye 

Y 

Yes 

. UnsPeGBee . _ 0.00015 _ __ . __feet 

251' 1rc 8.329 inches Nns cified 0.009151 feet 

1969; reh s 8 329 inches U ape fled , 0:00015 feet 

245 ahe8.329wpes U pealed _0400-5 .._f_eet 16 _inches 8.329 inches) Unspecified: 0.000161 feet 

122794]______,,.. 

0.1 1 

0.77 

13_2 _., 

043_,,, 

1] 

18 

Pipei 

Pipe. 

Yes 

Ves _,_ 

12• inches 

42„ Mhes 

8.329 

8.329 

nchesi UnMecifad 

inches_ Unspecified 

000015 

.0.00015 

feel 

feel 

D.111 

O1).1. 

_ 19 Pipe _ Yes 12 dnsl 8329 tlles Unspecified 0.00015 feel 0,,,. 

20 P' a Yes 569 N s l04O.00D15 8329 nch c _ eofed IeN 2. 

21 

22 

PI Pa Ppe 

Yes 

yes 

104, aches 

6rcMSI 

1239 

6065 

1 che_s _ Une Pecified aches llnspec Owl 

0.00015 

0,00015 

feet 

feat 

1.42 

0.00 

23 Ppe _ Yes . 288 hes _696$_. inches Un pealed_ 0.00015 „_ .. ,leer 01l ,.__ 

A5-505

LJ 

0 

RPP-24544 REV Id Calculation No. 145579-D-CA-056, Rev. I 

Attachment 2 

Page 15 of 46 

AFTA 3.01nput (tor S) 32.520081(:25 AM 

DMJMH.N 

AFTA Model, OGTS Ba. System TM MOM (lase 2(GleanFfflam NIW% 115*FAaaWeMHT) 

1 F1,; Lw^p L-,gth lNtlbulic Hydraufw FrIdion I FtDugluvss FtwgMex Losses (K) InItlalFbv 

3D PI Yes' 015 eaat S.04ir 0.000I5 red 0 

Kes_ i OS _"11 . S-12W fa^. I Unsp .-&ed __PALI^j_--- 

L- Rt - ---- --- - A 

s RN NOAMW! NrediansGeometry Material Sim Type TM.al Ambient Temp. 

7 

Itaam., 

2 I 3; "Md&.1 Mae StaiNex Stedi 6 k ah schedNe4O AdaW.^ 

3 4 PS. S^ -ISR -L taft! !LlIct sc a we!tq 

5 

C yGrairtop! F^Ve. 

5,6^ "wam Un edfledl 

61^ sc^W. Adwb. . ........ ... 

AIDab.ft 

6 SX Cvftd,k Pim SW.Iass eel' 6 !nO ahetjaJe4O Gamml Heat Tmmfer 115 

-7 8" -cawk(AMpe, m@ m- OwILSmm --sch 9 

--------- 

9,10 1 cv"dt,ai Ph. 

tNLO ADQ qe--nL-Heat 

TBLr tge E-'... 

Si;,,1161^ 

sÔL40 _G..,aJ Heat,Tmnsfe, ! .... ... 

Simh ld Ia,10 Gmeral HeaffmsW 115 

Geneml-Heal T 115 

SthNnIa,10 General Heal Transfer 115 

12 12,11: CYRW caTfta SI sM etltjle,10 General Heal Transfer' 115 

8jmd1 j SahiaduhalOt G.qe,m Heat Trwer:' 115 

15 

^gtn^jja Heat 

t 

16 15 16 Rpe Sla Ness Ste .I 8'nch schM. 1.10 

p %Rafar r . 

General Heat Transfer 

- - "... -- 

115 

16,17 w Cygnthdoetpipe SWIN.S.Steel . 8 ind nhedalejD General Heat Tfaasrer 115 

13 8 q Mjqq l Ejpe SbinlxsSled 8 inO .dreSwt- 10 ^gemr@LtLt mlws Transfer r - ----- -11- 

. ....... 18- 1 9YLO 6 2a!mp - R . . S.. ka*, mess a St stl . 

2D 19, 20; Gy%Wcal Fja, Stairtless8teet. 

j6im h . s et-AtL:L0 

Birich schedule l0 

-gne [m1IMN Mt^ r ...... ... . 

General Heal Twar., ! 

. 115 

lig 

21, 2T Gyv Wcal pipe SPI RI-ss st-4 --- 12j.nO 

22. ,n ! Cyr nd,ical Mp e . haJaIe4O 

3D_ 

3 12 C_yjmMqA! ffpe 4 12114055 St-ewll-ql^q! -.a C"w ... .... - 

8. 3D Cyhqd I^kl ffpe Sb sz Steel 5O 1ne4ule ^ 

,10 

Adi.t,.ft 

Adiabat 

-31- 14,31I_.G^jlindnri PI pe StainT.Steel 8,.h l a,êdWe 0.......... .. .. . Adi.bft 

Pipe Ambient Temp. SpedA 

Wit, GoWtf.n 

Nwe 

3 

None 

Nwe 

4 None 

5 Nans 

6 deg. F Non. 

7 ft, F Non. 

8 d", F None 

9 dart. F No.. 

10 de, F None 

11 d,. F Non e 

12 de , F' None 

13 

d,,, F 

14 

d,,, F 

Is d'. F N.. 

16 dea F Nan. 

F N-. 

18 da, F N.. 

19 da, F Mae 

20 dn. F . N... 

21 

Non. 

22 

23 

Now 

A5-506

• 

• 

• 

RPP-24544 REV Id Calculation No. 145579-D-CA-056, Rev. 1 

Attachment 2 

Page 16 of 46 

AFTAmay 4.01npu1 (3 01 8) 3!152 0 0 5 1025 AM 

DMJMH-N. 

A iuoawklodek OGT3 Bypass Sysbm TM Mod el Cartel! (Clean Mm. NYE 1508.115'F Ambient Ht) 

' . Pipe AmbienTemp• Spedd . 

Unts CoM'Nan :. 

30 Nona: 

Real- DTable 

Pipe ' KTOtzI SbMxd Mme Smooth Atgle W BuOergy CNinder Gab Globe pbg : Poppd 1 

:. Loese_st ..,_,.. -_Bens BeMS . Berds_ _ VBNas- r Valves- Valves... Valves - Valves Valves! Valves ! Valves J 

12 123 1 0.13 

t3 0.11 

;. 21 

21 1.42 

22: 0.00 1 

_ 23 . . ; .._011.. ___._.. i. .. .._....'_____.. ....__._—^___..- 

Pipe Tbra way Swing Check. UOCheck Tu lin,Diu Stop Check Slarpedged Long Conheassne Espansbns 

Losses Valves Valves Valves Check Valves VaNas Od&e Office i 

t3 

21_.. . _.. _....___ .. .... .. .. 

22 

23 

Pipe En trances Ewts OiSdental Noreycgmb Screen Tee Atltlt LOSS 

_LOSSx - _ ... I; Flow, eter ... 

I ^ 

_. .l.___.. 

1 

13 

15 ' 

._.:._ 

^ I 

... ......._. 

1 1.1 ' 

10.11) 

0.22 

21........ .. .. _ . _......__.. F_...._.._. . _...___. _ (1.62). 

" 23.: 

Area Chance Table 

Area Change Name 

.___. 

O .._. 

Object Elevatim 

__..... 

Eio dron I I dial Pressure 

..._. .....__. _..... 

Initial Pressure Daaze tab Type 

t... 

i Geometry 

_ 

Defined .'Is Units Source 

-;. 

3 

d 

5 

] 

Area Change _,.. _Ye 

Change yes 

Area Ch a Yes 

'_,_ Area CM1a 9?. __.. yes 

_. _0 

0 

0 

0 

Ieeli 

fk _ 

ledI 

reed. 

_ . 

_. _... ., 

.__ 

Co ¢al 

Co ical 

Cortical 

Conica l 

Conraaon 

Expans on 

Conhaton 

Conn. OOn_ 

Area Change Pngle Loss 

_ Factor 

3 22 0.4399 

4 22. 0.1552 

s zz. tl.4aoe- 

7 28.1 OA241, 

C2Mr.eaagg_on Table 

CompressatlFan" Name Object Elevation Elevation ailid Prewum initialPmsime • Database Spaniel 

Def ed Unlb i Units Soars Condition 

1] Nat-13D 

yes 

0' feet None 

ConjuessorlFan Pump Design Flow j Design FlayCurrent IMepe nden :Ind. Vadable DepeMent 

TVPa Rare I Rate Units i C f G V dew Unus Va'abte 

1] _Comp.IFanC ej ,.. :. ...__. Vol. Flow Rank , _. __aYmip _Presvxe Lass 

A5-507 

1

• 

E 

• 


Calculation No. 145579-D-CA-056, Rev. I 

Att a c hmen t 2 

Page 17 of 46 

AFTAnmw 3.61rryul (4d6) - - 3RSI2006 1035 AM 

DAUMHaN 

AFTArmw Mode, OGTS Bypass System T4l Modal Case2 (Clean FMefs, WEI ISM. 115 •F Ambient HT) 

i CompnNSORFan Dep, Vanaba 1 ComÔ CUrva j Comphan Curce CompJFMCmue Cmnphan Cm,o I Comb MC.. 

I .. :... Uik ! ... Co=nla Coradealb._ I ._ ConsbMC Cotslantd _... CwIS1eMa _. 

i] 

__.__. 

CanpressodFan 

'ux H2O SM.. l9248929: 29711 29E-031 •2285T14E-06 

RYWG FpW fluihM FlOwi Addatl Preis Spead^ + COnboi __ 

O1 0 

—._ 

CWbpl CWbol Nfien Compression 

. _...... Role I Rate Unb I Tvlse Dlscharee I Distlwmal1nW Exceatled Only Process 

Dead 5nd Table 

Dean End Name Objet Elevation Elavatbn 'Ini ti 

al Preswm :Ini tial PressureDatabase 

Dafuled i Ulm$ Lirdle I source 

30 To Main OGTSi Yes: 0 feet 

31 ' To TminRHEPA !Yes! 01 feet 

Genarst Comment Table 

General Component Name Object Elevelioe Spread. Initial Pressure Initial Pressure Database Special i 

.. _..._._._... ._.__. ..----._. Deed ..._ fi 

2 HEPAFlIler NO2-010 Yes 

16 i HEPA Fi 

_..__. Vnits 

0' feet 

...._..._—. Un its ....... source _. _-- ConddW 

--'--- None! 

lt . 

er 13611371 Yes 0; feet NDWi 

18 

22 

. .. 

I Backdraft Dampar 

"qaep&HEPAFift.1I 

__.._.... 

_ Yes 

Yes! 

e ..._ 

_ _0; 

0 

_..e....... 

ket _ ._.__..__ _.... _.. _._ .L.___... None! 

feet None' 

_ ........ ..... .. ...._ _ __.. .. Less .. 

S General Component Loss ^ Lou Independent t d Va riable Dep naent i Dep. VaneNe Lou 

Mode „_Va le.,_. _ Variable Una, Vanable ._ I Units _Constant a, 

2 I Gene ral la0immial Variable VG.S wRata R3/mn: Pressure LOU in. H2O aid.; -1465517E-1 7 

. 16.,,._„ Gannetpol mmial Va ri able .VG Flow Rate a3/mn Pra...WSS „ 0._H2O Std 3534499E-1 7 

18 General Poo al Variable Vol Few Rate ,: .Wmi rrPressure Lan in. W6 ,std ]W3767602. 

al Variable:_ V IFlo Rate: ,fW FtasYnp LOS _ .1-12OSld. -1,43656815-171 

.,,., .. ._ 22 Go tPol,,poKal , 

General Component I LOW Loss Less Loss 

CenMantb Constant C , _Comslantd_ Cons ta nt 

2. 0.00224_ 0 0 0 

16 _. ^ 2.826666E-03 0 .0 0 

16t68]i81E-06 3.46ta -OBi 0 0! 

22 0.001382 It 0- 0: 

H at Exebanner Table 

Heat Exchanger. Name I Object I Elevation I Elevation I In fiat Pres v e' Ini8al Pr sure I 

Units 

Calmed 

Units 

Seem SWme 

_...._ 

Special Type 

CoiM tan. 

6 ICV Plenum l ... Ye t01 Ise tl- __ None 

Not Exchanger 

,, 

Loss 

Modal _._ 

Lou r Independent 

. Value r Va riable 

Ind V nable 

Vnils, 

DeperN L 

Variable 

Dep. Variable i Loss Loss Lou 

Units Constant Constant Cons tant 

6 K Constant 1.5 I 

Heal E.O.N. Loss Lou 

C.Iamd _-- Consian . 

6 

Tang Tattle 

Tank 

1 

Name I Oble elpet 

Definetl Alm Presl Yas 

.Elevation 

0 

Fe aban' 

Irvt al Preis re lniaalP 

Unitss Unh is 

feet .,,, 

re I S n 

^_ Source 

Pressure 

_ 

14.3 

P uua 

Unlis 

purl 

Tempe atwe 

; 

115: 

20 Atm Pres; Yes 0 leaf _ I 14d _psa 115: 

21 Alm Presl .Yes - 0 feel _ .. ^... 14J PSai __. 115' 

A5-508

• 


Calculation No. 145579-D-CA-056, Rev. V 

Attachment 2 

Page 18 of 46 

AFTArl &OMpet (506) 3aWO 510:%AM 

DMA"N 

AFT Arro,VMOdeL OGTS Sypass System T-H MMel Case 2 (am F0lew, NYS 1509:115 T Ambien4 HT) 

, 

t TankTemperakee I Salanm.. Sapnca (Floe#1) 

Ursb Fnmgy. COrwen0a0gn_KM KOU{ 

(Plpe #2/ 

Kt0.K Q# 

(Pipe #3) 1 (Plpe Aq (Floe#5) (Pipe#5) ) 

KM . KOUt'KIn KOUt(KIn KOUt: ;KIn,KOut^ 

' t T &m Noi No! IPt)QO 

- 

211 . 

21 

_ ...._a? -E 

de#.F 

No`... 

— NW 

No-__L3L0 

NO; 

.. _._ ___._...__ _....._... 

: , 

IP2 0 0 

Tank i (Pipe#]) 

:KIP^K 0e1 

(%Pe #el 

KN K00f 

(Floe #9) 

KIRKOUt 

(Rpa #10) 

Kh!,KOUi 

(%p# p11) (Pipe#12) IPlpe#13) (Rpe#14) (Ppe#15) 

NM,KOM , (K tri,Kax _KIn,KOUIi KIn^,KOUI,!_KM,KOW„ 

. 

( Tank; (Rpe#16) (PIPe 91 7) (P-me#18) (Rpe#19) fPpo#20)- - (%pe#21) (Pipe#22) I (Pipe#23) . (Ppe#26) 

t KIn^K00t . 

, KIP,Kd!l NM,K Wt KIn^KOUt_ KN,.K Out KIn,KOu( . KIry KOU[; K1q ROyt ,KIn,KOW. 

1 

Tank ! (Rpe#25) 

KM KOO 

1 

20 

21 

Teew T 1 

Tee or Wye Name Obje ctElevation 

Defined I 

Ela.H. 

Units 

goal Ptas a lniliel Pressure 

Unlls 

Database 

Source 

Tewwye 

T - 

Loss 

T e- 

8 

9 

11 

Tee or Ves 0 feet' _ 

'-Tee or e. Yes 0'' feet 

Tea 

_„. o[Wye Yes 0- feet; 

WYes0eet 

etailed 

daoe 

EMEndelai@d; Oelmo 

id Teor^ e- Yes 0- fDetailed. 

Tee or Wye An91e : Pipas 

.. _.. _0.. _.. :._ 135:_.. 

9 ._ 150: 

30. 

13 a5: 

14.__... td6!...._ 

V.W. Table 

Valve I Name ! Objed Eleva!i'm El.go 

_^ OefneC_. _ Ungs, .. 

WtiM Pressure Initial Presswe 

Units., 

Database' spedal 

source t Condition 

Exit 

V.W 

Exit 

Pressure 

1 p ! HV-9011 Ves 

12 . _HV-902 1Yes 

0 

0 

ket 

teal 

Closed 

„ Closed 

No 

No.. 

15 V-166 Ves 0 feet ., ,_-_None 

Iii 1 V-16] Yes_ 0 feet None No' 

23 1 V-1 78Yes 1 0 reol None' No 

Val e I 611 

Pressure Umts 

C0A COA 

Units 

Loss Los 

Model V.W. 

1 OepeMent 

Vadxble 

1 0 Vae riabl l Depe d t Dep Vadablo ^ Loss 

Units Venable ;_. Umk Con5lanta 

f0 Oi COnstap! 1194 

11 I c Corgfsuml list - - 

^ 

15 I 

1g _ 

Cv Cstant on 

(^ mlaat 

Cy ConsUM 

2640 

2140 

300 .. 

._____.. _ .._ ..._ .. _....._. 

A5-509

I 

• 

AFT Art 10 bpd IBdel WSUM 1025 AM 

OM WON 

AFTArrox.MO .L GGTS Syp m System TJi Mudd Cam 2 to. Fillm . NYS 1508, 115T Ambimk N7 

Vdvs Lon Loss Loss Loss 

j...__. CoirslantE? , copsta0t c..: Con>fmÎd ,COnsbnle - 

10 

19 

23 

—.._ 

A5-510

7 

• 

• 

RPP-24544 REV let 

Calculation No. 145579-D-CAA56, Rev.1 

Attaclunent 2 

Page 20 of 46 

AFFAmwv3.DOuIPA Vof5) .' 3F2512006 

DMJMH,N 

AFT Ampw MOdeh OGTS Bypass System T44 Model Case 2 (Creed Filers, NYB 1598, 116'FAmNenL HT) 

TNe:AFT Arrow MOM, OGTS Bypass System T-H Mbde4 Case 2 (Clean Filers.. NYB 1500,115 T Ambient HT) 

Anaysfsmoom 3!S 0061023:30 AM 

Appllentonversioa AFTAnnw Venim3.0 (2 005.99. 11 4) - 

input File: MADemmstratlon Bulk VMSW Year 2006 W&kXCakd%Uw*10=Bypass Thermal Hydau0s AnalysislWak FIWIBypass FWN8 

Inch Pipe Flux Case t.wo 

ExeclNOn Time=11.51 se conds 

Total Number Ol Pressure la ratoo3= 0 

To utl Number Of Flow Oembons = 52 

ToW Number Of Enthalpy llera6anc 52 

Numbw()?Pipes=25 

NMnlob, Of Jane ions=25 

Maine Method= Gaussian Fdindnaton 

Length March S ol u ti on Method with Mantle Number lLNls 

Length Step Seem 12 inMes 

Mari NUmbernaament50.0t 

Pressure Tole rance= 0.0001 Few" Marge 

Mass Flow Rate Tdemnce=O."ll reWb'va Marge 

Enthalpy Tolerance= 0.0001 relative Marge 

Flow Relaxation-- (Automa tic) 

Pressure Rela"am m (AUlomaue) 

Reslummar Relaxation= (Automat.) 

F lu id DataOasc AFT Stand ard 

Fluid: Air 

Max Ftuld Tempera tu re Dam= 1001) deg. K 

Min FWId Temperalae Da a w 2(m ticg. K 

Molecular Weight 48.97 emu 

Gas Constant =106355 Stullbm-R 

Critical Pressure =37.25 am 

Critical Temporal.. =132.4t deg.K 

Acenbfc Fader=0.021 

Equ ation of Slate= RedfiM-Kwong 

Enthalpy Mode= Generalized 

SpedOC Heat Rude Acaracy= H igh 

Atmosphe ric Pressure- 14.3 psis 

Graviatiamu Accelcraun= / It 

Standard Pressu res 14.6911 pslx 

Standard Temperature- 60 deg. F 

TwEUtent flow Above Reynolds Number, 40W 

Laminar How Below Reyn ol ds Number= MW 

Total inflow= O. 7A2lbmisec 

Total Oulllowti 0.757216m1sec 

T ot al Energy Infbw=157.88tWs 

Total Energy Outflow= 157.3 Bites 

Total Heat Transfe rred Into System=-0.5593 Bluffs 

Maximum P re s su re is 14.33 Pa lo at Junction 17 Ontl et 

Minimum Pres su re 1513.76 peia at J.mAkm 1 7 inlet 

Maximum Slat. Temperatu re fs 124 .7 deg. F atJuretlon 17 Outlet 

Minimum Static Tempera ture is 115.0 deg. F at Junction 13 Inlet 

ease,/Fan Summa 

___ 

Speed Ove ra ll' Comp. BEP - BEP 

'. Fbw Flax ! $tag. Static Erfichm, Power Rau 0 - Was 

_. _.t /scfm). (03/min), ^_Qn H2O Std)__jin. HW .td).! (Pemam) (Percent) ^_(hPL lPerceni)_ (B3/se.)_ QlxNSec),, 

17 N31-130' 5948 7026 1576 15. 77 6140 1000= 2.545 104.1WA WA 

' Jet 1 Name %Mass Vol. OP OP Overat 

J4 % of 

BEP 

(Percent) 

9 NIA. 

Value Sure. 

A5-511

• 

• 

• 

RPM4544 REV Id 

Calculation No. 145579-1)-CA-056, Rev. I 

Attachment 2 

Page 21 of 46 

A"AamMOu"t czars) MWON 

OWUH.N 

.PTA Model, OOTS Bytims System ?-H IVIatle! Ciine 2 (OMMM. 101il 1 5W, 116 •F Ablain, HT) 

Jot bono, V.w. 1 M. I 'OP Slag Dp tausa . P swa. K valve state Cv Cv ciaL 

Type I Floe Idet 

@an. -fp-swL- Jewvvy 

X12 

i 15 

19 

-94' BmImal .... ^2--SP 160 

M-M, REGULARI 0.0000 1 No Solution ! No Nosduft 

V.166' MOULNtl 0.75)2 ;0.W5216 . 0.0052 19 m 1384 

t,167 ,.,T ARnj 0* 572 II1 M 14 ; D0.005136' 1432 

NDSDNHat 

0^.7... 9 

posedB tlseri 1196.0 

2.4,10.0 

4440.0 

ND Solution 

WA 

M RE""" 1W ----iA 

0.15/21 0.321421 : 0221952 : 14.24 13.99661 OPM! 306.01 MAji 

Hg^1,^x^5ame. Summa 

Jot Noun. Mass 

R. 

DPo 

.61 P (dr OT 

Roe Output Table 

Mp. Noon, IVE.SS VOL V.I. Vel. Moon m,in Mach 4 

dP Slag. Plit el. P stag. 

Flow 

had.) 

Flow . 

(Itillailn) 

to 

((OeY",) 

Out 

_(LgM.IDL 

gin Out Total 

I ria.mmobi.) 

In 

rm.H20std.(o)) 

w 

(P. H2O sid. (q)) 

I Pia 1 0.0 : 0.0 Om 00 0.00000 0.00006 0.006000. Omw 0.00000 

2 PIP. i O.D' 0.0 O.W DLQ 009w chww() . ....... O.DOELE)qq, -AgWo ... O.Wom 

3 

3 . 

3 FE. 1 0.0 0.0 0.00 limito 0.00000 

4 Pipe; wo 00 0.00 0.0 ( .OWN 0.00000 (LONOW: ILDWO 0.00000 

d 

. 5 .... .... Pipe.,. 

iKv. 

_ --,0. 

0 . _ 00 0- P0 

Piqi _0.0 - 0.99 

PIP, 0.0 0.0 0.00 

0.0I 

0.0 

0.0 

DOW 

0^, 0.10,0000 9 

O.WWO 

0 0.000004 0 

(LOOM 

0.000000 D 

6006^ i 

OW.WW: 

I . 0,0000 OO 

o-wnqg% 

0.0mm 

-0j02000 

OD 

Pipe! 0.0 cub 

9 pi,!, 0.0 00 

10 Pipe-i_ -..00 .. . 

0.0 

I pip 0.0- - Ap 

R ---- .-Pp QQ. 

13 Ppej (11 0 . 00 

14 . Mpol 

0.00 .0.0 

000.,,_.,_,,.-00 .-tKNOW, 

00 0.00060 

OM .0.0 - O.WWO 

-Q-09 

00..000000 

1100 0.6 -ilomm 

_30.66 1 1" ,8A OM619 

000OWi 

O.WWO 

O.Wilm 

o.^woij 

0.025 K i 

O.OWWO 

0000000 

0,000600. DW O : 

... 0. 0 . 

a." 

D.W1810- 

0.00 

. O.WW 

-11.24(5,1 

9.00-00 . 

. 11.2464 

_ jl.24(5,11^ 

.11.24 MI 

. 

O.MOOO 

0.00009 

... .. 0. 

tt 241643 

-11.24643 

-12.205V, 

15 

_18 

V6 7 

1 

Pipe'! 

R PP_ o 

. 594.8 

5914 . 8 

594.8 

698.2 

6M.8 

702^0 

686.0 

30.74 

30.78 

30.95i 

30.221 

1 

1.847.2 

1.812.81 

002625 

002629 629 

002643 

0.02515D 

0.026281 

OMI M 

0.026431 

0,025501 

D.^8199 . 

0.086%6. 

0.025395 

0.637010 

-1 2.2q^ 

-12,70781 

-14.770,1, ,., 

omfui 1 

2.5&3471 

-12.79451i 

, 41931 M 

O.9M541 

19 

m 

21 

Pipal 

Pipet 

Peel 

594.6 ! 

5948 , 

5948 

OW.2.. -- 

M 

6762 

30MI, 

13 A6j 

1.813..§ 

EI 07.1i 

0.025611 - F. 0.025§9 0_ 

... 0909910 

._.,. .02M,._ 

_91.59.8080 

0.011491 0.0115111 OMM7 

0.7183 

0.5) 13; 

0.00w i 

0.71339 

_.-O.026nj 

-0.06)111. 

22 

n 

30 

31 

PSe 

Ppe 

- . 

i5q 4. . 8 

0.0 

^M ^ 15 

no [ 

0.01 

5637 -.1 

`=0 

6.66I- 3.382.6! 0" .815: 0.048151 

3.41662 1 0.04927! 0.04934! 

0.01 , -0.0ow -- O.--v 1 - 

0.0 O.Dmool O.Wwo 

0.037(116^, 

6.6M47 _. 

DD 1- 

(Lobbow 

0 - 

n231 

- 

0.0000 

^ 

L02930! 

w.mn, 

Pipe P Slotic P stwt C QT &.g. T Stag. T Stag. I T Sanki T San. d" St., Hstag. 

In Out Inlet Outlet In out In 

I 

2 

19A. 

O.Wwo 

ILOMWI 

Q S h4 (9)). ._.(deg. F)(deq. F) . Coati. F) 

0.0000 (LOOMMOD 115.0 115.0 

G.WMOD G.WWWOD 115.0 115.0 

(ft. F) (ft. . F) ..... (81to trMI 

. _ 

115.0! 115.0 O.WWWWO 

115.0 115.0 O.WMINOW 

(BtWb 

206.1 

206m 1 

3 

5 

0.0 M; 

O-Wqw : 

O.wo00i 

OLMW 

,000000 

D.00000 

G.WODWOD 

0. mwww, 

(LOWNWO 

116.0 

115.0 

115.0 

115.0 

115.0 

115.0 

1 Issr 115.0 1 

115.0 ,11 5 0- 

115.0 1 15.0 

O.wwWDW 

O.WWWDW 

206.1 

206.4 

2W.1 

6 

7 0.000W 

G.WWO 

O.WOW 

D.WWOW() 

(LOWWWO 

11&0 

115.0 

115.0 

115.0 

115.0. 

115.0 

115.0 ! 

115.0' 

0.6 0606006 

OLOWWWWJ 

2W.1 

206.1 

A5-512

• AFTAO 

0 

RPP-24544 REV Id Calculation No. 145579-D-CA-056, Rev.1 

Attachment 

Page 22 of 46 

3.0 ,0utput (3of5) - 3/252006 

OMJ N: 

A M tidel.OGTS M SyPM&Jstan TdlMmd Gasp 2(Clean Men, IWO 1500.115-F AmMen4 Hy) 

.Pipe PStaOe PSlatle d< Stag. TStag. TSta% TSWIic; TSWOe dH Slag. HSta, t 

B 

In at ! Intil Wft ql Out S In 

j.:k24.S1a C9))_ ._CI19 r♦2G sw.-(9)1..:_1deff 

F1..._C4?9.FLt.Cgea_FL .lE)_Ld?g..Fl^_Se(wlpml... _(^t!96m1i 

i _ 0.00000,._._...._. 0: 00000 0.000OOOM_ , 115,0; 

,- 115.0 .. 115.0115.0 „ - 

10.000000000 ,.__206.7 

- 9 ( 0.00000 0.00000 0.00000000' 115.01 1760 1150 115.0 a0DODODam 205.1' 

10 i -11.2460.3 -t 124643 0.000000001 115.0 115,0 - 115.0 115.0: 0.000000000. ZOB.P 

17 I 0.00000 0.00000 : 0.00000000! 115.0 115, 115.0' 715.0 0.000000000 206.1. 

12 ! -1126643 -11.246M13 0.00000000: 115.0. 1150 115.0 .115.0 0.000000000. 206.1 

13 i -1124643 .11.24643 O.ODDDMi 115.0' 115.0 115.01 115.0: 0.000000000 208.1 

i 14 . 11.029.0 -12.38906 0.00561523' 115.0 115.0 110.9' 114.9 ! 0.001562005 206.1 

75 -7238906 -12.747"4 0.00024414 11541 115.0 114.9' 114.9 0.000121285 206.1 

t8 i -12.8919.9 -12.97868 -D.00006106 115.0 175.0 114.9 114.9` 0.000008043 206.1: 

D i -14.85516 -14.98058 0.00000000 115.0 17 5.0 114.9 174.9'. 0.000000270 208.1; 

78 0.78585 016809 -0.24407959 124.7' 124.5 126.7 .124.4 .-0.059566839 208.4 

1 19. 1 0.53755 .0.50267. -O.Oti860J52 ]24.5 124.4 - 126.6 124.3' 4.016742299 208.41 

-i 20 1 0.39051 420702 -2.72td9659 f2g4i 121.7 124.3 121.6 1-0.664116630 208.4-. 

21 ! -0.03635 -0.09400 0.00036621. 

^.. 22-..._...__._._-..... -1.62820 , __--„ _-1 ;96529 ._0.00600000,: 

175.0: 

iJ5.0 ... 

115.0 

11$.0 

t15.0 715.0: 0.000000000 2%.1 ' 

114.]` .. _..:...____.._.._..._.. 114.7' 0.000000000 .. .... _.06.... 206.1' 

23 -10.57713 -17.1]088 .0.00048828' 115.0 115.0 114.7 114.7' 0.000000000 206.1; 

30 :- 0.00000 0.00000 O.000OM; 115.0 115.0 116.0: 115.0 0.000000000 206,1: 

1 31 -1220527 - _ . 1220527 0_00000000; .._ 115.0.115.01 116:0;-115.0. 0.000000000 __-206.1% 

, 

Wipe HStag. H StaOC H SIaSe ^ Rho Rh oSlag. Hl eaTransfer Neal Fl Ux I Heal Rate 

Out In Out SIag.N OW Motlel 

(BIii86m1 • (BlWlbm) BN4bm bMM3 ' Ibmlil3) (&WS42) (BN)s 

1 MA 208;1 2MIJ 0.06179; -0;06119 . Miapapc 1_0_000E+00 ,0.000000000 

2 . 

3, - ,., 2 06,1 

A 206.1 

5 2061 

206.1 2061 0.06]19;,.00919 Ad'abatic I, 0,000E 00 _ OA00000000, 

206,1. 2061 0,06719 0067 19 Atlabatic', O,000E00- 0000000000 

_206.1- ^ . ,_. 206. 1- 0.06719 .006)19 . ... ,_._ AElaba^K - 0.000E 00 0.00,000000.0 

206.1 „-, _2061. ,. 0.06719 006719 Adibatiy 0.000EE00 0.00000.0000, 

6 

T 

ZW t 

206.1 

20611 ,. 

20611. 

2061 1 

2061 , 

006119 -,0067191 Gent Heat T 

006779 .006719 Gent Heat Tian. 

0.000E OD 

0.000E OD^ 

0,000000000 

0000000000 

8 

9 

_206,.1 

,21161_ 

2061^.___206.ti 

2015.0 111 

, 

10 

t. 111 

! 12 - 

13 

206,1 

_206.1 

206 ..... .11 

2416.1 

0.06719 .006719 L Gen1H -I Tian O.0 OE00 

20.8.1 0067 19 „0.06719 1 Gen7Heat Tran 0.000E 00 

2061. 2061 0.06529, 0.0135291 . Gent Heal Tan O.00OE 00 

206.1'. _ 206.11-10.067.19- 0+0919i Garill-IiialTnia. ;O.MEOO 

206.1 ... 206.11 0.06529.. 0.06529...... Gent Heat Tian. _. l ,..__._ 0.000Ea 00 

206;1 ^, .,, 2061 0.06529 006529 j_Gent HeaiT an d 0.E 000 00 

000,0000000 

0.000000000 

0000000000 

0000000000 

MOND= __... 

0000000000 

14 206,1 

206.0 206.0 0.08529 006512 _Genf Heal Tra . 1006E 06 _ 0.001182711 

15 2061, 206.0 206.01 0.06512 006506 Gent Heat Tmn,i IASIE06 0,000093336, 

16 206.1 2060.__.2060 006506 ,006502 Ge61 /teatTa_ LB62E06 0,000006090 

17 2(16.1 206.0 20601 006469:_ 006468 Genl Heal Tian. 2.851E-06 0.0000062,16 

1B 200.4 208.4 208.4 LO.W24 0.06626 Gent He at Tan. -5.910E-03! .0.0451 02514 

19 : 

20 

MA ^ 

207.7 

206.4 

208.3 

208.3 _._ O.M22 

_ __207] 006620; 

0.06623 

006662 

Gent Heat T.. 

Genl Heal Tran. 

-5.814EA)3 -0.012676M$ 8 4 8 1 

.4.907E431„: 0.5028522611 

21 - 206.1; 206.1 _ . _2061 0,06119 .006719 Ma ttatic O_000EMO1 _O.00QO mol 

22 

23 

30 

Ji 

206.1 206.0 

206.1 206;0 

20612061 

206.1 2001 

2060 

2060 

2061 

2061 

006703 

(106551. 

0.06119 

0.06512 

006702 

406541 

006719 

006512 

_ 

Adiabatic 

AO" b 1t 

Adiabatic 

Adiaba tic 

0.000E 001 

O.00OE 00 

O,.ObUE 11 00 

0.000E001 

0000000000 

0000000000 

0000000000 

OOOODOOM 

M JurcA'nn Table __ 

Jd Name Masflow tlP Stag PSag PSIag PStatc PStatt 

T UJ ncnon 

ra4t ) 

Total 

On. H2O Sid 

In 

m. H2O sitl 

f Out In I Out 

2 td foJ1 ('n H2O Std tall I (in H2O aid. 141) 

1 

2 

AM Poes 

HEPAFinel NO2-010 

00: 

00. 

OOD00 

00000 

_ 000000 

0000001 

00000 _ 0000001 

00000000000 

0.0000 

__...0.00001 

A5-513

I• 


Calculation No.145579-D-CA-056, Rev.1 

Attachment 2 

Page 23 of 46 

AFTArrow3.00upld (4 d5) - 3862006 

DMJMH+N 

AFT AIrew Mode1.00TS Bypass System T4l Model0 2(Clm Me% NYB 1508, tIS T knWeM,HT). 

JU Nama Mass F w dPSta9• PStag. PSlag. PSta66 PStaBD 

( TNUJUncBon T.1w in OM r fn Ow 

, _3 

H2O sm.) _^ti weosw.la>L 

.._. ]yam Charge r _:. _._OOr_.___ 0.000D _.._O.ODOW 

reo^rd. (g)L^. Cu

• 

• 

. 

RPP-24544 REV 18 

alculation No. 145579-D-CA-056, Rev. 1 

Attachment 2 

Page 24 of 46 

AFTA 3.0Ow (5 01 5). 32512006 

DMJMN-N 

AFT Avow Model. OGTS Bypass System T-N Model Case (Clean Filers. NYB 1506.115 T MbleM. NT) 

JM Sunk 

Nea 

._ 

I i _ _OA_0000 

: ...2 0.00000 

3 0.00000 

ncl'oa(LLw Table 

Jot Rpe, Pipe :. dP Stag. Total 

d Dr. ' (in. N2Ostd.) 

.... 

A5-515

• 

RPP-24544 REV id Calculation No. 145579 -D-CA-056, Rev.1 

Attachment 2 

Page 25 of 46 

A17Aji..3.01nWt (I d6) 3I25f200810:39 AM 

DMJMWN 

AFT Mdw Model. 0GTS Bypass System T-H Model .Cane 3 (UV fliers, NY61508, it$-FAmNed; HT) 

TNe: AFT Amm Madek OGM Bypass Syseam T-H Model Casa 3(Dlmy F6lem, NYB 15D9, 115 T Ambted, HT) 

Input File: M.Wemonsbadan SURVITIFisal Year 2006 WoAdCal oulafwnsbGTB Bypass Thermal Hydraulics MalysietWork F gn%ypass FIow8 

Wit Pipe Rev 1 Casa 3aro 

NumberGHSpes=25 

Ntwn ttOIJUrctions=25 

LengUi March SoLtion Method wM Mad, Number Umits 

Leng th Step Sl]a=12 Insists 

M Number lmrement=0.01 

Pressu es Tolerance, 0.0001 restive change 

Mass Flow Rate Tolerance = 0.0001 W.V. change 

Enthalpy Tolerance= 0.0001 relative change 

F Relaxation- (Mtomas) 

Pressure Relaxation= (Momafic) 

Raistaroe R.W.U.- (Automatic) 

Fhdd Database AFT St andard 

Fluid: M 

Max Flu ld Tempe rature Data= 1000 deg. K 

Idin Fluid Temperature Dab= 200 deg. K 

Molecular Weight -28.97 emu 

Gas Constant= 0.06655 Btu46mR 

C Scal Pressure =3].25 elm 

Crifical Temperature =13241 deg. K 

Acent ric Factor =0A21 

EquaBpn of Sete = Re01ir11-Kwong 

&flw0py Model= GenemNzed 

Spedfic Heat Rata Aces ary=High 

Ain esphedc P.., psi. 

Cxavitadonal Acceleration = I 

Standard Pressu re,-14.696 psis 

Standard Tempemture= 60 deg. F 

Turbulent Flow Above Reynoltls Number- M110 

Laminar Fie. Below Reynolds Number- 2300 

. 

, 

, . 

Tae Insatiable 

Rye Name i Pipe 

i Defined 

Length 

.. .. 

Leng thHyd raolis Hydraulq 1 

Units Diameter Dram Umts 

Fiction 

Data Set 

Roughn -Roughns es 

_Units 

. ._-. 

Losses (K) 

.._.... _. 

Initial 

Flow 

1 Mm Yes 69 ir¢hes: inchess , Unspe fed! 0:000151 feet, 2.931_._._ . 

2 : Pi 1 Yes 104 irohas: &M Mani Uns eared: 0.00015! feet! 0.211 

3 3 FE. I Yes 163 irohas! 4.026 inches; Uns ed0ed : 0.00D15i feet! 1.835 

4 _. 

!_5_ 

Pipe! 

Prpel 

Yesinches 

_39 ._. 6,065 , _ 

Yes 22. hesj 4.'. 026 

inshes^ Unspearied , _ _ 

inch es) Unsp, ecfied 

0.00015 

0 .00016_ 

..__(can.... 

feet 

0.161, 

0=32_..__, 

6 

] 

Pi of 

Mael 

Yes 

Yes 

]2 

141.5 

InrLes. 

inNesi 

6.065 

5.041 

InClesi 

inehesl 

Uns ecifietl O110D15. 

Unspecified'_ O.WDISi 

feet! 

feet! 

0.15: 

-0.47 i 

- 

e 

9 

10 

Pp 

,Ppei 

! 

PI 

Yes 

„ Yes 

Y 

6 

105 

8 

in has, 

h ' 

6.065 

6.065 

6065 

inchesl; 

mehes 

m he ' 

Unsp cfi d; 

Unsp afied - 

Uns ecfed' 

_ 000015 

0.00015! 

OW015 

leei l 

leei 

feet 

014!, 

01 

OOSI 

: 11 

12 

13 

14 

Ppe 

pipe! 

Tel 

Ppe 

Yes 

Yes 

Yes 

Yes 

6 

12. 

25t 

19W 

nches 

navl 

inM1 r 

nohes 7 

6065 .. 

6065 

8329 

8329. 

ches _ Unsp cf d 0.00015 

inches Un,eecfied _.. 0.000151 

Ut Uns afed DAOD15 

fn hes U.oesafi d 0.00015 

feet 

feet 

feet 

feet 

005 

122]941 

OH^ 

0.>] 

15 Pper ,, Yes 2>]5 Anchas 8.329 ches Unspeofed 0.00015 reel 132,. 

:. J6 FP''e! Yes ..,. 10 - _melest 832.9.,_ 

ches _Unspecified 0.00015 feet OA3^ 

: t7_ iQe Yes 12 1ncLesl 9. 329 inches Un d6ed 0.00015 feel 0.11 

18 ,vpel _ Ves 42 mW Si 8.329, inches Unspe c fed„ _ 0000'5......_.-lee,. 0.11 

19 Pme Yes 12 hx:nesi 8.329 Indies Unspecified 0.00015 feel 0 

, 

. 

20 Pipe Yes Sfi4 InrAesi 8 329 incbes U.neadged 0.00015 lee, 2.04 

21 Real Yes 104. 'inches! 12.39 4 ., inches_ Unsp._Ikd_ 6.00015_ feel 1.42 

22 . Yes 6 inches 6.00 inches UnspedS.E 0.00015 ,feet -0.04 - 

_ 23 ,. Pipe , .. Ves 260 .. i!m.'Lesi 6_065 Indies UnzpadfiM 0.00015 leer 0.11 .._ _.. 

A5-516

0 



Attachment 2 

Pago 26 of 46 

MTA..3.0 1W (2of 6) 312W2006 I0.38 AM 

Apt Aaa- Model. OGTS Bypass Systera T-H MWel Case 3 (Dirty Fiftere, IMS ISM, IIS*F Amblent, HT) 

I pipe 1; Name '. 

I 

pipe 

neg 

Lenaft Lenwh 

_ L Unlis [=. D% 

Is initial Fbw 

1 

5.W : 

Friction` R^!7rllou 

Mis a S4!1 

thnap" Met! 0.00011 teat 

losses (K)6 

i 31 Yes DSI feet Mw.-. arch- 1 1L. R.Caw 1000 

Mae lailialflo. Junctions 7 G-M&Y wleds! Size Type 11,enad 1 ArnInlentTent, 

t Units Dovm BousnJaw 

Cy—uricaLPipe, SWO __noWuwo _ ___ ... Adia laalki 

2 2,3 CytintaricalPip, sdnedtfla,40 A,flabafig! 

l.3 

.... 4 ...... . _ . 

_8 cCVqSLr"Rpz _jgRLlesL Sgttt. I _Aln^ qqirÂq 

4 q!_PyjKqjq 

_ ORA p SUL Lesj5^lM1 _q i _0 n schadu 40 

7 _—!a .. 

5. 6! CV5,unical Pips unspenJOW L 

&,RwtRL fs^ ... --, _- . - 

Axitabatta; ........ 

AdW a.: 

6.7 t Cylindrical Pip, Gln-dn acnefal.40i GereselltestTrzaars, 1151 

^----Aa:.cyon ^ Mp. S1.1als _General Heat T%nder 5 

0 13,9' Cffi wddcz^L^Qe SCqjn!e^sSaee1-_Aininch sdnedule Aq -^qkym rAt Heat ir 

9 9, 10! P&xlrazaiRm StainfossSteel; 6insin ^W^ General Heat Tramfiori 115 

115 

Elindi scinaftle ,14, Â"MTanslzr: 116 

12 12.11 Staint..Steel; Shnch .^1.0 G.naeal Heel Transfier l 116 

Cylhd. Lcql_Eqe__Sla1n.. Steel, Stnala sathedal. 10 _jqn 

.. .... ...... . 13,14 _ ,CyftdqqsMpe _^^ kftzs __ Steel L... 

flinch. 991, ^taul() 

--- ------ ---- General (3e heglLanskr,_ 115 

15 W .... 

^ .1. 14 ,4 ' _qyjigg. pine SqIjLlq^§!-L SinO ......... e bW.l QW . 1 0 .0 ngRI tinat . -- Transfer'____._. 

— 1 15.9 

Cidindflualljjxt ... Standess, Steel 8 inch sqhmOOLIO G.mnaf Heat Trernie r. Its 

17 -.1-611T.% (CArtd*ÎK,^- Sulafess snael - -Ain.h _adnW q IQ Gallon._LH.at Heat Transfer 

115 1 

Is 1 17. 18 ; CylintIrzalI . P . pe. 

I 

Stainless Steel flinch ..,schedule 10 General Heat Tnansfer. -il-51 

is, P , ^ C ^y9 a. ^Rijse VaW.as 5 aaqfl fli schedule, ad,e 10 G..apaf I 

20 .19,20. CylindricaMpe Stainless Steel-- Bindn sd,eda l- 1 0 General Heat Transfer : , .... 1151 

21 21, 12indn schedule.10- 

22.23 cylimecalmpa, SWja!qs,s Steel , 6ind 1 nagdUle40, -Adiat!x 4o.-1-- 

13 CyhnEfiwl P pe Stainless Steal . 6 indh schedule 40 Adlaballc^ 

30 a.m. CyHnd9caijFjpe ( , p,pmess sp,e, 51.W, ;;hedula,-Q 

31 1 4.31.-,Cyhnd&WPip*j Stainless Sleet 8 inch h.dula . 10 M bell 

Pipe M0,48at Temp. Special 

Units Condition 

1 None 

2 Non. 

None 

4 None; 

5 None 

6 deq. F None 

7 deq. F Non. 

8 d,. F Nona 

9 deq, F N. 

10 den. F None 

11 d,. F None 

12 d.q. F t'lans 

13 deg. F None 

14 d., F None) 

is d". F None 

Is deq. F 1,11one, 

17 deg. F None 

18 deg. F plane 

d4. F None 

YO F Nwe. 

21 None: 

22 None 

23 None 

A5-517

E 

17A 



Attachment 2 

Page 27 of 46 

AFT Affm 3,0 Fr,,,vt (3016) =Wmlomm 

DMJMH+w 

Model, ()OTS Byyass System T41 Motld Casa 3 (DiltyF.Rm. IWEI I-IM 116*FAvoW.nt HT) 

vetdseT—p- ! Speefel 

Units !Condfdort^ 

RmLmsTaW 

Rpe 

Loss. 

KTotal Staodard Kitre Smooth ;todte BA 

I 

Btflle;lly [Cylinder 

..Pqnd. , vapr^^ -VsNesj V^ valves 

Gah, 

valves 

GPobe , 

valves 

plug Powt 

; 

valves_I 

t2 123 1 (0.13) 

13 1 0.11 

21 1.42 

22 0.04 

Rp. Three way SwingLie s,tie- Cheek Taft Mc Stog, Cheek . ^3r"dpd L^ Conlredip 

oe 

Ewsloes 

Losses 

12 

Check VaNes vstv. Orifice Orifice' 

is 

21 

22 

23 

Rpe 

Leese 

iht;.. URS Uawmtal - 11ione',onoe I Screen Tee Addl Loss 

21 

23 1 j 

(GAR 

1 (1.1) (0.22) 

Area Chance Table I 

. - e 

I 

Area Change Name OEled aevotim amwo-Ina. w Pess.,. Inj U sw Database Type Geometry 

Unis UN's So.. 

3 Mee Change Yes 01.. feet C.,emd. 

4 Area Change Yes feet 

5 Yes con real 

7 6o. ^8,9e 's. * 

J., 

ConicalIZI 

n' 

Area Change M& Lose 

— LFadar 

3 22.1 D.4399 

4 22.1 DAW 

S 22.1 0.44 04 

7 26+; O.INI 

SZ,p,..osoF.o T.Ne 

C..â,e.IF. Name 1 Objed Elevation IniI!eIPsss.,. Initial Pressure =e 

i D.Enod S= 1 1 Units 

17 

p"sow 

N31-13D 1rwj 

__Yes 

P^^. 

. 

