ML092930135

Attachment 2, Braidwood Station, Unit 1, Lug Stress Calculation for 1MS06007S

ML092930135
Person / Time
Site:	Braidwood
Issue date:	10/09/2009
From:	Exelon Nuclear
To:	Office of Nuclear Reactor Regulation
References
2009-07204, CC-AA-309-1001, Rev 4
Download: ML092930135 (46)

Text

ATTACHMENT 2 Braidwood Station, Unit 1 Lug Stress Calculation for 1 MS06007S

CC-AA-309-1001 Exelkn. ATTACHMENT 1 Design Analysis Major Revision Cover Sheet Page I of I Revision 4 Nudear Design Analysis (Major Revision) Last Page No. 18 & A25 (Page i)

Analysis No.:' 2009-07204 Revision: 0

Title:

Lug Stress Calculation for 1MS06007S ECIECR No.:" 376251 Revision: 000 Station(s): 7 Braidwood Component(s):.

Unit No.: 8 01 1MS06007S Discipline: M Descrip. Code/Keyword:.1° __-_____: _

Safety/OA Class:"1 SR ""

System Code: MS Structure:

CONTROLLED DOCUMENT REFERENCES '-

Document No.: From/To Document No.: From*To Is this Design Analysis Safeguards Information? '. Yes IZ No [ If yes, see SY-AA-101-106 Does this Design Analysis contain Unverified Assumptions?" Yes 0 No 0 If yes, ATI/AR#:.

This Design Analysis SUPERCEDES: ,8 NA in its entirety.

Description of Revision (list affected pages for partials): ' Original Issue - S&L performed a finite element analysis on the shear lugs for snubber support 1MS06007S to determine the normal stresses on the flaw plane, of the linear indications discovered during A1R14. An Exelon calculation cover sheet and Owner's Review checklist are being attached to the front of the S&L calculation in order to enter it into the Exelon documentation system for future record retrieval purposes.

Preparer: 10 Chee W. Mak . (See page l) 07-13-2009 Print Name Siqn Name ' _ DatA Method of Review: 2, Detailed Review El Alternate Calculations (attached) E Testing [-

Reviewer: 22 Phuong H. Hoang (See page 1) 07-13-2009 Print Name Sign Name Date Review Notes: 23, Independent review Z Peer review El Ex,.a W 6 '04- - Avm CVI t ,16V Mr V., Ur q 4. , ,/Y)

(For External Analyses Only)

External Approver: 24 A. A. Dermenjian (See page 1) 07-13-2009

- Print Name Sio,n Name Date Exelon Reviewer: '* Alan F. Mikottis -- /Y- *OOP Print Name Date Independent 3 rd Party Review Reqd? Yes No No  : -O' 01, Exelon Approver: 27 Raymond J. Belair "/7.

Print Name (r arr4 Date,

CC-AA-309 Revision 8 I Page 17 of 17 ATTACHMENT 2 Owners Acceptance Review Checklist for External Design Analysis (FP4'a ii)

Page I of I DESIGN ANALYSIS NO. 100?- 07ZO9 REV: 0 Yes No N/A

1. Do assumptions have sufficient rationale? El 5] []

2. Are assumpiions compatible with the way the plant is operated and with the 0 licensing basis? []

3. Do the design inputs have sufficient rationale? []

El

[]

4. Are design inputs correct and reasonable? []

[]

5. Are design inputs compatible with the way the plant is operated and with the 5]

licensing basis? []

6. Are Engineering Judgments clearly documented and justified? 5]

[]

Are Engineering Judgments compatible with the way the plant is operated 5]

and with the licensing basis?

Do the results and conclusions satisfy the purpose and objective, of the Design Analysis? 5][ 5]

Are the results and conclusions compatible with the way the plant is operated and with the licensing basis? 55 [

i0 Does the Design Analysis include the applicable design basis 5][ []

documentation?

Have any limitations on the use of the results been identified and transmitted to the appropriate organizations? 5] 5:

12. Are there any unverified assumptions? 5]

Do all unverified assumptions have a tracking and closure mechanism in 5] 59 place?

14. Have all affected design analyses been documented on the Affected 5] 51ý-c Documents List (ADL) for the associated Configuration Change?

Do the sources of inputs and analysis methodology used meet current technical requirements and regulatory commitments? (Ifthe input sources or

15. analysis methodologyare based on an out-of-date methodology or code, additional reconciliation may be required if the site has since committed to a more recent code)

16. Have vendor supporting technical documents and references (including GE DRFs) been reviewed when necessary?

EXELON REVIEWER: ,*,#Ker71 DATE: C?7-/r-Y?.