6 

Design Flow J -D.sign Ro^ I ôertt Mdeôcl W Ind Variable Dependent 

17 C 

I 

PAF. Curve I 

Rate Umts Coalguration van.we Units V=w 

A5-518 

p

• 



Attachment 2 

Page 28 of 46 

AF7Armw 3.0 Input (4W6) 3!25/200810:38 AM 

DMAdH+N 

AFT AmavUod.% OGTS Bypass System T-H Modal Case 3(Dvly Fille rs, N 1508:116-F AmbRm%HT) 

CompressadFan; Dep Vadabb i Compl .Curve 1 CompJFaa Curve Co phan CWVa ComplFan CUnre Comphan CUrve 

r Urim i Coretanla Cortslantb " Constant._ Consmntd. __COnshnta _,,. 

--_' N. H2O Sld.: 1248420! 1.571429E-03: -2285714E4 8 Oi 0 

ComgessorlFan Run 

PlIm 

Row1.1nils 

Added Press. ! Speetl^l 

a 

me Disshamelkdls Exce retied OnN I C P. . 

. Ad_rabaticj 

Dead EM Table 

. Dead EM !Name :Object :Elevation Elevation Initial Pressure IMtlal Pressure Database 

DBTmed 1 1kd13 Was $WfCe 

30 To Main OGTS' Yesi 0 feet 

31 i To baInBNEPA Yes! 0 met, 

^.,.;Comdoa.ItTabla 

General Component Name O*d Elevalwn , Ele,.k. IrAWPressure W.lPressure I Dalabsse Special 

0.1mad - Undo Units Soume Cmxlilion 

2 HEPA Flier NO2-010 Yes 0; (eel Nona: 

: 

10 

„ 18 ... 

HEPA Ftller WIVI Yes 

Snkdrafl Dam3er [._... Yes. 

OI fe.tl 

I 

O'__._._feet _ __._....._._ .._..__.. 

I I None- 

__......_.._ None: 

22 . HmeerBHEPA 

Filler Yes Oi f e el r No. 

. 

General Component I loss Loss hdepeMeM . IM Va aDla Dependent Dep. Va able Lou 

Modei ,Naha_;_, Vo able ,___ , U 15 ,_. Venable Units Constant a,_. 

2 General Poi omlM Variable' Vol FlOw Rate: fl3/mm- Ressme LOSS la H2O Std 2331035E47 

'.. 16 I General Poy,.W Vanable _, Vd Fl Rate.;_ na/ .I Pressure L.sal nH2O Std 5.475231E-17 

_ 18 

n 

General-PWpwmwi 

Genaml POiymomral 

Vanablei Vd Flow Rate_ 

Va able' VOI Flow Rate , 

k3lrtnn 

kYmn 

Pressure Loss im H2O sid 

ReMm Loss -- _in.H2Osid 

7.923]8]E-02 

2.602085E-17 

General Component Loss Loss Loss Lou 

CWStaMD -; COeatente _UOnstanl d_ Condanl,e 

2 0004481 0. 0 0 

16 .,.,-_1 4373333E 03 0 0, _.. _.._0 

18 168]181, de 3 4618E-0e 0 0 

n 000zs02: 0 0 0 

Heal Exchanger Table 

i Heal ExManger Name Obl¢d- Eleva tion Ell . : imwei Pmssu e I I oisal Pmswre I Database Spe cial -Type 

Defined Wits Units Source C ditkm 

6 _ ICV PIen m1 _ . _ Y¢s 0^__ feed, None 

H atE Manger Loss Loss I de,x de 1, Ind Namable ` Dependent Dep. Variable Loss Los - Loss 

Model _Value - Va able Unts -__ Variable U bo Cooslama Co sta tb! Constamc 

6 K Constant. 1.5 

'. Heat ExcDangex: Lou Loss ' 

Cautantd Constant. 

6 

Tn fakTm e 

" 

Tank Name Oblett Elevalkrn Elevation f Idtul Preaso a Ideal RIM. 1 Database R¢ssWe !( Pfeswe I T—Pal.wr¢ 

_ _ _ _D fined .... Dn is ... Wits SowCe 1, UNts .. 

1 AM Pres Yes o loot! 1431 pa15 

20 At. Pres Yes 0 feet! 14.31 Pat. 115. 

. 21 Alm Pes . ,. Yes _0 feet _., „. 14.3 Pie ... t15; 

A5-519

• 

u 

RPP-24544 REV Id Calculation No. 145579-D-CA-056, Rev. t 

Attachment 2 

Page 29 of 46 

AFTAm:,W3.0InW (Sof6) 3125M 610:38AM 

OMJAIN-N, 

AFT AfrowModel. 00TSBypass Syslem T-N Model Case3 (Di rty R#eo%NY81 W8; ti6*FArdWenLNT) 

, 

Tra*1 T.ra"alure I Bala nce Balance i (P IPe#1) Tide #?) (Pip. #3) (Pfpe 04) I (Ppe#5) (RPetl6) 

Emrg r^;,CmcenhaGm; NM;KOW Kln^_K_Out_ KIn^KdA KInÔut_ KIneK OUI KInr,K OUt^ 

4 drai F, NO Mai jP11G.G! 

it, 

... .:. #g1. F — No = NOI 1P21)O.OI 

l_ ..._... __ 

Tork (Ppe#7) (RP.0) (Ph*#9) I (plea#10) I (ppe 911) (Mpa#12) (Pipe#13); lRroe #14) i (Pipe #t5) 

_Khy .KOut . Kln,_KON,..K[n,K Wt_ NWr KOUl KIn,K OW., KICK OUI KN KOVt KIn, ,K Out- i . Kln KOu( 

t 

. I Tank (Pipe#16) (Pipe #17) (Pipe#18) (fte#19) (Pipe 1120) Viae#211 

(Pipe p22) : (PIDe p23) (Pipe#24) 

_K Ip,KOU) KIPKOUI KN KOUI KIn,K, ln KOut !f.t!i.K OVI KIn KOUt _Kh KCut 

kl (Ppe #26) 

KI KOuI 

j 

Tee m W e Table 

i Tee or Wye Name Obje ctElevation Elevation Initial Preswrei ImliniPreuura Database TeeNyye Lou 

Defined Units Units Source T e Type, 

3 Teed e : Yes 0. feet' Round Straight: Detailed 

9 

11 

Teed e 

,:_Tee ar Wye i 

Yesl 

Yu^ 

0- feet: 

0_feM'. 

Rou nd Strai hti Detailed 

_ RouncIS"Ilt;_Oetaila 

13 Teed wva Yes) 0 feel ROand Straight Detailed 

14 Teeor a Yes 0 feet Round S trai hl. Detaile d 

Tee or Wye Pipes I 

8 135 

' .150..._ .._.. 

it1 30 

3 46 

1a _ ......,., 135- 

Valve Table 

-. Valve 

_ _ 

t Name Oblept El.tlan Etavalbn IrudalPreuere Initial Pressure Database I Special Ert 69l 

..... 

Defined Um U _ Units. ._ . Source Condition Valve .. Preugrp 

10 my-wi; Yes 

RW.W2 Yes' 

15 V 166 ..__. Yes 

0 

..- ..0 

_. 0 

feet) 

f el 

feet _ .. ._ -.. _.._ 

_ 

...... . .. .. ... 

_ .._..... 

I None. NO: 

Nene, N 

None: I No 

19V-167 Yes 0 _ feel! No..; 

23 V-1781 Yes 

0: feet None' No 

. 

' 

Valve i Eait CdM CdA Los Loss I nde endent Ind Variable Depardlent Dep Vanable Lou 

UKto t i Units Modei _Vape Vat acts_ V Is Vanabl Wa Conslantd- 

10 

12 

_ 

. ... 

Cv COmtant _.1194 

Cv COruWnt .11941 .. 

_ 16 Cv DOnsWM' 24401 

t9 __ .__C Ccmaftank j 24401 _.._ .. 

i... ^?.. i _..... .... Cv Cansbnt: 3001 

"- 

_... 

A5-520

• 

• 



Attachment 2 

Page 30 of 46 

AFTArt IOMpul (Btle) 3!2512 0 0 8 10:38 AM 

DWMH•N 

AFTA Modek MTS Syv Sy00!m T44 MWWCm3(DMy RAers, Nn 1508, 115-FAmb(eµ HT) 

hvalve l Loss Loa, , Lan 1 Less I 

A5-521

0 

• 

11 

AFT Anow3.00upW DMIMH-M 

(t of 5) 

3/2512008 

AFT And/n Model, OGTSass Byp System T-HModd Case 3 (DIM FlOen, NYB 15D8.115'FAmbkrt, HT) 

TiUWAFT Arrow Modal,OGTSBypeas System T-H Model .Case3(OOIy FlIWv% YB 1508,115'FAmMent,Hf) 

A WyNsrvn. 25/2D0610:3150AM 

Application version: AFT AOowVentla 3.0(2005.09.14) 

Input Fibs M1Demondralfnn BWkVYW"Yew2D06 WdMCdMaSDraXOGTS Bypass Income Hydau KcsAn"Work ay F9eSWYPass Flow 8 

InM W.P. Rev 1 Casa3am - 

- E,asalion Th. 1: 46.78 (105.78 seconds) 

Tdd NumberINPressure ltardias=5]2 

Total Number OI Eralbnv 196 

Total Num Number Of Entlelp nthelpy llemGOns = 196 

Nwnber Of Pipes= 25 

Numberlit Js•25 

Ma MeekMethod = i1a Gaussian Elimination minatl 

1en91h Mordn Solution Method vrilh MaN Numbn L1seft 

t algth Step Size= 12 inctues 

Mach Numbar lrsramenl= 0.01 

Pressure Tdma saw 0.0001 reative charge 

Mass Flow Rate Tdemnsr 0.000t relative ch"a 

- .. . 

Entialpy Toletance= 0.0001 relative chae rg 

Flow Relaxation= (Attlorms.) 

Peasswe Relaxation= (Automatic) 

Resistance Relaxation= (Automatic) 

Fluid Database: AFT Slandand 

Fsfd. Air 

Max Ffuld Temperatwe Data, IM deg. K 

Min Fluid Tempetalwe DaW= 200 deg. K 

M deMar Weight 48.97 am 

(3e. =fl.O6655 [Runum,R 

Cdtical Praawe =37.25 abo 

Cliilmal Tempeaure =13241 deg. K 

Acentric Factor =0.021 

Equation of State= Redlich4Cmotg 

Enthdpy Model= Generalized 

Speck Heat Ratio Accuacy-Kgh 

Almosphe nt, Pressure+ 14.3 testa 

Gravitational Acceleration=lg 

Standard Plenum- re pine 

Standard Temperature = 60 deg. F 

TurWlentS w Above Reynolds Number- 4000 

laminar Flow Below Reynolds Number-2300 

Total Inflovr- 0.8981 Woes 

Told OutOOVm D.8981 IbMsec 

Total E. W Wbv, 2535 Beef; 

Energy OdMnr-1910 Btu2 

Total Heat Trandemed Into System=-58.43 &Ws 

Maximum Prassa uis 

1494 psis d Junction 17 Outlet 

Minimum Pressure is 13.83 pole at Junction 171n ct 

Maximum Static Temperature is 815.0 deg. F at Junction 60dlet 

Minimum Slats Tempeature is 115.0 deg. F atJuncfion 23 Outlet 

COmOreasorlFan Summary - 

Jct Name Mazs I 

FI I 

Vol. 

Fbw 

I DP 

Stag. 

DP 

Static 

Overall 

' Efoc. ty 

Sped 0 wall 

Povre 

Comp. 

Ratio 

BEP 

O 

BEP 

Was 

(scfm) (h3kcin) (I.Moold.) (b 1 -12O std ) .jPercentl CPemenl)' lhp) lPamegt) (D3/aec)..-.(tEm/sec)- 

17 N311301 7055 1 966.51 14.24 14251 6]A0 1000 2.971 ___ 103J N/A WA 

: jet %of 

BEP 

(Pement): 

.. 17 WA 

Vol'. Summary 

A5-522

• 

• 

RPP-24544 RFV Id Calculation No.145579-D-CA-056, Rev. t 

Attaclunent 2 

Page 32 of 46 

AFT Art. 3.0 WW (2 d5) 3/252006 

DMJMH+H 

AFT Artav M6de1 OGTS Bypass System T-H Mod el Case 3 (Dirty FlOers, NTB 150% 11S TAmblard. HT) 

! Jcl Name 1 Vol. Mass { _DPStag I DPSWfie i PStafic f K ! Valve ' Cv CV ^ . 

Type Flay I. 4 i Inlet i 

Slate Fst. 

-10 

' 12 

HVSOT':REGULAR 

HV402' REGULM 

QdNsee li (Inim_' SP^L_,.(Wla.^ 

028609: 0.00586591 0_ 00586871 .14071 

0.06863'. 0.5. 000358 0.0003585: 14.0]. 

,00^1_,OpeO; 1194_0 

Q9]4i -. n 1194A 

WA' 

WA 

. 15 - 

19 

3: 

V-166: REGULAR 

V-161: REGULAR 

V4781 REGULAR 

0.89811: 0.0078699' 0.0018]56 113.98. 0.7770! n 

0.898/1! 0.00636921 O.ODTI]d]^ 16.33: 0.7770! One 

0.54598' 0.1634032' 0.183%1]1 14.241 13.7055: n 

2.440.0 'WA 

Zr 

300.0 WA 

Haat FxfllanDer Summa : 

&t mm ! Mass 

Flow Dina 

7 DP DT 

Loss. 

T 

INet 

T Heal 

Oullel - Ratein.; 

J.'.f93it._ agsF Fl. Cde9 Fl.:. (e!w;) 

10VPIepam: .0.35250.03881:002461!.,.]600114.78797;,_,66.191 

V.. Outnuit 

Pipe Name Was Vol. i Vel.us i Val. Ma Mach dPStag. pan. P Sues Out 

! Flow plow Avg Out : Aln Al eut Total In 

i- .....__..Cu/m7. _^0m^_CfeOVSecJ^_(1eeVmin)..... _..... .. _^. Pn. H2O S1Q.) Cm. F120 s[0, (9))I (m.H2O;Id.(q)). 

1 Mine 376.91 315.0: 26.156' 1,571.1 1 002233T :0022362' 0.4325368 0.0000 -0.43253678 

P'po. :2]6.91 316:4 26279. 1,5]]0 O.D22442^ 0022446: .,- _ 007]8/51 _.__ 16446 . ,._-1;92251182 

3 3FES 276.91 317.5 59.721'1 35993 0.051011' 0.051239 1.7453793 -1.9832 4.]285806] 

4 + Pi 276.91 318.0 26.413 t 584.9 0.422556 - O-M2 B' 0.0406270 -3.8395 4.88013339 

.,. @ _Pipe ,. 2]6.91 . 3 0051292 0051333.0:30]8310 ..__ -3.9412 .4,24902391, 

, 

, 

6 

7 

Pig, 

P e 

276.91 

278.91 

727.6: 

689.4: 

61.02 

_85.591 

3553.6 

4,788+6 

0.034694 

0.049146 

0.034004 

0.047467 

0.1227523 

0.66282601 

5.3234 

5484] 

-5.44618222 

4.12755585 

8 mas 2]6.91 663.9' 55.234 3.304.2 0.0328470.032799: 0.0482235 -8.12]6 -6.1]3]/9691 

9 Pipp 224.72 5362 ! 44.682: 2.664.6 0.026611 0.026529 0.00665241 -6.1609 -6.16752291 

10 

11 

J 

14 

- 

Pie 

Pie 

pe 

Pi a 

Pie 

224.72 

5218 

216.9L 

705.46 

533.6 

1244: 

__ 

611: 

893.5: 

44.429, 

ID.W6' 

28 B3ti 

47.482: 

2.653.5' 0.026540 10.026478: 

6180 OOD6179- 0006156' 

6092 OOO6t56; 006112 

15350 001 7278 •OOt6284 0. 

2402.4 0.036313 :0.032468: 

0.0164927 

0.00018561 

0.01296161 

0.05416941 

1.5365945 

-6.3299 

634401 

,_-,- 635971 

--6.34481 

-8.4176 

-6.34639182 

-6.34413515 

. -6.38]62238 

-6.39901018 

-7.95403051 

15 Pi ei ]05.46 903.3: 60.040: 2.372.4' 0.032466: 0.032283: 0.5633062 -].9540 -8.49]33448 

16 

9 

18 

_ )9 . 

20 

21 

u _. 

1 

Pie >0566 1 

Pi e, 705,161 

PiP.?.. 705.461 

Pie 70546! 

Pi 028.55 

Pipe :42655 

897-9 39.562 !2,372.5: 0.032302: 0.032299' 0.1316749 

906.7 39.998' 2.395.6 0.032630 . 0.032624 :0.0385944; 

887.1 39.116' 2342.0. 0.0317W' 0.031676 0.05593251 

686.4_ 39058__ 2,342.1„ 0031696;_0031687 OA072067 

876.3 39.056' 2288.5. 0.031704 0031363 099490371 

68].2 9.698 581.9 D.008281 0.008282:. 0.0301733 

_489.0 -40623;_ 2;43].5 , 0,03,4695; 0.034695 .0.0194820 

.8.7152 

-12]728 

1.4209 

1.11 72 

0.8949 

O.000D 

_ 12492 

-8.84684849 

-12.81135082 

1.3]308323 

1.10994458 

-0.00062640 

-0.0301]330. 

, ...4.26667771! 

23 Pie 428.55 ( 494.9 41.096 246]8 0.035096' 0.035127 0.3210566 5.7918 .6.11285210; 

30 Pi 0.00' 0.0 O.WD O.D 0.000000 0.000000 0.0000000 -6.1218 .6.12155585 

31 Pie OA01 0.0 0 .00 D O.0 0.006000 0.000006 0.000000D -0.9540 -7.95403051 

:Ppe P 1. 

POut I a Slag ]Sla ]Slag ] Static ] Out tlH Stag H 1. HSYag. 

In 

Out - IMet OuVel In WI I 

In Oul 

_Cm. H2O std in. H2O std (den. F7 Idea. Fl d F d . F d . F ! B1mIDm I BIWIOm Blulihm 

1150 _114.9 114.91. 0.00DDO 206,1 120-11 1 -0.13732 _.,. -0.569991 _0.00000104.. 115.6 115.0..114.9 114 ,91_0.DODOD_ . _.206.1 2 .1 

2 -_._,-?;902$9 -206050(_.. 0.00006106 J 15.0 . 

^._ 3_ - _ -2.69509 -444366` -0.00140381,_ . :115.0 ttSQ _ 1161 H4 7DA0000^ 206.1 206.11 

978t 06 ll - 4 - 401880 O.O O,PI0d 1150 1150 114.9 1149 0.00000 1206.1 2118 

5 -4.65]35 -496961 000024414 1150 1150 11431167 , 0_000001 2061 206.1! 

6 ,_. 5.69]032 _-575713 5245581055 8750 8225 8_747 8223 -1311316 393,81 3807! 

7 -6.133921 =6_]328] 8847631836 82251 7341 8220 733.6 22065]51 38D,7 ' 358,6 

8 b.41]5] -666292 386§28320, 73411 730.4 ]33.8 7302 ,- 0912701_ 358fiC 357?. 

A5-523

• 

0 

0 

RPP-24544 REV Id Calculation No. 145570-D-CA-056, Rev-1 

Attachment 2 

Page 33 of 46 

AFT Arrow 3.00utp01 P015) 

DMJMH.N 

AFTAndw MadeI,OGTS Bypass System T-H Model Case 3 (D0ty FOlers, NYB 1508, 115'FAmbimt, HT) 

Pipe i PSMWU. 

i m 

_. i rm. H2o add. NJ 

9_.. 1 _........ 4 ; 35723 

10 

-6.51920 

PSIetle 

Out 

IH12ogtl. (g1L 

8 556]5 

ES3282 

dT Slag. TSteg. 

Wall 

aeg: es_ F ^d 

-]1613':' 5254 ]30.4 

SAT2290W: 729.1 

TS1ag: 1 TSUVo TSiadc 

Outlet in Out 

d I Idea. Fl. 

723.11 

717.7' 

]302: 

]23.0 4 

723.0 

7175 

did Stag. 

iBtw ) 

_ -1 .69789 

-1.36242 

HStag. 

In 

_Ca!Wmm 

,....357 .7 

3%.9 

6 

HSmg. 

Out 

Lwm!nL 

355:9 

354.6 

' it 

12 

13 

14 

i 

i 

1 

4.35624 

4.36485 

4.42509 

4.71PIM 

-&35492 

48]765 

-&4]023 

-8.23802 

4.655D2930' MA 

-1 11 93359375 :7213 

-13261479492i 715.2 

-121.33561707 2995 

721.7' 

704.6 ; 

582.8'. 

178.1' 

MA' 

721.7 1 

715.2 1 

299.3 

721.7 

704.8 

5628 

1]6.0 

-2.154]1 

-4.21356 

32.67941 

-24)71969 

357.7 

355.61 

354.0 

251.2 

355.6 

351A 

321.1 

221.5 

15 

16 

I 

i 

-8.23802 

4.93579 

-&""9 

-9.12731 

4.82202148i 

-0.52]5268& 

178.1 

169.3 

169.3; 

168.8 

17&01 

16921 

169.2 

168.7 

-2.15633 

-0.12691 

2215 

219.31 

219.3 

219.2 

17 

18 

19 

! 

i 

i 

-13.05609 

1.15158 

0.84013 

-1109455 

1.09626 

083308 

-0.34875488i 

-1.43W8813i 

-0.402771M 

168.8 

178.5 

177.1 

168.41 

177.1 ' 

176.7: 

16&71 

17&4 i 

177.0 1 

10.3 

1T7.0 

176.6 

4.08524 

4.34976 

-0.09647 

219.21 

221.6 

221.2 - 

219.1 

221.2 

221.1 

' 

20 

21 i 

0.81168 

-0.0188] 

-027056 

-0.04905 

-1624743652! 

0.000386211 

M-7 

115.0 

1604): 

11&01 

178.6 

t 

115.0 i 

1602 

115.0 

337076 

0.00000 

221.1 

206.1 

217.2' 

206.1 

n -1.5/931 -1.59879 

t 23 ,: ..,,. __6;125]6 .,,. __ . .6. 44708 

30 i -6.12756 - .127% 

31 -7.95403 -7.95403 

0.00000000' 1150 11&W 

41.00024414 -115.0 -._1150 

0.00000000: 736.1 73411 

O.OD000000 98.1 118:11 

114.9' 

114.9 

]34.11 

1]0.1 

114.9 

_1143 . 

]34.1 

176.1 

0.00000 

, O,OW00 

MODOW 

0.00000 

X6.11 

206.1_ 

358.8 

221.51 

206.11 

20&11 

358.61 

221.Sj 

' Pipe HSI Vc i HStalk 

In Out 

_ S Wbm ! flBluftell 

Rno 

Slag. In 

IbMN 

Rho Sm9. 

Oud 

aAWI 

Heal Traralar 

Model 

I Hal ^ 

Flux 

IBiW fl2 1 

Heat 

Rale 

(BIWS) 

-. 1 296.11 206.1 0.06)19: 0.06712 Adiaba 0.00000 

0.00000 

0.00000` 

0.00000 -: 

0.00000 0.00000: 

0.00000 0.00000• 

0.000001 0.000001 

4.485261 4$2296' 

0.49927 .7.77862 

-04052 .0.32175' 

4137226 -0_.51]19, 

-036822 .0.38977' 

4).18026 -0.14313' 

-0.1]62] 1-0.27989 - 

-0.25414. .11.59095 

-0.07460 .26.69146: 

0038411 - 1.93663 

-003340 _ 4).11578: 

-0035111 0.07655. 

-D 06116 -0.31413 

-004056 ., -0.08843_- 

41.034801 -3.56619 

0.00000 0.00000' 

0.00000 O.O wo 

000000_ 0:00000: 

OWM I0.00008- 

O.Nml 0.00000 

tic 

2 206.1' 206.1 086688.' 0.06667: Adiabatic 

3 206.0' 206.0 0.066861 0.06656' Adiabatic 

4 206.11 206.1 D.06654! 0.06654'- Adiabatic 

5 

6 

7 

8 

206.0' 

593.7- 

380.6.' 

356.6' 

206.0 

380.6 

358.5 

35]]1 

D.06653- 

D.02853'- 

0.0290 

D.03183 

0.06647' 

O.D2969 

0.03183 

D.03192 

Adiabatic 

Gml HeatT.. 

Genl Heal Tmn. 

G del Heat Tran.. 

9 

10 

11 

357.7 

3559 

357.7. 

3559 

3545 

_0.03193 

003211 

00319E 

0.03212:_ Gen'1Heat Tran. 

003226 Gann Heat True. 

003214 Genl Heal Tr ue. 

12 - 355.6 351A 0.03214, 0.03261 Gml Heat Tran. 

13 - 353.9'. 321.1 0.03]62' 0.03842' Genl HealTmn. 

14 

15 

16 

17 

251.2, 

221.5' 

219.3 _ 

2192' 

221.5 0.050021 

2192 0.05931 

2192 0,0600_3 

21911005945 

0.05931 Gmi Heal True. 

006006 Ge lHeal Tran. 

008006 , Genl Heal , 

Tan; _ 

005948 Gml Heal Tran 

18 2215 22 

12 0060]1 006086 Gen, Heal Tran 

...19 221.2. 221.1 0.06000: 6 0.06086 . Gel Heal Tran. 

- 20 221.1' 

0.06081 006226- . Ge (Heat Tran. 

21 206.1 2061 0.06 19 006719 Adiabatic 

22 

' - 23 

30 

31 

206.0, 

206.0:_,. 

356.6 

221.5 

206.0 

20601 

3586 

221.51 

0.06698 :0.(16698 

O.OW21 0.06616 .. __ 

003183 0 631 63 

0.05931 0.05931 

A4lebalk 

AdaEalic 

Atlabadu 

Adiaba tic 

Ad Junction Table 

; Jet Name Mass Flax ^ dPStag. PStall. 

TMOJUrKOm TOW In 

_ - 

t Isctm7 ((. H2O std) (n H2O std. (90 

Alan 

i 

Plus! 27691 0.000000:. 0.00000 

2 _ HEPARIletNO2010 r ._27691'_ . t.4t2121 ,.. __063256 

__ 

PStag. PSlak, PSmOe 

Out 

In 

Out 

(in H2O std. fg)Z Iin H2O std (gIi 1 n H2O std. )L' 

0.0000 0.00000 

0.OWDI 

4_8446,. V.56999 __...[1.98261 

3 Ar Ch 1 2]691' 0060672 -192251 

-19632 

-206050' 

-2.69511 

A5-524 

I 

^ 

I

III • 

• 

E 

RPP-24544 REV id Calculation No. 145579-D-CA-056, Rev.1 

Attachment 2 

Page 34 of 46 

AFTAeoN3A0otPut (4 815) - 

DMJMH-N 

AFTMO Modal, OGTS Bypass System T-H Rbdet G903(o1Hy Mtea. NVB IWO. 115 •FAmW.1, HT) 

- 31262008 

. 

. 

;Jot Name - Mass Flow dP Slag. PStag. PSlag. 

PStedc PStaOc 

Thu Junc88n Total In out - 

M out 

,.9 :... .._. 

S 

[n_1120 sW. (g))%.LU5.N20 sU1..19)).)-.Cm. N20sW. (9)1 ..CaAR-Std.19)).. 

Area CM1A0g0 - --...26.91. 7 _ O.1t0921 .. _-3.72858._1:8395.. ..... _4,44366 -...,_3;9782, 

AreaC 

276.91 910.06105 3.88013 A.941T 4.018801 ' -4.6574 

6 IGV Plenum 276.91 1.074394• 4.24902! 3.3234 4.96576: -6.6470 

7 Area Clon2a 276.91 0.038586 -5."6161 .5,48471 535713 -6.133 

8 Team a WA' 0.000000 3.1956! -6.1276: 4.60091 4: 

9 Teew NIA Sea Losses -S.IM7! 4.17371 -8.38114; -6.3811 

-: 10 HVA01 22432 0.162371 -6.16752: .6.3299: 6.35675 65192 

11 Tae or Wye NIA See t.oeses -6.34484: -6.344a -&45194 4.4519 

1 12 HV-902 52JOI 0.009923 -6.34474 -6.3547: -6.35492 -6.3649 

13 TeeorMe NIA I See Losses 4.41746E -6.4174: -6.60562' -6.6858 

i 14 TeeorWye MAI O.000OW -7.95403' -7.9540' -8.23802: 42300 

4 15 V-166 705.461 0.217844 3.49733: -8,7152: A27779i -8.9958 

' 16 HEPARter1361M 705.46 3.925915 4.84685: -12.7728 .9.127311 -13.0561 

17 N31-130 705,46 -14240259 -12,81135! 1.4289`. .13:09455:' 1.1515 

18„ 

19 

9ackdraBfuen to 

V-167 

. __70546 

705.46 

-- _, 0.255927 

0.215057 

..,,1.37308: _ . 

1.10994: 

....1.1172 

0.8949' 0.83308: 0.6179 

20 A" Prey 705.46 0.000000 000000' MIMI 0.00000' 0.0000 

.?1 . _ „-,. Alm Pres...- 42855 . 0.000000 . 

0:00008- 

0.0000 

0.0_0000, 

,0_0000 

9 Healer& HEPA Filer 428.55 1.219023 

-0.03017 4 .2492. --- -0.04905: 

-1.5793 

i 27 V-178 428.55 4.523103 -1.26866 -5.7918 -1:59879! 41 258 

m 

31 

To MaIa OGTS O.W 

To Tr.4 eHEPAL ...... ..._ OW _. 

0.000000 

0,000000 

-6.12756 .6.1276 

_ _-7.95403 _,_.. _ .c795a0 

-6.12756: 

..___ 

4.1276 

. id dT Slag.TSla9 TSlag TStakc TStaUS i 

1 Inlet i Oullel M 

(deg. F i (deg. F Ide , f Idea. F1 i 

Out 1 

de . F 

]_95103 

. 

-7.95441 

dH HSIag. l MStag. "Static HSlm. - $wlc 

1 

2 

3 

d 

5 

5 

7 

B 

9 

10 

11 

12 

0.00000001 -015.0; 115.0 115.OP 

-0'.001159] 11501 115.0 114.91 

-0.011036621 115.0' 115.01 114.91 

000024411 _11501 .,1150 . '114. 7 1 

0 WD3662 115.0: 1150 114.91 

760.0000153 1150- 87501 114.7 

00001221 822.5 822.51 822.3 

O.WWOW 734, 1' 734.1: 733.7 

O.ODWO(XI 730.41 700.4 , 730.2 

1 

DAMN() 

1 MA! ]23.0 

000000001, _ _ _... 7 15.2 715.2E 715.2 

O.OW000OI )21.] 721.7 ' 721.7 

115.0: 

tta.91 

114. 7 1 

114.9 

1147 

874.7 

822.0 

733.7 

730.2 

723.0 

7152 

721]1 

Slag. In Out 

6tvi0rn estuarai t61u86m 

0.000 206.1 206.1 

0.000 208.1 206,1. 

0." 206.1 206.1'. 

0.000 NSA 200.1 

0.000 206.1 2061 

48].755 20&i 393 8 

0.000 380.7 _ 380.7 

WA 350.6 356.6. 

NIA 357. 7 357.7: 

O.WO! 355.91 355.9 

NIA. 354.0 35x0 

0.00D! 355.6 3556 

In Oul Area 

91ullea &.tent (1ea12) 

20&1 206.1 0.007734 

206.1 206.1 0.WT742- 

206.1 206.0 0.00]7]1' 

206.0 2061 0.007807 : 

206.1 2060 0.007810 

206.0 393 7 0.007816 - 

380.6 38D.6- 0.011753 

358.5 358.5 NIA - 

357.7 3577 NIA 

355.91 355.9 0.09173 - 

353.91._ 353.9 _...... N/A'_ 

355.61 355.6 0.002138- 

13 

14 

15 

0.0000000: 

00000000: 

06001831 

299.5 

1781 

1693 

299.5 

1781 

1693 

299.3 

IMA 

1 69 .2 

299.3 

17 8,01 

1692 

WA. 

_ NIA( 

0.066 

251.2 

22151 

2193: 

251.2 

2215 

2193 

.251.21 

221.51 

219:3, _ 

251.2' WA 

2215. _ NIA: 

2193;_0,0210]1: 

1 6 

17 

18 

19 

20 

21 

1 22 

23 

3D 

31 

6 662563$^ 168.8 

10.07287601 168.4 

-OAW12211 1771 

-0.0001836 

0.0000000 51150! 

000000011! 1150. 

DW11597 11&0 

00036621' 1150 

00000000: 7341 

00wml 17811 

1688 

178.5 

1771 

17 I176 7J 

11&0 

115.0 

1150 

115.0 

734.11 

1]8.11 

160] 168- 

168.3 178.4: 

177.0 ^. 1 77 0 

1 76.6! 1 7661 

115.0: 115.0 

115.Oi 116.01 

11501 . ^, 1149 

1149 1149 

73411 ,. -7341 

178.11 1781 

0.0001 

.2.460! 

_0.aoo! 

U.WOI 

0.0001 

00001 

OOWI 

0000 1 

0000 

0000 

2192- 

219.1) 

22121 

221.11 

206.11 

2001 L 

2061 

2061 

3586 

2215 

2192 

221.6 

2218 

221.1 

206.1' 

_2061 

2MI 

2061 

3586 

2215 

219.21 2192 . 0.02tOSI: 

219.11 221.51 0.021293. 

221.2 2212' 0.020875; 

221.1 221.1 0.0206825 

206.1 ZW.1 0.020472! 

20011 2001 0011969;, 

2061i 2060 0011970. 

20601 2000 0012000 

3566 _ 3586 0000000: 

221:5t__ 2215 OOmoo 

Jwdlon Lass Table 

A5-525

• 

0 

RPP-24544 REV Id CalculationNo. 145579-D-CA-056, Rev.1 

Attachment 2 

Page 35 of 46 

FFTArrow 3.00Nût ... (SOfS) 3854006 

OMJMHiN 

AFTAnwv Model; OGTS Bypvs System T•HMOtlaI Cane 3(OIM1y FiOen,NYB 1508, 115.•FPmdent.FTn 

j dc! Pip%; P(ps j dP5lag•Tobl I .. - 

A5-526

0 

• 

• 


Attachment 2 

Page 36 of 46 

AFT 3.01npM (1 of 6) 3125/20 0 6 10.31 AM 

DMRMI+N 

AFTAmw Model, OGTS Bypass System T4lMMd Cass 4(OMy Fate., NYB 1608, 115'FArnden1, HT) 

Tito AFr Arrwv Modal.OSTS ft. System T41 Model Cese4 (DMy Filte rs, We 15D% 115'F Ambient, HT) 

Input Rte: MODemwsba tfon Butt VIPFlscal Yaw 20M WwWakulOWs"iS eypaas Thermal HyUmollm AnalystslWmk F98SIBypass RM8 

bhM Pipe R" t Case tam 

Number Of Plpev 25' 

Numberm3unc9whs-25 

Length March Solution Method Wd Mar, skaobM 1.1"Is 

Lwhglh Step Size* 121mihes 

Mar, Nlao er ItsapolaW 0.01 

Pressure Tole a= 0.00 131 relative Menge 

Mass Flax Rata Towne 0.0001 f¢IaWO change 

Enthalpy Tolemr 0.0001 relative Mange 

Flow Ralatat.• (AutomeTic) 

Fressom Relaxed.- (AUlwnagc) 

Resistance ReMaton= (Automatic) 

FIUW Database: AFT Standard 

MWA, 

Max FWM Temperature Data= 10013 deg. K 

Min FNId Tempemlum Data = 200 deg. K 

Molecular Weiol =28.97 am 

Gas C at ppwal =000655 BNabm-R 

Credal Terppra oe -1 3arm 

Ace TempdmMe ^12 d1 dag. K 

E,u.%o .fSWe-021. 

Eauaton M Smle= RMfi lazed Enmepy MOde= eW 

Rat io Awt 

M.o 

pHeat io Accuracy =High 

AtosphMC Pressure = 14.3 esta 

a Accelerate.- 1 si g 

St,nd 

t.e 

Standard 

Possum ra=W psis 

StandardT 

1 w iaanlb 

Mw Above Reynolds Number- 

Laminar Fbw B.I. Reymlds Number- be00 23OO MOO 

, 

Pi In ul Table 

Pipe-- Name Pipe 

Oefi ed 

18rh3U Length I Hydraulic: 

U Is Diamator 

Hydraul< 

Dam Units 

Frictim 

Dale Sal 

Roughness I RougMeu f Losses (K) 1 Imual Fbw 

Units 

-. 

1 

2 

3 

4 

P"hye .,._ 

pea! 

FE.J 

Ppe 

Yes_ 

Yes 

Yes 

Yes 

66 .,, inches 

106 Mnes 

163 Inches 

39'-- nchea 

6.065. 

6.055z 

6.026 

6065 

nrheal Unspecl0ea_ 

inMes! Unspecified 

nches UnspeOfred 

ndnes„UnspearM 

0.00015 

000015 

00 015 1 

0,00015 

fast) 

feet 1 

feet 

,,,feet 

_ _ 2.931 

0211 

1635 

Oi6^ 

5 Fee Yes 22 bes 4.025 ntslwi Unsp.dfi ad 0_00015 feet 0.321 

t 

6 

1 

8 

9 

steel 

Pipe 

Pme, 

Pipe 1 

Yes. 

Yes 

Ves 

Yes 

72 inches 

141.5lOes 

,_6..,_ nches 

10.5 , nches 

6.065 

5.04] 

_ 6.065 

6.065 

nchesi U ..ce." 0.00015 

nomsh Uns afM 0.00015 

mches^ U ape fied Odeals 

nr,es „ U speafed-__0.00015 

fast 

feels 

feel) 

.,. . fast 

0.15 

0.4ii 

0.14 

_. 0 

10 Pioe Yes: 8 Inches 6.065 metiesi Uns eafi ad 0.00015 feet) 0.05 

fl Ppe. Yes 6'_ nMes 6.065 iQches t_ U specfed „_ 0.W015 _ _ feet 

12 Pipe 12. nrnas 6.065 nMes'' U sp kdl 0.00015 feet 1227941. 

13 Poe Y 251 imhea 8.329 nMes! U tied. 0.00015 feet) ON 

14 Pipe Ves' 1969 nMes 9.329 hv,esi 

i 

_ „ 

U peafetl^ _ 0.00015 _;. _. feet 0.]] 

{ 15 Pipe 

_ Yes 2P 5 , inches 8.329 imhesi. U ape find 0.00015 tot 1.32_ ..... 

I_ 16 Pipe Ves,18_, inches 6_329 inc h¢ -Urhspeofm0 , , 0.00015 . (earl .0.43 

._ 

t] Pie Yes. 12 inches 8929 motes! Un ogM' 0.00015 feel 0.11 

f 18 - Pipe Ves, 12, . moles .. 8.329_ ., _. , inches _UnpP . 

adOad_____ 0100015 __...__._ fee;!__.. 0.111 

-' 19 pips Ves 12_ ches 8.329 nMes . U ape fled .,, _ 0.00015 _feet 01 

20 pia Yes 584 Inures 8329 nMesi Unsoearetl 0.00015 feet 2.04 

;N ..__Pin Ves IN inches 12.39 1whets, Unspeoged 0.00015 . _feet 1A2 - 

j 22 ,Rye Yes . 6._, nMes 6.065 nMes' Unspeafed_ 0.00015 ._., feel 0,04 . 

!_23 Pipe. Yes 268_ _inches „ _6.065 inehesi_ Unaperlged . ,. 600015 (sell ,. 0.11 ,,,__.. I 

A5-527

• 

0 

RPP-24544 REV Id calculation No.145579-D-GA- 056a Rev.1 

Attachment 2 

Page 37 of 46 

AFT 3.01np Ut .. (2aw 3¢5200 6 10:31 AM 

DM3MHIN 

AFT Anow Model; OGTS Bypass System T-H MoOa Case 4 (D41yFiIXers. NVB 1508.115'F Ambient. HT) 

Frye Name Pipe j l Wh length Hyftwie, i HydrouR Fd.Sm RmgMass Roughness lnsses(IQ Imtial Floe 

G1MfleL;Diam. 

I 

i 30 f P Vass 0.5' lest S.047 ; Inches Uned 0.00016 feel 0 

i 31 i Pipe _.._Yes:_ „ Q,S ^, feet _8]29: inches Unspedfied OA0316 feel 0,,,____ 

I Pipe IM6a ' toms.: Geometry Maleda I Size Type Thetas. :. AmNeMTemp. 

l UMts Bountla 

i_1....(,.._.._.._i.._:.__12, Cy6Mrina WpeSginless Siael ., 61nrh.,_sNee00,40 _...:...___... Atliaba5d _..__.__....._ 

[ 2 ( 3f 'wi SbWess Stets. stwt wdl 040 ASâbelic 

3 1 i 34 CyRntlnral ape SNiMess Sleep 41ndtsdledW040 

',.4 ,.... :_( 4CylirWnca pipe StaWW _ess$Well Binch_,Wl We40 

' S 5 6: G calR ns neat Atliaba5c. 

6 6,7i C finddca pi Stainless Steel: 6inch s etlWe 40 Gelier4lHea Translw. 115 

:._ T __, .. i _?'^ 8 , CAN-,16=1 Pipe "I ties Sled? . 51nO sNtedu1840 ! eMW Hea Tra nsfer _,_ 115 

8 __. - 6.9j. Cyfrdneal Pipe ., Sral-IMStea;^ sdwU.40 General Heat 

9 ! 910' C inlnca Pia SleWess Sleet: 6inch sMMula40 .Genera Hea Tmnsiw. 115 

10,,11 6 L-wh sahetlyle 40 Ge.w Heat Trarerer _ ..... 115 

9.12: CTûW_d'a_I Rine Sk Iesi Steeh_6itM sMedpla40 Gen nl Heat Trms(w: __, 115 

12 t 12.11' WWdgelfte SlaMMSteel: 60mh sdiotlu 1e40 Geneal HealTransfw 115 

13 11,13i_CyIMMCaI Pipe . _.Slxl less S!eel w_8ImT .^scheEUle 10 General Heal_Trans(er _._.,,,_.,115, 

GylWdral Pipe ,Stainless SNe1;_3(nch sNeMlafO Genera Hea Trarefec ,_„_..._...115 

14,15 _Cyhnpdca PIPS 3temtasaVeelg, _8 inch scLetlutp l0 Genwat MealTranaw , _. _ 115 

i6 __._. .,__.. 1 5.16_ CyY4Mncal Pipe ,_SW:nless 6leel . _ , BNCh s "liltl0 General Hea[Trandw. 115 

. 9 

_._. a 16,17: . Cyfinddwl Pipe _Stainless Sled _S fndh scMtlyk lO General HAMT.Mer ..,_,__115 

18 

_ _ _ 1 7 18- Cylntldcal Plpe SlafMese Slea Vedt scictlutelU Ge eel Heat?ransfer _ 115 

19 _ _ 8 19 _ .Qy ndncal Py e Stess eml Stea 81nch schedue 10 General Heat Transfer 

115 

_29 1920 Cylnca dn Ppe Stainless Steel 8incp schatlyle l0 , G era: Heal Traosfw _, 115 

21 2122 Cy_liMrical Rpe Stainless Steel 12mch sehedulel0 Adlabalc 

22 22 33 . Lyl Mncal P pe &. etas SI I 6 NU schedule 40 Adrabatx _ _ 

23 2313 Cy(vWncalPPe Slalreew Steel 6nm schMW.40 iabatic Ad 

_30 _ _ 8, 30: , C/fM calPpe Slaulless Sled 5intlr schetlula40, Ad_ababc 

14, 31 ^ C7lmdneel P pe I Sla nless Steel , , 6 inch sMMWe 10_^ _, Adiabal c ._... 

Pip. Ambieet Temp Sleedal 

Cor3to n.; 

1 None: 

2 Nona 

4 No e 

5 None 

6 des. F - None 

7 deg. F None 

8 deg. F None 

9 [e .F None 

[ 10 deg.F None 

11 de4 F None 

12 des. F' None: 

13 : dep.F None 

-: 14 i d None. 

15 tleg. P None 

16 - de4 F None 

17 tleo F Nme 

18 deg.F None 

19 ' dn.F NDM. 

20 Eeg.P; 

21 None 

22 None: 

23 

Non e: 

A5-528

• 

I* 



Attachment 2 

Page 38 of 46 

AFTA 3.01npW (3016) 325200610.31 AM 

DMedH4N 

AFTAImw MWd.OGTS Bypass System T-H Model Case 4 (My Merl, NYS 15M 115-FAmbieM.HT) 

P-qa f Ambled Temp. I Spacial 

' Units. I Conwon i. 

3D None; 

Pis. L Table 

PPa H Total Stand rd Mire Smsolh Angle _ Ball Bu tterfly Cylinder Gave Globe Plug Poppet 

losses;_-,_._ _.. Sands Bends_ _ Bents Naives i Valves .- .,,Valves , _Valves _ Valves _ Valves. , Valves _ Valves_ 

12 123 1 0.13 

13 0.11 

1 5 

21 

:. 

I 

i.32_ __. 

_ 

--. __.. 

1.42 

........ ..... 

22 0.04 

23 _0.11. .. ..... ... .___._.._.._ .. ..... .... _. _I....... ... .. f_... . 

Pipe Tbea-vmy: Swing Check 

Losses ' Vahms Valves 

Lifl CheGC 

VeNes 

TINg Dim 

Check Valves 

Stop Check 

Valves 

3harpctl9ed j Lag Con tractions 

Orince ! Cd6ce' 

Expansions 

13 

23 

PPe EnVances Ex (s Ulf anM1 1 Hoeyco nmb Saee Tee Addi LOSS 

Losses 

12 

Flowmeler I 

"1) 

13 

15 

'. 27 .. 

..... .. _ ......... Ilr .._^... 

__. .. .... .. 

....._ 

... 

114.04). 

(O t1) 

022 

.(1.62) 

_. 

23 

0.11 

AreaChance Tabla 

Area Change Name 

._._.... 

j Object 

Dented 

ÊlevaOOn Elevat on 

In, 

_....... 

I filial Presme Inilui Pmsmr¢ ^ Database 

Units Source 

Type I Geometry 

3 .:.Ale Change 

4 Area Clronge 

5 Area Chan e1 

7 Area Change I 

Yes 

Yes 

Yes. 

0 _ 

_0 

0 

0 

feet! 

feet 

fed. 

feed _ 

_ _ 

I 

t 

i 

! 

Conml Contraction. 

Con rat Expansion; 

Connak Cwtac0on- 

Ceniwl( Coneacbom 

Area Change Angle Loss 

Fades 

3 22 0.4399 

4 22. 0.1552 

5 22 04404 

7 26.1 0.1241: 

CompressarlFam Table 

CompresmrlFan 

_ 

Name Oblest 

Defnetl 

Elevation Elevaton 

IMiU 

MNat Presswe Initial Pressure 

Urrls 

Database 

S.M 

Spedai i 

CoMitbn 

17 N31d30 Y 

..........__'_._. 

CanpresmrlFan Pump 

__ _ 

Type 

1 7Cgnp/Fan CUrve 

0 mat I 

... ___. _. 

Des gn Flow Design Flowi Ctreat 

Rale Rale Units ^ Confgumtwn 

—{— 

None 

...._. V . 

btleph.1, W. Variab leOV.Ld nt 

Variable Units VadaMe 

Vd. Flow Rate k3/min _Pressure L. 

A5-529

• 

0 

0 

I]oAJMN-N 


Calculation No. 145579-Ei-CA-056, Rev. I 

Attachment 2 

Page 39 of 46 

(sore) 

AFF Amow Model, OOTS Bypass System T-H Model Caw ,t(Dhy Fhers, NYB ISM 115'F AmlfoaL HT) 

W250%1^,3iAlvl 

Compressor/Fan DeR VaAaW. Compff.Cwe Camj`117..Cerve' Compff.n Cuwe CampjF..CUrve I CompdFmCam e 

Dead Eed 

U,ft 

12AeIni 

Constant. 

Z;7Ij 

25E -2.2&%14 -2.2&%149-06 0! -; 

I p 

neet^ M, e ^S^d ^ E.;Zi- 

i---Cw^ —! &; w1aeft (Iapasla. 

Rat e to lwft T YRP 4 DL.M jaS MsuchaMUnits' e^^ftded0nN P .s 

Dead End Nome Elwfioa Elevation 1 IAWPIMu- ; INUSI Pressure D-baaa 

DaBned Lleft i UNIS I Seem 

30 T. Man OGTS Yea (.at 

31 ToTmaBHEPA' Y. 0 faat' 

i 

r2eneral comgenergi; 

I • 

• 

• 

RPP-24544 REV Id Calculation No. 145579-D-CA- 056, Rev.1 

Attachment 2 

Page 40 of 46 

AFT Mow&0 Input (sots) ., 3YIMM1610:31 AM 

DMJM{NN 

AFTMOw MCd41, OGTS Bypass System T-H Model Case4(Dky F#en. NWI 1506. 115'F AmblenS HT) 

: Tank Tem orai Balance; Bakrlce (Pipe#1) (Pipe #2) (PNe p3) (Frye ifd) (Pipe#5) (Pfpa #6) ; 

It 

1 

..,..Units 

_ _ ..F 

Energy _^_COnoenVapon KN KWl " 

No: No._.._. 100 

Kky KOut Kln KOM' _._ K.m, K1M^. KIn,KOUI .._ __ KIn,KOUt,_ 

I 20 _deg:F 

21 _:-_-.. d F 

_ Noi_AQ0)0 ___B! 0 ___.._ 

N Nd fP21)0 0 

—_.T--- 

i Tank (Pipe Ar t) (Pipe il8) (%ce q9) (Pipe #10) (Pipe #11) (Pipe#12) CHI e#13) : (Pipe#14). (RIx iH5) 

KLry KOul_ _K In,K Wt_ KN^HOUt ", KIn,KOW_ KIn`Dut K. In^KOut K1KON _KInI K OUt_y Kln,_K OUt 

1 

2D _ 

F 

_ 

_I L l._ __ 

Tank ( Pipe 916) (Pipe#17) I (Ppe#18) (RPe#19) (Ppe#20) (Rce#21) (P4re#22) (Pipe 923) (Pipe#24) 

1 

Kln K_lTlt Kln,K, Mt Kln KOut Kln KOW Kin KOUt Kin KQUI Kln KDVI Kin KQIt I Kln KOUI 

_. 

21 ..... 

TaNC: (Rpe#25) 

Kln KO t 

1 

Ill 

21 

TeeorW eTable 

- 

Toe or Wye Name Object 

DeMetl 

8 T.a.rWy. Yes 

_ 9 T,,a.rVOe Yes 

11Teeor Wye__Yes 

13 Tee w W a yes 

Elevation Elevation Initial Pressure . Intial Pressure 

Units I.I.R. 

0'. feet 

0 feet 

0- - f e6 _ 

0 feel 

Database I TeeMtye Was 

Scarce T Tvoe 

Rountl Sbai Mi Detailed 

RouMStrai Mi Detailed 

L. ROy tlSbagN; , _Detailed 

I RoundStraitW Oetailetl 

14 Tee or WVe Yes 0 feet I Rountl SKalebl l Detailed 

Tee or Wye Angle Pipes I 

_— 

8 )0;, 

0 __150 ____, 

tt 3D 1 

VeN T I 

13 45 

14 135 

—^ 

__ 

Valve Name ^ Object Elevation Elevation Inil al Pressure Inlliat Pressure Database I said Ewt Exit 

. ^ O fined 

Units 

' 10 i NVSO1 vs 0 fee[ I 

12 . 1 NV-902 .Yes _._ _.. 0. feet .. ...._ _ 

15 V Yes 

0. feet! 

19 V•167^ as' 0 feeti 

Units Source 

....:_.._ _ 

Coodition_ Valve Pressure_- 

( Cbsetl No 

Gbsed_ NO' ,.. 

L. None_ H4{........ 

I None No 

23 V-178! Ves 0 feet) None No- 

Valve t Exd C#A : CdA Use Loss independent ; Ind. Variable Dependent Dep. Variable Loss 

_ posear-urst.s.. Upils Made) .., Value Va riable Units__ I Variable Wile "._Manta 

10 r Cw Constant; 1194 .. 

l2_ Cv Constant 1194 

15 GY COnstam 2440 _. 

...10 _.. Cv COnsl@e1 , . 2440 ._ i ... ... `. ..... _ __...... 

23 . I- Cv Constant ..300. 

A5-531 

l

E 

AFfArta "trout (B O18) ... 3R5120061R31 AM 

DMJMH+N 

FF'f Arrow AlOtlet OGTS Bypass Syriem Tds Model Caw a (Dirty Fl9ers, NYa l5alA 115'F Amalent Fin 

ValveLose Loss .Loss I toss 

i. ConslaM O;; . Constant O ! Conslantd Conslanle - 

to 

is 19 

A5-532

• 

• 

AFTAnmvw ooulglt (ids) 2!25)2006 

DMJMH.N 

AFT Arrow Modd. OGTS Bypass System Tit Mudd Cam 4 (D irty Filers, NYB 150 11,115 •FAmNenL HT) 

T15r. AFT Arrow Model, OGTS Bypass System T4 Mod el Case 4(D'irty Fihets, NYB 1608, 115'FAmbient.Hn 

Analysis runon:=5TN06. 102M AM '. 

App lication wrsim AFT Arrox Ve rsio n 3.0 (2005.09.14) 

Input File: M?Damonsbaton Buy VMfIswlÀ ar2006 WorlAC21wheons100TS, Bypass Thermal Hydrau lics AnabalAWodt F0es%Bypass Fkw8 

Inch Pipe Rev 1 Case t.a ro 

Execution Tune= 12.84 wwr ds 

Total Number Of Presum Nota t ions- 0 

Total Number OI Flow 0eraUOrrs=56 

Total Number Of Enthalpy lfemfians= 56 

Number Of Pipes-25 

NumbmeUJUnctlons=25 

Matrix Me0lod=Gaussian EUmhraUOn 

Length Mardl S ol u ti on Me6wd with Madh Number limits 

Length Step SiW m 12 hmhes 

Mach Number lnvamenl= 0.01 

Pressur e Tolerance-0.0001 Weiner change 

Mass Flow Rate Tole rances 0.0001 relative change 

Enthalpy Tduance= 0.0001 relative dwnger 

Flow RelaxaUOn= (AUtomaUe) 

Pmswre Retax elion+ (AUtomal lo) 

Resistanm Relaxa tion= (Automat ic) 

Fluid D atabase: AFT Standa rd 

Fluid: Air 

Max Fluid Tempera tu re Dal 1000 deg. K 

Min Fluid Temperature Data= 200 deg. K 

Molecular Weight -28.97 amu 

Gas. Consta nt =0:06655 BUdiomR 

C ritical Pressure =3725 Am 

C ridcd Temperature =132.41 deg. K 

Acen tric Factor =0.021 

Equation of Slots=fiedKd,-Kwon9 

Enthalpy Modal=Generalized 

Spe cific Heat Ratio kouracy = High 

Atmospheric %eswre=14.3 Pala 

Gravitatonal Accelera tion= 19 

Standard Pressure= 14.696 Pala 

S ta ndard Temperahre- W deg. F 

Turbulent Flow Above Reynolds Number= 4000 

Lam'mer Flow Se lovr ReynoWS Number= 2300 

Total InOmr- O.7 111 IbrAwc 

Total Outlovr- 0.7111 loMSen 

Tad Energy InBOw=148.2 glu ts 

T ot al Energy Om0ovn: 147.7 &cis 

Total Heat Transferred Into System= -0,5443 Btuls 

Maximum Pressure is 14.33 ps a, at Junction 17 Oultet 

Minimum Pressure Is 13.78 Pam at Ju lion 17 Wet 

Maxmum Stat ic Temperature Is 124.7 deg F at Junction 17 OuUet 

Minimum Static Temperature is 115.0 deg. F at Ju nction 13 Inlet 

er^ ss,E n Step.. 

-J6 

:.. 

IT 

Name Mass I Vol. DP DP Overa ll 

Flow Fbw l Stag Stall. Elency 

(;pfm) (XII, (in. H20 old.) (In.H2O std,) .(Percanq 

N31-130 .s5661 6601 r15.79f 157_ 9 _6740. 

Speed Oremll Comp. -.; BEP SEP 

Power Ros Q Mass 

CP cent).i'(!p) .(Percent) CWmc)-;- 1Wseg-; 

100.D 2.395 104.1 N/A: N/A 

BEP 

(Percent) 

17 WA: 

Voles S.M. 

A5-533

0 

AFTAnwmoulyut (20(5) 325 12008 

DMAWN 

- AFT A11owM d. OGTS Bypass System T-H ModelC 4(Dirt/FiMM NYS 1506.115°F Am bie nt, HT) 

I dct Name Vales Mw DPSM9 DPSMeo I PSMBn -K Va lue Stela !. Cv OV EsL 

1 

Type f Flow ( i 

Idet 

! -__ _ emhecb)(Eab)? tosMt - 

'X10 t_._.. _M/AOt^_REGULAR.^,_._, __ O.00M, _.._.. No S ,olutionl _ , NO SON6m}._ too _ Sdudon 

1 

1 - 

No .SpIWOI^_CbeeCBy.USer'.. te194,0 _._-_.___. 

'X12 HV-9021 REGULAR; OMNI No SdN,Mi No S&OW pb SOM6on 

15 V-166; REGULAR! 1171111 0.94693i 0.004595? 13M 

19 Vd67i REGULAR! 0.71111 0.0045321 0.006534' 14.32 

i 23 V-1]Bi REGU I AR 0.116 0.282496' 12829(16; 1452 

elo SOlutlon 

NO Stlulion; Gosed Useri 1194.0 No Sdudon 

M7810; ni 2440.0 W A 

0.78191 O M 20.0 84 

WA 

13.92511 ana 300.0 WA 

Heal 1mmetm, Summa 

Jet: Name Mass DP, .1P j DT 

Lou 

T 

!ut 

T H 

OuOetRta In 

(psldL[ M Cden.P) 

8 

Itlo9-F) Ce9 I 

115.. ._ 1150 _ WA 

1 

. 

_ 

. 

. 

pip Name Mau Vol. Vol. Vel. I Matl1 I Mx11 

Flow : Rm Av9 lin Out dln 0001 

- m2bil McVSec /eeVmin 

i 1 pipa 0:0. 0.0 0.00 0.0 0.909 0.80000 

2 „ Pipe)_ DO O,Oi 000 „__-00 000000 ,_000000 

.._ 3 ,3 FFS t! 00 - 0.01 OOD ..,00 000000;000000 

d Pi 1 00 O.OI 000 00 000000 0WWO 

,,.. 5 1'iP?s.. _. 00 _- 0.0;_ 000...,... 80 _000000..,000X0 

:_ 8 . P RDe .,_.. 00 00; _0.00. _..._. 0 0..0.00000 0099 

7 . „ Pipe;.. 00 . _ , -0.0. CLOD 

I 

_ (10 0,00000 , 000000 

8 Pipet _ 0.0, -0.01 

0.00 ., 00 0.00No 0XON 

9 Pipe! 00 ,.0.0r_ 0.9 .. ...0.0 0.00000 0.00000 

10 Pipe_ 00 00!, _,0011 -, __00 000880 ,_09000 

11 Pipe!,__ 00 _ 00. ! 000 00 0.00000 000000 

12 0pai .. 00 0.01 000 00 000000 000000 

_ 13 Ppa _.. 00 0.0, OOD 00 0 909 000000 

14 Pipet_ 5586 653;5! 28]5 -._17290 0.02456 _002461 

` 15 Pipet 55&6 ., 854.5 

1,7305 002461 _002463 

16 Pipet.. 5586 655.0; 28.85 1.7314 002464 002464 

17 P1peI; 5586 NO.D! 2907,...1,]44,5 002483 _ 002463 

dP SMg P$1.9. PStag. 

Towt In Oul 

n. H2O Std. In. H2O-sld. n. WO std 

0.000000 0.0000 0.00000 

0,000000 _.00000 ___0.900 

0.00900 _.0_0000 __0_00000 

0.800000 0.0000 0.00000 

0.000000: __.. -...- 0.090 _. _... 0;00WO 

-.. 0000000 -........0_8808.-------- 0_06804. 

., _0.000000 _0.090 _.0,00000 

866000() _ .., 00000 0,00000 6.0 

0.000000, 0.0000 _0.00000 

_0.000080 106592 - -10;6591] 

0.000000 00000 

_0 000,011! 

000009 -106592 10,65917 

08,00000 -106592 _10 165911 

0851)42 ..106592 1151092 

_ 0.311iI _ .,_ -__ 11.5109 _82733 

0.076344 119545 12.03081 

0.022439 , :t 6W 14.91620 

- 16 

19 

28 

- 

21 

22 

23 

_ 9 

31 

Pip! 558.6 - 644A 

,Pipet 558.6 (3 44.61 

558 6 643 ] 

Pi 'P. _5586 6351; 

Ppe__5586 63631. 

Pip' 651],__ 

Ppe 00 001 

P e 0.0- 0.61 

28.39 X702.9 

28.40 _1,7036 

28 40 16952 

1264 7585 

5302 3181 3 

5410 3,2508 

000 DO 

0.00 0.0 

0.02404 0.02404 

0.02405_0.02405 

002406 082403 

00199 00108D 

004529 004529 

004621 004628 

000000 000000 

0.00000 OA0000 

0.032813 

0.0,1356 

0 529803 

0050975 

OA32]8] 

0533088 

0000000 

0.000000. 

0.8677 

_--,_0.6325 

0 502] 

00000 

_16400 

-94925 

099 

-11.5109 

0.63485 

0.62817 

0.02690 

0.05098 

.1.67281 

10.02559 

0.00000 

-11.51092 - 

Pipe PMotto pStatic d]Stag. TSMg. TStag.. TStsOC TSM&! tlH Slag. HSM9. 

In Out ' INe1 O Out In Out - In 

_ (n M20 std. (9)) On. H2O std (9))l Cd@9.. F) 4..F)(8eg F) (tle9_F)_ (deg,F)'_ . _(6lUMeT) (DlpnEm): 

1 0:80000 O.B000D f_OAO00000D' 115.0 115.0 115.4 1150 0.000000800 206.1. 

2 0.00000 0.00000; 0.0000091 115.0 115.0 115.0! 115.0 0.000000000 29.1' 

3 0.WWO 0.909: OmowoX: 1150 115.0 115.0' 115.0 0.909991 206.1 

4 ___.,. .0.0900.. _009001,0.0090000-. 1150; ., 1150 115.0; 115.0.0.000000000..__206.1 

5 0.0900 _ 0.990! 0.09900: 115.0= 115.0 1150' 115.0 0.99009() 206.1 

_ 6 _ 0.990 0.9901 0.900009 115.0 - 115.0 115.0 115.0' O.OD90090 2W.1 

7 0.990 0.0090; 0.009900 115.0 115.0 115.0' 115.0 - 0.00900000 206.1 

A5-534

• 

• 

AFT Anow 3.0 OUtpW - (3 01 5) 3125/2000 

DMJMH-N 

AFF Armes Model, OGTS Bypass System T-H Model Casa 4 (E)MY Fdtem. NYS 1506,116-FAmWoM HT)' 

Pipe PSlow PStalk dT Stag. TSlsg. I TStag. TStaltu i TStadc 

I 

dH Stag.. HMag. , 

! In Out Wet 

i Outlet m 1 Out :i ` in 1 

_---;_(m_H2O Std: S9)1 rI. HZOStA (911 ..-5099 D___( .: ddee9_F).. CQ?ac F) i (de .F)r tBwn6m1._.(BSW 1.^ 

I B ;._.... 0.00006 ,----_-..,.0.00000 _ 0.0D000OO ! .._1150;.._: 11s.g ... 115:0 ... ii5.o^ r 0.000000060 ---z06.t^ 

.. 

! e i 0.00000 000000 0.00000000: 115.0! 115.0 115.0 115v o.00000o 000 206.1' 

( 10:. -10.85917 -10. 17 0=000OOD I115.0 11150 115.01 115.0', O.OD000M 206.1, 

11 1 O.DDD00 0-00000 0.0600'10601 115.Ui 115.0 115.0; 115.0! 0.000000000 2051 

12 6591] -10.65917 0. 0: 115.0 115.0 115.0': 115.0 i. O.OD000DD00 206.1! 

i 13 -t0.8591] -10.65917 0.00000606! 115.0 115.0 1150' .1150! 0.000000000 20511 

14 -10.82063 .1t.67274 0.00.549318: 115.0 115.D 114.9' 114.91 0.001502793 206.1' 

! 15 

16 

" -11.672741 

-12.11847 

-11.98928 

-12.19204 

0.00618311 1115.0: 115.0 

-0.0600Slt 11505. ! H 

114.9 ;114.91 

114.9' 114.9 

0.000114531 

0.000007439 

206.1! 

206.1 ` 

17 -15059 04 -15.08141 0OD000060 1150 : 115.0 114.9' 114.91 0.000009230 206.1[ 

18 0.70821 0.67548 -0.26451660' 124.7: 124.5 124.7 124.4 -0-062128137 209.4' 

19 -0.47306 0.46673 -0.07147217 - 124.5 1124.4 124.4. 124.4' -0.01 7449171 208.4i 

20 

21 

0.34320 4.18584 

-0:0320/ AA8305 

., ; .,2101]8-223462 

-2.81713867 124.4' 121.6 124.4:.121.5: -0.68]4]9547 

0.0003 1150: 115.0 115.0: 115.0 :o 0000 

. 0-00600600-,,- J15,0 , _ ,_115.0 . _114,81_„, 1165 _, 0_OD0000808 . __ , 

20641 

206.11 

2U6.1 

23 : .10.06571 4 0.59959 -0.00042725' 115.01 115.0 114.8. 1101.8: 0.000000000 206.7' 

30 0.00060 0.00000 0.000 w1150': 116.0 115.0 115.01 0000000000 2061- .. 

-1151092 _ -.,,.- _ .., -1151092 __0.000OOmi- 115.01_ , LS_0 „- „115,0.__ 1150,,. .0.000000000 ZM 

Plpe H Slag. H SWOC H SW;U Rho Rho Stag. Heat T ansler Heat FNx Neal Rale 

Out In Out Stag N ; OW Modal 

BlV bm ambeu B1u66 ;t ag 3 . M Btu/s82 Blela 

{ 1 206.1'. 206.1 20611 006719'_006719 -.-_, Ad abate 0000E 06 0000000000 

2 206.1206.1 -., 

2061 006]18...006719 Adiabatic 0000E OOI 0000000000 

3 206.1' 206.1 2061 006719; .. 006719 Adiabatic 0000E M 0000000000 

:. 4 206,1: 2061 ._. 2067 0.06719-.006719 AtOababc 0000E OD 0000000000 

5 208.1;. 2061 -,. 2061 1 0.06719 , _ 0.06719 Atlabatle „ O.000E OD 0000000000 

-, 6 2(161_,206.1 , __206.1] 0.06719 , _ 006719 1^Ge^7. Heat Tran. - . 0.000E40 0_000000000 

7 206.1-_ 206.1 20611 006719,_ ,. 006719 Gaul Heat Tran 0000E 06 0000000000 

8 2061: 206.1; 2061 006719 0067191 Genl Haat Tran 1 0000E 06 0000000000 

- 9 2MI 2061 2061 006719 006719 1 GenOHeat Tran l 0000E 06 0 000000000 

10 2061 2061 _2061 006539 006539 Genl Heal Tra I 0000E 00 DO0000_0000 

. 11 206E 2061 206 1 006119 006719 Gen; Heat Tran i OOOpE00i 0000000000 

12 2061. 2061 2061 006539 006539 Gaul Heat OOOOE 001 0000000008 

13 2061- 2061 2061 006539 ^., 009 653 Genl Heatan Tr r 0000E 00^ 0000000000 

14 206,0 2060 . 2061 008539; 0.06524 Genl Heat Tran . 2.987E-061 0.001068698' 

15 206.1 208.1 2061 0.06524 0.06519 Gent Heat Tran 1.615E46 0.060081448 

16 j 206.1 206.1_..,_.20611 0065-1, 7__0065151 „Gw Heat Tran. 1.617E06 0.000005290 

17 _206.1: 206.11 206.1- 0.06467 .__ 006466, Genl Heat Tan. _ 3.010E06 0000006563 

18 208.4 208.41 208.41 0.06622 0.066241 Gedl Heat Tran. -5.789E-03 -0.OWB0289 

19 2MA 208.4 208.31 0.06621 0-06621 t Genl Heat Tian. I b.691E-03 -0.012409204 

20 207.],2083_..20].7_0.06619:,,0066x3! Genf HealTra . ,_

C 1 

• 

AFTM"&o0uW (4015) 3257106 

DnuMH+N - - . 

AFfArtow Model, OGTS Byyass System T-H Model Case4(091y Fl1a(s. P4YB 1508, 175 •FAlnbien4 HT) 

JM 

`_3 

a 

5 

6 

_.. 

.Name' i Mass Flux ;' IPSWOg 

Tluu JUnctlon i. TOW 

_. Area Cbmri 00:.._.__:0:0000 

lvea0nen D.o 0.01. 0.0901; 

Area Ch 0.0 0.0000 

I VPbnumi DO, O.Nop 

PSla9. PSiag. PSI tk PSlatb I 

In ON 10 009 

ri2Q51UORW N!. r±zo sd _(9p (®!, n2o u0.0owi 

.._._....000000- 

. . ___..-0OD00 _-_....-_.OWE ___... .. 0.0000 

om000 0.000= 9 

o.oWW 

oWOO: 

060000 O.OWO 0.00000 O.WW: 

0.00000 O.WW: 0.00000 O.WW' 

7 

i 8 

9 

X10 

11 

X12 

13 

Area amum. 

T..Wye 

Teem of 

HV-901: 

Teew ei 

HV-092! 

Tee- ej 

- 00 

0.0! 

0.01 

0.01 

0.0; 

0.0: 

WA i 

O.ODOD 0.00000 

0.0000 O.OWW 

0.01100 0.0000 

No lff No SONfan 

0.0000 40.65917 

No Soution No SONBon 

See Losses -10.65917 

0.0000; 

O.WW' 

O.00Wi 

40.6592; 

-10.65921 

-10.6592: 

.10.6592c 

0.00000 

0.00000 

O.DOWO 

1403owan 

.10:6591 7 

No Solution 

-10.9940 - 

O.DDDO 

UNDO 

O.OWO' 

-10.6592' 

-10.6592- 

-10.6592. 

.10.9909 

14 Teem 

N/ A• 0. 1)(iW -11.51092 .11.6109 1 -11672 74 -11.6727 

15 V-1861 558.61 0.1271 -1162T33 -11.9545: -11.98928 -12.7166 

16 

.. i] 

18 

MPAF9lm1361137i 558.6! 

_... .. _... N31130586. 

Backdmft Durp.. 558.6 

2.8850 

._ 1_5.7859 

0.20M 

-12.03081 -14.8958 -12.19284 

._-14.91820._.... ^0867];_..._.. -15.0 ..... 

0.03485 06325' 0.67648 

_ 

.15.0590! 

O.N62: 

0.4731: 

19 

._20 

V-167: 

. AOn Pms L..__.. 

558:6 04255 

5586,.._... 

0.62817 D.W27' 0.46873 0.3432 

Opole, . 

21 

22 

23 

- 30 _. 

31 

A6n Pres 7 

Heater B HEPA Filler' 

V-1]81 

_ ._TOMan OPTS._ .. .. 

To Train B HEPA 

558.6! 0.090 

558.6' 1.5891 

558.6; 7619] 

0.0,,, „_O.OWO 

0.0. O.OWO 

.....__ 0.00000 -.._ _ .. - O OOW. L. .......__0_0. 0000 _....._.0.0000'. 

O600W O.OWD' 0.00000 I 0.0000 

-0.05098 -1.8409 -0.06305 Z2018 

-1.67231 -9.4925 -2.23462 -100657. 

....._ .. 0.00000 -_ ._.__O OOOU ,,.. ._000001_ 

-11.51092 -11.5109 -1151092; -11.5109. 

J11 Or Slag. TSWg -, cim.t TSWOCIn TSI tie 8to HStagl - H Out I HStal:el H 

Inlet -. OuOet Out I ^ 

Out 

Out Oul 

idea. F tl (deo F) Wei l. F!, Mon. F1 BtW uri BIWbm Blum. (lit"i lBlu96m 

1 OWOOOOW 1150 1150 ,.,1150 115.0 OOW 2061 201.. 2061 206.1 

2 0.0W00000 115.0. 1150 115.01 115.0(_ OOW _ -, 206 11 2W.1J 2061 206.1 

_. 3 1 000000000 115.0-__ 115.0 ._1150 11501 OOW 2061 206.11 2061 206.1 

4 000000000 1150 1150 ._1150_, 115011__ 0000 ., _2061 . 206_1__, 2061_.__206x1 

_._ 5 000000000 115.0 1150 1150 1150_ 0.000 -20611 21161 2061 ..... ._.206.1; 

6 00000000 115.0 1150 1150 1150 _-. Om 

206.1. 2061 2061 2061: 

_ 7 0000(1 _ 1100_ ,- 115.0 1150 115.0 OOW 2061 _2061 2061 2061 

8 0.00000000 115,0J- 115.0 , .... 1160 115.0 1 WA 20611 20.1 206.1 206.11 

._ 9 - _000000000 116.0` 1150:,_. 1150 115.0_ .., WA __.__206. 1 • 206.1 _206.1-, ,206.1 

X10 No SOWlionl No 6olulion^ 115.0 No Sdwion 115.0 O.WOi No Solution; 206.1 No Solution 206.1 

11 0000000011 115.0' 1150 ,..-_..Its. 115.0 NIA ._ 2061 1 209.1 . _ 206.1_ 206.1 

X12 No Solu tion No SOlylon' . 1150 NoS Im,, 1150 0000 No SOlubonl 206.1 NO Sd lion ,. _ 206.1 

13 ! O.00DWOW 115.0' 1150 114.9 114.9 2061; -2W_11 2W.1 206.0 206.0 

- 14 0 WOWOW 115.0' 1150 1149 114.9 NIAI 2061 2061; 2061 206.1 

15 1 0Ooo 6lo4 1150_. 1150 _1149 114,9 OOWI 2061 2061; 2061- ,__206.11 

t8 0.00231934 1150 1150 __ 1169 110 ;9 O0W1 206 1 2061_ 2061 206.1 

17 ( 9] 52566 34 115.0 120.7 1149 124.] Q.3T/ 2061 208.4 2961 208.4i 

18 , 1__0.00018311 124.5 124.5: 1244 124.4 9OW 208.4 208A 208.4 208-A! 

1 19 1 -000012207 ,124:0 1244; _1244- - _ - 1244 OWD 208.4 208A 2083-_. 208.3; 

20 1 6.O66WOW' 115.0- 115.0 115.0` 115.0; 0.666 209.1 206.1 206.1' 206.1; 

27 O.OWOWW'. 115.0 115.0. 115.0 116.01 0.1103 206.1 206.1 206.1 206.1 1 

22 1 -0.00158691 _ _115,0:-,. 115.0: 1150 114.8 -,.._ 0_OOD .,. _ 206.1 1, 206.1 206.1 2W.0 -, 

23 -0.00634]09 11- 5.0 115.0 114.8 114.8 O.OW 206.1: 20.1 206.0 2W.0' 

30 O.000DOOW 115.0 115.0 115.0 115.0 0." 206.1: 20.1 206.1 20. 1; 

O.000WWO' 115.0 1 115.0 ,- .__ ... 115.0 115A.O.OW 2011.,_.2061._. 206.1„ _2061! 

A5-536

0 

• 

• 

AFfA 3.00utput (So/5) 312Yl000 

DWMH.N 

AFTAImw MOde1, OGTS Bypass System FN MOdelOesed(DHy FflI¢ro.NYB150B, 115'FAmbien1. HT) 

imn nlow Table 

JOI wipe ' Pipe uP See, TOW 

... _.__. a.. __ Mr... (in. H2O W.) 

8 PT: In OA00 

P30 out 0.000 

P8 Out 0.000 

9 P8 In 0.000 

P9 Out 0.000 

-- P11 Out 0.000 

II P10 In 0.000 

t P13 Out 0.000- 

. P12 In O.Ow 

X13 P13 In' 0.000: 

Pfd Out 0.000: 

td - 

P23 

P14 

Im 

In 

0.6338- 

O.m 

Pt6 Oul 0.000= 

P31 Out 0.000' 

A5-537

DMJM H&N AEGOM 


- A tt achment 3 

is 

• 


Rev. No.: l 


Page 1 of 22 

ORIGINATOR: John Irwin ^, 03-25-2006 

Calculation Title: DBVS OGTS Bypass System CHECKER: ackMceweel^ 3-2Grcx 


OGTS Bypass System Fluid Flow Model Input Data 

A5-538

• 

is 


A5-539

a 

cis 

.A 

0 

• Calculation No. 145579-D-*6, Rev. 1 

Attachment 3 

Page 3 of 22 

OGTS Bypass System Fluid Flow Model Input Data, Piping/Component Descriptions and Flow Loss Coefficients. 

o: 

s 

OATS Byp>;ss System F1wd^Flpw M,o^^^` ^ +Ì 

0l^`3^'^^ ,. ^ ^ ° ^^ ^ ^ ,^^ 

'd rx 

a t'a 

_ . .u's 

J s z ^4. 

a 

^' 

^:,. .a S&^R ^"e^ Y.S.v., e. rl [. .ea b 1 

".d^'.a} t'if ^ :^„Ga^ , 

^^; 

°.x 

Iy 

a o,î 

Component Details Size Schedule Inside Dia. L ASHRAE ASHRAE Cv 

Fitting Loss 

No Coef. 

(in) (in) (in) 

.11 

ICV Box plenum HEPA filter, 35-NO2-010, 

Stream No. 9 

Atmospheric Junction 

PI hilet Housing and screen 16" square Intake 16 x 16 17.49 CR6- 2.120 

with birdscreen, 

(60%o en) S.Stl 

1/ER3-1 

" Inlet Piping, 6-AA-35- 

0218 

6" straight duct, S.Stl 6 40S 6.065 64.000 CD11-1 ARROW 

P1 NO2-010 Inlet Transition Flanders, Sudden 6 40S 6.357/24.0 ED4-2 0.810 

Expansion, 6 dia x 24 

SQ, 180° 

SQ 

Total 64.000 inches 2.930 

5.333 R 

J2 HEPA Filter, 36-NO2-010 Flanders, 0.12" w.c. 

Pre (0.24" Dirty)at 500 

cfm 

.12 HEPA Filter, 36-NO2-010 Flanders, 1.0" w.c. 24 x 24 x 

(2.0" Dirty) at 500 16 

cfm, P-007-W-43- 

N2-NU-51-23-GG- 

DU5 

ro

a 

A 

. • Calculation No. 145579-D-056, Rev. 1 

Attachment 3 

Page 4 of 22 


2 , 1 ^ M1Y: 

QGTp 

'C f ^^^^^^ 

^H./ ^ 

S1'NM1 l,^S'.µ/.Y 

Bypass Syeteln l`wd°E o 1a 1 

P C yr.'Y 

Component Details Size Schedule Inside Dia. L ASHRAE 

Fitting 

No 

P2 Outlet Transition Flanders, Sudden 

Contraction, 24 x 6 

°^ li 


12.0 

SQ/6.357 

Rnd 

`. 

^ 

ASHRAE 

Loss 

Coe£ 

ED1-1 0.500 

" Piping, 6-AA-35-0218 6" straight duct, S.Stl 6 40S 6.065 42.000 CDi I-1 ARROW 

" Elbow No. 1 90° Elbow, R/D = 

1.5, S.Stl 

6 40S 6.065 CD3-1 0.130 

" Piping, 6-AA-35-0218 6" straight duct, S.Stl 6 40S 6.065 62.000 CDl l-1 ARROW 

P2 Elbow No. 2 45° Elbow, R/D = 

1.5, S.Stl 

6 40S 6.065 CD3-3 0.080 


8.667 ft 

J3 Reducer 6" x 4", 22° 6x4 40S 6.065/4.025" 5.500 ARROW ARROW 

P3 Piping, 4-AA-35-0218 4" straight duct, S.Stl 4 40S 4.025 163.000 CD11-1 ARROW 

P3 Flowmeter 3 ea Size 1 Armubar 

flowmeter 

4 Vendor 1.635 


13.583 ft 

.14 Reducer 6" x 4", 22 0 4x6 40S 4.025/6.065" 5.500 ARROW ARROW 

Cv 

ro

a> 

N 

• 

• Calculation No. 145579-D-1056, Rev.1 

Attachment 3 

Page 5 of 22 

OGTS Bypass System Fluid Flow Model Input Data, Piping/Component Descrip tions and Flow Loss Coefficients. 

r ^. 

.a qri b r: 

3 aw z a 'kn,^ 

OGTS`$ppa¢s y$lf>pda^1 > 

b A4 ,^, ¢h, 4 

aj^ 

uacl^{^' 


Fitting 

No 


s" 

ASHRAE 

Loss 

Coef. 

P4 Elbow No. 1 45° Elbow, R/D = 

1.5, S.Stl 

6 40S 6.065 CD3-3 0.080 

" Piping, 6-AA-35-0218 6" straight duct, S.Stl 6 40S 6.065 6.000 CD11-1 ARROW 

" Elbow No. 2 45° Elbow, R/D = 

1.5, S.Stl 

6 40S 6.065 CD3-3 0.080 

P4 Piping, 6-AA-35-0218 6" straight duct, S.Stl 6 40S 6.065 33.000 CDl 1 -1 ARROW 


3.25 ft 

.i5 Reducer 6.1 4" 220 6x4 40S 6.065/4.025" 5.500 ARROW ARROW 

P5 Expansion Joint, EJ-501 4" 4 4.025 22.000 CR6-3 0.32 

(ICV Box CP) 

ICV Box Plenum, Stream No. 9 in, 13 out 

J6 ICV Box plenum CPs 

(inlet/outlet) 

Inlet and Outlet 

Losses 

ICV Outlet to Bypass Tie Point, Stream No. 13 

(ICV Box CP) 

P6 Piping, 6-VOG-35-0217 6" Duct w 90° Elbow, 

Internal to AWTE 

Crane 1.500 

6 40S 6.065 72.00 CDl l-1 ARROW 

Cv 

1

0 

Y, 

inaw 

. • Calculation No. 145579-D-056, Rev.1 

Attachment 3 

Page 6 of 22 


? 

OGTS Bypa^s^^ tSyste^ tl.' pw' 

^ t t? x 


Fitting 

No 


ASHRAE 

Loss 

Coef. 

P6 Elbow 90° Elbow, R/D = 1.5 5 40S 5.295 CD3-1 0.150 

J7 Reducer 6"x 5", 28° 6 x 5 40S 6.065/5.782" 10.250 ARROW ARROW 

P7 Expansion Joint, EJ-502 DME 5" size 5 4.9 24.000 CR6-3 0.270 

11 

Piping, 5-VOG-35-0217 5" Duct 5 40S 5.295 24.000 CD11-1 ARROW 

11 

Elbow 451 Elbow, R/D = 1.5 5 40S 5.295 CD3-3 0.10 

" Piping, 5-VOG-35-0217 5" Duct 5 40S 5.295 93.500 CD1l-1 ARROW 

P7 Elbow 45 1 Elbow, R/D = 1.5 5 40S 5.295 CD3-3 0.10 


11.792 R 

J8 Lateral Wye (For Bypass 45 0 Lateral Branch 5 x 5 x 5 40S 5.295 10.000 ARROW ARROW 

Flow) 

Flow, Main Flow 

Closed 

J8 

OGTS Bypass Main Ducting from Tie Point to 

HEPA inlet, Stream No. 13 

Lateral Wye (For Bypass 

ARROW ARROW 

Flow 

P8 Elbow 45 0 Elbow, R/D = 1.5 5 40S 5.295 CD3-3 0.090 

P8 Reducer Standard Reducer, 

5x6", 11° 

6 x 5 40S 5.295/6.065 6.000 ED4-1 0.050 

Cv 

:a 

a: 

tnl6< 

a-

in 

A^P 

• Calculation No. 145579-D-&6, Rev. 1 

Attachment 3 

Page o 7 22 


^ 

Q&x 

,,pas YsfC^4 

^ ^- $3 ^ vT . i -mot, l^` , 4 ^ 

FJ^^ 2^ 

^ 

^ uYr^4.alY. ,4 ^^n ^ 

^ ..vA., 


Fitting 

No 


J9 Lateral Wye, Forward 

Direction 

30° Lateral Wye; 

Main Flow 

ASHRAE 

Loss 

Coef. 

6 x 6 x 6 40S 6.065 6.000 ARROW ARROW 

P9 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 10.500 CDl l-1 ARROW 

J10 Valve, HV-901 6" Keystone, FIG. 

362-173, Key-Lok 

6 5.8125 2.250 ARROW ARROW 1194 

P10 Elbow 90 1 Elbow, R/D = 

1.5, S.Stl 

6 40S 6.065 CD3-1 0.050 

P10 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 8.000 CD1 1 -1 ARROW 

Jl l Lateral Wye Reverse 30° Lateral Wye, 6 x 6 x 6 40S 6.065 6.000 ARROW ARROW 

Direction 

Main Flow 

PH Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CDI l-1 ARROW 

PH Elbow 30 0 Elbow, R/D = 

6 los 6.065 CD3-1 0.050 

1.5, S.Stl 

J 1 2 Valve, HV-902 6" Keystone, FIG. 

362-173, Key-Lok 

6 5.8125 2.250 ARROW ARROW 1194 

P12 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CD1l-1 ARROW 

P12 Std Tee 6" Std Tee, Branch 

flow 

6 40S 6.065 ARROW ARROW 

P12 I Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CDI1-1 ARROW 

Cv

a 

Y, 

in 

A 

Calculation No. 145579-DA6, Rev, 1 

Attachment 3 

Page 8 of 22 


;^ 0^^^ A^^^s Y' te ^M1 ^^^^.M^î^0 

h }25 


Fitting Loss 

No Coef. 


P12 Elbow 30° Elbow, R/D = 6 40S 6.065 CD3-1 0.130 

1.5, S.Stl 

,111 Lateral Wye Reverse 30 0 Lateral Wye, 6 x 6 x 6 40S 6.065 6.000 ARROW ARROW 

Direction Branch Flow 

P13 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CDl 1 -1 ARROW 

P13 Reducer 6 x 8 Std Reducer, 6 x 8 40S 6.065/8.329 ED4-1 0.170 

19° 

P13 Elbow #1 90° Elbow, R/D = 8 l OS 8.329 CD3-1 0.110 

1.5, S.Stl 

P13 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 114.000 CD1 1 -1 ARROW 

P13 EJ-635 8"Expansionjoint 8 los 7.900 11.000 CR6-3 0.110 

P13 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 120.000 CDl l-1 ARROW 

x 


20.917 ft 

J13 Lateral Wye, Forward 45 1 Lateral Trough 8 lOS 8.329 10.000 ARROW ARROW 

Direction Flow (Air Inlet Bleed 

System@ Branch 

flow) 

P14 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 138.000 CD1l-1 ARROW 

" Elbow #1 900 Elbow, R/D = 8 l OS 8.329 CD3-1 0.110 

1.5, S.Stl

s 

Y, 

cn 

OAT$ Bypass S ^te^ ^1u1^^„iP^^^^de ^^^ 

Component Details Size Schedule Inside, Dia. L ASHRAE- 

Fitting 

No 


ASHRAE 

Loss 

Coef. 

" Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 15.000 CD11-1 ARROW 

" Expansion Joint, EJ-635 + 

5 others 

8" Expansion joint 8 7.900 11.000 CR6-3 0.660 

P14 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 1805.000 CD11-1 ARROW 

Total 1969.000 inches 0.770 

J14 45° Lateral 45° Lateral Flow 

Thru branch closed 

• Calculation No. 145579-D-C*6, Rev. 1 

Attachment 

Page 9 of 22 


164.083" ft 

8 x 8 x 8 lOS 8.329 ARROW ARROW 

P15 Piping, 8-VOG-36-0286 8" straight duct, S. Sit 8 los 8.329 65.500 CD11-1 ARROW 

" Elbow #2 90° Elbow, R/D = 

1.5, S.Stl 

8 los 8.329 CD3-1 0.110 

" Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 los 8.329 100.000 CD11-1 ARROW 

" Std Tee Std Tee, Branch flow, 

main flow dead 

8 x 8 x 8 los 8.329 ARROW 1.10 


P15 Expansion Joint, EJ-615 8" Expansion joint 8 7.900 11.000 CR6-3 0.110 

(HEPA Inlet) Total 277.500 inches 1.320 

23.125 ft 

Cv 

n 

r•. 

ro

• • Calculation No. 145579-D-06, Rev. I 

Attachment 3 

Page 1 0 of 22 

OGTS Bypass System Fluid Flow Model Input Data, Piping/Component Descriptions and Flow Loss Coef ficients. 

` : ^ ^ OATS ByPas^ ^ystg Rl^d^1^' ide ^ ^' , ^' 


Fitting Loss 

No Coef. 


OGTS Bypass HEPA HEPA Filter skid 

Filter Skid Assembly, 36-D58- 

138 

J15 Isolation Valve, 36-V-166 8" Keystone, FIG. 8 7.625 2.500 ARROW ARROW 2440 

362-173, Key-Lok 

P16 Inlet Transition Flanders 8 OD x 15 8.329 18.000 ED4-2 0.430 

W x 18 H x 18 L, 30' 

J16 HEPA Pre-Filter, 36-NO2- Flanders 24 W x 24 14.000 

136 H x 14 L, 0.12" w.c. 

(0.24" Dirty) at 750 

cfm 

J16 Test Combination Flanders 24 W x 24 20.000 

Housing H x 20 L 0.5" w.c at 

750 acfm 

J16 HEPA Filter, 36-NO2-131 Flanders 24 W x 24 20.000 ARROW ARROW 

H x 19.375 L, 1.0" 

w.c. (2.0" Dirty) at 

750 acfm 

J16 Test Outlet Housing Flanders 24 W x 24 20.000 

H x 20 L, 0.5" w.c at 

750 cfm

in 

oo 

00 

Calculation No. 145579-D-06, Rev. 1 

Attachment 3 

Page 11 of 22 


OCyTS B Wffl' a dY o 0 


Fitting Loss 

No Coef. 


J16 Outlet Transition Flanders 8 OD z 15 8.329 12.000 SD4-2 0.060 .04" 

W x 18 H x 12 L, 45 1 a 

750 

cfm 

OGTS Bypass HEPA Filter Skid Outlet Ducting 

With Fan to Stack 

P17 S1, Piping, 8-VOG-36- 8" straight duct, S.Stl, 8 IOS 8.329 12.000 CD1l-1 ARROW 

0319 w8 x8xI red tee, 

flow thru 

P17 Expansion Joint, EJ-616 8" Expansionjoint 8 ]OS 7.625 CR6-3 0.110 


1.000 ft 

J17 Fan, 36-N31-130 1125 ACFM Fan, ARROW ARROW 

NYB 1508, See Data 

Below 

P18 Elbow 90° Elbow, R/D = 8 l OS 8.329 CD3-1 0.110 

1.5, S.Stl 

" Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 6.000 CDl l-1 ARROW 

P18 Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 10S 8,329 36.000 CDl 1-1 ARROW 

Total 42.000 inches 0.110

v, 

A 

• • Calculation No. 145579-D-06, Rev, 1 

Attachment 3 

Page 12 of 22 


ft d 

,^ r Sn 

Component 

sz 

Details 

^ 

^xs 

OCaTS BYRkass S e k'ra 

1^m „ ^' o ya ^ ^ 

V 

X 

^ l t it 

g.. tx ..^.ave so['e .., i,`.k's^ W e .,. 

Size Schedule Inside Dia. L 

¢, 

ASHRAE 

Fitting 

ASHRAE 

Loss 

Cv 

No CoeE 


3.500 ft 

J18 Backdraft Damper SNUPPS Data See ARROW ARROW 

Below 

P19 Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 IOS 8.329 12.000 CDl l-1 ARROW 

J19 Isolation Valve, 36-V-166 8" Keystone, FIG. 8 7.625 2.500 ARROW ARROW 2440 

362-173,Key-Lok 

P20 Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 CD11-1 ARROW 

" Expansion Joint, EJ-617 8" Expansionjoint 8 lOS 7.625 11.000 CR6-3 0.110 

" Lateral Wye, Forward 45 1 Lateral Branch 8 lOS 8.329 24.000 ED5-1 0.610 

Direction Flow 

" Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 108.000 CDl l-1 ARROW 

" Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 loS 8.329 246.000 CD11-1 ARROW 

" Elbow 90 0 Elbow, R/D = 8 I OS 8.329 CD3-1 0.110 

1.5, S.Stl 

" Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 34.000 CDi l-1 ARROW 

" Elbow 90° Elbow, R/D = 8 lOS 8.329 CD3-1 0.110 

1.5, S.Stl 

" Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 144.000 CDI1-1 ARROW 

" Reducer 8 x 12 Std Reducer, 8 x 12 lOS 8.329/12.39 8.000 ED4-1 0.330 

28.5° 

P20 Sudden Expansion 12 x large 12 x 56 ED4-1 0.880 

Total 564.000 1 inches 1 2.040 

-3v 

w ^ 

4

Y, 

cis 

0 

• • Calculation No. 145579-D-06, Rev. l 

Attachment 3 . 

Page 13 of 22 

+ 


l 

X7'1{ Sfi h^k ^ pfl 

., s^L4^r .. 

y^'4.*^xn.["y„S'^^l 

"Î4tdu ^li^l 

Sfr^ 

t^, iN..CÎ `t T P 

^^^ts^ 

i 

i ^kS^^îhx 

.tax $ tp, ,Z^ >.^t eLu ^^ ssa ^% ^ .> 

QGTS Bypass System 

Component Details Size Schedule 

F 

Inside Dia. L ASHRAE 

Fitting 

No 

J20 OGTS Stack I atm pressure 

J21 Atmospheric Pressure 

Junction 

P21 Inlet Screen 16" Cicular Intake 


60% open) S.Stl 


47.000 ft 

ASHRAE 

Loss 

Coe£ 

16 15.624 CD6-1 0.970 

" Reducer 16" x 12" 16 x 12 los 15.624/12.39 14.000 ED4-1 0.120 

" Inlet Piping, 12-VOG-36- 12" straight duct, 

0409 

S.Stl 


1.5, S.Stl 


1.5, S.Stl 

P21 Elbow #3 90° Elbow, R/D = 

1.5, S.Stl 

12 IOS 12.39 90.000 CDl l-1 ARROW 

12 los 12.39 CD3-1 0.110 

12 los 12.39 CD3-1 0.110 

12 los 12.39 CD3-1 0.110 


8.667 ft 

Cv 

ro

• . Calculation No. 145579-D-606, Rev. 1 

Attachment 3 

Page 14 of 22 


y A 

a+ x 

R 

> S^ 1 

OGTS BypassSystem F1utd^Flav} n 

° arsw^> W qn "4 

ml) 

y' Yu `` 

Component Details Size Schedule InsideDia. L ASIIRAE ASHRAE Cv 

Fitting Loss 

No Coef. 


J22 HEPA Inlet Transition Flanders, Transition 12.0 dia x 11.250 ARROW ARROW 0.01" 

12" x 28" SQ x 28" SQ @ 

11.25' L; 300 250 

cfm 

J22 Heater Element, 36-N84- Watlow/Chromalox 2,000 

140 0.25' w.c. @ 1000 

cfm 

J22 HEPA Pre-Filter, 36-NO2- Flanders, 0.12" w.c. 24 x 24 2.000 

135 (0.24: dirty) at 1000 

cfm 

J22 HEPA Filter, 36-NO2-134 Flanders, 1.0" w.c. 

(2.0" dirty) at 1000 

cfm, P-007-W-43- 

N2-NU-51-23-CC- 

FU5 

24 x 24 5.875 

,122 Outlet Transition Flanders, Transition 6.065 dia x 11.250 0.002" 

6" x 28" SQ x 11.25" 28" SQ @ 

L, 45° 

Total Pressure drop at 1.382 

1000 cfm 

250 

cfm

OF 

N 

. • Calculation No. 145579-D-*56, Rev. 1 

Attachment 3 

Page 15 of 22 


". 1 C t C .14+ 

t t ^^^ 

OGTS By oss System Flurd FIR^^ Adel f , ,' ^ A 

Imff 

" 

Component Details Size Schedule Inside Dia, L ASHRAE ASHRAE Cv 

Fitting Loss 

No Coe£ 


P22 Piping, 6-VOG-36-0408 6" straight duct, S.Stl, 6 40S 6.357 6.000 CD11-1 ARROW 

w 6 x 6 x I red tee, 

flow thru 

J23 Valve, 36-V-178 6" Keystone, 6 2.250 ARROW ARROW 1194 

Variable Cv 

P23 Piping, 6-VOG-36-0408 6" straight duct, S.Stl 6 40S 6.357 41.000 CD11-1 ARROW 

11 

90 1 Elbow, R/D = 

1.5, S.Stl 

6 40S 6.357 CD3-1 0.110 

" Expansion Joint, EJ-614 6" Expansion Joint 6 40S 5.9 11.000 CR6-3 0.240 

" Tee 6 x 6 x 1 tee, flow 6 40S 6.357 12.000 ED5-3 0,260 

thru 



22.333 R 

J13 Wye #1 451 Lateral Branch 6x8 40S 6.357/8.329" 10.000 ARROW ARROW 

Flow 

Fan Curve, NYB Model Test Density: 0.0553 Mechanical 

No. 1508 lbn-/cu 8

a in 

w 

Calculation No. 145579-DA6, Rev. 1 

Attachment 3 

Page 16 of 22 


OATS Bypass ^Y^ye^lwd RI"oU^ od 1^^ + ^> = r 


Fitting 

No 

Q Ft/ Min dP, IN H2O Std Efficiency, 

0 12 67.36 

500 13.75 67.36 

1000 13 67.36 

1500 11.25 67.36 

2000 8 67.36 

2500 4.25 67.36 

3000 0 67.36 

Backdraft Damper 

Pressure Drop 

Ref. SNUPPS 90144 


24 x 24 prototype For 8" Pipe Area sch 10 Dia. 

Vs, fpm dP, inches w.c. Q, CFM sq. ft ft. 

700 0.13 264.9 0.378 0.694 

800 0.135 302.7 

900 0.14 340.5 

1000 0.145 378.4 

1500 0.18 567.6 

2000 0.23 756.7 

2500 0.27 945.9 

ASHRAE 

Loss 

Coef. 

Cv 

b 'v

R. 

A 

• • Calculation No. 145579-D-t*6, Rev.1 

Attachment 3 

Page 17 of 22 


k 

kW 

OGTS Bypass's tBBt^^lt1^ 1r 1 fl 16F 

Component Details Size Schedule Inside Dia. L ASHRAE ASHRAE Cv- 

Fitting Loss 

No Coef. 

3000 0.32 1135.1 

3500 0.36 1324.3 


b^n

0 

• 

RPP-24544 REV ld Calculation No. 145579-D-CA-056, Rev. 1 

Attachment 3 

Page 18 of 22 


A5-555

i 

N 

rn 

• • Calculation No. 145579-D-056, Rev. 1 

Attachment 3 

Page 19 of 22 

OGTS Bypass External Convection and Thermal Radiation Coefficients 

's i 

Y4 ar 

>a r m^ 

^VIe^dag=FreeConvecpontC4 

o^,^ ^^ ^. ,â ^ 4 

el op& a aatkL 

Twl = 875 OF 

Temperature End I 

Tw2 = 250 OF Temperature End 2 

Ts = 562.5 OF Average Wall Temperature 

To = 115 OF Ambient Temperature 

dT = 447,5 OF Temperature difference 

h = 1.45 13tu/hr-ft^2-°F Vertical Plane or Cylinder h = 0.19 * dT^1/3 

h = 1.38 Btu/hr-ft^2 °F Horizontal C tinder h = 0.18 * dT^1/3 

h = 1.68 Btu/hr-ft-2--F Horizontal Plate - heated face u h = 0.22 * dT^1/3 

Forced convection, flow across a cylinder (Holman 1990, e n. 6-21): 

0.32Rt 

x;2 Pr.ra 

N'ur.D =0.3+ ° 

[1 + (0.4 / PT}us ]"' L 

sre1.rs 

r Re 

(1+f ° ^ I ReQ- Pr > 1}.2 

+ 282,000 ! ) 

Nufd = 0.3+A*B/C Forced Convection, Nusselt No. 

A'= 0.62Rea !nPr' r' $ _ 1t Red/282,000 S18 ^43,' O., 1r't, 0`4L1xx T13 ^ 

D = 8.6 Inch Dia of Pie 0.21844 meters 

U = 0.1 Mph Free Stream Air Vel. 0.0447 m/s 

Ts = 562.5 OF Pipe Wall Temperature 294.72 °C 

To = 115 OF Ambient Temperature 46.11 °C 

Tf = 338.75 OF Air Film Temperature 170.42 °C 

vf = 0.00019 sq ft/sec Viscosity of Air 1.8E-05 sq. m/s 

Red = 5.45844E+02 Dimensionless Reynolds No. 

Pr = 0.7778 Dimensionless Prandtl No. 

N 

.p . 

N A. r 

.A; 

C 

a.

ON 

• • Calculation No. 145579-D-CO6, Rev.1 

Attachment 

Page 20 of 22 

OGTS Bypass External Convection and Thermal Radiation Coefficients

i 

Y, 

00 

• • Calculation No. 145579-DA6, Rev. 1 

Attachment 3 

Page 21 of 22 


^VIcAdams Free ConveÛon Cor el tiQn f -31 

al NOW 

;x a ^$ . fix ^1, "h ., ^.. a.S K i.e , e A^ .^ $ .§ 

Red*Pr = 424.57 The dimensionless numbers are: 

Nusselt, Nuz = k, or 1Vua — kD 

Rayleigh, 

g•S-P'cp(9T)O g•P-P•GPOTW 

PO4 _ k or Rao — 

v k 

r r 

Reynolds,. 

Re, = vL or Rep — VD 

Prandd, Pr = ° P. G° 

kr 

A = 13.322 B= 1.016 C= 1.132 

Stefan B = 1.714E-09 Btu/hr-ft^2-RA4 

emiss = 0.65 

Nufd = 12.26 Dimensionless Forced Convection, Nusselt No. 

Nund = 67.50 Dimensionless Natural Convection, Nusselt No. 

Nut = 0.3 + (Nufd- c)^' + (Nund - c ^' ^(I/') Combined Forced and Natural Convection, Nusselt No. 

c = 0.3 for Horizontal cylinder 

= 4 for Horizontal c linder 

Nut = 67.52 Dimensionless 

he= 1.38 Btu/hr-s .ft °F Combined Convection he = 7.81977 Watt/s m-°C 

k

h 


McAdarps 

^xecLlonvechon4^`òrrelatt^Y4s fo^•îâ^?^z^^ l 

.wz ^ " 

Radiation comonent: Stefan B = 1.714E-09 Btu/lu-ft^2-R^4 h, _ 

Ts —To 

emiss = 0.65 

hr = 2.45 Btu/hr-s .fa°F Th Radiation Coefficient 

ht = he + lu •Total HT Coefficient 

ht = 3.83 Btu/hr-s . ft-°F Total HT Coefficient 

= 1712.29 Btu/hr-s .ft Specific Heat Loss 

A = 2.25 s . ft for cylinder 1 ft long 

Q = 3855.18 Btu/hr for cylinder 1 ft long 

Q = 1129.84 Watts for cylinder I ft long 

Q = 1.13 KW for cylinder I ft lon 

.r 

L o y Vey` . 

.y^4V s ^ t;. > ,d`.,. 

Calculation No. 145579-D-*6, Rev. 1 

Attachment 3 

Page 22 of 22 

ro

0 Calculation 

• 

u 

DMJM H&N 1 AECOM 

No. 145579-D-CA-056 

Rev. No.: 1 

ORIGINATOR: John Hwm 03-25-2006 

Calculation Title: DBVS OGTS Bypass System CHECKER: k M C6nwell3—^C cZ 

Thermal Hydraulics Analysis I 

Equipment Data Sheets 

A5-560

• 

• 

RPP-24544'REV id 


A5-561

i • 

• 

• 

Standard Sizes and Capacities 

Flanders manufacturesstandard square 

and rectangular Nuclear Grade filters in 

a variety of saes and capacities. (Sizes 

and capacities for Round and Nippleconnected 

filters are listed in their 

respective sections in this bullefin.) The 

type (PUREFORW or Separator-Type) 

and depth of the filter element is a N 

primary factor in filter capacity. 

NOTE: The maximum allowable resin 

tanceat theAlaminalRatedCapacityis 1.0 

inch wg. (or 1.3lnch w.g. forcertain sizes 

listed in ASME AG7, Section FC, Table 

FC-4000-1). 

Available Filter Sizes and Capacities 

1 T inch PUREFORM'O Filter Element 

4 inch PUREFORMO Filter Element _ 

A5-562 

VA

f- - 

ANSI 

816.1041976 

Maximum 

Leakage - 

Test. 

Medium 

Press ure and 

Temperature 

CfassVI 

_ 

Nominal Port 

OWnuster (K) 

OubbMs per 

Knutes 

ml. par 

M1Gnuto 

Air or Nitrogen Service AP or 60 psig [14 bar d6e nen"L 

whichever is lover. at 50'to 1250F [10° to 529C) 

-, Class V 

2 3 

2112 4 

3 - 8 

4 11 

6 27 

8 45 

S x 10-dÙt0(nnl^l'psigim porlMat 

0.45 

0.60 

0.90 

1.70 

4.00 

6.75 

e r ' N^1' of ^ SoJt4^+1P'dtQ5D t9 t2b°F (10`0052 C) 

Ay, 

. ^;. 

.. .^ ....c 

Class IV 

,;' [5,]2 2x10] (n3/50Upaf^Blbntt8l(ÎHe^JfN[dlt fi 'y. .. 

0.01% vatve capacity at fulltravel Ala Water Service aP or SO psig 13.4 bardiOaeni 

to 

1.K-LCX polynen ckstomhand 6ra •sare seats pr*VWe ANSI Class V15wt& f. 

2.K-LCK metal seats provide ANSI Cie= IV shutoff. 

a Using the ANSYFCI spe ci 

fied calibrated meaurdng dev ice. 

Beterence AVBVFCl7a2 kv Further rnformatun 

• `1Y'Kî`°"^1^^`rt3 s° "iì2^'* 

r^'o`' i^.t'^""'^^`'r, w.. - ?.• a`"'"7. 

Angle of Opening CL150 CL300 

Size on.) 10' 20' 30' 40' 50' 60' 70` 80, 90' 90' 

3 6 12 24 43 U 100 139 IN 220 215 

.23 4¢' `80 130- -; 194 9.69, '360 426, 423'( 

.. 

5 30 4L 83 

149 2242 Me 504 679 795 Tai 

",' 6 '' a0 70 730, 230'!. 370 550'' 76DJ;OfO"' 1;195 ) f4e:." 

a 

10 

.. 83 

.:144 

117 ,. 

;20Z ., 

251 

:455-. ., 

:3T 

.754 < 

E% 

-S,iHS 

t,052 

'.: 1821 

1.496 

.42631 

LOUT 

`,3;54t 

2.440 

4;540 

2.3 00 

12 2DB 804 678 1061 1.625„ 2,768 3.830 oa2s G,91 6 6D'J_ 

7j tY88'I ,,908';j 3,121, 'x'4416 ,6275 H3p0 7920;; '_ 

18 

415 .)1373 

0.32 

',-5'}H 

003 

18121; 

1 .422 

15119^: is 

2289 3.514 

2.990 ., , 

:' 

52 51 7,8'0 1go4D 9,590 

4735 ";87;8 , ', 91815 S2;4fi0 .11.890:' .,. 

20 

24 

h'i 

-:'6'iD 

686 

"991 

1,300 

2,076' 

2.816 

3803 `.; 

4;010 

'. 6:Oo4 , -::. 

6;175 - 6.175 12,656 

9.091 .-t3301, - • ,18;466 

15,430 

„21,660 

14.720 

90.6Wi^; 'i: 

3D 1.015 l.SFA 3,240 4,670 9.465 11-,200 21,400 29,e00 30.000 35.500 

r-36 ' _1;460;?3i?D 4,640` 5,%07 '13,700 -C 2LOW '.304 '- 44;000 - '66;OW : ' 55,500;- 

'n ^v1t 

'E Mt"'"J.,3,1 

_J'i'ci`s4P' 

°^r,,..sa?c. 

t 

The combination of inle rforonce fit sea s 

r 

v-^'r7. 

_Actuator Type Figure 

"r'`^rc"' 

Remark 

T; ^p,•5' 

and bi-e ireclional packing makes the Hands F/Ai La e.r lack 

K-LOK especia lly weit suited for vacuum 

service. 

Gsu 

pneimatle 

'cqb aOd F{i00 Series 

F-AU 

. . 

With extended nav,,q adapter 

Standard K-LOK high performance 

naives are rated to an absolute pressure 

or 4 x 1 0 5 inch Hg. Higher vacuum 

soolicationsare available. 

Gear &P reeumahc 7;459 t F79U Cgtlulchd)[6 gear unit`l'rgvides narvral°' 

.. ,.. override ror Itx .. ifeysrora.pnsurnatic . actuator - 

Elec tric F7,7 

..____^^_...^ _^._.___._.....__^^T_^—__-- 

t ^ x s c vn J y^ ., zb 

f ^•5. -1 ^êY 

1 

t 3le {, 

A5-563 

S'£„^5 

F ;'j- Nn J ^ 1 S' ^Y y r" 

..n 

r s{ ,^y-^f 

'^rP^^3; i

• 

• 

The New York Blower Company 

Fan-to-Size 

Fan Selection Data 


Attachment 4 

Pages of 8 

Proiect: 

Location: 

Contact 

Product Pressure B lower Arranaement I 8 

SizelMlode" 1508 Drive bMe7 Direct 

Wheel T e: Steel 

Wheel PAatenaL' 316 SST 

Wheel Width: 100.0% Wheel Diameter. 1 100.0% 

n..e...+:.... r..«.+;+:..nom 

Volume Flow Rate: 1 125 CFM Fan Speed: 3500 rpm 

Fan Sta ti c Pressure: 12.8 in ivq Fan Input Power. 3.49 bhP 

Outlet Velocity-, 3223 ftfmin VP/SP ratio: 0.0374 

Altitude above mean sea level): 360 It operatinqTemperature: 250 Deg F 

Operating Inlet Airstream DensitT. 0.0653lbt1t3 

Sta ti c Efficlen : 64.93% Mechanical Efticien : 67.36% 

Maximum Opera ti ng 

250 Deg F Maximum Safe Operating Speed: 4000 rpm 

Temperature: 

C+.... A- A rnn ANinnc 

Volume Flow Rate: 1 125 CFM Fan S eed: 3500 rpm 

FanStatic Pressure: 17A in w Fan input Power: 4.73 bhp 

Density at Mean Sea Level ' 0.0750 IbIR3 Max. Safe Speed at 70 De F: I 4000 r m 

n_.._^n_.-.-..:_ _1 D_i:._^..• ..d:...ror.......... In..erc mf-'- 4rrnr_49l ur^fre\ 

Center Frequency (Hz): 63 125 250 _ -500 1000 2000 4660 8000 

Octave Bands: 1 2 3 4 5 6 7 8 Overall 

Total Fan Power Levels': 88: 95: 95. 89. 85. 83. 78. 76. 99.2 

Inlet Power Levels": 85. 92. 92. 86. 82. 80. 75. 73. 96.2 

Outlet Power Levels- 85. 92. 92. 85. 82. 80. 75. 73. 96.2 

-AS corenca rcr polni or meraaon liccûuri ran inri wr vc/ 

"tFnsiie^cad Inlet and Cufiaf paver ratings are 3 d6 !o ••ver than total fan cower!evels under the asunrpian that"tral° of the sound po^. •er can be 

attributed to each opercng. Silenced pover ratings include this 3 d6 reduction aswe9 as the silencer a ttenuation_ 

Estimated Sound Pressure Levels Expressed in dB (pressure levels refe re nce 2x101 aticrobar) 

Directivity[Reflection Factor (0) is 4, qua rter-Spherical radiation; Distance is 5 ft.: A-weighting is in use. 

The estimated sound pressure level outside the fan due to an open inlet OR outlet is 80.6 dBA at 5.0 feet. The 

estimated sound pressure level outside the fan When BOTH inlet and ou tl 

et are ducted is 69.1 dBA at 5.0 feet 

(Housing Radiated Noise). 

Your Representative: 

Baxter Air Enginee ri ng 

12625 NE Woodinville Dr 

Woodinville, WA 98072-8206 

Phone: (425) 486-6666 

Fax: (425) 486-8260 

E-Mail: baxterna"baxair_com 

•.7 Version: t1r^00-R l 

f^=l, =CO2; 

A5-564 

Pdn:ed. O';izi?00; P^f

Y, 

in 

rn 

Pressure Blower 

1503 Steel 

A rr.: 3 

C 

a^ 

12.5 

10.0 

to 7.5 

2 

'n7 

C 

«s 

IL 

5.0 

2.5 

M 

VGsi4P: 1.71.1000-R {Rua, 2002) 

_ 

J 

f1 

• 

The New York Blower Company 

Fan-lo-Size 

Volume Flow Rate: 1,125 CFM 

Nan Static Press'.: (2.3 in wg 

Speed: 3500 rptn 

Power: 3.49 bhp 

^f 

/ 

f 

tau\Press 

- --- - --- ^'--.._. --........_..---- ----- -- - 

I 

_ vae r 

f^ 

— 

stem Cu rve 

0 500 1000 1500 2000 2500 

Volume Flow Rate (CFM) 

[0 .7€.1000-R --Feb, 2002] DatePripted:l/i9/2006 

Copyright C01 999 Tha New York Blower Company. 

Temp.: 250 Deg F 

Altitude: 360 ft 

Density: 0.0553lbfft3 

Outlet Velocity: 3223 ft (min 

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RPP-24544 REV ld Calculation No. 145579-D-CA-056, Rev.1 

Attachment 4 

Page 8 of 8 

•.. TYPICAL PRESSURE DROP AS FUNCTION OF FLOW VELOCITY FOR AWV MODEL 

NOD-.71 TORNADO INTAKE DAMPER PER AMCA 500., FIGURE 5.3 FOR INDUCT 

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REF.: SNUPPS 90154; 24" X 24" E 42" ' X 42" PROTOTYPES 

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Rev. No.: 1 


Attachment 5 

Calculation Title: DBVS OGTS Bypass System CHECKER: ac ki o 



Page 1 of 32 

ORIGINATOR:John Irwin, 03-25-2006 

ASHRAE Fundamentals Duct Fitting Loss Coefficients 

A5-568 

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RPP`-24544 REV Id Calculation No.'145579-D-CA-056, Rev.1 

Attachment 5 

Page 2 of 32 


A5-569

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FITTING LOSS COEFFICIENTS 

Fittings to mpporl Bxemples 6 a0d:7 mud some orlhemom 0mnm0*93 arc rcpAotcdberc. 

For the caueplate. *. ftdatahase sce the Durl Fift/4 baa8ase (ASHRAE 2002). 

CD34 Elbow, Die Stamped, 90 Degree, rlb=1.3 

ROUND FITTINGS 

D, in. 3 d. 5 6 7 8 9 10 

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C,. 015- O.A3 034 0,2s 0.26 025 0.25 

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RPP-24544'REV id Calculation No:145579-D-CA-056, Rev.1 

Attachment 5 

Page 4 of 32 

Dud Deign 35.29 

CD344 Elbow, 3 Cores 45 Degree, r1D a 1.5 

A In. 1 6 9 12 15 18 21 24 27 30 60 

C. 031 0.17 0.33 0.11 0.13 0,09 D," OAe 0.07 0.07 11{17 `j 

CD347 elbow, Dlitercd, 45 Degree 

D, 1.. 3 6 9 1215 18 21 24 27 6D 

C„ 0.34 0.54 0.34 035 0.34 0.34 034 0,34 0.33 0.34 

CD64 Screen (Only) 

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CD9-1 Damper, Butterfly 

RPP-24544 REV Td Calculation No. 145579-D-CA-056, Rev. 1 

Attachment 5 

Page 5 of 32 

2W ASMUE Handbook-Fundamentvla 

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1.0 -256.25 X1535 -11.33 -2.63 0.2 61,21 IA2 1;31 1.09 

0.5 02 ..3,62 -036 0.54 037 0.8S 388 0.91 -0.95 I' l l 

0:3 -16.42 -2.11 40 1 0.54 0.72 Mlk 0.80 0.93 DA 

41.4 -3026 -5.59 4.79 0.22 6.54 064 0.66 0.64 04 

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D, -9S.fq -15..31 -3.65 -0.45 0.4.1 274 0.77 071 OAI 

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0.5 -35,41 -5.9.1 -1, 16 4.09 0,15 0.59 0.60 0.57 01 ;55 

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as 47,4 -12,38 -3.24 -0169 0.13 0.38 OA2 0.3'7 0.31 

03 - -9&35 -16.38 4,20 -0.95 0.09 0.40 0.45 0.34 0.30 

1.0 -121.48 a20.27 -5,24 _03 0.06 0145 0.51 0.43 0.31 

0.9 02 7.52 Oat 0 164 a79 0.82 035 0 183 0.93 1 32 

03 -034 -095 0.28 6.60 0:71 0.76 0.80 0.31 ) x0 

0.4 -17.96 -170 4.40 0,72 0.43 0.50 0113 054 0.60 

as -28.5s 4.65 -1,05 -0.07 026 0.37 0.40 0,41 0.42 

0.6 -41.45 -6.97 -•1.77 -0:35 0.12 0.23 032 0.32 0.32 

0.7 -5661 x.65 -2,53 -0.65 15.0(1 0.21 0:39 0.26 0.24 

11.8 -74.1 9 -12.71 -3.49 -097 -0.12 0.16 221 0,22 0,13 

09 -93.84 -16.21 -0.50 -1,30 -0.23 0.13 021 0.19 0.14 

1.0 -11592 -20.06 -5.61 -1.66 434 0.11 0.21 0.18 9.11 

LO 02 -3as 0.10 0.62 0.76 0.81 0.8.1 °" 017 092 1.11 

03 -9.22 -1.00 0.23 056 0.63 0.74 0.78 O.^s6 1.11 

0A -17. 176 -2.74 -0.50 0.14 0.37 045 0A9 0.52 060 

0.5 -23.31 -4.82 -1.2t 41.20 0.15 0.28 0.33 031 033 

0.6 -1.06 -7.21 -201 4.55 -0.04 0.15 0.22 0.23 11121 

0.7 -%,09 41.49 -2.91 -09 2 4.23 0.03 0,12 0 1 14 0,13 

28 -7339 -13.37 792 -1.32 - 0.41 -0104 O.O= 406 006 

0.9 -92.998 -1635 -5.04 -1.75 4.60 -03 7 -0.03 -0.01 -002 

1.0 -114.85 X0.74 -6.2s -221 -0.79 -0.20 -co -007 -009 

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23 -11.65 -1.94 -b:2b 032 0.60 0.77 0:)0 1,03 ;,10 

0.4 -3.56 -120 DA$ 0.47 0.63 0.82 0.92 1.02 1.11 

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0.4 -56.18 -1059 -3:21 -1,02 -D20 03 33 026 0.29 Da? 

0.5 -4104 7-74 -216 -0.S6 0.02 0.23 030 0.30 D27 

0.6. 43,51 -5172 -1.43 -0.27 0.16 0.0 0.33 0.31 028 

0.1 -2639 -4.12 ' -0.90 -0.01 0.7 0.35 013 0.32 0.23 

0.8 -20.75 -3.06 -0.49 0.76 035 0139 0.37 0.33 028 

0.9 -16,9 2.14 -0,17 0.31) OAI OA1 0.38 9.33 D.25 

X1.0 -12.64 -139 0.10 0.41 0.46 0,44 039 0,33 0,28 

0.6 0.2 -146.06 3116 -11.09 -4.56 -1-89 -0.68 41 12 01 10 0.16 

0,3 -108.19 -23.55 -7.12 -169 -&97 -D.I4 0 107 03 7 0.17 

0.4 -81.00 -75.40 -4.80 -1.65 -0.45 -0.01 0-17 9.2D 0.18 

0,5 -Q.13 -11.39 3.30 -0.99 -0.17 0 1 13 0.22 022 0.19 

0.6 -43.43 -&At -2.75 -054 0.03 222 0.26 024 0.18 

0.7 ISAO -623 -1.49 -0.22 0.18 0.27 0.29 0,125 0.19 

03 -+30.07 -4-59 -0,50 0103 0:70 O.Y. 0.31 0.25 0.19 

0.9 -2164 -317 -0.44 0.23 6.39 0:38 0.33 0.26 0.19 

1 10 -18.54 2:0 -0.06 11139 0,46 002 0.34. 227 0.!9 

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0.3 -3.17.33 -29.41 -3.78 1.7 -!A4 -0.45 4.04 0.10 OAO 

0.4 -110.40 -21.07 -6 141 236 -0.77 -0.14 0.09 035 0.11 

- 0.5 -84.67 -75.50 - A* -1.48 -0.36 0.05 0.17 0.17 m 

0.6 -66.02 -11.56 -3.19 -0.86 -O.O3 0.18 0:23 0.19 0.12 

09 -51.97 ..8.63 --245 -0.42 0. 12 0:27 0127 03o 0.32 

0.S 4 1.04 -6.37 -1.35 -0.08 0.27 034 0.'29 021 0.32 

0.9 42.30 -4 413 -0.72 0.19 039 (1,39 012 022 O.0 

1.0 -?5.: fi -3.12 -0.21 0.40 0.49 rl.,3 U:53 0.'3 0.13 

0.8 0.2 -1159,75 -55 m70 -196 ^329 -7 ,H -1.43 -0.46 - 0.0 0.03 

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04 -144.25 -27 158 -3.74 -3 1 16 -1.09 --0,26 105 0.11 9A6 

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Calculation No. 145579-D-CA-056; Rev.1 

Attachment 5 

Page 17 of 32 

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0,8 752 2.25 123. 1137 070 0.61 056 0:52 0.49 

09 6.95 3 1 19 622 4%7 D.10 0.61 0.56 0.52 0.49 - 

1.0 6.76 ail 1121 0.56 070 0.61 0.55 0.5 2 0,49 

0.4 11.2 90.:1? 12.10 ?91 L85 LOS 074 0 1 55 0.45 0.38 

0.3 49.69 7.50 2.74 1242 0.0 0,63 0.51 0.43 03 7 

11.4 10,96 531 221 123 *.3Z 0.61 0.49 0.42 937 

0.5 2 1,00 4,40 1,91i 1.17 0:78 0159 0.48 042 0.37 

0.6 15.43 378 1.76 IX, 0.75 0.58 41.48 041 0.37 

0,7 1736 3.44 1.67 IA-1 0,75 0.57 0.4 9 PAI 0.37 

0.3 1 101 80 - I,6 3 1,02 0,73 057 0.41 Dill 217 

0,9 @A0 3.22 1.61 1,07 D.73 057 0.47 0;41 0.37 

1.0 1267 3.25 1.62 1:02 0.73 0.57 047 0.41 0:37 

V n,3 02 126.36 1699 5.39 242 132 0.31 0.54 0.35 0.28 

03 65.9: 3023 3b3 !,79 JAS 11, 6 8 048 0.35 027 

0.4 

OS 

0:5 

38.E -1 

.'SM 

1?5-c 

-7.27 

4 74 

4:95 

2.87 

2.

• 

• 

E 

DuctDesign 

EM-3 Tee,Dr > 10 In, Conrergillg(C6nanoed) 

RPP-24544 REV ld Calculation No. 145579-D-CA-056, Rev. 1 

Attachment 5 

Page 38 of 32 

CVelucl(bx/wkJi 

A,64,, 4,14, 01 0.2 03 OA (s 0.6 0.7 6.9 )9 

0.6 02 146.22 2032 6.54 2192 9,54 0.84 0.54 033 0.30 

03 70.93 -14.05 431 2.11 1.70 .033 0.46 030. 0.19 

0.4 3566 8:37 3.44 180. 1.06 0.61 6.43 0x8 0.13 

0.5 23.61 ` 6.70 3.00 1.64 0.99 0.64. 0.42 US: 018 

0.6 17.11 S98 292 137 0.97 0.62. 0.41 027 6.18 

0.7 15.63 5:81 Z 17 I56 0.96 0.62 0.41 027 0.19: 

0.8 1719 598. 2:82 L57 0.97 0.62 0,41 027 Q18 

0.9 20.79 018 292 1.61 0.98' 0.63 0.42 027 0,18 

I.0 25.82 494 3.07 1.66 1.00 064 0.42 D28 0.18 - 

0.7 D2 13739 20,74 7Al 321 1.70 096 0:54 029 013 - -- - 

0.3 $8.74 11..96 4.73 ?-39 1.34 037 0,47 036 012' . 

0.4 27.78 &52 5.84 206 1.21 0.73 0.44 024' 011 

0.5 16.04 121 3.50 134 913 1171 0.43 034 0:11 

DA 13.91 6:97 3A4 1:92 1.14 0.70. 0.42 024 0.11 

0.7 17.28 7.35 3.54 1195 1.16 0.171 043 024 0,11 

0.8 24,08 8,10 3,73 MR, 1,19 0,72 0.43 D,24 0.11 

0.9 31A7 9.11 399 2112 1.23 0.74 0.44 0:75 0.11 

E D 43.86 10.30 430 2.3 129 076 0.45 0.:5 0.11 

3543 

Da 0.2 92.97 17.35 6.54 321 1:75 0.99 0.55 027 0.08, 

03 26,99 70:02 467 2.52 1.46 - 0.96 0.48 0.24 007 

0.4 6.75 9,77 4.09 2131 337 Mj 0.46 D.23 0.05: 

0.5 4.83 7.56 4.03 229 1,36 0.89 0.46 033 006 - 

O6 12.05 9.36 1124 2.37 137 0.81 0.47 0.21 0.07 

0.7 24.51 9.75 4.40 2.49 1.45 0.85 0.49 024 007 

0.8 40.23 11,49 5.05 2.66 1:52 - 0188 0150 0 2 9 D.07 

0.9 .`-813 13.48 5.37 2.95 L60 0:92 0.51 0.25 0197 

LD 7.54 15.65 ru1 3.05 169 0.96 0.53 O.J 0.08- - 

1l.9 0.2 1077 1005 520 291 1.10 0." (1.55 0.25 00 

p.3 -2127 649 4.28 2.57 1 S6 0.93 052 0.24 0.05 

p,4 i9J 1 6.7-e 4.34 219 L57 0.93 0.52 0.24 O.Ig - 

0.5 -129 S:19 4.80 2.46 1.64 Wn 0.54 0:24 0104 

0.4 19:39 11.07 5.45 3.011 174 EA1 il 56 625 01 t 

27 45.97 11% 421 3121 1116 1.07 0.59 0.27 O.DS 

ri.8 7490 17.€8 7.05 3.59 198 1.13 0151 028 0.05 

09 135.44 2259 7.93 3.59 2.12 1.19 0.64 0.29 (! 06 

1!t 137,43 :4.12 51155 323 226 126 0.67 0.31 0.D6 

IA 0,2 -+JR.78 -0.17 3.15 3.40 1.59 0.99 0.56 033 0.03 

0.3 -75.42 2.54 3,95 "(5 Lo 303 0.58 0,26 0.03 

0.4 1837 466 02 404 1.86 1 I. 0,62 028 0113 

0.5 3M 11.35 6.14 3.48 201 1.20 0:65 029 0.04 

06 44,66 16.52 7.43 3.94 2.24 1.29 0.70' 1231 0.04 

0.1 94.88 21.46 8.76 4-3 2445 ).39 O75 1133 0.05 

09 1+201 24.10 10.12 412 166 348 0.79 0.35 0.06 

0.9 139.73 32.00 13.19 5.4t 2.89 1.S& 0.84 037 0.07 

1,0 237.90 37.35 1258 592 3XIS 1.68 D%8 0:39 0.07 

A5-585

• 

0 

35A4 

EDS-6 Capped %v, Br=cb with 45-0firim Mhmr, 

Branch 90 Degrees to Mcin t- tS 

A,IA, 0.1 01 03 0.4 

C, 1,26 I 'm 0.94 0,96 0,81 - V6 0.171 057 0.64 4A4 

RPP-24544 REV Id Calculation No. l4M j9-1)-CA-056,Rev. 1 

Attaclunent 5 

Page 19 of 32 

03 0.6 4.1 4.8 69 1.0 

EDS ?9 Symmetrical Wye, 60 Dear", Db , ^ D j, Cornrerging 

Â 

Dbt (11' min, or 

42' max.) 

T 

o 

D. - D min. or 

b2 ( 

12" max.) 

C01 \âitl¢f 

ASHRAE Handbook-Fundamentals 

A,1A, OA M. 0.3 0.4 05 9.6 0.7 0.9 0.9 

U. - 11.95 4,89 -0,09 0.41 0.62 0.74 OU 4.50 Ir. 9 

03 -11.95 _L89 -0.09 (kll 01112 0,74 OXI X250 0.79 

klz -45,43 A39 -144 4.41 0.33 0:5,C 0'3 9 1.03 1.13 

03 -yfiY8 -2.92 -0.09 0S9 096 1 ;02 hn", 1.10 !.N 

0.4 0.2 4294 -14.VJ -4.26 

-1 _1)_; 4 -0,10 0.33 11.50 C07 0, 63 

0 -5295 -9.4J2.$6 

-9.4J .^6 

9 QV 0.10 0.40 049 OR, 

0,4 -28.86 -622 2iJ 437 0119 0.55 0.-1 2 M11) o"Is 

0.5 *2 

t.0 

OA 

013 

1.12604 

-9107 

-56.41 

-3058 

-21147.44 

-101 -S.M 

-IOX 2 .911 

-532 -1 96 

.,ZS4 

_173 

-10.82 

000 

-0.95 

-0.46 

-00 

0.32 

-0.E3 

QA4 

QM 

0.43 

0,16 

02 t 

030 

0 47 

0.26 

0.19 

6,31 

OX 

O.Z$ 

0.28 

0,29 

0.41 

O ' Z 

0 3 

04 

0.5 

-209M 

-1471 3 

-.%22 

-3 9.11 

-211.69 

-16.07 

-1193 

-12.)" 

-835 

3.38 

-4:35 -L54 

-3.20 -4.13 

- 1X4 -0.71 

-0.40 

-0129 

-0A 7 

-0.09 

0.06 

DOS 

004 

*07 

022 

0.17 

0.11 

0. 

0.21, 

OA 

0.6 x O.q. 

1) 

0A 

9137 

-197 37 

-1 

15 

-S4.52 

4&92 

-21.41 

;ji 

-i-.03 

-Rx* 

I V. 

-6. 21 

I.Ir 

_V)l - 7 

-135 

1,011 

-0.76v, 

--O.P.4 

-0'S5 

-0411 

-11,14 

0.±°i 

too! 

.(1.17 

0,09 

-J 115 

-P,69 

JA -11.70 511 ;;.(13 

0. -],0] -1mH 19 - 761 -'.;rd0 _e?Y 10?. ,.-- 

-.173.113 . 0.4 

-' T. ,j) 

247,11 41K11 -S(_ 2 

X 08 

&Lq 

-9.93 

- 1. 1 4 

1 

-9,14 

:1.15 20 

4 0 -r- 1ji 

4 45 

A5-586 

Ac A. 

Q I Ab 

"I

a 

Y, 

00 

-11 

^rnll 

P 

P 8 

pp 

POP= 

L L 

16 &11111 1l, 4 

Iron. 

I 'it 

m 

t 

A Ii 

. "bt 

M 

IV 

is

RPP-24544 RBV'Id Calculation No. 245579-D-CA-056, Rev.1 

Attachment 5 

Page 21 of 32 

• - r. 

• 

• 

Duct .DOMP. 

.. 

SDY-2 C0oicalHellm00ttJS0^dcu CDatNCtiOn, 

. Pleaum so Round, SuWYAfr5ysemx(fbn#n#e4. - - 

oYaluta(CDnr7nQe0) - 

- A.M1 MD. 0 10 20 30 45 60 - 98 120 150 .180 

0,40 . OA15 034 0.32 0.31 0,29 0.25 0.27 025 030 0.32 0.34 

- :0.030 034 0.31 0.28 D.25 032 020 023 0,26 0.30 034 

0.075 034 029 ' 024 D.20 0.17 0.16 0.19 024 0.29 0.34 

0.700 034 '027 0.22 017 0.14 0.12 4 17 on 0.28 0.34 - 

0.150 D34 025 0.15 D.lu D.It 0.10 0.13 O21 Dr Dan. 

-_ 0.300 0,34 0.23 0.16 0.12 0.10 0,10 `0.15 0.21 0,27 0314 

0.600 034 098 0.12 0.09 0.05 0:08 0.14 020 0.27 034 

0.60 0,025 0.25 0,24 0.23 0.22 a2D 0.20 021 0.22 ' 023 025 

0.0!0 D.25 0.23 02 1 0.18 0.16 0.15 0.17 0.19 0.22 0.25 

0.075 024 021 6.18 0.13 0.13 0.12 0.14 098 621 025 - - 

- 0.100 015 0.20 0.16 D.13 091 OM 0.12 OJ6 0:21 015 - - - 

O.M 025 0.14 0.14 0.10 DA8 O.DS 0.11 0.16 0.20 023 

0300' O25 0.17 0.12 0:09 0.07 0.07 0.11 OAS 0.20 025 

OfM 023 0.14 0.09 0.09 0.06 0.06 0.10 0.15 020 0:2S 

'O.SO 0.025 0.13 ON 0.13 0.13 0.12 902' 0.12 0.13 0. 14 0.15 

0.050 D.15 0.13 0.12 0.11 DAD 0.04 0.10 0.12 0.13 OAS 

0,075 OAS 0,13 0,10 0.09 00,8 0.177 OAS 0.10 0.31 9.15 

0.103 0.15 0.12 0.10 0.07 O06 0.05 007 0.10 092 US 

4)J50 0.15 0.1E 0.08 00,6 010S 0 104 OA?. OA9 OJZ 0.15 -" 

,03CO 0:13 0.10 0.07 0A3 0.04 0.04 O97 0.09 OJ2 OJS 

0.600 0.15 *AS 0.05 0.04 0.03 0.04 ,0.06 0.09 0.12 0.15 

0.90 0.025 0.04 0.08 00,8 0.09 OOr, 0.07 0.07 OAS 0,08 0.09 

DASll 0.0 0.09 OA7 0.06 006 0.05 11.66 0.07 0)i8 0.69 

0575 0,09 0.07 0.04 0,05 004 0.0 4 0116 0.06 O05 0.09 

0.10 0.0 0.07 0A6 iO 4 0.04 0.03 0.04 0.06 0.07 0.09 

D150 0.09 0.07 0.0$ 0,01 003 0.03 O04 On6 047 0.09 

0309 0.09 0.06 0.04 0.03 0:03 0.02 0.04 0,05 0,07 0.09 

0.40 1) 0.09 D.05 0A3 0.02 0.02 0.0 2 OM 0.05 0.07 0.09 

SD2-6 Stackhead 

1),,11 0.3 -70 -03-0 -0 7 O,tl OJ1.n 

Cn 1 29 41oz Man 5.10 4.17 2.56 1.60 10,0 

A5-588 

1 1 I 1 ^ 

IIIQ 

^^ Q 

40 

3S $7:' 

DEin, 

TD - 

De-D < 1.0 -L)"D = t 

1 in.

. 

• 

35.43 

SD4.7. Tmsl tlon, Round to hound, SupplyMr Systems 

Co Valves 

A,Lt 1 10 13. 20 30 45 60 94 120 160 180 

0.10 0.05 005 005 O45 0A7 OAS 0.19 029. 9.3A OA3 

0.17 0.05 004 ON 0.04 06 PAY 0.18 0.28 0.36 0.42 

oZ5 OAS ON 004 OA4 0:06 OX 0.17 027 435 OAl 

0.50 0.05 OAS 0.05.' 0.05 0.06 0.06 0.12 0.18 0.24 Ot% 

1,00 O.M 0.00 0.00 0.00 O.OD OM DAD O.OD 0.00 0,03 

2.00 0.44 0,52 0.76 139 1-12 1.32 1,28 1.24 1.20 1.20 

4.00 2.56 3.32 4.80. 776 9.76 10.88 1024 10.09 9.92 9.92 

10,00 21,00 25.00 29.00 5BA0 76.00. MOO 8100 84.00 83.00 93.0 

16.0 5176 -.34.29 9718 153AO 215.04 22329.223.28 225.28 r5.28 223.28 

S114.2'rra"Woe, Rectangular to ltontul,Supply Air Syslens 

C. Vidurs 

B 

0 

"iA 24544 REV 1d 

- . - - CalmAntinn Mn 14'MO-P-CA-056_ Rev_ 1` - 

01 

A, 

11131 IM 

,^tetd, 10 IS 20 30 45 60 90 120 150 180 

0.10 

0.17 

0 

005 

0. 05 

0.03 

0.05 

0.0 

004 

0.05 

D.04 

0.07 

0.06 

0.09 

4.07 

0.19 

OAS 

029 

US 

0:37 

036 

0.43 

0.42 

25 

OSO 

1110 

2.00 

4:CO 

096 

O.t16 

0.00 

06O 

4.00 

0.05 

OX 

400 

0.94 

5,76 

0.05 

0.07 

0.0 

1.0 

.7.20 

0.44 

0:05 

DBA 

1.20 

S.'32 

0.06 

0.06 

"0 

132 

9.25 

4.07 

6A6 

040 

t32 

992 

0.17 

0.12 

0.00 

732 

10,24 

0.27 

478 

*.Do 

1.28 

1424' 

035 

024 

4W 

1.24 

10.24 

041 

016 

0.00 

1.20 mna rw 

1024 

I 63'6 30.00 

16.00 76.%0 

30.00 

123.24 

33.00 

135.63 

64.00 

166AO 

?5.00 84.00 S9A0 91.00 91:01 58.00 

197,12 225.5 24220 250.9% 250.95 '239.118 

SDS•:144yo, 45 Degree, Diverging 

VWmes 

A,,m, 0.1 012 03 0.4 0.5 0.6 0.7 0.8 0.9 

0.1 0$3 0.39 OAS 

0.2 235 0.38 0.31 0,39 050 0.49 0A5 

41.3 6 29 1.02 0.35 0.30 4133 0:19 n ,14 0.48 44n 

OA 1 2, 41 225 074 A.18 030 0 . 3) 035 0.39 043 

0.5 20.58 491 1_37 0.62 4:38 0.30 030 0.92 036 

OA 50.75 6:29 2.25 1.02 0.56 0.39 031 0.30 031 

03 53,0,'. 9:10 336 1.57 283 0.52 03s 031 030 

0.8 5729 12.41 4.71 215 122 0.74 0.30 0.36 032 

19 7,1.59 t 3_2d 629 3.06 1 ,69 1 .02 Gel? 0.3 8 0-49 

C, Valuer 

: I,m, 0.1 0.2 0.3 OA 0.3 0.6 0.'7 0.8 0.9 

m.3 

.. 

Os 

01: 

6.20 

0.90 

2.9% 

6.25 

11:13 

On 

q. 1 2 

00 

037 

p40 

015 

6.13 

0-1^ 

U.;: 

0 13 

0.16 

0.14 

0.13 

0.1 . 1 

,!13 

0.28 

D,IS 

01, 14 

11.13 

Od= 

0.16 

0.11 

0.1 , 1 

0, 1': 

07n 

6,14 

0.14 

U!4' 

(06 

0.13 

c.14 

034 

0.15 

0.15 

O:: 1::.1,2 f.'t; 0.33 L15 O.14 5.14 0„3 C.1? 0.14 

0.8 =n.55 3. -0 1 0.20 O.iS 116 1 O.ii ;.1 0.1: 

11.,4 5 4 ^Y, 11.:4: 1330 P. '.9 DI(., U. ES C.I4 013 

e l 

A5-589 

Dc - • 17, (1' ml-. at I T',M.0 

0. 

A,

• 

• 

Duct Design 

SD5-Me,Diverging 

C, Values 

A,IA, 0.3 0.2 0.3. 0.4 OS 0.6 0.7 0.8 09 Oc 

0.1. 1.20 0.62 0.80 1.28 1.99 2.92 4.07 5.44 7.02 Ac 

0.2 4.10 1.20 0.72 0.62 0.66 0.86 1.01 1.28 1.60 

0.3 8.99 2.40 120 0.81 046 0.62 0.64. 0.70 0.80 

0.4 15.89 4.10 1.94 1.20 0.88 0.72 0.64 0.62 0.63 

0.5 21.80 6.29 2.91 1.74 1.20 0.92 ' 0.77 -0.68 0.63 

0.6 .35.73 .8.99 4.10 2.40 '1.62 1.20 036 0.81 0.72 

• 0.7 48.67 12.19 5.51 3.19 2.12 1.55 1.20 0.99 0.85 - - 

0.8 63.63 15.89 7.14 4.10 2.70 1.94 1.49 1.20 1.01 

0.9 80.60 20.10 8.99 5.13 336 2.40 1.83 1.46 1.20 

C Value, 

Q.1Q< 

A,/A, 0.1 0.2 0.3 0.4 05 0.6 0.7 0.8 09 

0.1 '0.13 0.16 

0.2 010 0.13 0.15 0.16 0.28 

0.3 0.90 0.13 0.13 0.14 0.15 0.16 0.20 

0.4 2.88 0.20 0.14 0.13 0.14 0.15 0.15 0.16 0.34 

0.5 6.25 0.37 0.17 0.14 0.13 0.14 0.14 OAS 0.15 

0.6 11.88 0.90 0.20 0.13 0.14 0.13 0.14 0.14 - 0.15 

0.7 18.62 1.71 0.33 0.18 0.16 0.14 0.13 0.15 0.14 

0:8 26.88 2.88 0.50 0.20 0.15 0.14 0.13 0.13 0.14 

0.9 36.45 4.46 0.90 0.30 0.19 0.16 0.15 0.14 0.13 

SD5-10 Tee, Conical Branch Tapered into Body, Diverging 

Ca Values 

Qe19 

AyIA, 0.1 0.2 0.3 0.4 OS 0.6 0.7 0.8 0.9 

0.1 0.65 0.24 

0.2 2.98 0.65 0.33 0.24 0.18 

0.3 7.36 1.56 0.65 0.39 0.29 0.24 .020 

0.4 13.78 2.98 1.20 0.65 0.43 0.33 0.27 0.24 0.21 

0.5 22.24 4.92 1.98 1.00 0.65 0.47 0.36 0.30 0.26 

0.6 32.73 7.36 2.98 1.56 0.96 0.65 0.49 0.39 9.33 

0.7 45.26 10.32 4.21 2.21 1.34 0.90 0.65 0.51 0.42 

0.8 59.82 13.78 5.67 2.98 1.80 1.20 0.86 0.65 0.52 

0.9 76.41 17.75 7.36 3.88 235 1.56 1.11 0.83 0.65 

C Valnes 

A,M, 0.1 0.2 03 0.4 0.5 0.6 0.7 0.8 0.9 

0.1 0.13 0.16 

0.2 0.20 0.13 0.15 0.16 0.28 

0.3 0.90 0.13 0.13 0.14 0.15 0.16 0.20 

0.4 2.88 0.20 0.14 0.13 0.14 OAS 0.15 0.16 0.34 

0.5 6.25 0.3? 0.17 0.14 0.13 0.14 0.14 0.15 0.15 

0.6 11.88 0.90 0.20 0.13 0.14 0.13 0.14 0.14 0.15 

07 18.62 1.71 0.33 0.18 0.16 0.14 0.13 0.15 0.14 

0.8 26.88 2.88 0.50 0.20 0.15 0.14 0.13 0.13 0.14 

0.9 36AS 4.46 0.90 0.30 0.19 0.16 0.15 0.14 0.13 

A5-590 

Oc 

Ac 

0.1 A. 

%I Ae 

- 

p 12`mm) 

0, 

As 

35.49

Daet Design 

RPP-24544'REV 1'd 

CR3.9: Maw, Mitered, 90 DtUtt, SinglbTbicknm VAR"OS im YAnt SpaNne) 

o'edl 

i=2ein. 

s-t.5h 

CR3-12 Elbow, Mitered, 90 Degree, Single-Thidknces Vanes (3.25 in. VaneSpadne) 

—D.33 

rFastn. 

s=3,25 in. 

• AA 

Harr 

• 

C,=I)25 

AR 

FLOW 

CR3.15 Mow, 0literet"O PeWte, Double-Thicirnas Vanes (2.125 in. Vane Spacing) 

A5-591 

5 

r=2:0in. 

s= 2.125 in.

C113-17 Elbow, ZShnped. 

C, Val.a 

Ll1V 

H/3V 0.0 0.4 0.6 0.8 '1,1 1.2 IA L6 1.8 2.0 4.0 8.0 10.0 100.0 Q 

• 0.25 0.00 0.68 0.99 7.77 2.89 3.97 4.41 4.60 4.64 4.60 3.39 3.03 . 2.70 2.53 A. 

0.50 0.00 0.66 0.96 1.72 2.81 3.86 4.29 4.47 4.52 4.47 3.30 2.94 2.62 2.46 

0.75 0.00 0.64 0.94 1.67 2.74 3.75 4.17 4.35 4.39 4.35 3.20 2.86 2.55 239 

1.00 0.00 0.62 0.90 1.61 2.63 3.61 4.01 4.18 4.22 4.18 3.08 2.75 2.45 2.30 

1.50 0.00 0.59 0.86 1.53 ISO 3.43 3.81 3.97 4.01 3.97 2.93 2.61 2.33 2.19 

• 

r _i 

-0S in. 

s = &25 in. 

2.00 0.00 0.56 0.81 . 1.45 2.37 3.25 3.61 3.76 3.80 3.76 2.77 2.48 2.21 2.07 

3.00 0.00 0.51 0.75 1.34 2.18 3.00 3.33 3.47 150 3.47 2.56 2.28 2.03 1,91 

4.00 0.00 0.48 0.70 1.26 2.05 2.82 3.13 3.26 3.29 3.26 2.40 2.15 1.91. 1.79 

Co = KrCp 

6.00 0.00 0.45 0.65 1.16 1.89 2.60 2.89 3.01 3.04 3.01 2.22. 1.98 1.76 1.66 where K. = Reynolds number correction factor 

8.00 0.00 0.43 0.63 1.33 1.84 2.53 2.81 2.91 195 2.93 2.16 1.93 1.72 1.6 1 

Reyn olds Number Correction Factor X, 

Re/) DOD 10 20 30 40 60 Bo 100 140 500 

K, 1.40 1. 261.19 1.14 1.09 1.06 1.04 1.00 1.00 

A5-592

• 

I 


Calculation No.145579-D =CA-056, Rev. 1 

Attachment 5 

Page 26 of 32 

3>uet Design 35.55 

CR6..! Scram (Ony) 

CaYaiuea. i "Wa 

A. 

A (JA, 0.30 035 0.40 OAS 050 065 6.60 0.65 0.90 035 0.80 0.90 1.00 

1 

$GREEN 

02 135.00102.507510S9:0041.25.3LSO 2423 181514.5011. 00 8.00.3.50 0.00 

0.3 69.89 45.56:3,33 R4418.3)14.0010.78 833 6.44 .4,89 3.S6 1.56 0.00 SCREEN 

Q 

44 38.75. 25.63ISJ5 BJ51031 7.88' 6,06 4,69 3.63 2,75 200 0.88 OM HI x W/- Ha xW4 

M 24.50 I6.A012.tO 8.80 6.6D 5.04 3.88 3AO 2.32 116 1.20 0-56.0.00 15n 

0.6 17.1 1139 833 6.11 438 3.50 20 2.08 1.6 1.22 0.89 0.39 D00 

0 

.4. 

12,63 8.31 6.12 4.4 4 259 257 1.98 1.53 1.18 0.900.65 a22 7 ROD 

09 0.69 6.0 6 4,69. 1,44 258 1.97 1.52 u7 0.91.0.69 050 022 0.60 $GREEN 

1 .0 5.06 3.10 2. 

610 4.SU 3.DO 20 

050 

22 1,04 1.56 f 20 093 :0.72 0.54 0.42 0.17 0.00 H I xUrs ^ 0 

1.0 620 > 1.45 1.26 0.97 493 0.32 31 0..14 '0 Q00 104 x5Vp 

12. 4,31 2.85 2.08 653 1.15 9.80 O.d7 OS2 D.40 O.lt 0.22 OJ0 DAO 1 

1.43.15 2.09 1.53 1.12 0.84 0.64 0:49 030'0.30 a22 0.16 OW HO - 

A 

- - 

" 2.42 1.60 1. 17 016 0.64 0.49 0.38 029 023 0.17 0.13 005 0.00 

1,8 1.91 1.27 091 068.051 0.39 030 0.23 018 0,14 0.10 0.04 0,00 n '+OeaaraeraTi9 afaxoe0 

20 1.$5 1.03 0.75 0SS 0-41 02 all 0.19 03 5 0.11 O 05 00t 0.60 

25 0.99 0.66 0.48 0.35 026 020 0.t6 412 0.09 0.07 0.65 092 0.00 

s.ca of tlad 

3.0 0.69 0,46 033 9.24 0. 18 0.14 011 OAS ON 06 0.05 0.04 0,02 0..0 A 1- croft-ses3innaFSVd 

4A 0,39 0,76 0.19 0,14 0.10 0,011 0,06 0,65 0-04 0.03 0.02 1101 0.00 

Mdafi!argwAmp 

smn.rtiaOC4Ma 

6-0 037 OAT OR 0.06 005 004 0.03 OX 0- 02 0.01 001 OM 0.00 

'- 

0264 Obstruclion, St000th Cylhssler hl Rectangular Duct 

H 

dW(Aa < D.3 

where 

ro dv 

R 

3M 

OxIO 

R01500 

0.: 

0:5 

-OO 

300 

0.0 

0.01 

D.61 

063 

DIM 

0.95 

0.10 

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0.08 

0.07 

r,,vnn,m 

S„7A„ 

0110 

an 

0.17 

0.11 

0.16 

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035 

028 

028 

0:26 

0.20 

0.47 

038 

0.38 

0.35 

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-- 

OdI00O 0.00 0.05 

400 0.00 0,04 

500 0.90 0103 

400 0.00 0:02 

1000 D:A)O 002 

c,vbh 

S,0lA, 

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0;04 

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40a 

VD 

400 

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0.00 

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0.09 

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0.41 

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0.05 

02 1 

a.t7 

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0.14 

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$25 

0.25 

0.19 

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0.11 

026 

0.74 

0.37 

034 

0:25 0.1 

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200 

300 

400 

500 

600 

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A5-593 

Day 020 

0.23 0.38 

O,Z> 636 

9,22 030 

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0.11 0.15 

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0.04 J.rfl 

02fi 0.35 

O.zl u.'_8 

0.21 0.38 

0.1 0.26 

0,140 0.19 

0,10 0.€4 

1.07 

0.06 0.09 

1123 0.32 

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219 0.25 

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0.22 

0,12 

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(004 O.i'r'r 

0015

35.56' 

CR9-1 Damper, Butterfly 

Co Values 

RIW 0 10 20 30 40 50 60 65 70 90 

0.12 0.04 0.30 1.10 3.00 8.00 23.00 60.00 100.00 190.00 . 99999 

0.25 0.08 0.33 1.18 3.30 9.00 26.00 70.00 128.00 210.00 99999 

1'.00 0.06 0.33 1.18 3.30 9.00 26.00 70.00 128.0D 210.00 99999 

2.00 .0.13 0.35 1.25 3.60 10.00 29.00 80.00 155.00 230.00 99999. 

CR9-3 Damper, Parallel Blades 

0 

C Values 

y 

LIR 0 10 20 30 40 50 60 70 s0 

6.3 .0.52 0.79 1.49 2.20 4.95 8.73 14.15 32.11 122.06 

0.4 0.52 0.84 1.56 2.25 5.03 9.00 16.00 37.73 156.58 

0.5 0.52 .0.88 1.62 2.35 5.11 9.52 18.88 44.79 187.85 

0.6 0.52 0.92 1.66 2.45 5.20 9.77 21.75 53.78 288.89 

0.8 0.52 0.96 1.69 2.55 5.30 10.03 22.80 65A6 295.22 

1.0 0.52 1.00 1.76 2.66 5.40 10.53 23.84 73.23 361.00 

1.5 0.52 1.08 1.83 2.78 5.44 11.21 27.56 WAI 495.31 

• CR9.4 Damper, Opposed Blades 

E 

C. Values 

LfR 0 10 20 30 40 511 60 70 80 

0.3 0.52 0.79 1.91 3.77 8.55 19.46 70.12 295.21 807.23 

0.4 0.52 0.85 2.07 4.61 10.42 26.73 92.90 346.25 926.34 

0.5 0.52 0.93 2.25 5.44 12.29 33.99 118.91 393.36 1045.44 

0.6 0.52 LDO 2.46 5.99 14.15 41.26 143.69 440.25 1163.09 

0.8 0.52 1.08 266 6.96 18.18 56.47 193.92 520.27 1324.85 

1.0 0.52 1.17 2.91 7.31 20.25 71.68 245.45 576.00 1521.00 

1.5 0.52 1.38 3.16 9.51 27.56 107.41 361.00 717.05 1804.40 

CR9-6 Fire Damper, Curtain Type, Type B 

C„ a 0.19 

A5-594 

2005 ASHRAE Handbook-Fundamentals 

HxW 

SLIP IN FRAME 

l 

a 

A. 

NW CRIMPED 

"^ - 2(H -MLEAFEDGE 

where 

N= number of demand, blades 

W =dud dimension parallel to blade ads, in. 

H=dudba06k Oh. 

L =sum of damper blade lengths, in. 

R = perimeter of dud, in. 

HxW 

SLIP IN FRAME 

0 

Aa 

0 

0 CRIMPED 

LEAF EDGE 

L!R= NW 

2(H ♦ W) 

where 

N = number of damper blades 

W =do, dinners ion parallel to dada ads, in. 

H = dud bdghl, in. 

L sum of damper blade lengths, in. 

R = perimeter of dud, in. 

MOUMING ANGLE(TYR) 

SLEEVE, IA f 

TYPE"B"FIRE 

0 DAMPER (VERT. 

Po OR HORIZ.) 

'S" SLIP 

.FIRE BARRIER

• 

• 

• 

ERM Maw. 90 Degree, Variable In1eUOutlet Arm% 

ExhaustfReturn Systems 

C, Vacua 

1rd 

770. u OA LO . Ii 1.4 1.6 2.0 

US L76 1:13 1.24 Lb1 1.OD 1.06 1.06 

Lot 1.70 1-16 Lis 1 102 0.95 0.90 0,84 

4.00 1,46 L10 0.90 0.8 1 ON 0.72 0. ( 6 

RAW 1.50 1.0.4 0.79 0.0 0.63 0.60 O.SS 

ER4-1 Transition, Rectangular, Two Slit" Parallel, 

Symmetdrnl, ExhansURetarn Systems 

C. Values 

0 

'l, A r 10 IS 20 30 43 60 90 ) 0 150 I" 

0,06 . 0 '6 O t110 0.56 0.71 0 e6 iAYl 09 1) 07d 0.93 

010 0:14 0 1( 0?f 0.53 069 OV 0.9' 091 v).92 0.91 

0.25 0.17 1119 02 2 042 0.60 0.68 0.70 0.69 0.67 0.66 

O.SO OA4 0.13 Mi 0;24 0.35 0.37 0,33 0$7 0.36 0.35 

100 0.00 0-06 0.00 0.00 0.00 0.00 0.00 "0 0.X0 0.00 

2.(J0 0.19 0.20 0.2 1) 0.20 0,24 4.23 4.54 0.13 1.02 1.09 

4,01) o.e1 1).64 0,64 064 ASS 1.12 175 .433 5.65 6.60 

6.00 1.02 IA4 1-44 - 1A4 1.90 >_.ti 6.56 1020 MOO 15.20 

)0.00 5,01 1,60 SAO 5,00 6,50 8.02 19,10 39.10 37.10 43.10 

RPP-24544 RSV id Calculation 346.145579-D-CA-056, Rev. 1 

Attachment 5 

Page 28 of 32 

Duet Des'Ign 35 57 

MU-1 Hedlmonth, Plenum to Round, EAwaWRofurn S ystems 

C. values 

. 

A,IA3 tlAO CAI Dan 0.03 0,04 0.05 0,06 0.08 0.10 6.12 0.16 0010 10.0 1)Q 

13 ( I12 

H„xMJ, 

0,20 0.15 0.14 Ui2 0.10 0,03 0.07 0.05 OM 0.0) 0.01 0,01 

Di 

FAN 

2.0 0.13 0.11 0.03 0.08 0.03 406 0,05 004 0.03 0.02 0.02 0.01 0A1 

23 0.08 0.07 0.05 US 0.04 0.04 0.03 0.02 0.02 UDl - 0A1 OA OAO 

r - 

- . 

3 0 0.06 0.05 0.05 0.03 0,03 0.02 0.02 0.02 0,01 0.01 0.01 0.00 0.00 

10 0.03 0,03 0.02 0.02 0.02 0.01 0.01 0.01 0.01 0.01 000 0.00 0.00 

- 

810 0101 0101 D.OI 010 0.0 0.00 0.00 moo 0A0 O.W 0.00 ant OAO 

F,114,3 'f'ronsilion, Rectm)g9)nr to Ronal, ExhatutiMclurn Systems 

^•µµ•.^• MW^~: C Value, 

A,.A, 10 t5 20 30 is do 91) 129 I5D 

7 

180 

DO6 U_ 1) U.44 fl-ii 0.65 0773 0.83 0," OM 1TV 093 

0.10 OZO 9.50 u.53 0.64 0:75 0.141 0. 119 G.9t 091 033 

Q.1 5 1 15 0.3E 0

• 

35.60 


Calculation No. 145579-D-CA-056; Rev. 1 

Attachment 5 

Page 29 of 32 

2,05 ASIMERandbook-Fundamentau 

W-3 Plain Diffuser (Two Sidea Parallel), FuemscLa[ga 

A,". Rr11D06 : 8 

C, VMea 

0 

10 14 10 30 45 60 90 120 

Ho 

AL 

q 

fl. 

FREE 

DISCHARGE 

1 SO - 0.00 0,00 0A0 0.00. 0,00 0,00 DAM OA8 O.DD 

11 

100 -0.00 0.00. DAD 0.00 O.OD 0.00 0,00 0.00 -0.00 1 W 3 

2D0 0.00 . 0.00 0.00 0.W 0.00 0.00 0.00 0.00 0.0 1)- I+^ -4 

400 D.CO 0.00. "0 0 10D 0.00 0.00 0.00 0.00 0" 

2000 D.W 0.00 0,00 0,00 O.OD 0,00 O:CO 0.00 :0.00 

2 SO O,A A5 1 036 0.63 0.$0 DA LOS. JA9 1.09 

IOD OAS 0.30 066 0.63 0,80 096 L04 1.09 1.09 

2OD 0.44 0.41 DS3 0.63 0.74 0.93 1.02 1.08 IM 

4r731 0.40 0.42 DSO 0.62 0.74 0.93 1.02 1.05 IM 

2000 0,40 0.42 0.50 0.62 0.74 0.93 1.02 1.05 1,03 

- 

4 - 0 0:34 0.35 DAR 0.63 0.76 0.91 1.03 1.07 /_01 

]OD 0,31 036 0.45 0.>3 0,72 0:88 1.02 1A7 1.07 

2DD 0.26 031 OAl 0.53 0.67 0:83 D98 .1.06 IA6 

4100 0.22 0.27 0.39 0.33 0.67 053. 0.96 1.06 L06 

MOO 0,22 4L27 . 039 0.53 0.67 093 0.96 1.06 i-D6 

6 -V 0.12 0.34 0.41 O.S6 030 084 0,% 1.09 LOS 

700 9. 27 030 0.41 0.56 0.70 0.84 OA 1.05 LOS 

200 0.24 0.27 0.36 0$2 0.57 0.91 0,94 1.06 1. 116 

4DD 0.20 023 0.30 032 0.67 0.81 0,94 1.06 1,06 

2900 0.18 0.24 0.34 O.SO 0.67 0.51 0.94 1.05 1..05 -- 

. 

. 

• 4N2-5lyrang003'DJffO,re^ Prcr. Disebmge Y! ._ 

.. _..,_. 

Ce Yallrc4- 1 

xYl4 

FREE ^2 

O ,v^._ gISGHA.RGE 7 , ''[t 

A,1,1, Re/100 8 10 14 20 3D 45 60 90 120 

] soD.OD O.GO 0.0. 07 0. 011 DOD 0.00 O:W O.W a`DD 

too 0.00 oleo 0.00 ON OAO DAIO O.OD O.M. 0.00 

2410 iL00 O.L'0 0.00 000 000 0,00 0:633 C"M 0 40 

400 0.310 D.W O.w (1.01) OA0 000 Ow Oxe 0.00 

2MIO 000 0.0 0.00 DAD DAD 090 0.0:1 O.DI 0.00 

50 0.65 0,65 0.74 0.S2 71.92 LOS ?.l0 L119 1.05 

30il QLI 0,G6 073 D.3( D90 I 'm I 109 I n9 1 108 

200 0.57 0.61 0.70 0.19 LMD LM 1.09 1108 Ms 

400 UO 0.56 0.64 0.76 0.95 1,02 1.07 Los 1.08 

20W 0.50 0 1% a64 0.76 0.88 1:01 1-07 1.09 1.05 

Oislarge rot0jao-JO2 

Lam} 

,_^^ 

Dot 

4 50 0.53 O.w 4.69 0.73 "0 7:02 1.07 1.69 1.09 

IDO 0:43 0.55 0.66 0:7S 0:70 1.02 3.07 LOY 1.09 

2 100 0112 0. 3:1 0.62 0.74 0.57 JXO 1.06 1,08 LtIR 

400 036 0.44 056 VL5 0.84 0,49 1,06 1.0. 

2AW 036 (14 4 0.56 6.10 O.S1 0.99 1.06 1.09 lxS 

6 SO 0.50 0.57 VC, 0:77 0.91 1.02 lA7 1.08 1.0a 

100 0X1 0S1 0.63 0 76 0,95 J.02 1A7 LOS 1:03 

200 0,41 0.49 0.60 0.73 0.48 1.09 1.06 LDS Lf-A 

4*e 1).3= (kJ/ 056 0.7 3 0.84 0.98 ).Or LOS LDS 

2,YJ o34 0.4.4 OS6 0.73 0.96 0.68 1.06 1.68 i.r/5 

t0 YJ 0.45 0.53 0A4 0 14 i1.85 09: I.1D 1, I2 1,12 

103 0.40 (1,45 062 0.73 0.55 0.97 LID 1,12 i11 

7..09 0,34 044 1156 0.69 082 0.95 1.10 1..13 LII 

408 0.28 0,40 055 0,67 0,V 0.93 1,09 1.11 1.11 

_2100 0.25 0.40 12.55 0.67 0.8CI 093 1-09 112 I.31 ....... _ 

tiR* 6 PDrmnuial D1lpntr, xitb RaII^.:, 

1 1b k 113 IU 241 341 0 GO 6O NU 10 (I^1 0 14.0- ^ 

+II r",a 

FR 

{3'9 0 fj OlU 0.1 02 L ri^ I) 0: 0. 1 6^)IS UI4 -3 

i .7- Git{.tCAR 

It 114 I: 11 N 6 b S 

A5-596 

li 

- 1 ^^ 

PL:NI

0 

• 

Duct Design 

SR3-1 Elbow, 991)i'gree, Yari314e1ul0UMUct 

Areas, Supply Air SyV ems 

C, Yalu s 

W 1w, 

113W10.6 U 110 U IA 1.6 2A 

025 0.63 U_92 114 1.64 2.14 2.7i 4.24 

1.00 Obl 0.87 1.15 1.47 1.96 230 3.16 

4.00 O53 11.70 0.90 1.17 1.49 L84 2.64 

WHO 0.54 0.67 0.79 0.99 1.23 L54 2.20 

SR44 Transition, Rectangular, Two Sulu pa"Ifel, 

Syntmcirieal, Supply Air Systems 

C Yalau 

B 

to 15 20 30 15 60 90 120 ISO 190 

0.30 0.03 0.05 0.05 0A5 0.07 0.03 0.19 0.29 0.37 OA3 

0.17 0.05 0A4 6.96 0.44' 0.05 0.01 0.13 0.23 06 0.42 

0.25 OAS 0.04 0,04 0,04 0.06 ON 0.17 0.27 0.35 0.41 

050 0.0( 0.05 0.05 0.05 096 0.07 0.14 0.20 ON 0.27 

1.00 0.00 000 0.00 0.71 0.00 0.08 4.00 0.00 0.74 1.00 

2:00 0.56 042 0.40 0.96 1.4 1.40 152 1.43 1.44 1.40 

SAO 2.72 303 3.52 6.72 9.60 10.38 11.20 11.04 10.72 ]0.56 

10.00 24902f11fJ '34.00 53.00 49.110 82,00 93.00 93.00 92.00 91AM 

16.00 66.56 69.12 MAO W.36 t8t.76 210.16 15600 25144 25053 250.53 

SR4-3 Transition, Round to Rectangular, Supply Air Syslein3 

0 

t,IA, 10 15 20 30 43 60 9O 120 150 130 

0.10 0.0s 205 205 07)T-0.0-7 21FS 0.19 029 0.37 i1,43 

0.17 0.05 003 0:05 0.04 0.06 0.07 0.19 0;13 0.36 0.41 

01.25 094 11.0.5 DJ)S O.W. O.D6 0.137 0.17 0:27 0.35 0.41 

O.SO 0.06 0.07 f.?01 0.05 0.06 0,06 0.12 0,13 0.24 0.2c 

I.M. Q00 0110 O:IYJ O.OJ OXVJ 0.1;0 OXI) IVO fl,frA OAO 

2.00 0.60 UZ 3.0 1„2,0 '132 ?.32 1 12 123 124 1211 

4.00 4.1:0 575 720 N. +2 9,2R 9.92 p124 11).Z= 10424 10.24 

HU30 WC.) 010 510:1 is,0:i 714n 340 "91)7 91.UJ 9L6U a"a 

.p ti0 :0.50 3 .3i6Y iC ii i c2 i25 14 1 -N 250. S 5rv,gcF 219.03 

A5-597 

F 

F 

L 

j{ 

FROM '4 g 11 0 _ "o `' 

PAN 

A,1A 1 4 u >l 

w-4

0 

• 

35.62 2005 A$112AE iândbook-FuRitalnetrtels 

Slt5-3 SMDDtb Aya of TypeA,+.10 3A„ Rr00t490° to 03ain, Diverging 

Cy y.tv 

A,fA, AfA, 0.1 0:2 03 04 

M/QC 

aS 0.6 0.7 0.5 09 

0.50 0,25 

050 

LO 

3,44 

11.00 

60.00 

0.70 030 

237 L06 

13.09 41S 0.10 

0.64 

206 

0.17 0.16 

0.52. 0,47 

096 0-47 

0,16 

0.47 

0,31 

QA? 

0,47 

027 

0.16 

OAS 

0,26 

0.75 0.25 

050 

23 9 

MOO 

0.55 035 

250 0F9 

0.31 

.0:47 

0,33 033 

034-. 033 

036 

0.32 

037: 039 

0.36 0.43 

L00 70,00 16,310 5,67 2,62 1.36 0179 0153 0141 036 

1.00 0.2$ 

0.50 

1.00 

3.44 

1550 

67.00 

0,73 OA2 

3.0 L11 

1375 5.11 

0,33 

062 

2.31 

030 , 031 

OAS 13:12 

1.23 0.31 

C, Vulcea 

0.40 

DAO 

0.59 

0.42 

0.42 

0.47 

0.46 

0.46 

0.46 

A,Me A,IA, 0.1 0.2 03 DA 

M;Q 

OS 0.6 0.7 OS 09 

O.SD 0.25 3.75 1.62 0.50 0.17 0.05 O.00 -0.02 -DAL' 0.00 

075 

0.50 

1. 00 

025 

7,50 

5,00 

19-13 

1.12 0,7.5 0A6 

0.62 0.17 0.06 

3.38 S1 0,28 

0,05 0,09 

0.08 0.09 

11.OS -0.112 

0.14 

0.12 

-0.02 

0.19 

0,15 

O.W 

0.23 

0.19 

0.06 

0.50 

LOU 

'20.61 

16.33 

3;23 075 

2.81 0.63 

O,t4 

0.31 

-OA2 -005 -0:0.5 -0.02 

-0.02 -O:DS 0.01 t'Lt* 

0.07 

0.07 

1,00 0.25 46.1;9 9.50 332 1.31 0.52 0.14 -0,02 -1105 -0.01 

0,50 

3.00 

35.0P 

33:00 

6.75 

7.50 

2.11 

2.44 

075 

0.81 

O.Z4 "0 -010 -0.09 -0.04 

0711 -003 -0.1A -0.06 -0.02 

SRS: Wye of (he'CypoAa +,gy^ rl^, A_r^rJ„i5lltgrtt, Diverging 

C, Voices ..-1,^ 

O.1 02 013 0.4 

2>+Q: 

05 0.6 0.7 06 0.9 

0,1 

0.2 

OS 

DA 

C.5 

DAA 

L24 

5.94 

1036 

17,75 

0.52 

0.56 

LO3 

1.38 

'3.25 

D.57 

0.94 

0.5 2 

Dill 

3,14 

0.58 

0.45 

0.4. 1 

0.41 

0.5 

0.64 

0.51 

0:14 

6.33 

4:57 

054 

DA6 

031 

0.70 

0.59 

0.49 

0.31 

PM 

0.50 

052 

032 

0.73 

0.62 

0f4 

Dad 

0 0.6 26.66 5,04 1,76 0;83 

0.40 

0.50 

0.31 

236 

0-%0 

0.32 

030 

0. 11 0 

0:11 

030 

0-'. 37.73 7.27, 156 1.16 0.67 DA4 0.35 031 03 D 

08 49.92 192 3:99 MO 0.87 0.55 41.42 0335 '032 

QfQ, 

C, 

O ' s 

32 (A 

IL? 03 OA 05 

6,50 2,22 087 0.40 

0.6 

0,17 

SRS-S Tee of the Type A, +A, >A,,A,=A, Divo-ling 

Co Valcn 

os 

0.03 

4aA 01 Pt 03 04 Ifs 0.6 0. 1 0,8 09 

0I 1 (05 0 OS'J 057 axe OST 0$7 0 %1 0-S6 

0 516 1 Y 3 1 3 099 096 IM 04.1 5}89 

0.3 t E1. 126 16 1.1 3 1' F ! 2 I7 10.5 II I 0 97 0.94 

(1.4 

(15 

Ob 

0 

16.3: 1 

14.25 

56 

4&5 ^: 

4.36 2.24 I:8 

C,31 03 1 91) 

0 - (I! 241 

1' .! J 1,1 

1. 11 

1 15 

464 

tin, 

0.38 

3.03 

2 

t4 

0.90 

O)+ 

1 

H 

0.7S 

11$4 

(ISW 

106 

0- 72 

13: i 

081 

1:t,f, 

0.n ISt3 P 1 72 6.,:6 '. t. 24 : f.". 1. '11 1.20 I A17 

Q1? U.1 I 03 U7 D 06 98 LO 

( Ale $0 _- Ov ) L•t. i i`.. (kW 

1.0 

0.04 

A5-598 

ae 

r Ac 

n4Vo = 3A 

rè=^z 1c 

A< - a, 

qy.p 

N -^^.^ ^ A tH ^. 

c,,

• 

• 

• 

RPP-24544 REV Id Calculation No. 145579-D-CA-056, Rev. I 

Attaclunent 5 

Page 32 of 32 

Tel: ASHRAE DUCT FITTING DATARASE 

Fwa VersWA2.5.0 Thuftdoy, Februmy2k 20OW 

INPUTS- 

ICRW) Orifice, Thick-Edged 

(Idelrhik 1956, Diagram 445) 

OUTPUTS 

Height (Ho, in.) 5.3 Velocity (Vo, fpm) 2054 

-Wf-dth (Wo, In.) 5.3 Val Pres atVo (Pv. in, %vg) 0.26 

Height IHI in.) 49 Loss Coefficient (Co) 0.27 

Width (W - 1. in.) 4.9 Pressure Loss (in. wg) 0.07 

Lengtb (L, In.) 24.0 

Flow Rate (O, cfm) 400 

L;/Di: > 0.015 

D h = 2A I / ( H 1 -1 

A5-599

• ûauavav r .. 

Task/Project 8: Demonstration Bulk Vitrification 

,System A77977 

CaldulationNumber.' - Revision SaletyRelated? 

_ 145579-D-CA-058 p f Jea+ Y-SS 

:Reviewer/Checker(pdntname): K.J.McCacken. 

Reviewer pedonned or supeMsed subject calculat ion. 

_ __X—NO _YES Justification Attachment_– ,_pages 

A lternate Vedficatkm method app roved WA Method Calculation Independently Checked_ 

Date 

03127/06 

ITEM(S)CHECKED ACCEPT OBJECT IVE. EVIDENCE INITIAUDATE 

.YIN SHEETS 

1. Cover forms prc Perl y completed. P Y P9 1-12 

2. Calculation Sheet headers complete with calc. no., rev., etc. Y Pg 1 -12 0 ^^^ 6 

3. Calculation Sheet contents complete per format. Y Pg 1.12 

E 

4. Listed attachments included. Y Pg 1 >>J 

5. Calculation Objective clearly described. Y Pg 3 Section 1.1 and 

1.2 

6. Criteria are suitable and properly referenced to task-specific documents. N/A Calculation 

determines head loss 

i7. Assumptions and data described and attached or referenced to task 

documents. 

Y 

and thermal effects— â 3Jo 

no criteria necessa ry 

8. Calculation method identified and appropriate for the design 9 activity. tY Y P9 8 Section 4.0 

9. Calculation results reasonable and co rrectly described in Results & Y Pg 9-10 Section 5.0 

Conclusions. 

10. Computer Program identified with version and revision. Y Pg 8 Section 4.0 last 

Pg 5 Section 2.2 and 

A tt 

achments 4 & 5 77f 6 

Paragraph 

jo 3^ 

11. Computer Program references method used, etc. Y Pg 8 Section 4.0 2 rrd 

Paragraph m g)a3 

12. Computer inputloutput provided. Y A tt 

achment 2 s 

13. Computer runs traceable to calculation. Y Section 6.0 3J^^ 

14. Computer input data within permissible design input range. Y Attachment 2^ 

15. Computer Program validationlverification addressed. Y Pg 9 Section 4.0 last 

REMARKS 

None 

K. J. McCracken =2^r`t" S 

Reviewer/Checker P ri 

nt Nam" nature 

Data 3^^7^C C 

J. J. Irwin Date 3 a7 

• Origin int Name &Sign e 

EP 3.9-4F October 2003 

A5-600 

_ 

G,

2. Spreadsheet Owner, Organization, MSIN, & Phone No.: John J. Irwin, 375-7866 

1, SVF 1129 Rev. 0 

la. No. Pages: 2 

3. Spreadsheet File Name and Version No.: M:\DemonstrationBulk VfllFiscal Year 2006 Work\Calculations\OGTS Bypass 

Thermal Hydraulics Analysis\Work Files\Bypass Duct Elements 8 inch.xls 3/24/06 

4. Function and Purpose of Spreadsheet: Calculate Thermal Hydraulic K-Losses and Heat Transfer Coef fiecents for DBVS OGTS 

Bypass . System 

S. Spreadsheet Category: [ Critical Spreadsheet' Q Non-Critical Spreadsheet [] Multiple-Use Spreadsheet 

6. Associated Document(s): Calculation 145579-D-CA-056 6a. Attachments: NA 

7. Scope of Ve rification: 0 Input Data 0 Formulas Changes Only Macros/Add-ins Other 

8. Scope Desc ri ption: Scope of verification was limited to 15% of the input fields to the calculation and the Exte rnal Convection 

and Thermal Radiation Coefficents 

9. Verification Checklist: Yes No NA 

a. All unique formulas in spreadsheet have been checked that they correctly pe rform their intended func tion. 0 0 11 

b. Non-unique formulas have been reviewed to confirm that they have been correctly copied. 0 0 q 

G. All values are cor rectly labeled with units. 0 0 0 

d. Formulas were checked for dimensional consistency. 0 11 11 

e. Spreadsheet contains no hidden pages or formulastdata on hidden ranges/pages have been verified. [a El q 

f. Links to exte rn al workbooks have been verified. 11 q 0 

g. Input data used in the sp readsheet are appropriate and have been checked against their original source. 

El 11 0 

h. Spreadsheet has been reviewed for common errors. See TFC-ENG-DESIGN-C-32, A ttachment C for guidan ce . Q 11 11 

I. Assumptions in the spreadsheet are reasonable and supportable. El 0 0 

j. Macros contained in the spreadsheet have been veri fi 

ed for correct opera ti 

on. 11 0 

Q 

k. Add-in software is commercially available software, suitable for its intended purpose, and is a production version of the 0 

software (e.g. not be a'beta" or lest version). 

1, Spreadsheet contains a documentation sheet with spreadsheet purpose, methodology, assumptions, and reference to 

current SVF No. 

M. A change log is included for multiple-use or revised single-use spreadsheets and all changes in the log have been verified. Q 

n. If the spreadsheet is a critical spreadsheet, a published spreadsheet description document has been produced that 0 q Q 

provides a description of the spreadsheet purpose, assumptions, methodology. 

o. Spreadsheet has been protected against inadvertent change per TFC-ENG-DESIGN-C-32, Section 4.6.3. Q q 0 

p. All errors identi fi ed du ring verifi ca tion have been corrected and the spreadsheet is suitable for its intended purpose. q^ 11 q 

10. Comments: (Explanation for any Items marked "No" must be provided) 

See a ttached pages for verifcation evidence (32 pages attached) 

11. Approvals/Clearance: Printed Name: Si to : Dale: Release Stamp 

Spreadsheet Owner: John J. Irwin 

Spreadsheet Ve rifier: Ku rt J. McCracken 3 1^)d7^ 

Owner's Manager: Ja-Kael Luey 3`2 v4 

LCCB Approval (if required): 

Clearance Review: 

When completed, submit the original hard copy signed SVF form together with a protected electronic copy of the spreadsheet (in'.xls or *At format) to 

the Document Control Service Center for records retention and release. See Form Instructions for how to transmit spreadsheet electronic file. 

Page 1 A-6003-781 (01/06) 

A5-601

• 


CH2M HILL SPREADSHEET VERIFICATION AND RELEASE FORM 

Cleared for Public Release? q Yes []No Restricted Use. q yes 5No Restriction Type: 

1. SVF 1129 Rev. 0 

1a. No.Pages: 2 

0 When completed, submit the original hard copy signed SVF form together with a protected electronic copy of the spreadsheet (in '.xis or'.xll format) to 

the Document Control Service Center for records retention and release. See Form Instructions for how to transmit spreadsheet electronic file. 

Page 2 A-6003-781 (01/06) 

A5-602

DMJM H&N A3Ivi 

Calculation No 145579-D-CA-0564 ^ r { Sô-- 

CA 056 

: 0 

Rev. No. 

RPP-24544 REV I d 

ORIGINATOR: John Irwin 

200602 22 200 o^ 

Calculation Title: DBVS OGTS Bypass System CHECKER: Jack McConwell 


6.0 Calculations and Analyses 

Project Number: 1455791,15579 

Page 13 of 13 4-2 

The APT Arrow model, as shown in the figure, considers the process loop as follows: 

N p 

Aim P— 

r^^ 

ACn Rm 

nl 

Fr-J] 

l.i 

Î 11 Am. P— 

I"'^^ 

II I 

L^^ 

02-22- 

P , 

P11 11J 

rz 

8 waw s r;o 

v MPA r1.lw 

J2 

rl MEPA10, 

P22 

s 

VSJ PI9 

b JiC JIS IIF'PA )d'n 111 

N N Is ;CV Plerwln n Je J? W901 ill JI{ V-156 'W", N,M 

Vt 9 1- FS PS P, P) 

C^ P9 

v-ln 

PÌC PI) FT4 PIS Pty P" 

-. ^' Ple 

i9 1 Jls I Jie 

f J,: P—d' 

,NI LIV.902I (lempw 

T. W- AI 

Fol B klfÂ 

NnRi.V 

^^ J J]I V 

L, (, NFP^ ll1r I. 

IIn no>o,P 

^J 

PV `1 

P3, 

en P.., 

7(F^ ro))wns 

_ P1, 'y.(r 

19 

v-ro, 

L'^ 

♦YnPâ 

$ J I,e v 'sl rj 

JV6 via 4 

J, 

'9' ){ a 

KV P,Prum ^^ ! 

P] [^}{{ H 

.._.^.. ,...^.3 

NV-90, 

P9 -- PIO [^,.^^^{^^l ^^^ 

111 

P4 

,^k1^""V.V^4 

PIy 

'P).^RP 

s15 ) 

co^ 

,.,]0 

CO3 

P. 

Jr 

L C JII 

JpIry voi I 

b.aaab 

IJ.mPr 

OGIS of Pn 

r^ The drawings used to develop the AFT physical mode! are contained in Attachment 1. 

TIZe AFT Arrow Input and Output Files for the various cases analyzed are in 

Attachment 2. Attachment 3 contains the flow coefficient and physical configuration 

Form EP 3.3-2F, April 2005 

A5-603 

e MF.P

110-.. 

A,*,- 

RPP-24544 REV 1 d 


Attachment 2 

Page 9 of 9 

AFT narrow 3. (1 of 6) 2/17/2006 12:42 PM 

DhUPAH +N 

AFT Ar rove Model, OGTS Bypass System T-HI, W-1 

Title: AFT Arrow Model, OGTS Bypass System T-H Model Case 2 

Input File_ C1AFT Products%FT Arro.-ABypass Flow 8 inch Pipe Re y B.aro 

Number Of Pipes= 25 

Number Of Junctions = 25 

Length March Solution Method with Mach Number Limits 

Length Step Size = 12 inches 

Mach Number Increment = 0.01 

Pressure Tolerance= 0-0001 relative change 

Mass Flovi Rate Tolerance = 0.0001 relative change 

Enthalpy Tolerance = 0.0001 relative change 

Flow Relaxation= (Automatic) 

Pressure Relaxation = (Automa ti c) 

Resistance Relaxation = (Automatic) 

Fluid Database: AFT Standard 

Fluid: Air 

Max Fluid Temperature Data = 1000 deg. K 

Min Fluid Temperature Data = 200 deg. K 

Molecular lrleight =28.97 amu 

Gas Constant =0 06855 6tti:1bm-R 

Critical Pressure =37.25 atm 

Critical Temperature =132.41 deg. K 

Acentric Factor =0.021 

Equation of :hate= Redlich-K:vong 

Enthalpy Model = Generalized 

Specific Heat Ratio Accuracy = High 

Atmospheric Pressure = 14.5 psia 

Gravitational Acceleration= 1 g 

Standard Pressure = 14.696 psia 

Standard Temperature = 60 deg F 

Turbulent Flow Above Reynolds Number= 4000 

Laminar Flow Below Reynolds Nuniber = 2300 

[lino 1-1 Tohin 

Pipe Name Pipe Length Length Hydraulic Hydraulic Friction Roughness Roughness Losses (K) Initial Flow 

Defined 

Units _ Diameter Diam. Units Data Set 

Units 

I Pie Yes 64 inches 6.065 v inches Unspecified 0.00015 feet 2.9 

2 Pipe Yes 104 inches 6.065 inches Unspecified 0.000 1 _5 feet 

3 Pie Yes 163 inches 4.026 inches Unspecified 000015 feet 

3 FEs Yes 62 inches 6.065 inches Unspecified, 0.00015 feet 

5 Pie Yes 22 inches 4.025 inches Unspecified 000015 feet 

6 Pi _ Yes 72 inches 6.065 inches Unspecified 0.00015 feet .1 

Pie Yes 141.5 inches 5.047 inches Unspecified 0.00015 feet WA46 

8 Pie Yes 6 inches 6 065 inches Unspecified 0.00015 feel' 

9 Pi,e Yes 10.5 inches 6.065 mrhes Uns ecified O.00D15 feet 

10 Pie Yes 8 inches 6.065 inches Unspecified 0.00015 feet 

11 Pie Yes 6 inches 6.065 inches Uns ecified 0.000'15 feet Am 

12 Pie Yes 12 inches 6.065 inches Unspecified 0 00015 feet 309545 

13 Pie Yes 2 inches 8.329 inches Unspecified 0.00015 _ ___feet ^'•9 

14 Pie Yes 1969 inches 8.329 inches Unspecified 000015 feet ^1 •" 

15 Pie Yes : 27Zt ` inches 8.329 inches Uns ecified 0.000 15 feet 1 1 ' C^ 

16 Pie _ Yes 18 inches 8.329 inches Unspecified 0.00015 feet 

17 Pipe Yes 12 inches 8.329 inches _Unspecified 0.00015 feet r0k1 s1'RStr 

16 _Pie Yes 42 inches 8. 329 inches Unspecified 0.00015 feet U`11` 

19 Pie Yes 12 inches 8.329 inches Unspecified _ 0.00015 feet 0 

20 Pie Yes 564 inches 8.329 inches Uns ecified 0.000 1 6 feet t- ':'2.14= 

2 1 Pie Yes _9.04 inches 12.35 inches Unsecihed 0.00015 feet ?. 48 i , z f 

22 Pi Yes G inches 6. 065 inches Uns ecified D 000 11 5 feet S 04- 

23 Pi e Yes 268 inches 6065 inches Uns ecified 0.00015 feet 0-11 ^?• ! 

30 Pipe Yes 05 feet 5 047_ inches Unspecified 0.000'15 feet 01 

iS

W 

RPP-24544 REV I 


Attachment 2 

Page 10 of 50 

AFT Arrow 3.0 Input (2 of 6) 2/17/2006 12:42 PM 

DMJ1r1H+N 

AFT Arrow Model, OGTS Bypass System T-H Model Case 2 

Pipe NamePipe Length Length Hydraulic Hydraulic F riction Roughness Roughness Losses (K) Initial Flrnf 

Defined Units Diameter 1 Diam Units Data Set Units 

31 1 Pipe I Yes 0.5 feet 8.329 inches Unspecified aGOO151 feet 0 

Pipe Initial Flour Junctions Geomelry Material Size Type Thermal Ambient Temp. 

Units U ,Down) 

Boundary 

1 1,2 C3dindrical Pie Stainless Steel 6 inch _ schedule 40 Adiabatic 

2 2 3 C lind rical Pie Stainless Steel 6 inch schedule 40 Adiabatic 

3 3,41 Cylind rical Pie Stainless Steel 4 inch schedule 40 Adiaba tic 

4 5 Cylindric.)] Pie _ Stainless Steel 6 inch schedule 40 Adiabatic 

5 5.6 C lind rical Pie Unspecified Adiabatic 

6 6.7 Cylindrical Pie Stainless Steel 6 inch schedule 40 General Heat Transfer 115 

". 7, 8: Cylindrical Pie Stainless Steel 5 inch schedule 40 General Heat Transfer 115 

8 Y 8 91 C lind rical Pie Stainless Steel 6 inch _schedule 40 General Heat Transfer 115 

9 10 Cylindrical Pie Stainless Steel 6 inch schedule 40 General Heat Transfer 115 

10 , 11 Cylindrical Pi Stainless Steel 6 inch schedule 40 General Heat Transfer 115 

11 12 C indrical Pie _ Stainless Steel 6 inch schedule 40 General Heal Transfer 115 

12 r_12, 11 C lindrical Pie _ Stainless Steel 6inch schedule 40 General Heat Transfer 115 

13 13 Cylindrical Pie Stainless Steel 8 inch schedule 10 General Heat Transfer 115 

14 , 14 Cylind rical Pie Stainless Steel 8 inch schedule 10 General Heat Transfer 115 

14 15 Cylindrical P ipe Stainless Steel 'fit}# General Heat Transfer 115 

16 15 161 Cylindrical Pie Stainless Steel 8 inch schedute 10 (_general Heat Transfer 115 

17 16, 17 1 Cylindrical Pipe Stainless Steel 8 inch schedule 10 General Heat Transfer 115 

18 17 18 r Cylindrical Pie Stainless Steel 8 inch schedule 10 General H eat Transfer 115 

19 18 19 C^ lindrical Pie Stainless Steel 8 inch schedule 10 General Heat Transfer 115 

20 19, 20 C ind rical Pie SLunless Steel 8 inch schedule 10 General Heat Transfer 115 

21 21,22 C lindrical Pi a Stainless Steel 12 inch _schedule 10 Adiabatic 

22_ 22 23 Cyl indrical Pipe Stainless Steel 6 inch schedule 40 Adiabatic 

23 23 13 C lind rical Pie Stainless Steel 6 inch schedule 40 Adiabatic 

30 _ 8, 30 C linoncal Pie Stainless Steel 5 inch schedule 40 Adiaba tic 

31 

14 31 , Cylindrical Pie Stainless Steel 8 inch schedule 10 Adiabatic 

A5-6O5

AFT Arrow 3 

DMJMH +N 

sr, 

RPP-24544 REV 1 d 

(3 of 6) 

AFT Arrow Model, OGTS Bypass System T-H 


Attachment 2 

Page 23 of 50 

Pipe K Total Standard Mitre Smooth Angle Ball Butterfly Cylinder Gate Globe Plug Poppet 

Losses Bends Bends Bends Valves Valves Valves Valves Valves Valves Valves Valves 

12 1.31 1(0.21) 

13 (I 

15 1.1 

21 3.48 

22 1 

23 1 0.11 

Pipe Three-way Swing Check Lift Check 

Losses 

12 

13 

15 

Valves Valves Valves 

21 

22 

23 

-- 

Tilting Disc 

Check Valves 

Stop Check 

Valves 

Sharp-edged 

Orifice 

Pipe Entrances Exits Differential Honeycomb Screen Tee Add'I Loss 

Losses Flowmeter 

L12 

1 0.04 

0 1'I 

Long 

Orifice 

2/17/2005 12:46 Pt41 I 

Contractions Expansions 

Area Change . Name Object Elevation Elevation Initial Pressure Initial Pressure Database Type Geometry 

Defined 

Units 

Units Source_ 

3 Area Change Yes 0 feet Conical Contraction 

0392 

Area Chancio 

Area Change 

Yes _ 

Yes 

0 

0 

feet 

feet 

"Conki 

Coni 

E iio 

tttrA - 

Area Change Yes D feet (onicati •'-t)ntrBG 

Area Change Angle Loss 

Factor 

3 21 0.439151 

2Z —0-4WID4 

MY ... ; Po 28. 0.1241176 

CompressorlFan Name Object 

Defined 

17 N31-130 Yes 

Elevation Elevation Initial Pressure Initial Pressure Database Special 

_ Units 

I Units Source Condition 

0 feet None 

Compressor/Fan Pump Design Flow, Des+g17 Flow ' Cunent Independent Ind. Variable Dependent 

Type 

Rate Rate Units Conti uration :unable Units Vanable 

17 Com ./Fan Curve Vol. Fbw Rate 113?min Pressure Loss 

Compressor/f an Dep Variable Contp /Fan Curve Comp.lFan Curve ComplFan Curve Compffan Curve CompiF3n Curve 

_Units Constant a Constant b Constant c Constant it e 

17 in. H2O std. 1 12.46429 2 171429E-03 -2.285714E-05 0 

A5-606

.*I— 



Attachment 2 

Page 25 of 50 

AFT Arrow 3 0 Input (5016) 2117:2006 12 -46 PM 

DMJMH+N 

AFT Arrovr :model. OGTS Bypass System T-H Model Case 4 

Tank (Pipe 47) (Pipe #8) (Pipe k9) (Pipe N10) (Pipe #11) (Pipe #12) (Pipe #13) (Pipe f1 14) (Pipe 4'15) 

K In K Out K In. K Out K In K Out K In. K Out K In, _K Out K In K Out K In K Out K In K Out K In K Out 

1 

20 

21 

Tank (Pipe #16) (Pipe #17) (Pipe # 18) (Pipe #19) (Pipe #20) (Pipe 421) (Pipe #22) (Pipe #23) (Pipe 424) 

K In K Out K In, K Oui K In K Out K In K Out K In K Out K In K Out K In K Out K In K Out 

— 

K In K Out 

20 

21 — 

Tank (Pipe 425) 

K In. K Out 

1 

20 

Tee or Wye Table 

Tee or Wye Name Object Elevation Elevation initial Pressure Initial Pressure Database TeelVllye Loss 

Defined Units Source -. Type Type 

a. :.Tee or W Yes 0 Round., 

9 Tee or ' a Yes _ _ _ 0 Y^ feet Round Strai h1 Detailed 

11 Tee or Wye Yes) 0 _ feet Round Straiight Detailed 

13 Tee or Wye, Yes 0 feel Round Straight . Detailed 

Tee or Yes 0 feet ".:. liîlyd5 ht ' Distat 

Tee or Wye Angle Pipes 

MAN 

.; 

9 120 

11 30 

13 45 

"d tit 

A_ B. C 

Valve Table 

Valve Name Object Elevation Elevation Ini tial Pressure Ini tial Pressure Database Special Exit Exit 

Defined Units Units Source Condition Valve Pressure 

10 HV-901 Yes 0 feel Closed No 

12 

15-: 

HV-902 

-V 

Yes 

V4 

SIt ' 

0 

0 

feet 

feet 

`^' 

Closed 

None 

No 

No r,g' . ? 

19 V-167 Yes 0 feet 

_ _ _ None No 

23 V-178 Yes 01 feet 

None No 

Valve Exit CdA CdA Loss Loss Independent Ind. Variable Dependent Dep. Variable Loss 

Pressure Units Units Model Value Variable Units Variable Units Constant a 

1 0 

Cv Constant 1 194 

12 Cv Constant 1194 

f Cv Constant 

19 — — — _ 

^ Cv Constant 2440 

- 

23 

Cy Constant 300 

Valve Loss Loss Loss Loss 

10 

12 

f5> 

'19 

23 

Constant b Constant c Constant d Constant e 

— 

— 

A5-607

Vi 

0 

00 

3 

P2 Outlet Transition Flanders, Sudden 

Contraction, 24 x 6 

OGTS Bypass System Fluid Flow Model 

12.0 

SQ/6.357 

Rnd 

ED1-1 0.500 

" Piping, 6-AA-35-0218 6" straight duct, S.Stl 6 40S 6.065 42.000 CD11-1 ARROW 

" Elbow No. 1 90° Elbow, WD = 

6 40S 6.065 CD3-1 0.130 

_ 1.5, S.Stl _ 

Piping, 6-AA-35-0218 6" straight duct,S.Stl 6 40S 6.065 62.000 CD11-1 ARROW 

FP2 Elbow No. 2 45° Elbow, WD = 

1.5, S.Stl 

6 40S 6.065 CD3-3 0.080 

Total 104.000 inches 

8.667 ft 


Fitting 

No 

(in) 

(in) (in) 

^ J3 — Reducer 6" x 4" 

6 x 4 40S 6.065/4.025" 

ASHRAE 

Loss 

Coef. 

5.500 ED4-1 0.220 

P3 Piping, 4-AA-35-0218 4" straight duct, S.Stl 4 40S 4.025 163.000 CD11-1 ARROW 

3 

7 

Flowmeter 3 ea Size 1 Annubar 

llowmeter 

4 Vendor 1.635 


13.583 ft 

J4 'Reducer 6" x 4" 4 x 6 40S 4.025/6.065" 5.500 ED4-1F. 

6IV IF ml 

1'y 

OGTS Bypass System Fluid Flow Model Input Data, Piping./Component Descriptions and Flow Loss Coefficients. 

2l^.-TJ 

40W 

Cv 

l 

7 

10 

IV 

N 

A 

Â. 

tr1 

1 

a

3 

lh 

all 0 

^t 

OGTS Bypass System Fluid Flow Model Input Data, Piping/Component Descriptions and Flow boss Coef ficients, 

P4 Elbow No. 3 45° Elbow, RID = 

1.5, S.Stl 

OGTS Bypass System Fluid flow Model 

6 40S 6.065 CD3-3 0.080 

" Piping, 6-AA-35-0218 6"- straight duct, S.Stl 6 40S 6.065 12.000 CD11-1 ARROW 

Elbow No. 4 Q Elbow, R/D = 

6 40S 6.065 GDS 0.080 

1.5, S.Stl 

+ 

" Piping, 6-AA-3 5-0218 

_ 

Elbow No. 5 7 

6" straight duct, S.Stl 

.9d' Elbow, R ,D = 

6 

6 

40S 

40S 

6.065 

6.065 

12.000 CD11-1 

CD3-3 

ARROW 

0.080 

y$ 1.5, S.Stl 

P4 Piping, 6-AA-35-021 8 6" straight duct, S.Stl 6 40S 6.065 38.000 CD11-1 ARROW 


5.167 ft 

.15 Reducer 6" x 4" 6 x 4 40S 6.065/4.025" 5.500 ED4-1 

P5 Expansion Joint, EJ-501 4" 4 4.025 22.000 CR6-3 

(ICV Box CP) 

B I ICV Box Plenum, Stream 

No. 9 in, 13 out 

J6 ICV Box plenum CPs 

inlet/outlet) 

C ICV Outlet to Bypass Tie 

Point, Stream No. 13 

280 acfm at -2.46" 

w.g. and 875 °F, 108 

scfm or 513 lb/hr 

(0.143 lb/sec 

Inlet and Outlet 

Losses 

280 acfm at -2.46" 

w.g, and 875 °F, 108 

scfm or 513 lb/hr 


Fi tting 

No 

Crane 1.500 

ASHRAE 

Loss 

Coef. 

Cv 

t+^ 

4 

G.^ Y 

b 

lv 

C 

n..

D 

v, 

0 

1 .` 


(ICV Box CP) 

P6 Piping, 6-VOG-35-0217 6" Duct w 90° Elbow, 

Inte rn al to AWTE 



6 40S 6.065 72.00 CD11-1 ARROW 

P6 Elbow 90° Elbow, R/D = 1.5 5 40S 5.295 CD3-1 

J7 Reducer 6" x 5" 6 x 5 40S! { 6.065/5.782" 10.250 ED4-1 D-aif1'" ' 

P7 Expansion Joint, EJ-502 DME 5" size 5 4.9 24.000 CR6-3 

" Piping, 5-VOG-35-0217 5" Duct 5 40S 5.295 24.000 CD11-1 ARROW 

" Elbow 45° Elbow, RJD = 1. 5 5 40S 5.295 CD3-3 0.090 

" Piping, 5-VOG-35-0217 5" Duct 5 40S 5.295 93.500 CD11-1 ARROW"° ` 


J8 Lateral Wye (For Bypass 

Flow) 

D OGTS Bypass Main 

Ducting from Tie Point to 

HEPA inlet, Stream No. 

45° Lateral Branch 

Flow, Main Flow 

osed 

280 ac - a .46" 

w.g. an 75 °F, 108 

Sc r 51 lb/hr 


11.792 ft 

5 x 5 x 5 40S 5.295 10.000 ED5-2 0.040 

JS 

13 

Lateral Wye (For Bypass 

Flow) 


P8 Reducer Standard Reducer. 

5x6", 11 

6 x 5 40S 5.295/6.065 6.000 ED4-1 0.050 

-7c' — 4= Z 

Bmr++^2 SQ,^ 

v, 

C

a 



Direction 

30° Lateral Wye, 

Main Flow 


6 x 6 x 6 40S 6.065 6.000 ED5-2 0.290 


Fitting Loss 

No Coef. 




362-173, Key-Lok 

6 5.8125 2.250 1194 

P10 Elbow 90° Elbow, R/D = 

1.5, S.Stl 

6 40S 6.065 CD3-1 0.050 

P 00 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 8.000 CDl l-1 ARROW 

J11 Lateral Wye Reverse 

Direction 

300 Lateral Wye, 

Main Flow 

6 x 6 x 6 40S 6.065 6.000 ED5-2 0.110 

Component Details Size Schedule Inside Dia. L ASHRAE ASHRAE 

Fitting Loss 

No Coef. 


J9 

Pl l 

Lateral Wye, Forward 

Direction 

Piping, 6-VOG-36-0286 

30° Lateral Wye, 

Branch Flow 

6" straight duct, S. 

6 x 6 x 6 40S 6.065 6.000 ED5-2 0.610 

Sri 

6 40S 6.065 6.000 CDl l-1 ARROW 

I'll Elbow 300 Elbow, R/D = 

6 105 6.065 CD3-1 0.050 

1.5, S.Stl 


362-173, Key-Lok 

6 5.8125 2.250 1194 

P12 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CDl 1-1 ARROW 

Cv 

b 

N 

A 

C 

a

Y, 

N 

0 V 0 LJ 


P12 Std Tee 6" Std Tee, Branch 


flow 

P12 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CDll-1 ARROW 


1.5, S.Stl 

J11 Lateral Wye Reverse 30 0 Lateral Wye, 

Direction 

Branch Flow 

6 40S 6.065 CD3-1 0.050 

6 x 6 x 6 40S 6.065 6.000 ED5-2 0.240 

P13 Piping, 6-VOG-36-0286 6" straight duct, S.Stl 6 40S 6.065 6.000 CDl 1 -1 ARROW 

P13 Reducer 6 x 8 Std Reducer, 

19° 

P13 Elbow #1 90° Elbow, R/D = 

1.5, S.Stl 

6x8 40S 6.065/8.329 ED4-1 0.170 

8 los 8.329 CD3-1 0.110 

P13 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 114.000 CD 11 -1 ARROW 

P13 EJ -&3;!^r 8" Expansion joint 8 10S 7.900 11.000 CR6-3 0.110 

P13 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 lOS 8.329 120.000 CD11-1 ARROW 


20.917 ft 


Direction 

45 0 Lateral Trough 

Flow (Air Inlet Bleed 

System@ Branch 

flow 

8 los 8.329 10.000 E135-2 0.290 

P14 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 l05 8.329 138.000 CD11-1 ARROW 

" Elbow #1 90° Elbow, RID = 

1.5, S.Stl 

8 l05 8.329 C133-1 0.110 

" Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 l05 8.329 15.000 CDl l-1 ARROW 

" Expansion Joint, EJ-635 + 

5 others 

8" Expansionjoint 8 7.900 11.000 CR6-3 0.660 

û N 

a 

MLA 

C^] 

C

io. tj 

chi, 

I 


j UCCTS Bypass System Fluid', w 1V> e ^ ^ '^ 


Total 1969.000 inchesa: 

J14 45° Lateral a o 

i 

164.083 ft 

I 8 x 8 x 8 los 8.329 ED5-2 .. 

P15 Piping, 8-VOG-36-0286 8" straight duct, S.Stl 8 10S 8.329 CD11-1 

" Elbow #2 90° Elbow, R%D = 

8 los 8.329 CD3-1 

" Piping, 8-VOG 36-0286 

1.5, S.Stl 

8" straight duct, S.Stl 8 lOS 8.329 CD11-1 ARROW 

StdTe^ ;514-Tee,'Br^ch 

main fl ow- dead 

8 x 8 x 8 10S 8.329 ARROW 

Piping, 8-VOG-36-0286 8" straight duct, S,StI 8 10S 8.329 - 'tkLO& CD11-1 ARROW 

P15 „ p TZSinitlbint, EJ- 15, 8” Exp ansion joint 8 7.900 11.000 CR6-3 

(HEPA Inlet) o# inches 

23.125 ft 

E OGTS Bypass HEPA 

Filter Skid 

HEPA Filter skid 

Assembly, 36-D58-138 


Fitting 

No 

1 15^. Isolation Valve, 3b-V-1 .$" a}'stg FIG. 

=173, y 


8 7.625 2.500 

ASHRAE 

Loss 

Coef. 

Cv 

',V4A I 

i 

v, 

d

D 

v, 

• 1 I 



P16 Inlet Transition Flanders 8 OD x 15 8.329 18.000 ED4-2 

W x 18 H x 18 L, 30' 

J16 HEPA Pre-Filter, 36-NO2- Flanders 24 W x 24 14.000 

136 H x 14 L, 0.12" w.c. 

(0.24" Dirty) at 750 

cfm 

J16 Test Combination Flanders 24 W x 24 20,000 

housing H x 20 L, 0.5" w.c at 

750 acfm 

J16 ' HEPA Filter, 36-NO2-131 Flanders 24 W x 24 

H x 19.375 L, 1.0" 

w,c. (2.0" Dirty) at 

20.000 

_ 

750 acfm 

J16 Test Outlet Housing Flanders 24 W x 24 20.000 

H x 20 L. 0.5" w.c at 

750 cfm 

J16 I Outlet Transition Flanders 8 OD x 15 8.329 12.000 SD4-2 0.060 .04" 

W 18Hx 12 L, 45° @ 

750 

cfm 

Total Pressure drop at 2.12 

750 cfm 

F OGTS Bypass HEPA 

Filter Skid Outlet Ducting 

With Fan to Stack 

b 

N 

v^ 

a 

m C 

a

v, 




Fitting Loss 

No Coef. 


P17 Sl, Piping, 8-VOG-36- 

0319 

_ 

8" straight duct, S.StI, 

w 8 x 8 x 1 red tee, 

flow thru 

8 lOS 8.329 12.000 CD11-1 ARROW 

P17 Expansion Joint, EJ-616 8" Expansion joint 8 lOS 7.625 CR6-3 0.110 

J17 Pan, 36-N31-130 1125 ACFM Fan, 

NYB 1508, See Data 

Below 


1.000 ft 


1.5, S.StI 

8 lOS 8.329 CD3-1 0,110 

" Piping, 8-VOG-36-0319 8" straight duct, S,St], 8 lOS 8.329 6.000 CD11-1 ARROW 

P18 Piping, 8-VOG-36-0319 8" straight duct, S.StI' 8 10S 8.329 36.000 CD11-1 ARROW 


3.500 ft 

J18 Backdraft Damper SI\LTPS Data See 

Below 

P 19 Piping, 8-VOG-36-0319 8" straiahtduci, S.Stl 8 lOS 8.329 12.000 CD11-1 ARROW 

119 Isolation Valve, 36-V-166 8" Keystone, FIG. 

362-173, Key-Lok 

8 7.625 2.500 2440 

P20 Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 CD11-1 ARROW 

11 

Expans ion Joi nt, EJ-61 7 8" Expansion joint 8 Ios 7.625 11.000 CR6-3 0.110 

-0 

b 

N 

.A 

a

Y, 

a 

1 



" Lateral Wye, Forward 45° Lateral Branch 

8 lOS 8.329 I 24.000 ED5-1 0.610 

' Direction 

Flow 



" Elbow 90° Elbow, R/D = 

1.5. S.Stl 

8 lOS 8.329 CD3-1 0.110 

i i Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 lOS 8.329 34.000 CD11-1 ARROW 

" Elbow 90° Elbow, RD = 

1.5, S.Stl 

8 10S 8.329 CD3-1 0.110 

" Piping, 8-VOG-36-0319 8" straight duct, S.Stl 8 10S 8.329 144.000 CD11-1 ARROW 

" Reducer 8 x 12 Std Reducer, 

28.5° 

8 x 12 10S 8.329/12.39 8.000 ED4-1 0.330 

P20 Sudcen Expansion 12 x large 12 x 56 ED4-1 0.880 

J20 OGTS Stack 1 atm pressure 


47.000 ft 

Component Details Size Schedule Inside Dia. L ASIIRAE 

Fitting 

No 


J21 ^ Atmospheric Pressure 

Junction 

ASHRAE 

Loss 

Coef. 

Cv 

N 

Cr7 

2 

C-

v^ 



P21 Inlet Screen 16" Cicular Intake 16 15.624 CD6-1 0.970 


(60% open) S.Stl 

" Reducer 16" x 12" i 16 x 12 lOS 15.624/12.39 14.000 ED4-1 0.120 

" Inlet Piping, 12-VOG-36- 12" straight duct, 12 lOS 12.39 90.000 CD11-1 ARROW 

0409 S.Stl 

" Elbow #1 90° Elbow, R/D = 12 10S 12.39 CD3-1 0.110 

1.5, S.Stl 

" Elbow #2 90° Elbow. R/D = 12 lOS 12.39 CD3-1 0.110 

1.5, S.Stl 

P21 Elbow #3 90° Elbow, R/D = 12 lOS 12.39 CD3-1 0 . 110. 

1.5, S.Stl 

Total 104.000 inches ^.0 

_ 

8.667 ft 

J22 HEPA Inlet Transition Flanders, Transition 12.0 dia x 11.250 ED4-2 0.780 0.01" 

12" x 28" SQ x 28" SQ @ 

11.25" L, 30 0 250 

cfm 

J22 Heater Element, 36-N84- Watlow/Chroinalox 2.000 

140 0.25" w.c. @ 1000 

cfm 

J22 HEPA Pre-Filter, 36-NO2- Flanders, 0.12" w.c. 24 x 24 2.000 

135 (0.24; di rty) at 1000 

cfm 

75 i HEPA Filter, 36-NO2-134 Flanders, 1.0" w.c. 24 x 24 5.875 

(2.0" dirty) at 1000 

cfm, P-007-W-43- 

N2-NU-51-23-CC- 

FU5 

E 

b 

N 

.A

3 

to 

a` 

11 0 0 

J22 Outlet Transition Flanders, Transition 

6" x 28" SQ x 11.25" 

L, 45° 

Total Pressure drop at 

1000 cfm 

i 

P22 Piping, 6-VOG-36-0408 6" straight duct, S.Stl, 

w 6 x 6 x I red tee, 

flow thru 

J23 Valve, 36-V-178 6" Keystone, 

Variable Cv 

P23 I 

1 



1.382 

6.065 dia x 

28" SQ 

11.250 SD4-2 0.110 0.002" 

@ 

250 

cfm 

6 40S 6.357 6.000 CDl1-1 ARROW 

6 2.250 1194 

Piping, 6-VOG-36-0408 6" straight duct, S.Stl 6 40S 6.357 41.000 CD11-1 ARROW 

" Elbow 90° Elbow, R/D = 

1.5, S.Stl 

6 40S 6.357 CD3-1 0.110 

" Expansion Joint, EJ-614 6" Expansion Joint 6 40S 5.9 11.000 CR6-3 0.240 

Tee 6 x 6 x 1 tee, flow 

thru 

6 40S 6.357 12.000 ED5-3 0.260 



J13 Wye #1 45° Lateral Branch 

Flow 

Fan Curve, NYB Model 

No. 1508 

Test Density: 0.0553 

lbm/cu ft 

22.333 ft 

6x8 40S 6.357/8.329" 10.000 ED5-2 0.610 

Mechanical 

ro 

A 

A 

A 

C

a 

Y, 


Q Ft/ Min dP, IN H2O Std Efficiency, 

% 

_ 0 12 67.36 

500 13.75 67.36 

1000 13 67.36 

1500 11.25 67.36 

2000 8 67.36 

2500 4.25 67.36 

3000 0 67.36 


Backdraft Damper 

Pressure Drop 

Ref, SNUPPS 90144 

24 x 24 prototype For 8" Pipe Area sch 10 Dia. 

Vs, fpm dP, inches w.c. Q, CFM sq. ft ft. 

700 0.13 264.9 0.378 0.694 

800 0.135 3023 

900 0.14 340.5 

1000 0.145 378.4 

1500 0.18 567.6 

2000 0.23 756.7 

2500 0.27 945.9 

1 3000 0.32 1135.1 

3500 0.36 1324.3 

0 

ro 

ro 

N 

a 

C 

a

?,.., 

RPP-24544 REV 1 d 


Attachment 5 

Page 6 of 14 

Te : ASHRAE DUCT FITTING DATABASE 

Fax: Version 2.5.D Friday, February 10, 2006 

{CR 63-3) Orifice, Thick-Edged 

(Idelchik 1986, Diagram 4.15) 

He-gh-. Mo, in.', 5.3 'Je:ccity (Vo, four; 208` 

Width }j%lo, in.',' 5.3 Vii PresatVo P.-. io. •rn) t126 

He-gh: M1, ir..; 4:P Lass Cc-:-fncient (Cc} 

Width x';11, in. , 4:i+ Pressure'_oss (:n. ,act, 0.07 

Lengh ^L, :n.) 24.0 

Flux Rutz (0, chi,; 4C9 

L/Dh > 0,015 

Dh = 2A, /(H i + W1) 

^— L--^ 

NE50 ONE fylo)^^ E 

Fe p 7 _ 's

• 

I Q 

• D 

A a 



41tachment 5 

'^wr,; a '(e . 3 of 14 

Y- of 

Ta: ASHRAE DUCT FITTIRG DATABASE 

Fax: Version 25.0 Friday, Februarf 10, 2006 

(CD34) Elbow, Die Stamped, 90 Degree, dD =15 

(UMC 1985, Report SRF785; Idek;hik 1985, Diagram 6-1) 

Diameter (D, in.) 6A Ve:xity ('Jo, fpm) 7tF 

Flax Rate M, cfm; .. 4C5 Vei Pre atVo. ::+o-v. 7 IM, 

Loss Cce^ X13.. 

Pressure _os5(ke: tig). 0'#S 

A5-621

• 

E 

a 

• 



Attachment 5 

Page 4 of 14 

T •: ASHRAE DUCT FITTINGDATABASE 

Fax: Version 2.5.0 - Friday. February 10, 2005 

(C63-3) Elbow, Die Stamped; 45 i, a 

(i1MC 1985, Report SRF785; Wefchi a =1,^' 

INPUTS 4SlSP€ ; 

Diameter (0, in_) 5.31. 1 Ye?oc ,L^; ^^, Z855 

Film ;Rate Std, efrn) 4C0 lmt-m ke., 043 

D 

Q 

A 

A5-622 

Loss 

,y 

8.89 

Pressure toss (n. a^g) G.D4 

45*

• 

11 

r1 

LJ 

Tel: 


ASHRAE DUCT. FITTING DATABASE 


Attachment 5 

Page 8 of 14 

Fax: Version 2.5.0 Friday, February 10, 2006 

1h1PSlIS 

(ED4-1) TransBion, Round to Round, ExhoustfReturn Systems 

(Idelchik 1986, Diagrams 5-2 & 5-22) 

4 911M 

0r.k': Sz'i # 

Diameter (Do, in.) 

Diameter (D1, in.) 

Angle (Theta, deg.) 

Flow Rate Q, din) 

K,44 

, 

406 

Velocity 0/0, fpm) 

Velocity (V1, fpm) 

Vel Pres itVo (Pvo, in. wg) 

Vel Pres at V1(Pv1, in. vrg) 

1842 

3810 

021 

0.88 

Loss Coefficient (Co) 

0.22 

Loss Coefficient C7 

0.05 

Pressure Loss (in. wg) 

0.04 

Aa/A, < or > 1 

A5-623 

WIMILIl

0ti 

12 

lift, 

t6 

A `-K 

20 

z, 

ry 

206 304 678 1,061 

360 ..::. L ltt' k+{.`. 

we 432 803 

1fYa1; ^1 

rb3 C a ,AMID 2,319 

„6 O F 991 V'.' 3 

1 016 t 5..,7 3,2a0 4,670 

1 480:.. . 2 9pD:', . 4,,6,10 ' ^^^' 


A4sl Maximum '1?9 "Pressure an 

81_6.104-1876 _Leakage Mteidi1t.11it Temperature 


Attachment 4 

Page 4 of 8 

Glass V1 Nominal port 

D arnctcr (In.) 

Bubbles p t 

M nutO 

mL per 

Minute 

Air or N6raw, , Gerv)tto ett, 50 psIg 114, bw ditlMBnik3)t, 

raltfrttever Is Sher, at W to 125'F'(1T to 52'Ci 

2 3 0. as 

n- ''^ V 

2,12 

3 

4 

6 

a 

4 

6 

11 

27 

4s 

0.60 

0' 90 

1.70 

4.00 

6.75 

L X-LOX potytvir, alastombr and Gre•safe roata pins-Ida AN& Class VI sl„Wlt. ~ 

2. K-LCK metal Seals provide ANSI Class IV Sruttot;'. 

3, Using the ANSIeW spa.]lted measuring device. 

Refererce ANS*Ct 7 0-2 for fur itwr `03fmaiiun_ 

9 to 

1D ---- 34 Sf 76 

106 134 103 

t631 _, 

8 

e 

15;` 

t0 '-J 

12 94 

?S '. 44: 

^'1 " zlr^?^ki^K'. 

43 97 1oD 

80 ;,3Q ' )39: 

"Ala.:1 s?C"A'si>i15 

138 186 2" 

2.69'` "j Ss . _ ;`3.4?S 

1T^{ 

245 

41 _`;; 

3D 

$ 

4 

70 , 1 

149 

230 

242 

1 

306 604 673 786 

"00^^^ 

78S. .. 

1 19a Â.Fr^1r 

_ 

f° 

Angle of Opening 

CL 300 

9)20 (in.) 10° 20° 30' 40" s0" 60' 70' 80' 90` 90° 

3 

4 

6 

83 1 17 261 437 05 1.052 1406 2,oDy1 

7 110' 

2 "' 

^s'7=. 

Tho combina tion of irder)erence lit soak 

and bi-dirr_clional packing makes the 

K-LOK especially wo)1 suited for vacuum 

ScM6ce. 

Standard K-LOK high performance 

,,,ilvcs arc rated to an absolute_ pressure 

of 4 x 10 5 inch 119. Nigher vacuum 

epol^cations are available. 

o.oao 

6,794 166% 13,430 f4;7Y0 

214ry 0D^ $" 38,D00 35 

.!^+•5,.^t,î*>a"—d',ibî.'"^v...;e^.-..h s;.....:;?.k —7.^ ..;^.•_. 43..`1 s'L^,.w31 

Actuator Type Figure Remark 

Henc84 K4D1 Loverlock 

Getii:'. F!{201^ FGOD Se)Ees, _ , ;Ty- 

PrIp, u1 a2c rF79L Mh extunded Pawl adaplet 

C4aar a)?1Setr1R4iC F4a9 79U Deriu".cltiable gear llttri pbOYhic.S tn>4nual 

ov4?+rkle for OW Keys r* j>iFeu»atk a)ctu ta' 

searlo 1-777 

r" 

ZiTMM

37th.. 

of 

C^ 

t 

01G I'S Bypass System llnid Flow Mo e.ei 

A ICV Box plenum HEPA filter, 35-NO2 .010, S tream No. 9 406 acfin at -2.24" w.g. and 77'F, Ibd sofin or tbd lb/hr (TBR) 

1 j Atrnosplm7ic Junction 

Compotx-tM Details Si/x: Schedule Inside Dia. L ASIIRAE Fi tting No :AS1 IRAE Loss Coef. Cv 

(m) (6) (uQ 

PI Intel Housing and screen 16" square Intake wi th birdscrecu, (60% open) S.Stf 16 x 16 17.4906454372773 CR6-I 1ER3-1 - 0-97-' U IS 

" Inlet Piping, 6-AA-35-02 18 6" straigh( duct, S.Stl 6 40S 6.065 =5'12'7 CDI I-1 ARROW 

P I NO2-0 10 Inle9 Tunsi(ioo Flanders, Sudden Expansion, 6 dia x 24 SQ, 180' 6 40.5 6.065124.0 Sp ED4-2 0.81 

Total inches =+SUM(16:18) 

=+G9/12 ft 

J2 HEPA Filter, 36- 1,102-0 10 Pre Flanders, 0.12" w.c. (0.24" Dirty) at 500 efin 

1 2 jUIEPA filler, 36-NO2-010 

Flandl ;rs, 1.0" w.c. (2.0" Dirty) at 500 c5n, P-007-W-43-N2-NU-51 .23-GG- 

DUS 24 x 24 x 16 

Total Pressure drop at 500 cfin 1.12 

P2 Owlet Transition Flanders, Sudden Con traction, 24 x 6 12.0 SQ/6.065 Rod EDI-I 0.5 

" Piping, 6-AA-35-0218 6" s traight duct. S.SO 6 40S 6.065 =3'12+6 CDI 1-1 ARROW 

' Elbow No. I 90' Elbow, RID - 1.5, S.Sll 6 40S 6. 9 65 CD3-1 0.13 

" Piping, 6-AA-35-0218 6" straight duct,S.Srl 6 40S 6.065 =5.12+2 CDI -1 ARROW 

P2 Elbow No. 2 45' Elbow, R/D ° L5, S. Sit 6 40S 6.065 CD3-3 0.08 

Total= +SUM(G 18:621) inches -+SUNi(118:121) 

=+G22/ 1 2 ft 

Component Details Size Inside Dia. L ASHRAL Fitting No ASHRAE Loss Coef Cv 


A Rcduccr 6" x 4" 6 x 4 4US 6.065/4026" 5.5 ED4-1 0.22 

P3 Piping, 4 AA-35-0218 4" straight duct, SSit 4 40S 4.026 =13'12+7 ME 1-1 ARROW 

P3 Flownretcr 3 ea Size I Atnubar Bowntcter 4 Vendor --0.545.3 

Total -+SUM (G28:G29) inches =-1SUM(128:129) 

-tMil2 R 

14 $ ., ", ^ "^àD.T aIG 4 x 6 40S Q4A2ol^, _ ^_ _ E044 ow 

1 14 Rlhow No. 3 ^ # w, RID = 13, S.SII C, 40S 6.065 CD3 " "t^ 0.08 

' Piping, 6-AA-35-0218 6" s tr aight duct, S.Stl 6 405 6.065 12 CDI I - I ARROW 

' Elbow No 4 a. Elbow, RID = 1.5, S.SII 6 40S 6.065 CD3-3 008 

' Piping, 6-AA-35-0218 6" straight duei, S.Sll 6 40S (1 .065 12 CDII-I ARROW 

" Elbow No. 5 6+4R 90" Elbow, RID ° I.S. S.StI G 405 6.065 CD3-3 0.08 

P4 Piping, 6 AA-35 .0213 6" s traight duct, S.Sil 6 4 0S G.OGS -3.12+2 CDII-I ARROW 

Total =+SUM(G34:G39) inches -+SIJM(114:139) 

=+640/12 

ft 

J5 "' 6" x 4" I{T 6 x 4 40S 6.065/4.026" 5.5 ED4-1 yi4 _ROv 

PS lExpansion Joint, FJ-S01 4" 4 4.025 22 CR6-3 0.37 

16 (ICV Box C'P) 

B ICV Box Plenum, S tream No. 9 in, 13 on( 280 acfnt at -2.46" w,g. a,td 875 °F, 108 sefrn or 513 Ib/lu (0.143 Ib/sec) 

1(i ICV Box plonun CPs (iule tfou0cl) Inlet and Outict Losses Crane (.5 

C ICV Outlet to l is Point, Stream No. 13 280 acfin at -2.46" w.g. and 875 'F, 108 sefm or 513 lb/hr 

Component D etails Size Schedule Inside Dia. L ASHRAF Pitting No ASH RAE Loss CocC Cv 

(in) (m) (in) 

(ICV Box CP) - .• 

P6 Piping, 6-VOG-35-021 7 6" Duc(w 90" Elbow, Internal to AW'fE 6 40S 6.065 =6.12 CDI 1 -1 ARROW 

P6 Elbow 90' Elbow, RID -- 1.5 5 405 5.295 CD3-1 0.15 

17 6 x 5 40S 10.25 ED4-1 ,. 4 A ARP-&-P 

P7 Expansfon Joint, EJ-502 DME S" size 5 4.9 `- 24 CR6-3 

" Pipiug. 5-VOO-35-0217 5" Met 5 40S 5.295 24 CDI 1-1 ARROW 

" Elbow 45° Elbow, RID - 1. 5 5 70S 5.295 CD3-3 0.09 

" Piping, 5-VOG-350217 5" Duct 5 40S 5.295 =.7.1?+9.5 CDI 1-1 ARROW 

P7 Elbow 45' Elbow, WD - 1.5 5 40S 5.295 CD3-3 0.09 

foul =+SUM(G58:G62) inches =+9U+f1lt[S$Îd"LF ^.. _ 

=4663112 A 

18 lateral Wyc (Fox Bypass Flow) 45' Latu2l Branch Flow, Main F low Closed 5 x 5 x 5 4US 5.295 110 ED5-2 0A4 

-I- 

- 

o +C 


A5-625

Kin ^ 

1t71 

D OGI'S Bypass Main Ducting from Tic Point to II EPA inlet, Stream No. 13 280 acfm at -2.46" w.g. and 875 "F, 108 mfm or 513 IbA ir 

J8 Lateral Wye (For Bypass Flow) 

P8 Elbow 45° Elbow, R/D _ 1.5 5 40S 5.295 CD3.3 0.09 

P8 Reducer Standard Reducer, 5x6", 11' 6 x 5 40S 5.29516.065 6 ED4-1 0.05 

19 Lateral Wye, Forward Direction 30' Lateral Wye, Main Flow 6 x 6.x 6 40S 6.065 6 EDS-2 0.29 

Component Details size Schedule Inside Din. L ASHRAE Fitting No ASHRAE Loss Coef. Cv 


P9 Piping, 6-VOG-36-0286 6" straigbi duct, S.SII 6 40S 6.065 t0.5 CDI 1-1 ARROW 

J10 Valve, HV-901 8" Keystone, PIG. 362-173, Key-Lok 6 5.8125 2.25 1194 

P10 Elbow 90u Elbow, R/D - 1.5, S.Stl G 40S 6.065 CD3-1 0.05 

PIO Piputg,6-VOG-36-0286 6' s traight duct, S.Stl 6 40S 6.065 8 CDII-1 ARROW 

Ill lateral Wye Reverse Direction 30' Laeral Wye, Main Flow 6 x 6 x 6 40S 6965 6 EDS-2 0. f I 

Component Details Size Schedule Inside Din. L ASHRAE Fitting No ASH RAE Loss Coef. Cv 

(in) (in) (in; 

J9 Lateral Wye, Forward Direction 30° Lateral Wye, Branch Flow 6 x 6 x 6 40S 6.065 G ED5 2 0.61 

Pit Pipiog,6-VOG-36-0286 6"straigladuct,S.S tl 6 40S 6.065 6 CD11-1 ARROW 

Pit Elbow 30' Elbow, R/D - I.S. SSII 8 MS 8.329 CD3-1 COS 

J12 Valve, HV-902 8" Keystone, PIG. 362-173, Kcy-Lok 6 5.8125 2.25 1194 

P12 Piping,6-VOG-36-0286 6" straight duct,S-Stl G 40S 6.065 6 CDII - I ARROW 

P12 Std Tee 6" Sid Tee, Branch flow 

P12 Piping, 6-VOG-36- 0286 6" s traight duct, S.Stl 6 40S 6.065 6 CDII-1 ARROW 

P12 Elbow 30" Elbow, R/D = 1.5, S.Stl 6 40S 6.065 C'D3-I 0.05 

lit Lateral Wye Reverse D irection 30' lateral Wye, Brauch Flow 6 x 6 x 6 40S 6.065 6 EDS 2 0.24 

P13 Piping, 6-VOG-36-0286 6" s traight duct, S.Sil 6 40S 6.065 6 CDII - I ARROW 

P13 Reducer 6.x S Std Reduce, 19° 6x8 40S 6.065/8-329 ED4-1 0.17 

P13 Elbow #1 90' Elbow, R/D - 1.5, S.Stl R IOS 8.329 CD3-1 0, I I 

P13 Piping,8-VOG-36-0286 8" straight duct,S.StI 8 Ios 8,329 -9.12+6 CDII-I ARROW 

Pt 3 N.J + - 8" Expansion Jo int 8 10S 7.9 11 CR6-3 CM I 

P13 Pipung,S-VOG-36-0286 8".ctaight duct, S.Sil 8 IOS 5.329 -10*12 CDII - I ARROW 

Total --+SUM(G94:(-,99) inches -+SUM(194:199 

- 

H 3 Late ra l Wye, Forward Direction 45' Lateral l -rough Flow (Air Dilution System n) Branch Bow) 8 108 8.329 10 ED5-2 0.29 

P14 Piping.8-VOG-36-0286 8" s tr aight duct, S.Stl 8 IOS 8.329 = 11*12+6 CDII-1 ARROW 

" Elbow 0 1 90' Elbow, WD - 1.5, S.Stl 8 IOS 8.329 CD3-1 0.11 

" Pipung,8-VOG-36-0236 8" s traight due(, S.Stl 8 IOS 8.329 15 CDII - I ARROW 

" Expansion Joint, EJ-635 + 5 others 8" Expansion joint 8 79 11 CR6-3 -0.1 i *6 

P14 Piping, 8-VOG-36-0286 8" Straight duct, S.StI 8 IoS 8.329 -76*12+32*12f 6-21-8+44 . 12 CDII-1 ARROW 

= +6100112 

Total --+SUM(G 10-0:6.108) inches = 1SUM(i 104:1108) 

J14 45' Lateral 45° Lateral Flow Thm branch closed 8.8.8 108 8.329 E05-2 A Q A tow 

PIS Piping,S-VOO-36-0286 8" straight duct, S.Stl 8 IOS 8.329 -6*12+5.5-12 CDII-1 ARROW 

' Elbow #2 90" Elbow, R/D - 1 S, S.S 11 8 10S 8.329 CD3-I !-. 8l .-f 

" Piping,8-VOG-36-0286 8" straight duct, S-311 8 Iris 8-329 -8*12+4 CDII-I ARROW 

" Std Tee Std Tee, Branch flow, main flow dead 8 x 8 z 8 los 8.329 ARROW 

" Pipueg, 8-VOG-36-0286 8" straight duel, S.Sil R IOS 8.329 ^-8*12+5 CDII-1 ARROW 

PIS Expansion Joint, FJ-615 3" Expansior- joint 8 7 9 I I CR6-3 

(IIEPA Inlet) Total -+SUM(G113:6118) inches #SUM 11-1 

-+G119/12 

O 

E CX3TS Bypas IIEPA Filter Skid 

HEPA Filter skid Assembly, 36-D58-138 

Compo e"t Details Size Schedule hnside Din. L AS] IRAE Fitting No ASHRAh Loss Cmr, Cv 

_ +G 109/12 

(in) (in) (un) 

J I S Isola tion Valve,; _ , ^11 .lC#,' 173, Key-Lok - 7.625 2.5 

P16 hnlct Transitiun Flanders 8 OD x IS W x 18 H x 18 1., 30' 8.329 18 FD,4-2 0.43 

J16 I IEPA Pr -Filter, 36-NO2-136 Flanders 24 W x 24 li x 14 L, 0.12" w.e. (0.24" Dirty) al 750 cC 14 

J16 'Deer[ Combutation Housing Flanders 24 W x 24 11 x 20 1., 0.5" w.c at 750 acfm 20 

ft 

It 

Y" 


A5-626

1) 

"I HEPA Fnhcr, 36-NO2-131 Flanders 24 W x 24 H x 19.375 L, 1.0" w.c. (2.0` Dirty) at 750 acfin 20 

J16 Test Outlet I lommg Flanders 24 W x 24 11 x 20 L, 0.5" w.e at 750 cfin 20 

116 Ou1kt Transition Flanders 8 OD x 15 W x 18 H x 12 L, 45' 8.329 12 SD4-2 0.06 -04' Gil 750 cGn 

F OGIS Bypas HEPA Filler Skid Outlet Dueling Will, Fair Stack 

Total Pressure drop at 750 cfm -0.12+0.S-I+0.5 

Competent Details Size 

On) 

Schedule buide (in) Dia. (bn) 

L ASHRAE Fitting No ASHRAE Loss Coef. Cy 

P17 SI, Piping. 8-VOG-36-0319 8" straight duct, S.StI, w 8 x 8 x 1 red ice, flow thin 8 )OS 8.329 12 CD11-1 ARROW 

P17 Expansion Jo`vnl, EJ-616 8' Expansion joint 8 los 7.625 CR6-3 0.11 

Total =-SUXi(G140:G141) inches =+SUM(1140:1141) 

=+G14Ui2 (t 

J17 Fan, 36-N31-130 750 ACFM Fan, NYB 1508, Sec Dala Below 

PIS Elbow 90' Elbow, R/D = 1.5, S.SII 8 IOS 8.329 CD3-1 0.11 

" 

Piping,8-VOG-36-0319 8" straight duct,S.S11 8 los 8.329 6 CDII-I ARROW 

PI8 Pipng, 8-VOG-36-0319 8" straight duct, S.S(I 8 loS 8.329 36 CDI I-1 ARROW 

Total =+SUM(G146:Gt48) itches +SUM(114G:(148) 

-+G 149/12 ft 

Jig Backdraft Damper SNUPPS Data See Below 

P19 Piping,8-VOG-36-0319 8" straight duct,S.StI 8 IOS 8.329 12 CDII-1 ARROW 

119 lsnlation Valve, 36-V-166 8' Keystone, FIG. 362-173, Key-Lok 8 7.625 2.5 2440 

P20 Piping,8-VOG-36-0319 8" straight duct,S.Stl 8 los 8.329 CD] 1-1 ARROW 

" Expansion Joint, LJ-617 8" Expwision jowt 8 I OS 7.625 11 CR6-3 0.1 I 

" Lateral Wyr, Forward Direeriou 45' Lateral Branch Flow 8 Ms 8.329 24 ED5-1 0.61 

° Piping. 8-VOG-36-0319 8" straight duct, S.SII 8 10S 8.329 =9'12 CDII-1 ARROW 

" Piping, 8-VOG-36-0319 8''stmighl duct, S.Stl 8 IOS 8.329 -20.12+6 CDII-I ARROW 

' Elbow 90' Elbow, R/D 1.5, S.S0 8 10S 8.329 CD3-1 0.1 I 

" Piping, 8-VOG-36-0319 8" straight duce, S.Sd 8 10S 8.329 =2.12+10 CDf 1-1 ARROW 

" Elbow 90' Elbow, RID = E.5, S.Stl 8 Ms 8.329 CD3-1 0.11 

" Piping, 8-VOG-36-0319 8" suaigbl duct, S.Sil 8 10S 8.329 -12'12 CDII - I ARROW 

" Reducer 8 x 12 Std Rcduccr, 28.5° 8 x 12 IoS 8.329/12.39 8 ED4-I 0.33 

P20 Sudden Expansion 12 x large 12 x 56 ED4-1 0.88 

Total -+S1)M(G156:G165) undtes -+SUM(I156:1165) 

=+G I66JI 2 n 

120 OGTS Stalk I ann pressure 

JS-IIypassHSPA-Cdtee,.3dd)S&SAD- ,• - ac m or Lb3hr 

121 Aimospl:erie Presstrc Junction 

Componatt Details SIZC Schedule Inside Di.. L ASHRAE. Filling No ASHRAE Loss Cocf. Cv 


P21 Inlet Screen 16" Cieular Intake with birdscreen, (60% npen) S.Sit ! 6 15.624 CD6-1 0.97 

" Reducer 16"x 12" 16x 12 los 15.624/12.39 14 ED4-1 0.12 

" Inlet Piping, 12-VOG-36-0409 12" straight duct,S.Sd 12 loo 12.39 90 CD 11-1 ARROW 

" Elbow• p 1 90" Elbow, R/D - 1.5, S.StJ 12 !OS 12.39 CD3- I 0.11 

' Elbow e,2 90' Elbow, R/D = 1-5, SSti 12 IOS 12.39 CD3-1 0.11 

P21 Elbow 81 90' Elbow, R7D = 1.5, S.S(I 12 loS 1239 CD3-1 0.11 

Toter =+SUM((il74:GI79) inches =+SUM(Il74:1177) 

-+G[80/12 fl 

J22 HEPA Inlet Transition Flanders, Transition 12" x 28" SO x 11.25" L. 30' 12.0 dia x 28" SO 11.25 ED4-2 0.78 0.01" L 250 cfm 

122 Heater Elanera, 36-N84-140 Wallow/Cluontalox 0.25" w.c. (o) 1000 cfm 2 

122 HEPA Pre-Filtn, 36-NO2-135 Flanders. 0.12" w-c. (0.24 dirty) at I(M cfm 24 x 24 t 2 

122 HEPA Filter, 36-NO2 -134 

Flanders, 1.0" w .e. (2.0" duty) at 1000 cfm, P4)07-W-43-N2-NLJ-51-23-CC- 

FU5 24 x 24 5.675 

122 Owlel Transition Flanders, Transition 6" x 28" SO x 11.25" L, 45' 6.065 dia x 28" SO 11.25 SD4-2 0.11 0.002" (J, 2SO cfm 

'focal Pressure drop at 1000 cfm L 12 

P22 Piping, 6-VOG-3G-C408 6" straight duct, SSll. w 6 x 6 x I red Ice, flow thnt 6 40S 6.065 6 CD I -I ARROW 

123 Valve, 36-V-178 6" Keystone, Variable Cv 6 2.25 1194 

P23 Nping,6-VOG-36-0408 6' straight duct,S.Stl 6 40S 6.065 -3'12+5 CDII-1 ARROW 


A5-627

'11^' I 

" Elbow 90` Elbow, R1D = 1.5, S.St1 6 40S &065 CD3-1 0.1 I -- - 

' Expansion 1ouu, G-614 6' Expmtsion Joint G ( 40S 5.9 11 CR6-3 024 

" Tee 6 x 6 x 1 tee, flow tltru 6 40S 6.065 12 ED5-3 0.26 

P23 Piping,G-VCG- 36-W8 6' straight duct,S.Stl 6 40S 6.065 -17.12 CD11-I ARROW 

Towl •d SI1M(G194:G198) incltcs =rSUMQ194119R) 

-+6199112 

fl 

113 Wye Il1 45' Lateral 3rmw3, Flow 6 x 8 40S 6.06518.329" 10 ED5-2 0.61 

Pan Curve, NYR Modcl No. 1508 Test Datsity: 0.0553 IbuJcu ft Mechanical 

Q Ft/ Min V, IN H2O Std Efficiency. 

0 12 67,16 

500 13.75 67.36 

-5004B207 13 67.36 

500+0 2 08 11.25 67.36 

500+8209 8 67.36 

=500+821 D 425 67.36 

-500+8211 0 6736 

8ackdraft Damper Pressure Drop ReC SN(JPPS 90144 

24 x 24 wolotypc For 8" Pipe Area sch 10 Dia. 

Vs, fpm dP, ntcbcs w.c. Q, ChM sq. R ft 

700 0.13 -+8217•ES217 =+PIO•1:217^214 =8.329112 

800 0.135 -+8218•ES217 

900 0.14 -+8219•E$217 

1000 0.145 -+8220•F$217 

1500 0.18 =+8227•ES217 

2000 0.23 -+8222•ES217 

2500 0.27 -+p223.15217 

3000 0.32 -+8224•E$2l7 

3500 10.36 =+8225•ES217 


A5-628

i 

Y" 

c^ N 

j of 


Free Convection Correlations for air at 1 atm. (Holman 1990, Table 7-2) 

Twl = 875 OF Temperature End 1 

Tw2 = 250 °F Tem erature End 2 

Ts - 562.5 

OF 

Average Wall Temperature 

To = 115 

OF 

Ambient Temperature 

dT = 447.5 °F i Temperature difference 

h = 1.45 Btwhr-ft, ,2-°F Vertical Plane or Cylinder h = 0.19 * dT^l i3 

h = 1.38 Btu/hr-ft^2-°F Horizontal Cylinder h = 0.18 * dT^1/3 

h = 1.68 ! Btu-'hr-ft^2-°F Horizontal Plate - heated face up h = 0.22 * dT^ 1 /3 

Forced convection, flow across a cylinder (Holman 1990, e n. 6-21): 

0.61Re^,`Rr"3; Rey, 

Nufd = 0.3+A*B/C Forced Convection, Nusselt No. 

A = 0:62Red"2Pr"3 B = 1+(Red/282,000)^5/8]^4/5 1 to .4' 

D = 8.6 Inch Dia of Pie 1844 meters 

U = 0.1 Mph Free Stream Air Vel. -~-0.0447 m/s 

Ts = 5625 OF I Pi e Wall Temperature 294.72 °C 

To — 115 OF Ambient Temperature 46.11 °C 

Tf = 338.75 OF Air Film Temperature 170.42 °C 

= 0.00019 1 sq ft sec Viscosity of Air 1.8E-45 s . m/s 

Red = 5.45844E+02 Dimensionless Reynolds No 

Pr = 0.7778 Dimensionless Prandtl No. 

kf = 0.0146 Btu/hr- ft-°F Thermal Conductive 1) 253 W/m-°C 

1v N.p 

si

M. 

v, 

w0 

1 

j 

1VIcAdams Free Convection Correlations for air at 1 atm. (Holman 1990, Table 7-2) 

Red*Pr = 4'4.57 The dimensionless numbers are: 

Vusselt, ivu^ ~-^- or ,b'uc F-•—^ . 

RBV170'ds, 

.tea_ 

: ;3 P c„ ST1L3 

or Pa., a 9 

v ;, • k. 

Ref = ^L or Rem 

V t' 

A = 13.322 B = 1 .0-11:6 C = 1.132 

Stefan B = 1.714&09 Btu/hr-ft^2-R^4 

emiss = 0.65 


Nufd = 12.26 Dimensionless Forced Convection, Nusselt No. 

Nund = 67.50 Dimensionless Natural Convection, Nusselt No. 

Nut = 0.3 + [(Nufd- c)^' + 'und - c)^ `'(li' Combined Forced and Natural Convection, Nusselt No. 

c = 0.3 for Horizontal cylinder 

= 4 for Horizontal cylinder 

Nut = 67.52 Dimensionless 

he = 1.38 Btu/hr-s .ft-°F Combined Convection he = 7:$1977 Watts m-°C 

Pr = 

r 

^t b 

'C 

N 

.A 

.A 

C 

n

Y, 

w 

i 

Radiation component: I 


McAdams Free Convection Correlations for air at 1 atm. (Holman 1990, Table 7-2) 

Stefan B = 1.714E-09 Btwhr-ft^2-R^4 

emiss = 4.65 

h. - 

(i T„ 

r T. 

hr = 2.45", Btulhr-s .ft-°F Th Radiation Coefficient 

ht = he

ME 

EM 

A 13 C D E F G H 

- i McAdams Free Convection Correlations I 

[2 

Tw I = 40 Temperature End I 

-- 

3 

Tw2 = 20 

Temperature End 2 

4 

Ts 

F 

Avers Ave Wall Temperature 

5 TO - 0 -F Ambient Temperature 

6 

7 

dT -tl34-05 -F 

RttVhr-ft'2-*F Vertivil Plane orC rider h - = 01 . 9 *Tl/3 d ' 

El h= NAr-ftA2-IF Horizordal h - 0.18 * dT^1/3 

11 Forced convection, flow across a c)jinde 

12 

4 

16 

h Btu/hi--ft^2-IF horizontal Plate - heated face up h = 0-22 • dT^ 1/3 

F;'Eb. 

0-3 -1- wo- ( 

tI (0.4 -2182,000 1 

^y 

02 

--.._ ._..—._--- 

17 

-,--Nufd 0.3+A OBX Forced Convection, Nussell N 

18 D- U 

U -01 

inch DiaofPipc meters 

- 

mph Free Stream Air Vol. -aWOMW 

20 TS - --+M -F —(820-32YLt *C 

21 To:- —W -F Ambient Temperature -4fB21-32YI.8 C 

22 

Tf - - -+(13- - 821)12 Air Film Temperature "B22 -32".8. C 

23 

vf= -10.7639*f43 sq ft /sac Viscosityof Air O.OW1739 . mIs 

24 Red = =+El 9*E WIM dimensionless Reynolds No. • 

25 Pr - 0.777826 di^^nsònless-- PraMtl No. 

26 kf= :^577789-06^ BIWIr-fl-IF Thermal Conductivit;-' 

27 Red*Pr 

28 

29 

30 

32 

33 

4 

'7 

F-r 

T 

39 A =4.62!BZ4-(Jf2r.D25A.3) B 

40 Stefan 0 -0.00000000IM fllu/hr-fk^2-R^4 

41 erniss-10.65 

42 Nvrd = i-0-3f-WtT90 dimensionless 

Forced Convemion, Nusselt No. 

A3 Nund -+DR OBI M607 dimensionless Natural Convection, Nusselt No- 

44 ' Nut 0.3 + KNufd- Srj 

Combined Forced and Natural Convection, Nusselt 

45 

46 

c=0.3 

.=4 

for Horizontal -q!'!n45rfor 

Horizontal r 

4 7 Nut= dimensionless 

48 he= Btu&r-sQ.ft-*F Combied Convection be 

49 

5o 

51 Stefan B Btu/hr-R^2-R^4 

52 

emiss -O'&' 

53 

hr='=414148"OW 0Y,4,4 0 B2 + Btwbr-a.R-*F 'n Radiation CocfficieM 

54 ht- tic +hr Total HT Coefficient 

55 714m =+953+898 Bt Total HT Coefficient 

§p-ific Heat Lom_ 

58 A- °+P 4818112 forcylinder I ft long 

59 Q - -f-851-1358 Btulhr for cylinder I ft lon g 

so x.2 93071 4854 Watts fort I ft I r 

61 

62 

63 

KW for jc 

index 

ft long 

-- 

--- 

wt 


A5-632

££9-Sd 

PI AgS tt5K-d" 

_ 

N, 

i— ^..: ... S9atL0E6Z000'azbZ'aL80. L8tl-L - t'e'tot. :E98'980:E90Cs3Nt ns-= s L t'sEl."980 E80'998 :EB81S3 W(15.= SLt L8 !i 

—^-- - - _WO/tLOC6Z000'0.AZ' 0.980 99V9 = SE9Z St4 ... .... ., Slt 98 

S8'aLL 006'O:Z62'O:S90: - Ott .. ... Sit S9 

w*OlQOmzOOO-Ozvz"0.980. tUV-tBB - " _ Z9LZ tCt SLi - ._. Stt 98 

-. 99'atLOC6Z000'O.Z6Z'O.E90.Eetl ).i ". ^_ 6EBZ - CZt , ., 'OS SR E9 

UD7csa . N 58'aK0E6Z000'0.Z4Z'O.LBO. t8tl4@8 . = l• l'9.098IIL8'o80 LL0133N11 ms- = S t'S-.O90LL'J'O88L[e 1S3Nf1 Ltlftsic SZ- t8 i 

- -' S9'OlUOC62000'0.2tZ'9.980. 69tl .= 9LLC Ot- 0 

SZ. 09 

- 

'- - SWOlttM6Z000"0.ZtZ"0.6L Od6LV-- : OLOE st ost SZ- 6L 

- - - - S9atLOC6Z000' W 0,91O. 8LV'9 _ •- L

• 

• 


• Subcontractor Calculation Review Check list 

DBVS OGTS Calculations 

Subject: Off-Gas Treatment System BY-Pass Thermal Hydrau lic Analysis 

The subject document has been reviewed by the undersigned. 

The checker reviewed and verified the following items as applicable. 

Page 1 of 1 

Documents Reviewed: 145570-D-CA-056, Rev 1, By-Pass Thermal Hydraulic Analysis 

Analysis Performed By: AMEC 

• Design Input 

• Basic Assumptions 

• Approach/Design Methodology 

• Consistency with item or document suppo rted by the calculation 

• Conclusion/Results Interpretation 

• Impact on existing requirements 

Checker (printed name, signature, and date) 

Lois Payn^\`== ^^ ^7no _ ^/ 6^ 

Organizational Manager (p rinted name, signature an 

ate) 

David 1I Shuford 24 ! S/ 171Z1416 , 

A5-634

• 

• 

L J 



A5-635

145579-V-CA-004

• 

• 

CALCULATION SHEET 

M 


CAL C. No.: 145579-V-CA•004 Rev: _1 DATE: March 7, 2005 

CALC. TITLE: Off-Gas Chiller 

PROJECT NO.: 145579 PROJECTTITLE: Final DBVS Design 

Design Ve rification Required: q Yes q No 

Calculation Type: q Scoping ® Prelimina ry q Final 

Superseded by Calculation No.: q Voided 

ORIGINAL AND REVISED CALCULATIONSIANALYSIS APPROVAL 

IRM 

REV. ORIGINATOR: DATE: CHECKED: DATE: APPROVED: DATE: 

A A. Pr Iiincevk 16-Nov-04 WA WA F. Sweet 16-Nov-04 

B A. Pdjincevic 03-Dec-04 WA WA F. Sweet 15-Dec-04 

C A. Pdjincovic 20-Dec-04 S. Hamlyn 20-Dec-04 F. Sweet 20-Dec-04 

0 A. Pdjincevlo 21.Feb-05 D. Willi mson 21-Feb-05 F. Swee 21-Feb-05 

1 lu,Y ar. n o t-WtC Ib^ko5 

AFFE&ED DOCUMENTS r 

DOCUMENT NUMBER: TITLE: 

145579-V-DS-011.1 Off Gas Chiller Skid Pump Data Sheet 0 

145579-V-DS-012 Off Gas Chiller Data Sheet 2 

RECORD OF REVISION 

REV. REASON FOR REVISION: 

B Suppo rting PFD added 

C Full Process Coo li ng Calcula tion and PFD added 

0 Hand calcula ti ons done In MathCAD 

1 Changes per RCR. 

ATTACHMENTS 

DOCUMENT NUMBERAD: TITLE: 

REV. 

NO.: 

DISC, LEAD 

INITIALS 

TOTAL 

PAGES 

Attachment 1 MathCAO Off-Gas Calcula ti ons 6 

A tt 

achment 2 Drawing: F-145579.00-A-Ml (Rev. D) Full Trager Off-Gas Treatment 

d-ruler Operating) Process Flow Diagram 

1 

Attachment 3 Drawing: F-145579.00-A-0022 (Rev. OE) Full DBVS Tra ger Off-Gas 

Treatment Process Flow Diagram 

1 

Attachment 4 

Calculation 145579•V-CA-002, 'Ductwork Pressures', Rev C, Attachment 

2 Sheet 1 and 2 

2 

Attachment 5 Ch illed Water/Glycol Schematic 1 

Attachment 6 2001 ASHRAE Handbook - Fundamentals Pg 29.18-19 2 

Attachment 7 1989 ASHRAE Handbook - Fundamentals Pq 332 & 4 2 

Attachment 8 

Data sheet 145579-V-DS-12.1, Appendix A, Pg 11 .15 of 116. York 

Inte rnational Selection Data Form 150.62-EGI 'Air-Cooled Sc roll Chnlers 

Style C YCAL0014 —YCAL0134' 

5 

Attachment 9 1 AIM Heat Exchanger Catalogue, CS-STC Se ri es, Pq 41.50 10 

p.^0e;gwn ussrav R.. JAW Page t of 

A5-636



CALC. No.: 145579-V-CA-004 REV: 51—I DATE: March 7, 2005 

CALL. TM.E: Off-Gas Chiller 

PROJECT NO.: 145579 PROJECTTITLE: Final DBVS Design 

1 INTRODUCTION 

1.1 PURPOSE 

1.2 SCOPE 

amecO 

The purpose of this calculation is to determine the basis for Off-Gas Chiller cooling 

capacity and sizing and Off-Gas cooling system. 

The scope of this calculation includes analysis of the cooling requirements of the 

heat exchanging equipment located in the existing off-gas trailer, which is the part 

of the Off-Gas System shown on Process Flow Diagrams (PDF). 

1.3 DESIGN INPUTS 

• DWG F-145579-00-A-0031 Rev D, Full DBVS Traitor Off-Gas Treatment (Tri- 

Mero1 Operating) Process Flow Diagram 

• DWG F-145579-00-A-0022 Rev OE, Full DBVS Trailer Off-Gas Treatment (Full 

Flow Operation) Process Flow Diagram 

• Chilled Water/Glycol Schematic (Attachment 5) 

• Calculation 145579-V-CA-002,'Duetwork Pressures." 

1.4 CRITERIA- 

No external criteria referenced. 

2 ASSUMPTIONS 

The following assumption Is used in this calculation and within the body of the 

calculation and attachments. 

1. During the Full DBVS, and when the Tri-Meru is operating, the Off Gas 

temperature changes through wet scrubber, between stream 19 and 29. 

• ' Tri-Mere Is a registered trademark of Tri-Mer Corporation. 

-C• euChW14W?WV4:A-W4 tO.ON dwul P4 IAx Page 2 of 3 

AS-637


CAM Nos 

145579-V-CA-004 

eALC.TrrLE: Off-Gas Chiller 

PROJECT NO.: 145579 

3 


REV: F1_1 DATE: March 7, 2005 

PROJECTTITLE: Final DBVS Deslgn 

amec'0 

2. The cooling required is the capacity for sufficient heat removal in order to cool 

the air from stream #19 temperature to stream #29 temperature. 

3. Since the vendor data is not available heat exchanger is assumed to be the 

type in attachment 9 with pressure drop of 5 psi. 

4. Pipe length is to be 100ft. 

5. Static lift (elevation difference) Is to be no greater than 10ft. 

6. Chiller temperature differential Is 10•R as suggested, with engineering 

judgment (as being most common and efficient), by York International, 

Attachment 8. 

METHOD OF ANALYSIS 

Calculations were performed using a handheld calculator and later done again 

using MathCAD software. 

4 RESULTS AND CONCLUSIONS 

• Required cooling capacity is when Full Process is on: 32.25 tons 

• Selected chiller rated capacity: 40.8 tons 

• Required pump flow rate: 87.73 GPM 

• Required total dynamic head: 44.7 ft-water. 

5 REFERENCES 

1. 2001 ASHRAE Handbook —Fundamentals. 

2. York International, Form 150.62-E61 'Air-Cooled Scroll Chillers Style C 

YCAL0014 — YCAL0134','Selection Data'. 

S. 1989 ASHRAE Handbook — Fundamentals. 

4. 'CS-STC Fixed Tube Bundle/ Liquid Cooled Heat Exchangers", American 

Industrial Heat Transfer, Inc., Copyright 2004. 

C4. aa.A149MV.CA4N lo• a.4 ahU4 a« 1. Page 3 of 3 

A5-638

• 


145579-V-CA-004 

Attachment 1 

0 MathCAD Off-Gas Calculations 

0 

AS-639

• 

Calculation No. 

145579-V-CA-004 

Rev. No.1 

Calcula tion Title 

Off-Gas Ch iller Calcula tion 



Prole 

Ori9inator.-3:7r-C1 

Date:/1listh -7, D^ 

Checker: 

DateOAP p^ 

MathCAD Unit Setup: 

Due to the lack of incorperated units the following relationships must be 

specified to aid in further ana lysis. 

noJoules: 

Tonn of Heating Capacity: 

Inches of Water. 

Feet of Water. 

Flow Rate: 

• Density. 

• 

Specific Heat 

Temperature: 

Heat Capacity. 

Volume: 

Accelera tion due to Gravity. 

1. Cooling Requirement 

1.1 TRI-MER OPERATING (Attachment 2) 

- Sensible Heat, 

(Equation 22. Ch 29, Ref. 1) 

Standard Flow Rate: 

(Mass Based SCFM, Stream 29, 

Tri-Mer Opera tion, Attachment 4) 

Standard Air Density: 

W 1000joule 

Tonn:=12000 EBTU ITonn - 3.517kW 

hr 

in1120.^ 249Pa 1psi - 27.69inI120 

fiH20 = 12inII20 

3 ft3 

Dsec 

sec 

kg = 0.0624 lb 

m3 ft3 

kJ 

0.239 BTU 

kg•K = 

Ib•R 

K- I.8R 

k7 

- 0.43 BTU 

kg Ib 

gal - 0.134 ft3 

8 = 32.17 R 

sec 

qst : 8.(CA + CV•W)•QS eT 

3 3 

.S . 657 ft min- 

Qs-0.31 - 

8 := 1 .2 8 - 0.07 Ib 

m3 ft3 

A5-640 

Page 1 of 6

E Ca lculation No. 

145579-V-CA-004 

Rev. No.1 

Ca lculation Title 

Off-Gas Ch iller Calculation 

Specific Heat of Dry Air. 

Specific Heat of Vapour. 

Humidi ty Ratio: 

(H20 Mass Flow to Air Mass Flow 

Ratio from Attatchment 2 Stream 29) 

Dry Bulb Temperature Difference: 

(Between Stream 19 and Stream 29, 

Attachment 2) 

Sensible Heat 

(Equation 22, Ch 29, Ref. 1) 

• - Latent Heat: 

(Equa ti 

on 24, Ch 29, Ref 1) 

Change in Humidy Ratio: 

(Diffe rence of H2O Mass Flow in 

s tream 29 to stream 19 over Air 

Mass Flow, A ttatchment 2) 



qst `47.07kW 

qlt:= S•Aq•QS AW 

Orlginator:L t+^ 

Date: I4olc^,, a^ 

Checker: 

Date: p I yo-. pS 

CA := 1.006 CA = 024 M 

kg•K1b•R 

CV := 1.84-1l - CV - 0.44 8721 

kg•K Ib•R 

W:= 53 

2891 

W=0.018 

AT:=(304 - 85)R AT-219R 

qst := S• ( CA + CV-W)-QS-AT 

AW 53_7 

:m 

2897 

Approximate heat content of 50%RN Aq := 2500 kJ 

less heat content of the water at kg 

condensate temperature 

(Standard Condi tions) 

Latent Heat qlt:= S•Aq•Qs•AW 

(Equation 24, Ch 29, Ref 1) 

qst = 1338Tonn 

AW = 0.016 

Aq =1074.81 BTU 

lb 

qlt =14.77kW qlt= 42Tonn 

-Total Cooling: Tri-mer Operating qtot tri :- qst+qlt gtott ri -61.84kW 

1.2 FULL PROCESS (Attachment 3) 

- Sensible Heat 

• (Equa ti 

on 22, Ch 29, Ref. 1) 

Standard Flow: 

(Mass Based SCFM, Full Flow, 

qsf:- S•(CA + CV W) . QS AT 

gtottri = 17.58Tonn 

ft3 3 

Qs:=2874 —Qs-1356 m — 

min sec 

A5-641 

Page 2 of 6

• 

is 


145579-V-CA-004 

Rev. No.1 

Calculation Title 

O ff-Gas Chiller Ca lculation 

Because 

q:oifull>gtottri 

2. Equipment Selection 



glotyi = 17.58Tonn 

gtotfull . 3225Tonn 

qrequired := glolfull 

qrequired = 3225Tonn 

Originator 

Date:"? °s 

Checker. 

Date: O'( IykV 0 

York air cooled scroll chiller will be selected to cool p ropylene glycoVwater 50% by weight solution, with 

freezing point of -25 F. 

Selection: 

Type: YCAL0042EC 

Rated Capacity. 40.8 Tonn 

Input Power. 57 kW 

Equipment selec ti 

on, performance data and correc ti 

on factors a re per 

"York Inte rnational- Form 150.62-E61 'Selection Data' 

-Capacity Correction for Proplyene: 

Qrated:= 40.8Tonn Pinput:' 57kW 

Efficiency. Eff = ON Eff ^. 0.928 (50"1") 

KW 

Q:= Qraad•Eff Q=37.86Tonn 

Input Power. KW :- qrt Q P• mput' Eff 

Q 

-Flow Through Chiller (Coo li 

ng Fluid) 

KW = 45.06kW 

GPM formula: 

(Ref 2) 

grequimd' GF 

GPM z 

AT 

GPM FITON Factor. 

(Ref 2) 

PI . R 

GF:= 272 

min Tonn 

Page 4 

• Temperatu re Range: 

(Assumption 6) 

&T:= I OR Temperature range is selected as sugested, 

with enginee ri 

ng judgement (as being most 

common and efficient), by "York 

A5-643

0 NisE 


145579-V-CA-004 

Rev. No.1 

Calculation Title 

Off-Gas Chiller Calculation 

3. Pump Selection Calculation 



Origlnatoc 

D ate: 7r^ yyb!>1 

^(x'05 

Checker: A 

Date: 0.1 t-t brit, 05 

grequired'OF Intemationar'Selection Data'. 

GPM 

:_ 

AT 

GPM = 87.73 gal 

min 

OH-Gas Chiller Calculation (145579-V-CA- 004) to be Revised 

3.1 PROPLYENE GLYCOL PRESSURE DROP CORRECTION FACTOR 

50% by weight mixtu re 

Cooler Pressu re Drop Correc ti 

on 

Factor for P ropyene Glyco l/Water. 

• (Data Sheet 145579-V-DS-12.1, 

Appendix A, Page l 1 of 116.) 

3.2 EQUIPMENT PRESSURE LOSS 

32.1 Cooler Pressu re Drop 

Flow Rate: 

(From Section 2 of this calculation) 

Pressu re Drop: 

(From Cooler Cu rves, Pg 14 of 114) 

Cooler Pressure Drop (factored): 

APf := 1.247 

GPM - 87.73 gal 

min 

AP := 6.5ftI120 

32.2 Scrubber #1- Heat Exchanger P ressu re Drop 

Scrubber Pressu re Drop: AP-- 5psi 


Heat Exchanger P ressu re Drop: APh ex = AP•APf 

(Conse rvative Approach,eonected 

- for propyene glyco l) 

3.3 PIPING AND VALVES 

V2 

Head Loss: AHI 5 k. 

• (ASHRAE Fundamentals) 2.8 

Table 2 - K factors for welded pipe fittings: 

(2001 ASHRAE Fundamentals Handbook) 

Pipe Diameter. Dx 3in 

AFcooler = AP'APf APeoo1R = 8.11=0 

A5-644 

AP- 11.54 11112O 

Aphex ° 1439ftH2O 

Page 5 of 6

0 

\J 

• 


- ^(q 

Project Number. 145579 

amFr'C" 


Page 6 of 6 

Origi Date* ^GO 

Calcula tion No. 

Date: /►9eY c^n`l, o S 

145579-V-CA-004 

Checker. 

Rev. No. 1 

Date: O H 1t20s 

Calculation TiUe 

Off-Gas Ch iller Calcula ti 

on 

90 deg Elbow: 

keib : 34 

Globe Valve: 

kglobe = 7 

Swing Check Valve: kswing = 2.0 

Pipes & valves are s ized as per guidlines in Ch. 35 'Pipe Sizing' of 2001 ASHRAE. 

Volume Flow Rate: GPM = 87.73 gal 

min 

Flow Velocity. V .^ 4-GPM 

Sum of k factors: 

Head Loss: 

Pipe Losses: 

(1989 ASHRAE Fundamentals 

Handbook, Pg 33.4, Fig 16.1) 

Pipe Length: 


Pipe Loss: 

Total Pipe & Fit ting Losses: 

Total Required Static Head: 

Heat exchanger may be 

elevated up to 10 tL 


Total Requi red Head: 

V = 3.98 ft 

WrD sec 

Fittings & Valves (Attachment 51 

10 x 90 deg ree Elbows 

4 x Globe valves 

4 x Swinging Check Valves 

k:= 10•kelb+4'kglobe + 4'1swing 

All, = k• ^ AH, = 9.71 R 

2.8 

HPiPe 

k=39A 

2Sft (For commercial pipe, Sch 40) 

looft 

Lpipe = looft 

A112 Hpipe'Lpipe 

AH2 2SR 

AHIgss _ AH l 

doss ° 34.7 ft 

llatatic} loft 

All loss + llstatic 

Ai-1--4 -447 4- R 

A5-645 

+ AH2 + (Aphex + APeooler)' ft 

M120

0 

0 


145579-V-CA-004 

Attachment 2 

• F-145579-00-A-0031 

Full Trailer Off-Gas Treatment (Tri-Mer Operating) 

Process Flew Diagram 

A5-646

7 

0 


145579-V-CA-004 

Attachment 3 

F-145579-00-A-0022 

Full DBVS Trailer Off-Gas Treatment 

Process Flow Diagram 

A5-648

• 

0 


145579 -V-CA-004 

Attachment 4 

Calculation 145579-V-CA-002 

Full DBVS Ductwork Pressures 

Attachment 2, Sheet 1 &2 

A5-650

• 

11 

0 

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RPP-24544 REV 1 d 

145579-V-CA-004 

Attachment 5 

Chilled Water/Glycol Schematic

• 


CHILLED WATER/GLYCOL SCHEMATIC 

----------------- --------- 

I I I 

I I oo I 

I 

,. I I 

30 

I I 

I I I 

I 

I P 

PUMP 

NO I CHILLER 

I 

I 

j 36—D61-058 

36—D-58-056 — 

I NO --- NO r — 

--------------1---------- 

CHILLED WATER RETURN 

, I 

I NO 

I SCRUBBER #1 

I 36—D30-076 

I 

I I 

I I 

, I 

I NC 

SCRUBBER #2 

36—D30-047 

I 73"0 

I I 

NC I 

SCRUBBER I 

NO CONDENSER I 

I 36—D10-040 1 

i NC I 

L----------------------------- J 

WET SCRUBBER SKID 

Attachment: #5 

Calc. NO.: 145579—V—CA-004 

Rev No. 1 

Sheet: 1 of 1 

SKETCH IS BASED ON MID: 

F-145579-36—A-100 

F-145579-36—A-101 

F-145579-36—A-102 

F-145579-36—A X106 

Originator: -T.AA Wl^ I Checked By: f9• o 

Date: - -7 Maid\ ?.mom f Date: 07HA-e of 

A5-654 

I

0 


145579-V-CA-004 

Attachment 6 

2001 ASHRAE Fundamentals Handbook 

0 Pg 29.18-19 

0 

A5-655

• 

s 

29.18 


• HEAT GAIN THROUGIIrf UORSURFACES 

• 

I a space with a din. 

Attachment: 6 separa ti ngphysical 

Cale. No.: 145579-V-CA-004 ue It given by 

+ Rev. No: 1 (20) 

Sheet 1 of 2 

Originals: 

Date: lti 

Checked by - 

adjacent and 

. t Date: O`Ttf&R_6S -u, Tempera turerb 

a Idtrhes or boiler 

above the outdoor 

g spaces should be 

wn except that the 

• I contains no beat 

rat Baia rb-4 may 

rdoor air and con- 

• _,__ ^^ ê•—.-_^ -.anus 3 l(. In some 

t^ the air temperature In the adjacent apace wi ll eovespood to 

• the outdoor air tmperahe or higher. 

Floors 

For floors directly In contact with the g round or over an undaground 

baseme nt that is add= ven tilated nor conditioned, beat 

ttansfet may be neglected for cooling lad estimates. 

INFILTRATION AND VENTILATION 11EAT GA IN 

Vent il 

ation 

Outdoor air must be int roduced to ventilate conditioned spaces. 

Chapter 26 suggests minimum outdoor air requdnmeius for reprotenta 

tive applications• but the minimum levels am not necessarily 

adequate for all psychological attitudes and physiologi cal respouses. 

When maximum economy in space and load Is essen tial, 

as in subma ri ne& oromer re stricted spsoes, as little is OS Us of outdoor 

air per person an be suBlelect, p rovided that recirculated air 

Is adequately decontaminated (Consoluio and Pe cora 1944 

Local codes and ordinances frequeady spe ci fy ven tilation 

requirements 

for pub lic places and for Industrial Insta llations. For 

exa mple. minimuum requirements for Ufa practice in besot&' open- 

• Ming rooms arc given in NFPA $Wndard 99. Although 100% out- 

. door air is sometimes used In operating rooms, this s tandard does 

not *ulm I% and limiting the Outdoor air to 6 to 8 changes per how 

. is finding Increasing aoaptence. 

ASIMAE Srmrdord 62 moommeods m(Olo am v entilation ra tes 

for most common applications. For bed applica ti ons. ncb ss 

office, 101.1s per peasou B suggested. 

. Vent ilation air is annua lly introduced at the air-conditioning 

apparatus rather man direc tl 

y into the conditioned Rum and thus 

becomes a cooling Coll load componeraimtead of & spaceload compomrnt• 

Calculationsfaestimating this *again am discussed W ct 

inthe section on Beat Gain Calculations; Using Standard Air Values. 

Reducing her gain from Outdoor star by using filmed reciteu- 

^c 

2001 ASHRAE Fundamentals Handbook (SI) 

the Cooling &coo n. infiltration CsJcub ms ate usually limited b 

doors and windows. Air leakage through doors an be estimated 

using the informa ti on in Chapter 26. Tab le 3 in Chapter 26, 

adju sted for the average wind velocity in the loca lity, may be used 

to compute in filtra tion for window s. In calculating window lac. 

tra tion for an entire suucutm, the tuW window area on a ll side$ of 

the bu il 

ding B not Involved since wind does not act on a ll 

tides 

simttha0eously. In any ease. infiltration from all windows in any 

two adjacent wa ll 

exposures should be included. A 1mowtedge of 

the preva iling wind d irection and velocity is betpfid to selecting 

expOsuses. 

When ecoaonica lly feasibl e, sufficient outdo or air should be 

int ro duced as ven tilation air through the air-condidaaing equipment 

to maintain a constant outward escape of air and thus elimina te the 

infiltratrom por ti on of the gain. The press ure maintained must bvm 

come wind pressure th rough cracks and door ope0lags• When the 

quantity of outside air introduced through the cooling equipm en t is 

00 suffidMt to n the required press= to el imina te infdha• 

lion, the entire infiltra tion load should be included in the space beat 

gain calculations. 

Standard Ali Volumes 

Because the apeeifie volume of air v ades appreciably, alcula• 

lions are more accurate when made on the basis of air mass inst ead 

of volume. However, volume valu es am often requ ired for seloction 

of coils, fans, ducts, etc., in which cases volume valu es based on 

meacumeot at standard condi tions may be used for rxvnte 

results. One standard value Is 12 kg (dry airyms (0.833 nalk4l. 

This deadly co rr esponds to about 16°C at sa turati on and 21 0C dri 

air (at 101325 kPa)_ Beca use air usua ll 

y panes through the coils, 

fans, ducts, em, at a density dose to s ta ndard, the accuracy dcsbW 

norma lly requires no correc ti on. When sirflow is to be me as u re d at 

a particular condi tion orpoio% such as at a coil entrance orcxlG Ibe 

corresponding specific volume can be read from she psychromeaic 

chart. 

Fsample•3. Stand ar d air calculation. Assume outdoor air at suodaa 

condi tions Is Bowleg at 10 mrla. Wbat Is the 1 1 us we when the Wdoor 

sir in at 35'Cdry-butt and 24'C wet-bulb (0.193 msAg)7 

Solution: The measured rate at that cond i tion sbould be 10 

(0.8919.133) -10.7 m31s. 

Heat Gain Calculations Using Standard Air Valu es 

Alt conditioning design often requires calcula tion of the 

fo ll 

owing. 

1. TOW beat 

Total heat Baia 4r eonespoading to the change pf a given saadatd 

flow rate 0, through an enthalpy, d$'ereaadh is 

where air density. 12 kgW. 

2. Sensible beat 

4r.12Q^h 

Sendbb beat gain ga earapoodmg to the change of dry -b%* 

umpctatme ,U for given aullow (shdad coo&bons) Q is : a 

4.=12(1.006+1.84W)Z& 

d Iced air In combiorion with outdo or air'shoAd be consid ered. 

where 

L006 . spod& bus 0(&y akIsl/(kg•&) 

W. bomkity redo, it Redmoiated air can also be hated to costnal odor (see 

lnflltrat(on 

$(waeryag(*)-' 

1.84. specific beat of watifvVoc kIA4-lii) :eta 

The specific heats wefor& range front about 73 so90°Cp 

The p rinciples of estimating In filtra tion in buildiogs, with 

emphasis on the bating season, am discussed in Chapter 26. For 

W- 0,tbevalueofl20(IA06+1.84W)=1 21;whcnW-M0l 

value is 123; wh en 8'. 0.02, the value Is I25; ad wben W,i 

Chapter ^. 

' 

13 

of th4 volume and Cbapta 44 of the 1999 ASHRAE lfmdbook- 

Apparadoet). 

A5-656 

I

RPP-24544 REV 1 d 

0 Nonresidgnt(al Cooling and Heating Load Calculation Procedures 29.19 

• 

0 

the value is 117. B ecause a value of W-0.01 approximates coodl 

• found in many sk-conditioning problems..tbe sensible bat-6oru 

change (in q') can normally be found as 

3. ;Latent but 

q, = 1 .2iO & 

(23) 

Latent heat On qt co rr esponding to the change of humi dity ra ti o 

AW for given airflow (standard conditions) 0, is 

qn=1.20x25000AW-3010OAW . (7A) 

where 2500 is the approximate beat content of 50%rfi wpm at 246C 

less the he at content of water at 1 OZC 50%rb at 24iCis a common 

design condi tion for the space, grid 10 •C is tiormil condensate tempetamne 

from cooling and dchumid*Ing coils 

The cons ta nts 120,1.23. aod3010 are useful in air-condi tioning 

calculations at sea (101325 kN) and for normal tempera tures 

and sttoimre radon..For oth er condi tions, more precise values 

sbculdbe used For an al titude of 1500 m (81336 kPa), approprine 

viiSu arc 1.00.1.03, and 2500. 

LATENT HEAT GALS] FROM MOISTURE 

THROUGH PERMEABLE BUILDING MATERIALS 

Tho diffusi on ofmoisture through all commonbu ildingmaterials 

is aoaturd phenom enon that b always present Chapters 23 and 24 

cover the principl es and specific methods used to control moisture. 

boisture 11203for through walls is often neglected in the usual comfort 

sir•coudidorag application beauu the actual rate is quite 

aman and the corr esponding latent bat grin is lnslgnificanL The 

permeability and permes oce values for vatious bu il 

ding materials 

are given in Table 9, Cha pter 25. Vapor retarders are frequently 

InsWled to keep moisture transfer id a minimum. 

Certain indust rial applicatio ns call for a low moisture content in 

betaaintamed in a conditioned space. In s uch cases. the lat es t beat 

Sim accompanying mois ture t ransfer through walla maybe grater 

abuts any oth er Latent but gain. This gain is computed by 

qT a UAAp.(ha - ht^ (25) 

Worm 

6 . bunt beat gai o, W 

N . pemwsea of wall assembly, ap/(a•mr•F&) 

A . wow sf 64II surfaM ma 

dip.. reps presses diffe reaee. Ia 

ly.aotbalpy Ytawnetndidoer, klhg . 

ly w mdralpy of won eondawed at cooling sill khkg 

. 2500 kbks wban room bmpawre is 24-C and eoadeosate off 

=3 Is lore 

HEAT GAIN FROM 

MISCELLANEOUS SOURCES 

7be calculation of the cooling load is affe cted by so& fa ctors as 

(1) type of HVAC system, (2) e(fect(veneas of hat exehaoge sum 

h014 (3) he Incaution, (4) dad beat On cc long. (5) d oes lalsM 

(b1hatexpeaction ggheiog systems, m type of mtmn air syumn. 

bated u sequeam of bodfividuîl psychometric p^maamiems. The 

1009 stawarword method fist defines all ]mown (or deshed) 

ante points on a psye3sg i6euk chart. Nex4 the actual craning and 

11"g dry-nod wet-brills condi ti ons we calculated for such coml'osents 

as the cooling and/or hinting toils (based on tone or space 

k0 l. rise mount of outside aQ Introduced Into the system duough 

69 equipment, and the amount of heat gain or loss at various poiota. 

the space conditions 

W sought can acNellybe met bythe tdesigned dd 

aiat &Ilientbleandlatenthat changes to the acres ktnvels from 

the space condi tions through the moue, air system and equipment 

back to the conditioned specs If the designee successful (i.e.,within 

the degree ofeDmctness of the various design a ssump tions),appro• 

priste equipment componen ts can siWy be selected. If not, the 

designer must judge it the resul ts will be *ckse enough- so satisfy 

the needs of de p roje ct. or if one Of »sutopdom and/ordes(gn 

criteria must first be modi fied and the calcula ti ons rerm. ' 

Heat Gain from Faro 

Fans th at circulate air through HVAC systems add energy to 

systemby one or an of the following processes: 

• Tempera ture; rise in the airstream from fan ioeMclency. 

Depending on the equipment, fan effi ciencies generally range 

between 50 and 70%, with an average v alue of 65%. Thus, some 

35% of the energy required by the fan appears as i nsumaneau 

bat gam to the air being transpor ied. 

• Temperature rise in de airstream as a consequen ce of air &uric 

and velocity pressure. Tbc "useful" 65% of the total fan en ergy 

that creates press ur e to move airsprads out throughout the en tire 

air transport system In the process of conversion to sensible bat. 

Desiguets commonly assume that •lhe temperatre change 

equivalent of this bat oc curs at a single point in the system, 

depending on fan location as noted below. 

• Temperature rise from heat gene ra ted by motor and drive 

inefriciencim The relatively small gains from fan motors and 

driv es am normally diuegardod un le ss die mot or andlor drive are 

physically lo ca ted within the condi tioned sirstremo. Equatio ns 

(/). (3), and (9) may be used to estimate bat gales from typical 

motors. Bete drive losses a amoften 

estimated a 3% of the motor 

power rating. Convenion to temperatu re rise is calculated by 

Equation (26). 

The locati on of each fan rela ti ve b other elem ents (primarily ti c 

cooling cols) and the type of system (e.g. single zone, multlw e, 

double -duct, terminal rebea4 VAV), along with the concept of 

equipment enntrol (space temperature alone, space tempeV2r= an d 

relative humidity' etc), must be ]mown befo re the analysis can be 

complete&A fan located upstream of the too li ng coil (blowtbrough 

supply far , return air ho, ou tside air adds the beat equivalent of 

its Inefficiency to the sintaeamat that point: thus, a s li 

ghtly elevated 

en 

tering dry-butt temperature to the cooling toil mots A fan 

located downsre m of the cooling coil r aise s the dry-bulb temper` 

atum of eirleaving the cooling coil.This rise can offset by seduc- 

Ing the coding curl temperature a. alte rn atively, by in cr easing 

airflow across the cooling co il u long as i ts impact on spare eomdidous 

is consid ered. 

Attachment: 6 bjected to rig . 

Cala No.: 145579-V-CA-004 pply duct sys- 

Rev. No.: 

1 

oteibodry^hdlb 

an 

Sheet 2 of 2 oquivakot 

Originator :1^y 

Date: m o S 'ply ducts L a 

Checked by. y and must be 

Date: NMZAS my our temper` 

L Inward lak- 

-Ity va ri 

ations. 

A5-657 

mces due to the 

Chapier34bas 

I our leak tunes 

•egrdpment and 

i

• 

0 


145579-V-CA-004 

Attachment 7 

1989 ASHRAE Fundamentals Handbook 

Pg33.2&4 

A5-658

C 

g 

41 

N 

O 

2 


33.4 1989 Fundamentals Handbook 

Attachment 

7 

it indBow an 

and Bowman 

Calc. No.: 145579-V-CA-004 to mew pipe. 

Rev. No.: 1 mt'âm'- 

IS loM %for 

Sheet 1 of 2 rms. Carrier 

.craw friction 

Originator. 

Date: flngirL. o 

athemnosive 

nrdeonrdrded 

Checked by. 

Date: MlefdLOS 

ad stod. 1101d.' 

kr.0941) and 

csor cold and 

l0 657a Aged 

• (1983) recomunco 

ted cast 

r concrete 

xiskin is Doi a 

• red fn Europe . 

. ' i ft303ears . 

Extensive age-related flow da ta am available for use with the 

Hazen-WObiams emp irical equa tio n. Di fficulties arise in its cup. 

p liatiott. however, bemuse the original Harm Wfl0ars rough 

mess coefficients am valid only for the spe ci fic pipe diameters, 

water velocities, and water viscosities u sed In the original expetfinents. 

Thus, when the Cs amextrnded to dif(crentd ameAM 

wlocides, and/or w2terviscoside4 errors of up to about 5074 in 

pipe capa city can o ccur (Williams and Haan 1933, Sanks 1974 

Water Hammer 

When any moving nuid (not just water) is abrup tly s topped as 

when a vale closes suddenly, l arge pressures cis a develop. While 

deta iled analysis requires knowledge of the elastic p roper ties of 

the pipe and the now-t)me h istory, the limiting case of rigid pipe 

and instantadeous cl osure Is simple to calculate. Under these 

conditions, 

where 

Pa - 0cr ry& (9) 

Pa i. pressure rise caused by waxer hummer, to^r 

& Auld demity, lb./ft) 

y Q - wlo city of sound in the fluid, h/s 

V - fluid now w3oft DA . 

e, for'riater is 4720 ft/s, although the el as ticity of the pipe 

redrfs 

tss the effective value. 

Ftara0e3. What is the maximum pressure rise If water ttowiog at 10 

•. fds is stopped Instantaneou sly? 

Sofuttac pa - 624 x 4720 sc 10/322 - 91468lb/fts 

- 635 psi 

Other Con si derations 

Notdisaussed Inlletan In this ehapte; butof potentia ll y great 

f nporamareanumberofphysfcalwOdreWaleorai kmtionse 

pipe and fitting design, materials, andMr sing methods must be 

appropriate forwvrkingpr essures and temperatures encountered, 

as well as b eing suftablyresistant tochemricalattackby the fluid. 

Other Piping Materials and Fluids 

For fluids not Ineluded •itt this ehaptsxor for piping materials 

of tfrftetent dimensions, manufacturer's literature frequently supp 

lies pressure drop charts The Darcy-Weisbadt equation and the 

Moody chart or the Coleb rook equation can be used as to alta. 

na ti ve to pressure drop charts or tables 

HOT AND CHMLED WATER PIPE SIZING 

The DavyWcisbach equation with friction factors from the 

Moody diart or Colebrook equation (o; ahernadv ft theHazeo-, 

Williams equa tion) ii fundamen tal to ealculadrig press ur e d rop 

in hot and ch illed water piping; however, ch arts calculated f ro m 

these equations (such as Figures 1, 2, and 3) provide easy deter 

rops for specific fluids and pipe stiadards, 

-mination ofpmssum d 

In addition, tables of pressu re d rops can be found in Hydrau li c 

Institute (1979) and Crane Co. (1976). 

Most tables and cha rts for water are calculated for p roperties 

at 60'P. Using these for hot water int roduces some error. although 

the answers am conservative !A. cold water cale-watious overswe 

the pressure d rop for hot water. Using 60T water charts for 200T 

water should not result in er rors in Ap exceeding 200/c 

Range of Usage of Pressu re Drop Charts 

General D esig n.Range.The general range orpjpe friction bss 

used for design of hydronicsystems h between I and 411/100 n. 

A valueor2.5 ft/100 It represen ts themean towhkh most systems ms 

am designed Wideraanges maybe used 14 specific d esigns, if certain 

precau tions are taken. 

Piping Notsa Closed loophydronic system piping Is genera ll y 

sized belowartai rs arbitrary upper Omit%such as a WWty limit 

• of fpsfor2-Itupfpeandunde, and apressumdrop Omhof 4 ft 

FLOW RATE, U.S. gallmin 

11g.) Fddion Loss for War In CoumercW Stee Pipe (Schedule 40) 

AS-659 

q: 

i

2I 1 


Tablet 8 Factors-73ra6ea npc jp ruoss 

Nemieel 5W -W lwwg- Swing MR 

ripe Suodud Radlut 4S Retura Tee- Te-- Globe Cate Angle Check Mouth Squ are Pre)eeted 

Dta.,us Elbow Eibaw, EOww Bend I3u Bade Valve Val" Valve Valve Inlet LIH Lad 

10 

IS 

20 

25 

32 

40 

30 

65 

s0 

100 

23 

21 

1.7 

13 

13 

12 

ID 

0.69 

0.80 

0.70 

- 

- 

0.92 

0.78 

0.65 

034 

0.42 

035 

031 

024 

038 

037 

035 

034 

037 

• 032 

031 

030 

029 

028 

23 

2.1 

1.7 

13 

13 

12 

1.0 

015 

090 

0.70 

0.90 

0.90 

0.90 

0.90 

090 

090 

0.90 

090 

0.90 

0.90 

27 

24 

21 

1.8 

1.7 

1.6 

1.4 

13 

12 

1.1 

20 

14 

10 

9 

173 

8 

7 

63 

6 

5.7 

M40 

033 

028 

024 

0.22 

0.19 

0. 17 

0. 16 

'0.14 

0.12 

• 

- 

- 

6.1 

44 

3.6 

23 

21 

1.6 

13 

1.0 

8.0 0p5 

M 0M 

3.7 0.05 

3.0 0.05 

27 0.05 

25 0M 

23 . 0p5 

22 0.05 

21'4 0.05 

20 • 0p5 

OS 

OS 

0.5 

03 

OS 

03 

OS 

0.5 

OS 

OS 

1p 

1 .0 

1 10 

1.0 

Ip 

Ip 

1.0 

1.0 

LO 

Ip 

swor.Larb- aq D- Dom (HY&-0e kvditw 1919). 

Tabk 2 YFadors--Flanged Welded Pipe Fit tings 

Nomlad NI• WIwog• 4S*Laog• Retool Retorts Swing 

• Pipe Standard Radius Radius Bead Bred Lee&- Tee• Ike- Globe Cate Angk Deck 

INa.,sm Elbow Elbow Elbow Standard Radius Line Branch Val" Val" Val" Valve 

25 0.43 MI 0.22 0.43 0.43 02 6 • Ip 13 - 4.8 2.0 

32 0.11 037 0.22 0.41 038 0.25 093 12 - 3.7 2.0 

40 

So 

65 

0.40 

038 

035• ' 

035 

030 

0.28 

021 

020 

0.19 

0.40 

038 

033 

CM 

030 

017 

0.23 

020 

0.18 

090 

0.9 4 

0.79 

10 

9 

8 

- 

034 

027 

3.0 

25 

23 

20 

20 

20 

M 034 015 0.18 034 025 0.17 0.76 7 022 22 2p 

100 031 0.22 0.18 

150 029 0.18 0. 17 

• 200 027 0.16 0.17 

250 025 0.14 0.16 

300 0.24 0.13 0.16 

Sweelsdexere^g fMra Dock (lt1'IbNtiL f0arkuu 1979k 

031 

029 

027 

023 

024 

022 

OAS 

0.43 

0. 14 

0.13 

0.15 

all 

0. 10 

0.09 

on 

0.70 

Ob2 

O38 

033 

050 

65 

6 

5.7 

5.7 

5.7 

0.16 

0. 10 

048 

0.06 

0.05 

_ 

7.1 

2.1 • 

21 

21 

21 

20 

20 

20 

20 

2.0 

9T Elbow 

45' Elbow 

Rumen bend 

(1801) 

Regular meaded 

Long &u drudcd 

Regular 5langed 

Long-ndia Ranged 

Regular dreaded 

Long-ra&u 0mgW 

Regd ar Welled 

Regular flanged 

Loograd'nuflmged • 

T0ble3 Appmdmate RaageofVatiatioaforg FOdon 

*20% above 50m Ike Threaded, gee or branch 

*4096 below So 

Flangedflneurkmch 

225% 

Globe valve TDaeaded 

*35% 

Flanged 

*30% 

Gate v alve Tbrnded 

*10% 

Flanged 

*10% Angle v alve Threaded 

*25% 

Flanged 

*35% 

t3•eck v alve Threaded 

*70'b 

Fanged 

TSble 4 Comparbou of KFadon f ro m Ralase7er (19990) with Prevlow Releteece Data for Elbows 

-- - Rahmeltr Valoes 

*25% 

235% 

*25% 

*25% 

*25% 

*50% 

320x. 

250°a -- 

250% 

,200% 

-80% 

Provkus IULs Vales 0.6 m/a L2 MIS 24 n/a 

50 m st and .14 elbow (Uucadcd) 030 a I p (Ip) 034 0.6 OL8 

100® lmg-udius elbow(w*Med) 022 to 024 MM) 0M 026 024 

100 mm anMard elbow (welded) . 031 10 034 0.40 037 034 

30 asmaedod0ge0»w(50x4 6) (&m%deM - 0.76 0.81 027 

50 vus erpa06ng e lbow (40 x 5% ( kudeD - 0.65 039 054 

loom reducing elbow (101) x 80)(welded) - 0.72 037 0.45 

100 kam ap0ed'mg elbow (80 x 100) (Welded) - 0.28 0.28 027 

50 tons se I(SOx40)(tres" - 099 637 029 

50 me eapamko(40 x A(dnaded) - 020 0.16 0.13 

100 m sedum (100 x"(vowed) 022 0.40 023 0.14 

100 m 4ryaadm (8 1) x 100) (wel" - 0.17 0.11 0.11 

•netan letnooe rs Fteeanm (19lq a,e. Ca (14161, d Hydrm&LmO+e 09791 NmMe In a rehonlable 1 d716N 2, Moe 

Attachment7 t 

Ca 1c. No.: 145579-V-CA-004 

Rev. No.: 1 

'Sheet 2 of 2 

Originator. •W 

Date: S- 

Checked by: 

Date: n ^Q ; 

50n 

50M 

50 on 

100, 

100: 

too 

$00 

501 

$01 

100 

IT 

IOf 

rpm 

En' 

din 

spe 

w)

11 

0 


145579 -V-CA-004 

Attachment 8 

Data sheet 145579-V-DS-12.1, 

Appendix A, Pg 11-15 of 1169 

York International 

Air-Cooled Scroll Chillers 

Style C YCAL0014 — YCAL0134 

Selection Data 

Form 150.62-EG1 

A5-661

• 

N 

Selection Data 

• O 

l0 Y 

S 

Ya 

co > ^- o 

rn 

ti 

U) 

r^ 

L 

Z 

O 

0 0 0M 

OOUC] 

E 2 

' cS 

ul 

Z 

• ¢Utry 

GUIDE TO SELECTION 


Capa city ratings forYORKYCAL Packaged Air-Cooled 

Liquid Chi llers • shown on pages 16 th rough 39 cover 

the major ity of design applica ti ons for these units. For 

unusual applications or uses beyond the scope of this 

catalog, please consult your nearest YORK Office' or 

representative. 

SELECTION RULES 

1. Ratings - Ra ti ngs may be interpolated, but must 

not be extrapolated. The Ra ti ngs given on pages 16 

through 39 and the DESIGN PARAMETERS given 

on page 11 indicate the li mits of app li ca ti on for these 

chille rs . 

2. Cooler Water-Ra ti ngs are based upon 2.4 GPM 

per ton which Is equal to a 10 0 17 chilled water range 

and a 0.0001 fouling factor for the cooler at sea level. 

Tables on pages 16 through 39 give capacity, compressor 

kW required, cooler GPM and unit EER 

3. Condenser-Ratings are given in terms of air on 

condenser In deg rees Fahrenhei t. 

4. Copper Fin Condenser Ratings - Sin ce thethermal 

conduc ti vi ty of copper Is sligh tly higher than 

aluminum, app ly the following correc ti ons to the 

standard ra ti ngs. Tons x 0.97 and comp ressor kW 

x 0.99. 

5. Performance Data Correction Facto rs - Ra ti ngs 

are based on 0.0001 cooler fou li ng factor, 10'F 

chil led water range and at sea level. For opera ti on 

at diffe rent conditions, apply the app ropriate correction 

factor from the following table. 

ALTITUDE 

SEALEVEL 

20 Ft 

4000 FT. 

sDOO FE 

FOUL0IG FACTOR 

0.0001 0.00025 

TEMP 

SPLIT 

TONS 

COMDR 

kW 

TONS COMPR 

kW 

a 0.994 0.999 0.991 0990 

10 1.000 1.000 0.993 0.999 

12 LOOS 1.001 0.999 0.999 

14 1.000 1.002 1.005 1.000 

S 0.990 1.010 0.904 1.OD9 

10 0.995 1.010 0.990 1.009 

12 0.999 1 1.0 11 0.995 1.010 

14 1.004 1.015 0.998 1.011 

a 0.903 1.021 0.977 1.020 

10 0390 1.024 0393 1.021 

12 0.994 1.025 0" 1.024 

14 0.997 1.026 0.993 1.025 

8 0.978 1.035 0.973 1.084 

10 05112 1.037 0.978 1.035 

12 0.987 1.037 0380 I 1336 

r-1-4-T 0392 1.030 0906 I 1.037 

FORM 150.62-EG1 

6. Ethylene Glycol Correction Factors - The following 

factors are to be applied to the standard 

ra ti ngs for un it s cooling ethylene glycol. 

ETHYLENE GLYCOL 

%WEIGHT TOWS COMPR GPM'FiTDN PDRSOP FREEZE PT 

10 0.965 0.997 24.1 1.034 26 

20 0.961 0.996 24.9 1.062 16 

SO 0.974 0.995 26.1 1.096 5 

40 0.966 0.991 27.5 1.134 40 

SO 0.957 0969 29.1 1.172 .12 

7. Propylene Glycol Correction Facto rs - The fol. 

lowing factors are to be applied to the standard 

ra ti ngs for units cooling propylene glycol. 

PROPYLENE GLYCOL 

PRESS 

O 

%WEIGHT T OWS COMPR GPM'FITON FREEZE PT 

10 0.983 0.996 24.2 1.048 27 

20 0.974 0.995 24A 1.086 19 

30 0.961 0.990 25.1 1.134 8 

40 0.948 0.98 26.0 1.186 5 

50 0.928 0984 Z72 1.247 •25 

METHOD OF SELECTION 

To select of YORK Packaged Air-Cooled Liquid Chiller, 

the following data must be known: 

1. Design Capacity In tors refrigera tion (TR). 

2. Entering and Leaving Liquid Temperatu res. 

3. Outside ambient air temperature in deg rees F. 

4. GPM of chM cl li quid. 

Determine capa city requirements from the following 

form ul a: 

TRx24 

GPM 

RANGE ('F7 

EXAMPLE - WATER CHILLING 

1. GIVEN: Provldeacapad ty ofSOTcnsat42'Fleav 

Ing water 10 4F range, 0.0001FF 80'F alr on the 

condenser, at sea level and 60 Hz. 

2. FIND: Unit Size 

Compressor kW Input 

YORK INTERIUMO AI 145579-V-DS-12.1, AppendixA 11 

Page 11 of 116 

AS-662

W 

• 

• 

3. From the Ratings on pages 16 - 46: 

SELECT. YCAL0050 (Eng lish Units) 

53.1 Tons 

48.7 Compressor kW 

11.7 Unit EER 

4. Calculate Comp ressor kW at 50 Tons: 

kW = 50 x 48.7kW = 45.9kW 

53.1 

5. Calculate GPM: 

GPM = 50 Tons x 24 = 120 GPM 

10-F Range 

6. F ro m Page 14, read 10 ft of water cooler p ressure 

drop for GPM: 

7. AYCAL005O Is suitable. 

EXAMPLE -Brine Chilling 

1. GIVEN: Provide a capa city of 34 tons cooling 

30% by weight Ethylene Glycol from 

50-F td 401.0.0D025FF, 95-F air on 

the condenser, 60 Hz and 4000 IL altitude. 

2. DETERMINE: 

Unit Size 

kW Input 

Ethylene Glycol GPM 

Cooler Pressure D ro p 

3. See Ethylene Glycol correction factors, for 30% by 

weight Ethylene Glycol.. 

12 

READ: .974 Tons factor 

.995 Compr. kW fa ctor 

26.1 GaIlF/ronsfactor 

4. See Performance Data Correc ti 

on Factors for 

0.00025 fouling factor and 4000 R alti tu 

de. 

READ: .083 Tons fa ctor 

. 1.021 kW factor 


S. From RATINGS on pages 16-46: 

145579-V--DS-12.1, AppendlxA 


SELECT. YCAL0040 (English Uras) 

36.1 Tons 

38.6 Compressor kW 

6. Detemime YCAL0040 b ri ne cooling capa city 

and Compressor kW requirement 

A Tons - 36.1 x .974 x .983 = 34.6 

S. Compr. kW - 38.6 x .995 x 1.021 = 39.2 

7. Determine average full load Comp ressor kW at 

34 tons: 

34 tons x (392 I(W) - 38.5 Compressor kW 

34.6 tons 

8. Determine Ethylene Glycol GPM: 

Tons x Gal. 71minribn factor 

GPM = 

Range 

GPM = 

34.0 x 26.1 

GPM = 88.7 

9. Determine Cooler Pressure Drop: 

/C- tee Ethylene Glycol cor rec ti on factors for 

30% by weight Ethylene Glycol. 

10 

READ: 1.096 Pressu re D ro p Factor 

B. See page 14 at 88.7 GPM for the YCAL0040. 

READ: 6.5 FL HO P ressure Drop 

C. Cooler Pressu re 

Drop = 6.5 x 1.096 or 7.1 FL 

H2O 

10. YCAL0040 Is suitable. 

^^w 

Originator. 

Attachment: 8 Date: 7L29LL O 

Calc. No: 145579-V-CA-004 Checked by. 

Rev. No.: 1 Date: D7 Nib. O q- 

Sheet 2 of 4 

A5-663 

YORK INTERNAnoNAL 

I 

H

• 4 Design Parameters 

• 

O 

O 

V r 

L' 

_o 

J 

J3 

^ Y 

.5 y u m 

c0N 

O'OUO 

co 

Y ^ 

n 

Ml 

4j 

W O Z 1j Z m 

e) 

Q U C ^ 

I 


ENGLISH UNITS 

LEAVING WATER 

FORM 150.62{G1 

YCAL TEMPERATURE COOLER FLOW GPM AIR ON CONDENSER 

MIN' MAX' MIN MAX MIN' MAX' 

0014 40 SS 25 60 0 125 

0020 40 55 25 60 0 125 

0024 40 65 30 70 0 125 

0030 40 55 35 170 O 125 

0034 40 55 35 170 0 125 

0040 40 55 60 325 0 125 

0042 - 40-• 55- 60- 325- 0 125 

0044 40 55 60 325 0 125 

0050 40 65 60 325 0 125 

0060 40 65 60 325 0 125 

0064 40 55 100 350 fl 125 

0070 40 55 100 350 0 125 

0074 40 55 100 350 0 125 

0080 40 • 55 100 400 0 125 

0090 40 55 138 525 0 125 

- 0094 40 55 138 525 0 125 

0104 40 65 150 625 0 125 

0114 40 55 156 625 0 125 

0114 40 65 156 1 625 0 125 

SI UN ITS 

YCAL 

TEMPERATURE •C 

LEAVING WATER 

FLOW-VIS31 AIR ON CONDENSER C) 

MIN' MAX' MIN MAX MIN4 MAX' 

0014 4.4 12.8 1.6 3.8 -17.7 51.7 

0020 4.4 12.8 1.6 3.8 -17.7 51.7 

0024 4.4 12.8 1.9 4A -17.7 51.7 

0030 4.4 12.8 2.2 10.7 -17.7 51.7 

0034 4.4 12.8 2.2 10.7 -17.7 51.7 

0040 4.4 12.8 3.8 201 -17.7 51.7 

0042 4.4 12.6 3.8 20.5 -17.7 51.7 

0044 4.4 12.8 3.8 20.5 -17.7 51 3 

0050 4.4 12.8 3.8 20.5 -17.7 61.7 

0060 4.4 12.8, 3.8 20.5 -17.7 51.7 

0064 4A 12.8 6.3 22.1 -17.7 51.7 

0070 4A 12.8 6.3 22.1 -17.7 51.7 

0074 4.4 12.8 6.3 22.1 -17.7 51.7 

0080 4.4 121 6.3 25.2 -17.7 51.7 

0090 4.4 12A 8.7 33.1 -17.7 51.7 

0094 4.4 12.8 6.7 33.1 -17.7 51.7 

0104 4.4 12.8 9.8 39.4 -17.7 51.7 

0114 4.4 129 9.8 39A -17.7 51.7 

0134 4.4 12.8 9.8 39.4 -17.7 51.7 

NOTES: 

1.For havOW brio@ Mmperodne be low 407 (4A-C), c ontact Yom nert YORK Office for app lica llon requhementa. 

2. For leaving watertemperabae hoer Mari SS•F (12.8•C), contact Ow nearest YORK OMCe for application guidelines. 

3. The evaporator Is protected against free zing b -207 (•2&MC) wOh an dec trle heater as standard. 

4. For operation at for penNres below 25•F (J.9•C), the opgoral LowAmbisM IQ will need to be bstdkd on the ayslem (fwYCALC014. 

0080 models o*j 

5. Foroperudw at mn" lures above 1157 (461.0), the op6ond Rgh Amblenl qt will need lo be Insta lled on the system. 

YORK ttrT RNAmot1Al. 145579-V DS-12.1, AppendfxA 13 


A5-664

E 

• 

Wafer Pressure Drop 

n 

100.0 

0 10.0 

0 NNd 

a 

1.0 •k 


ENGLISH 

10 100 

1000 

F low, GPM 

E 

MODELYCAL COOLER CURVE 

0014,0020 A 

0024 e 

0070,0074 C 

0040, 0042 0044, 0060, 0060 D 

0054,0070,0074 E 

0080 F 

0090,0094 0 

0104, 0114, 0174 H 

Note: Water Pm&wm Drop Cwves may adend past the minimum and m *MM water Dow renges. See page 17 for mWmum and 

Mw*Met low pdnts. . 

14 145579-V-DS-12.1, AppendlxA 


Attachment 8 

Calo. No.: 145579-V-CA-004 

Rev. No.: 1 

Sheet 4 of 5 

Originator. W 

Date: -7 M or 

Checked by. 

Date: 0.7 tgF^0 

s

0 

• 

Q0 

a 

a` 

1000.0 

,00.6 

10.0 

10 

RPP-24544 REV 1 d 

sl 

11111_tt^tfa__tl tlt t111111_fit_tt___t n n n 

_..________. 

WE MllME 

......__..WAN__a00V 

_.,._.U...,W,,.___...., 

^,MMM%II11D//IMMMMI111 

^tt_^nnt__tt__ to_tr_tt^tr_t____. n 

,tttt_fit____IInnttttttltt_t^____ nn 

1.0 10.0 

Attachment:. B Flow.LIS 

Calc.'No.: 145579-V-CA-004 

Rev. No.: 1 

Sheet 5 of 5 

Originator: '—P'1 

Date: O 

Checked by. 

Date: 

0 NAiQe 

MODELYCAL COOLER 

0014, 0020 A 

0024 B 

0030, Oo34 C 

0040,00420044,0050,0060 

0064.0070.0074 

Note: Water Pressure Drop curves may extend peel Om minhmm"mw6man wakr Sow fangs. See page 13 for muaman and 

matmum flow points 

D 

E 

rOF M 150.62-EGt 

YORK ItdtERNAmONAL 145579-V-DS-12.1, AppendixA 15 


A5-666 

100.0 

t

0 


145579-V-CA-004 

Attachment 9 

American Industrial Heat Transfer Inc. 

CT — STC Series 

• Fixed Tube Bundle / Liquid Cooled 

Heat Exchangers 

Catalog Pg 41-50 

A5-667

0 

• 

CS & STC Series overview 


Attachment: 

Calc. No.: 

Rev. No.: 

42 copy a Sheet 

9 

14557D -V-CA-004 

1 

2 of 10 

Originator. 

Dale: 

Checked by 

Date: 

CS SERIES 

Fixed tube construction heat exchangers with NPT 

connections. Made of steel with copper cooling tubes and 

cast Iron end bonnets. Standard sizes from T through 6' 

diameters. Standard one. two, and four pass models are 

available. Options Include 90110 copper nickel and 316 

stainless steel cooling tube, and zinc anodes. Can be 

customized to fit your requirements. 

STC SERIES 

Similar in design to CS series with fixed tube construe. 

lion and NPT connections made of 316 stainless steel. 

Standard sizes from 7 Through 6'diameters. Standard one, 

two, and four pass models are available. Larger diameter 

units availablo upon request Can be customized to fit your 

requirements. 

CS 2000 SERIES 

Rbced tube construction heat exchangers wit:t A.JL. 

ange connections. Made of Steel with copper coclirn 

tubes and cast kon end bonnets. Standard 10' diameter 

from 111 to 442 sq. R. Standard one, two, and four pass 

models are available. Options Include 90/10 copper nickel 

and 316 stainless steel tooting tubes, and zinc anodes. 

Can be customized to fit your requirements. 

(See Page 51) 

CS 2400 - CS 4800 SERIES 

S1raR tube la rge capacity heat exchangers with 

fixed tube bundle. Standard one, two and four pass units 

available. Sizes from 12' to 24' diameters. Made of steel 

with copper cooling tubes and steel channels. Options 

Include 90!10 copper nickel and 316 stainless steel coot- 

Ingtube, and zinc anodes. Can be customized to fd your 

requirements. 

W 

0.11YP14ZO57 

n-rmo w Ahtm 

AS-669

0 

0 Ln 

CAST BONNET 

Provides flu id Into 

tubes with minimum 

restriction. One, Iwo, 

or four pass Interchangeability. 

MOU NTING \ 

BRACKET 

Heavy gauge steel 

mounting brackets 

are adjustable In 

orientations to 360 

degrees. 

Drain 

Example Model 


BAFFLES 

THREAD 

CNC precision CNC manufactured baffles to 

FLOW CAVITY th reading to provide Provide maximum lurbuience and 

Generouslyslzedtoal• accurate leakproof heat hansfet with a mnknum fl 

uid 

law for minimum pres. Mrvtebtli1ns. Pr e 

ssure drop.' 

sure drop and more \ 

un rm 

if 

o flow. 

DRAIN PORT 

ports allow for 

easy draining of tube 

side. Op tional zlno anode 

can be Inse rted In 

place of Nub. 

•-- —. / .... FULL FACE GASKET —.—..._ 

TUDE JO INT Full-face composite 

Ro ller expanded tube gaske t. 

Joint to tubo•sheet Attachment 

UNIT CODING 

Op tions 

CS & STC Series overview 

Cats No.: 

Rev. No.: 

TUBE SHEET 

Precision-machined 

tube-sheet provides 

for long lasting high 

strength service. 

145579-V-CA-004 

1 

Sheet 3 of 10 

FINISH 

Gray semigloss 

enamel Can be 

used as a base 

for additional 

Coals. 

BUNDLE ASSEMBLY 

CNC pre ci sion manul c 

hired pans to guarantee 

a close lit between 

the baf fles, tubes, and 

shell. Clearances are 

minimized to p rovide for 

maximum heat transfer. 

Originator: 

Date: v 

Checked by. 

Date: 011`1A-205 

CS - 1224 - 4 - 6 - TP - CNT - B - Z T Zinc Anode 

Modef 

Shelf 

01amster 

Z.1 Zlrx; Anode 

2Z. 2 Zinc Anode eta 

CS 6W.325' Effective Spacing Code 

C LlTubig 

STC 800. 

1000. 525• 

1700. 8.07 

Inrlax l) 

15, End Bonnets 

Baroc.COpper 

2A' n, Blank - Cast Iron 

3.0' Diamnenter 

SP 

PAWS 

OPnaa 

1.0' 6.318' TP.2P 

CNT.SwilCum OpVon$ 

BM 10.5v FP.4 pass STS.Sakiasa Stets B. Dime 

8.0•C. Carbon Sleet 

STANDARD CONSTRUCTION MATERIALS & RATINGS 

eon. A►m 1 e* epe ba * w.senreb d"lpdWxxw wawa mew. ' _I 

Copznpl402001 AmwP_mkxusbWNeat Trarefer.kr 39os 173Z^1 ^ 40099 lot t tarn rm80o bx:a Pt7I731•hn0 w.wairm. 

JR5-6 0

CS & STC Series selection 

WMP 1: Calculate the heat load 


The heat load in BTU/HR or (Q) can be de rived by using several methods. To simplify things, we will consider general specifications for hy. 

draulic system oils and other fluids that are commonly used with shell & tube heat exchangers. 

Terms 

GPM . GallonsPer Minute 

CN . Constant Number fora given fluid 

AT = Temperature di0'ercndal across d= potential 

PSI . Pounds per Square Inch (p=um) of the operating side of the system 

MIT . Horsepower of the electric motor ddving the hydraulic pump Q - arm / l m 

r w a wowaa twos x two) 

Tt° a Not fluid entering tempe rature in OF 

T. . Hot fluid exiting temperature in OF 

ti. • Cold fluid iemperawn: ent ering in OF 

t aie a Cold fluid temperature exiting in OF 

For example purposes, a hydrau lic system has a 125 HP (93Kw) elec tric motor installed coupled to a pump that p roduces a flow of 80 GPM @ 

2500 PS1G. The temperature differential of the oil entering the pump vs exiting the system Is about 53°F. Even though our return line pressure 

ope ra tes below 100 psi, we must calculate the system heat load potential (Q) based upon the p rime movers (pump) capability. We can use one 

of the fo ll 

owing equations to accomplish this: 

To de rive the required heat load (Q) to be removed by the heat exchanger, apply ONE of the following. Note: The cal culated but loads may di[ 

fer slightly from one formula to the next. This is due to assump ti ons trade when es timating heat removal requirements. The factor (v) represents 

the percentage of the overall input energy to be rejected by the beat exchanger. The (v) fac tor is generally about 30% for most hydrau lic systems, 

. however it can range from 20'%-70% depending upon the installed system components and heat being gene ra ted (e. servo valves, proportional 

valves, ete—will increase the percentage required). 

FORMULA EX4.%ME Constant for a given fluid ( CN ) 

A) Q - GPM x CN x actu al AT A) Q =80 x 210 x 53°F = 89,040 "R 

e) Q - [ (PSI x GPM) / 1714) x (v) x 2545 a) Q -[(7500x80)117141 x 30 x 2545 = 89,090 eruf 1) Oil 

e) Q - MIIP x (v ) x 2545 _ tin 2) Water..M.._....._._._...CN = 

D) Q = Kw to be removed x 3415 e) Q =125 x.30 x 2545 = 95,347 sTu4 t 3) 50%!? Glycol..._._.. = 4 0 

_ x) Q • HP to be removed x 2545 D) Q =28 x 3415 = 95,620 smltm 

• 

STEP 2: Calculate the Mean Tempera ture Difference 

When calcula ting the MTD you will be requi red to choose a li quid flow rate to derive the cold side AT. If your water flow is Unknown you may 

need to assume a number based on what is available. As a normal rule of thumb, for oil to water cooling a 2:1 oil to water ratio is used. For cepplica 

tiots of water to water or 50 % Ethylene Glycol to water, a 1:1 ratio is common. 

FORMMA 

HOT FLUID AT = Q 

Oil CN x GPM 

I xAmnE 

AT = 89,090^f "' uep 1em 

Jt a) = 5.3°F = AT Rejected 

COLA FLUID A t = BTU/hr 

89 090 BTUfhr 

At 

= 4.45°P = ^TAbsorbed 

Water CN xGPM 

x 

'D lora2:l ra tio) 

T,, . Ilot Fluid entering temperature in degrees F TI =1253 T 

Tee, • Hot Fluid exiting temperature in degrees F T. = 120.0 OF 

tin a Cold Fluid entering temperature in degrees F L, -70.09F 

ter„ = Cold Fluid exiting temperatu re in degrees F ter, a 74.5 OF 0 p 

T, a • La a S[smaller temperature difference) = rS 120.0017-70.0°17- 50.0617 a 500°F a 3M 

l 

TI, . tei1 L (larger tempe ra ture differencel \ L / 1253°F-743°F = 50.8°F 30.8°F ^{ £ 

STEP 3: Calculate Log Mean Temperature Diffe rence Q MTD) - D 

Attachment 

9 

To calculate the LMTD please use the following method; Calm No.: 145579-V-CA-004 

L- Luger temperature difference from step 2. 

M a S/L number (LoeATm err TAat a A). 

Rev. No.: 

Sheet 4 

1 

of 10 0 

m 

LMTDI =L%M LMTDI=50.8x.992 (nom TAmmA)=5039 t 

To comet the LMT'D, for a multipass heat exchangers calculate R & K as fo ll 

ows: Q U 

FotcatuIA EXAMPLE 

B•n 

R= 

Th. -Tow 

t -^ 

1253°F-120°F 5.3°F 

R= 

4 - F = 7V = (L17=R) 

the wrrec6on factor CFa 

r(ROM rO' 

=CHID, z CFa 

K= 

er 

Tin-t„ 

_745°F-70°F 

K- 

124.5°F-70°F 

= 43°F 

55.4°F 

= 

(0.081=K) 

e=5039x1.5039 

,are A*9fMA0 4A" 

AIMbe ndaVe.naab daatp,dut. nQ aa^W r,oara 

^ Copyr$itOaow Arriaicart lndntriallNalTmrrateA ate. asm ttewtn wee. Z. aowo tr:t mes>, rnd000 tac tMrt nt•roto w°waare°m 

S

STEP 4: Calculate the area required 


O (BTU / 11R) 89,090 

Required Area sg1L = LMTD, x U (FRont TABLE C) 50.39 x 100 =17 68 sq.fL 

STEP S: Selection 

CS & STC Series selection 

a) From TABLE E choose the correct se ries size, baffle spacing, and number of passes that best fits your flow rues for both shell and tube side. 

Note that the tables suggest minimum and maximum informa tion. Try to stay within the 20-80 per ce nt range of the indicated numbe rs. 

Example 

Oil Flow Rate = 80 GPM = Seri es Required from Table E = 1200 Series 

Baffle Spacing from Table E = 4 

Water Flow Rate = 40 GPM = Passes required in 1200 series - 4 (FP) 

b) From TABLE D choose the he at exchanger model size based upon the sq .fL or surface area in the se ries size that will accommodate your now 

rate. 

Example 

Required Area . 17.68sq .ft Cl osest model required based upon sq.fL d: series a CS -1224 - 4 . 6 - FP 

If you require a computer gene rated data sheet for the applica ti on, or if the informa tion that you are trying to apply does not match the cormsponding 

informa ti on, please contact our engineering servic es depa rtment for fuller assistan ce. 

TABLE A- FACTOR MILMT0 = 6t M' TABLED- Surface Area 

25 .72t .75 .870 

At 21S 26 t .728 .76 .664 

A2 251 27 .734 .77 .879 

.03 277 28 .740 .78 A86 

.04 - 298 29 

246 .79 .BM 

A5 .317 .30 353 50 .1196 

A6 ,334 .31 6 .7S9 .81 902 

A7 .350 32 7 .76S 92 907 

A8 .364 .33 7.604M8 

.771 .83 913 

49 .378 34 .612 59 .777 .84 918 

.10 .391 3S .619 60 .783 55 923 

.11 AM 36 .626 .61 .789 96 928 

.12 A15 37 .634 .62 .795 97. 934 

.13 .427 38 .641 .63 .801 .88 939 

.14 A38 39 .648 .64 .806 .89 .944 

'.15 .448 AO .555 .65 513 .90 949 

.16 A58 Al 662 .66 818 91 .955 

.17 A69 A2 .669 2 .67 .8 3 92 959 

.18 A78 .43 .675 .68 929 93 964 

.19 .488 A4 .682 59 .536 .94 970 

20 A97 AS .689 .70 940 95 97S 

21 308 A6 .695 .71 .848 96 979 

22 .515 A7 .702 .72 952 97 966 

23 524 .48 .709 

% .991 

24 533 A9 .715 .73 .74 964 .99 % 995 

factor for 

05814 

J 

- 

a 

- CS-1236 35.3 17.7 

05524 - - CS-1248 47.1 23.6 

CS-6M - - CS-1260 58.9 29S 

' CS-1272 70.6 55A 

05414 - - 051264 am 41J 

CS824 - - CS-1296 84.0 472 

CS436 - - 

CS" - - CS-1724 40.1 238 

CS-1738 60.1 353 

CS-1014 47 4.6 CS-1748 90.1 47.1 

CS-1024 14.9 79 CS-1760 100.1 589 

051036 22.4 11.8 CS-1772 1202 70.7 

051048 29.9 15.8 CS-1784 1402 82.3 

CS-1060 37.4 1 19.8 CS-1796 1602 .942 

CS-17108 1602 1041 

CS-1224 216 119 11 4 s.17120 1 2002 1 1179 

R . Attachment: 9 60 65 100 140 220 29 180 14 00 

1 

Ca1C. No.: 145579-V-CA-M 50 60 100 160 240 4S a20 25 160 

Rev. No: 1 TABLE C 

Sheet 5 of 10 

- 400 Water Water 

Originator 350 Water 50% E.G" 

Date: /37a O 100 Water os 

300 50% E. Glycol 50% E. Glycol 

Chocked by: 90 5o16EG" on 

Date: 0 

•etc ram w^wws Milp-.. rara^y,o^ .ro.noa^. 

GOpyltyla 02004 Amrkan kwua0181 FAat Translar. BIG 3905 Prole 1A 21 M1 1.90099 I* I (MY) Tai-1000 10c 1 (847) 731-1010 w AtAep9 I dr,

CS & STC Series 

The selection chart provided contain an a rray of popular sizes for quick 

sizing. It does not pro-de curves for a ll models available. Refer to page 44 

8 45 for deta iled calcula ti 

on Information. 

Computer selection data sheets forstandard or spe cial models are avaBable 

through the engneedng department of Ame rican Indust ri al. To use the 

fo ll 

owings graphs cor re 

ctly, refer le the Ins truction notes r1.5r. 

1) HP Curves are based upon a 401 approach temperature; for 

example: oil leaving a coder at 125T. using SWF coo ling water 

(125•F -WF.4 ( rF ). 


3) OIL PRESSURE DROP CODING: 4• S.psl ir. 10 psi; 0.20 psi; 

A. 50psi. Cu rv es that have no p ressure d ro 

p code symbols kale 

that the dl pressure drop Is less than 6 psi for are Bow rate Shown. 

If 4) Pressure Drop is based upon o4 with an a y ol 100 SSU. 

I It the average oil Nscosfly Is other Nan100 l n mul tiply the 

Indicated Pressure Drop by the correspo mg value from corrections 

table A. 

6) Corrections for approach temperature and oil viscosity a re as fo ll 

ows: 

2) The oil water rat io of 1:1 or 2:1 means that for every 1 ga ll 

on of dl ,,,,,,s wnrl 40 

circulated, a mi ni mum of 1 or 12 ga llon (respectively) of 851F water H.P.(v, aa ^,r,r) w H.P.(,,,,, lae^ x (AEI 40 x B. 

must be circulated lo linatch q)e Curve res ults. 

500 

400 

300 

200 

150 

W 100 

JO 80 

U 80 

? 70 

W 60 

0 50 

cc 40 

a 

= 30 

20 

15 

10 

8 

8 

. 7 

6 

5 

HEAT ENERGY DISSIPATION RATES (Basic Stock Model) 

Ratio 

1. su-1 3+FP 21 Originator. 

2. 514 -34-FP 2:1 

Ira 

3. 624.1.3-4-FP 2:1' ,' 

7•'^': ? ^î_s 

Date: 7 y17a. d 

(?'" 

{. 624.34-FP 2/ t :(r a + ^'tA + 

Checked by. 

T 

S. 614-1.7.4-FP2 1 . 

1< 

i 6. 814 -4-4-FP 21 

' 

Date: 

T. e24 - 1.7.44P 21 

. S. 824-44-FP 2:1 _ y -:• ;, 

8. 836 . 1.74•FP 2:1 e: •• 

- 10. 638-41•FP 21 4' s + 

11. 1014.2-6-FP •.8^ 

Z, 

12 101F6&fP2.1 

13. 1024 . 26FP 21 -. _'' "' e..^. :•• 

^. 

14. 3024 .56-FP 21 

-' 

13. ta36.2$FP21 F' 

16. 1036.56FP 21 ' , < ^ 264 

17. 1221 . 25&FP 21 

•.. i-: }^.,-:u .:''a 

18. 1224 . 6 4-FP 21 

- 

19. 1238.258-FP 21 

+ .. 20 

20. 1236Tt„ 

-66FP 

will r 

21. 1248 . 2.5&FP 21 

3 .^ t + 

- :22 1248 . 66FP 21 r2,9;y .!'.i't,. ?^ +7. `.F! 

23. 1260 . 2-45&-4FP 21 y:y 

24.' 1260 r : t '. `.: 'P:,, L•,^^ 

. 66FP 21 

25. 1724 . 3.5&FP 21 :1. 

26. 1724.8.4-6-FP21 

•' ,: .. 

.... 

27. 1736-3.58FP 21'' 1Z 

7 !` ' •SSA w%. 

28. 1736 . 8.45FP 2:1 

. 29. 1740 . 3."TP 21 ' 24s .y ^ > 

f 

r 

.' ^ i ' :"•Y ^' -. rq^ ;;, ;: 

.'. 30. 1748-a46FP 21 

1, 

.. 31. 1760 . 3S4FP 21 , p , ^ •._ '. 

n ♦ x? y !d -y:` 

• 32 1760 . 84&FP 21 p> 

Q i 

.:.rte w r.-.::f'6- 

7 33. 17M-3S&FP 21 

S' C,, .y1: rH. 34 1772 . 8.44-FP 2/ •, g:P 1•: f1 

i§^î 

a 

r: 1' ^: h . f+i .r. Yx ^ +tt tiyF^ ':'i. 

1: 

8 

7 

{ vlscoslTV 

r 

r` 

•.. , 

', 

':; * 

n- 

CORRECRONS 

. 

:.4 

'f Avg Oil 

" SSU A B 

0 0.83 Wr 

3 4 5 6 7 8 910 15 20 40 60 80 100 200 

GPM (Oil Through Cooler) 

rral.MHn rererveeew b.W walawNe Mdpr wwJ neat 

46 COPYr^l 02004 MrrlCan hWueeW Heal TnMlw. W. am allure lid zit a am W 1047) M-toot lac 1047) MI .1010 enrw eTaa.e 

., 

"' 3,. 7 Attachment 9 

Cale. No.: 145579 V-004 

t- 

Rev. No.: 1 

Sheet 6 of 10 

. ' y f100 4.00 1.53 

2 

.•^ ` 

AS-03

0 

u 

• 

. . 

- I .E 

COMMON DIMENSIONS &WEIGHTS 

JF4.25 

WMIMEM 


IP 

oS."M c11200. Oa400 a CS400 

a cs000 

SINGLE PASS (SP) 

TWO PASS 

CS Series dimensions 

eats u.1_xli^.f1®m^m^ 

5.88 1 1.431 A4 &00 

1 1 - 

:5, NIMMMMUM 

•.^-. Vii': 

723 1 1.99152 1 4.991 

:.t iivi 4f1{^^ ©FT:7^^ 

&44 1 1.00 1 ' 0 1 2001 1.44 

7.0611.811.12.5011.88 

&641 1.0012 1 150 1200 

7.06 1 1.81 1 2 12.0012M 

FOUR PASS (FP) .991 I I I I I 

10.00 

17.00 

450 

231 

2.75 4.18 1.62 .36+x0.88 (2) 1.00 17 

20.00 27.00 24 

9.00 1&62 32 

.&00 19.00 312 26.62 350 425 US A4+x1.00 

1.50 

31.00 38.82 

.C25 

57 

8.00 17.12 

43 

&T5 19.00 &S2 27.12 4.00 525 2.00 A44x1.00 (2) 1.50 67 

31.00 39.12 • 2S 72 

25 . 3 

3025 99.13 110 

7.75 47-Z 4.16 51.13 4.50 &2S 2.50 A44x1.00 (2) 200 135 

5425 83,13 M 160 

66.25 75.13 185 

17M 97.50 1 140 

Attachment g 50 Originator. 160 

Cale No.: 145579-V CA 004 Date: s- aoo 2600 

Rev. No.: 1 so 

Checked by. 

. Sheet _ 7 of 10 ^ Date: 0"1 MK2bS 1 

Capnv.^.« .. ..._.....^._ +wsROw..._. -r_. . ...1010 WW.A%Ao0 I 

A75-674 

340

• TWO 

• 

CT!_ Carime r/i.nnncinnxr 

r^- 

i J: STCIMISTC1 

i 

it I pm 

1 

Î " 

E-&Rw 

COMMON DIMENSIONS & WEIGHTS 

II^ 


2w. BTO4004B eO 

&=4M 

SINGLE PASS (SP) 

PASS (TP) 

FOUR PASS (FP) 

y^} ®©am© 

d i1 

723 1 1.99 1 -% 1 400 I . 

^l 

:,• ., LOU IQC 

7.051 1.81 1 M 1 1501 Im 

.î.r..< 

Z7 2 

3.70 •38 q .75 I1A0 

17.88 

27.88 4.44 

39.61 

18.81 

28.81 4.81 

.63 

.75 

28.13 

41.13 

53.13 &44 1.00 

"(3500 

7.06 1 1.81 1 1 2.001 250 

3.12 430 ?91 275 4.18 1b2 2e/x0.86 (2) 1A0 

20.00 27.00 4 

8.00 1&62 32 

4.12 &oe 19.00 3.12 26.62 3.So 425 1.75 A4+x1.00 (2) 1.50 41 

31.00 38.62 25 63 

9.00 17.12 

6.12 &75 19.00 3.62 27.12 4.00 525 200 A44x1.00 (2) 1.50 5S7 

91.00 39.12 25 72 

825 27.13 as 

30.25 39.13 110 

6.12 7.75 4225 4.16 51.13 4.50 62S 2.50 A48x1.00 M 200 135 . 

5425 63.13 '^ 160 

6625 75.13 185 

&oo to 

Attachment 

Cale. No.: 

'7 9 

145579-V-CA-004 

Originator. 

Date: 

Checked by. 

b 1 

1 

SheeNo 8 of 10 - 

Date: 0-1 H t,4- OS 1 

t WcMT w^wiw^M 4W 

48 1 COPO n02ow AS-675

RPP-24544 REV )d 

CS & STC Series installation & maintenance 

• PIPING HOOK-UP A ._..-_.Hot fluid to be cooled 

8 .__----Coded fl 

uid 

C .__.___._.. Cooling water In 

D ___-Coo lingwatorcut 

CJ 

0 

Receiving I hista llation 

a) Inspect unit forany shipping damage befo re uncrating.ln?icate ati dam. 

egos to the buc king fums'dot iveryperson, and mark iton the recoiving bV 

before accep ti ng the height. Make sure that there Is no vi sible damage to 

the outside s ur face of the heat exchanger. The published weight Infortmtlon 

located In t hi 

s b roch ur e Is approximate. True shipment weights are 

determined at the time of shipping and may va ry. Approximate weight 

Inforrnati on published herein is for engineering app ro ximation purposes 

and should rot be used for exact s hi 

pping weight. Vince the warran ty is 

based upon the unit date code located on the model iden tification tags, 

removal or manipula tion of the Iden tifica tion tags will void the manufacturers 

warranty. 

b) When handling the shell b vibe heat exchanger, spe ci al care should 

be taken to avoid dropping the unit since mishandling could cause the 

heat exchanger to crack and leak exte rna lly. Mishandling of the unit Is 

not covered under the manufac turers warranty. All units we shipped with 

par ti al woodreonugated cardboard containers for safe handling. 

c) Storage: American Indust rial heat exchange rs are p ro tected against 

the elements during shipment t the heat exchanger cannot be Installed 

and phi Into operators Immediately upon re ce ipt, certain precautions a re 

required to preve nt deterioration during storage. The respons ibil 

ity lot 

Integrity of the heat exc hanger(s) is assum ed by the user. Ame rican 

Industrial will not be resporrale for damage, co rr osion, or other deterioratiad 

of the heat exchanger during transit or sto rage. 

Proper storage practices are Important when considering the high coals of 

repair or replacement, and the possible delays for Henn width require long 

lead tines for manufacture. The following li 

sted practices are provided 

sdefy as a convenience to the user, who stint make the ir 

own decision 

on whether to use a ll or any of them. 

I) Heat exdrenge rs not to be placed In Immediate se rv ice, require precautionary 

to preve nt co rr osion orcontarninsdon. 

2) Heat exchange rs made of ferrous mate ri als, may be pressure-tested 

using compress ed air at the taciory. Residual off coa li 

ng on the Inside 

surfaces of the heat exchanger(s) as a resu lt of ushing does not 

the possibil ly of Internal m c orro sion. Upon receipt, fill 

the heat 

exc angier(s) w ith the app ro priate grade of oil or aptly a corrosion 

preven ting In hi 

bitor for storage. 

3) Corrosion protection compounds lot Inte ri or surfaces for lag tern 

storage or other applica tions are app lied solely at is request of aurom 

m Upon request, American Indus trial can p ro vide a customer 

approved corrosion preventative t ava il able when Included In the 

A SP -----Single Pass 

..^_^._..-Two Pass 

___.._...__Four Pass 

ONE PASS TWO PASS FOUR PASS 

o ri 

ginal purchase order specifications. 

4) Remove all did, water. Ice, or snow and wipe d ry before moving heat 

exchanger(s) Into storage. Heat exchange rs are generally s hipped 

empty, open drain plugs to remove any aocumufaled condensation 

moistu re, then reseal. Accumula ti on of moisture usua ll 

y Indicates 

corrosion has already sta rt ed and reme dial ac ti on should be taken. 

5) Store In a covered, envi ro nmentally stable area The Ideal sto rage 

environment for heat exchange rs Is In a dry, bw-Ixxddi ty abnosplhere 

which Is sealed to p revent the ent ry of blowing dust rain, or snow. 

Maintain In stmospfhedc tempe ratures between70`Fand 105°F (large 

temperature swings may cause condensation and m oisture to form 

on steel components, t hreads, shell, etc-) Use thermomete rs and 

humi dity Indicators and maintain the atmosphere at 40% relative 

humidity, or lower. 

d) Standard Emmet Coaling: American Indust ri al provides Its standard 

products with a normal base coal of oil base air cure anamel paint The 

enam el paint Is applied as a tempora ry protective and esthetic coaling 

prior to shipment. Wh il 

e the standard enamel coa ti ng Is du ra ble, American 

Indust ri al does riot warran ty fl as a long-term finish c oating. It Is strongly 

suggest ed that a more durable gnat coating be app li 

ed after Insta ll a ti on 

or prior to long-term storage In a corrosive envlrdnmM to cover any 

accidental scratches, enhance esthetics, and further prevent corrosion. 

It is the responsibility of the customer to provide regular mai ntenance 

against ch ip s. scratches, etc_ and regular touch up mainte nance must 

be p ro vided for long-tern benefits and co rrosion prevention. 

e) Special Coatings: American Indust ri al offe rs as customer options, 

Afr-Dry Epoxy, and Hereslte (Alt-Dry Phenol ic) coalings at addi ti on al 

cost. Ame ri can In dust ri al oilers special coa ti ngs teal request. however 

American Industrial does not wa rr anty coa ti ngs to be a pernenert solulion 

for any equipment against corosion. 0 is the responstb lity d Ina 

tusk-- ..,ratcthes.e1c.— 

and' Attachment 9 -turn benef it 

s 

and 

Cola No.: 

9Ar Rev.No.: 

Insta 

deal{ Sheet 

servk 

exd 

Pan Originator 

0w Date: 

âwn^r,." Wmke "w. Cheated by. 

Copy right O 2004 American kxknuW Heal Transfer, the 8903 Pe 173af Lwow Date' 

W'D 

145579 V-CA-004 

1 pedslouddbe 

9 of 10 

I g of system 

Oy.Verity lbe 

n AV- o r 

_. -- -eti a tube cheat 

it loo within the 

anger, contact 

-676


CS & STC Series installation & maintenance 

g) Flan the installation to meet the requirements Indicated on the piping 

Ins'allation diagram as i llustrated above. If Is recommended to put the 

tot uld b be cooled through the she lf side and the c old uld through the 

tube side. The Indicated port assembly sequence In the diagram max& 

mizes the performance. and moirrdzes the possib ility of thermal shock 

In instances where the uids we required to be reversed, trot ndd In the 

Mesandeold uldIn Oesheathe heat exchangerwll work with reduced 

pe rformance. Insta ll 

ation may be ver tical or ho rizontal or a combina tion 

thereat. However, the Installation must allow forcomplete draining of the 

heat exchanger regar dl 

ess at single pass. two pass, orIO rpass constru c. 

km Complete drainage Is Important to p re vent the heat exchanger from 

keezing, overheating at a old. or mineral deposit buildup. 

For fixed burde heat exchangers, provide sutaclentdearance atone end 

to allow or the removal or replacement of tu bes. On the opposite end, 

provide anaghapace to removal of the compote bo nn et to provide 

sufficient clearance to perm it 

bibs ro il 

ing and cleaning. Aloes accessible 

room for scheduled cleaning as needed. In cl 

ude thermometer wells and 

pressure gauge pipe pods in pip in g 10 and from the heat exchanger lo. 

catedas dose o the heat exchanger as possible. For more lnfonnaaon 

please contact American Industrial. 

• h) h is recommended to use exible hose whe rever poss ib 

le to reduce 

vbm0on and aloes slight movemen t. However, hoses are not re quired. 

Hydrau lic ca r rying Ines should be sized to handle the approp ri ate ow 

and o meetsyslem p ressu re drop requiremen ts based upon the systems 

paramete rs, and not based upon the units supply and return connec ti 

on 

size. We recommend th 

at a low cracking pressure direct a cting relief 

vain be Installed at the heat exchanger Wet to prote ct I kom pressure 

spikes by bypassing of In the event the system expe ri ences a high ow 

surge. It preventat iv e Duration Is used I should be located ahead of the 

cooler.on both then and tube side to catch any scale or sludge Imm the 

system before it 

the coder. Falum to inrstan l it 

ers ahead of the 

heat exchanger could lead to possible heat exchanger fa il u re due to high 

pressure I the system filters plug. 

g Standard shag b tube coolers are built wi th a mned tube-sheet corn 

struc tion However, the differential operating temperature between the 

en leringshelslde uldandtheenteringlubeslda uldshoutdnotexcoed 

1504F. It this condition exists, a seve re thermal shock could occ ur leading 

to product failure and mixng of the uids. For appl ic a tions with a differential 

temperatures of 150'F or more, we recoavnend using a sedes w ith 

a calling tube-sheet, u-tube, or expansion Joint to reduce the poten ti al 

for the e ffec ts of thermal shock 

0 Water requiremen ts vary from loca ti on to location. 0 the source of coalfrig 

waters from otter than a municipal water supply, It Is recomnended 

that a water "nor be insta ll ed ahead of the heal exchang er to p revent 

dirt and debds from entering and dogging the ow passages. I a water 

modtdallrg valve Is used it recommended to be Insta lled at the Inlet to 

the tooter to reg ulate the water ow. 

k) For steam ser vice, or other related applications, please consul our 

enginee ri 

ng depa rtment for additional Information 

Maintenance 

a) ktspedthe heats changerforloosenedbans, connections, rust spots, 

corradmandfor klemd orederrel uldleakage.A4ryconodedeu rtaces 

sho ul d be cleaned and recoated w it h palnL 

the panicutarmate rial of construction. With straight tube heat exchangers 

you can use a rod to ca refully push any deb ris out of the tubes. 

d) Zinc erodes am normally used to reduce the dsk of tallure due to 

electrolysis. Zinc anodes are a sac rificial component designed to we ar 

and dissohre through normal use. Nannaly, zinc anodes are applied to the 

water supply side of the heat exchanger. Depe nrIng upon the amount of 

corrosive action, one, two. three, or more anodes can be appled to 

fur th 

er re duce the risk of fa llure. American Industrial Heal Transfer, Inc. 

offers zinc anodes as an option, to specified and Installed at the request 

ourdrsromers. his the responsibil yof the cusloner to pedodlcaay deck 

and verify the condition of the zinc anode and replace It as needed. 

Applications va ry due to water chem ic al makeup and quality, material 

diffe rences. temperature. ow ra te, piping a rr angements, and machine 

grounding. For Rose reasons, zinc anodes do not billow arty scheduled 

tacbry predetermined maintenance plan moreover Ineymust be checked 

rou ti nely by the customer, and a maintenance plan deve loped based 

upon the actual wear rate. 

It substantial wear occurs or zinc dissolves without replacement, premature 

tailum or permane nt damage may o ccur to the heat exchanger. 

Ame ri can Indust ri al does riot warranty tustomerapp li 

cations. h is the responsib 

iliyof the customer to verify and apply the proper system mate rials 

of construction and overa ll system requiromens. Failures resulting from 

property app li 

ed or misapplied use of zinc anodes) Into non•specitied or 

specified app lic 

ations wi ll be the sole responsib il ity of the cusomer. 

e) A routine maintenance schedule sho ul d be developed and ad)usted to 

meet your systems requirements based upon water quality, etc .... Fail. 

ure to regula rly maintain end clean your heat exchanger can result In a — 

reduc ti on In operational pedomianee and lie expectancy. 

Note: Since applications can va ry subs tantially, the Installa tion and 

maintenance InlonnaOon contained In Mats catalog should be used as 

a basic guideline. The sate Insta ll 

ation, maintenan ce, and use of any 

American IndusMat Heat Transfer. Inc. beat exchanger are soley Me 

responslbdiry of the user. 

O.aG' 

•—'•^ 0.75' 

II +,_ 

A9-a00 dxo AB-1000 

M

• 

is 


• Figure l: Subcontractor Calculation Review Checklist. 

Subject: Off-Gas Chi ll 

er Calculation 

The subject document has been reviewed by the undersigned. 

The checker reviewed and verified the following items as applicable. 

Documents Reviewed: 145570-V-CA-004 Rev. 1 

Analysis Performed By: 'AMEC 

• Design Input 

• Basic Assumptions 

• Approach/Design Methodology 

• Consistency with item or document supported by the calculation 

• ConclusiordResults Interpretation 

• Impact on existing requi rements 

Checker (p rinted name, sigmature, and dale) 

Thomas 11 May 

Organizational Manager (printe 

d 

name, signature and date) 

David II Shuford1 `f J^f /f 

A5-678 

Page 1 of 1

• 

• 



AS-679

0 - Hanford Site

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