Print /Sign 7

ISSUE

SUMMARY

Form SOP-0402-07 DESIGN CONTROL

SUMMARY

CLIENT: Exelon UNIT NO.: 1 Page No.: 1 PROJECT NAME: Braidwood Station PROJECT NO.: 11329-121

• NUCLEAR SAFETY- RELATED CALC. NO.: 2009-07204 - [ NOT NUCLEAR SAFETY-RELATED TITLE: Lug Stress Calculation for I MS06007S EQUIPMENT NO.:

IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDNVOIDED & REVIEW METHOD Original Issue INPUTS/ ASSUMPTIONS N VERIFIED

[I UNVERIFIED REVIEW METHOD: Detailed Review REV. 0 STATUS: Approved DATE FOR REV.: 7/13/2009 PREPARER Chee W. Mak DATE: 7/13/2009 REVIEWER Phuong H. Hoang // DATE: 7/1312009 APPROVER A..A. Dermenian DATE: 7/13/2009 IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDNOIDED & REVIEW METHOD INPUTSI ASSUMPTIONS El VERIFIED O UNVERIFIED REVIEW METHOD: REV.

STATUS: DATE FOR REV.:

PREPARER DATE:

REVIEWER DATE:

APPROVER DATE:

IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDIVOIDED & REVIEW METHOD INPUTS/ ASSUMPTIONS O VERIFIED O UNVERIFIED REVIEW METHOD: REV.

STATUS: DATE FOR REV.:

PREPARER DATE:

REVIEWER DATE:

APPROVER DATE:

NOTE: PRINT AND SIGN IN THE SIGNATURE AREAS SOP0402.DOC.

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 2 of Page 18 Lug Stress Calculation for 1MS06007S TABLE OF CONTENTS.

1.0 Purpose and Scope

....................................................................... .............................. Page 3 2.0 Design Input and Assumptions ...................................................................................... Page 4 3.0 References ............................................ .... ................................. ............................... Page 6 4.0 M ethodology ................................................................................................................. Page 7 5.0 Calculation..... ............. I ........................................................................................ Page g.....13 6.0 Results / Conclusion ...................................................................... ......................... Page 14 ATTACHMENTS:

A ANSYS Input .................................................................. ............................

I 25 Pages SOP0402.DOC

L~ArlncIv Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 3 of Page 18 Lug Stress Calculation for 1MS06007S 1.0 PURPOSE AND SCOPE The purpose of this calculation is to determine the normal stresses on the flaw plane of the linear indications identified by the WesDynel-T, data Reports (Reference 3.9) on the lugs of support IMS06007S due to the following loadings\:t MT Axial Force of 100 kips

• Bending moments of 1,000 in-kips

• Pressure loading of 1,000 psi

• Thermal transient stress due to fluid temperature change of 100 0F/hour.

This calculation is applicable for Braidwood Units 1 and 2 provided that the geometry of the lugs and design parameters listed in Section 2 are the same.

S0P0402.DOC

StMg~kft ~L...LscIV, Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 4 of Page 18 Lug Stress Calculation for 1 MS06007S 2.0 DESIGN INPUT & ASSUMPTIONS 2.1 Input Data:

2.1.1 Per component lug and stanchion schedule drawing, Reference 3.3.2, the lug size is 2.5" thick x 5" wide x 16" long with weld size of 1.5". A total of 8 lugs (4 on the top of the pipe clamp and 4 underneath the pipe clamp) are attached to the MS pipe. The MS pipe OD is 32.75" with thickness~of 1.344". The material of the pipe and lug are carbon steel SA-155 Gr. KC65 CLI (which is equivalent to SA-515.Gr. 65 per ASTM A155, Reference 3.4.1) and SA-515 Gr. 65 respectively. The maximum operating temperature and pressure are 557°F and 1092 psig.

2.1.2 Per Appendix I of ASME Section III code, reference 3.1, the coefficients of Thermal Expansion (cc), Thermal Conductivity (K), Density times Specific Heat (pCp) and Modulus of Elasticity (E) for carbon steel are tabulated in Table 1.

Table 1: Material Properties Temp. K pCp E (OF) (Btu/hr-ft-°F) (Btu/ft3 -OF) (in/in/PF* 10-6) (psi* 106) 70 31.50 55.34- 6.07 29.90 100- 31.00 56.27 6.13 29.81 200 30.00 .57.19 6.38 29.50 300 29.10 59.05 6.60 29.00 400 28.10 60.88 6.82 28.30 500. 27.20 62.70 7.02 27.40 600 26.20 64.52 7.23 26.70 700 25.30 67.23 7.44 25.40 S0P0402.DOC

EEý-a f r0 L~Asn dVI' Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 5 of Page 18 Lug Stress Calculation for 1MS06007S

2.2 Assumptions

2.2.1 The thermal transient calculation was based on a very conservative heat transfer film coefficient of 4,000 Btu/(hr*ft2*OF).Thus, no further verification is required.

SOP0402.DOC

~rge.4~ LLU I, CIV" Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 6 of Page 18 Lug Stress Calculation for 1MS06007S

3.0 REFERENCES

3.1 ASME Section III, Division 1 - 1977 Edition.

3.2 ANSYS Finite Element Analysis, Version 11, Sargent & Lundy SVVR 03.7.596-1101, "ANSYS/Mechanical/CFX-FLO, Version 11", Rev. 0, dated 2/8/08, PC-ANSYS64-1.:

3.3 Braidwood Unit 1 Drawings:

3.3.1 M-1MS06007S; Sh.s I & 2, Rev. F.

3.3.2 M-914, Sh. 36, Rev. D.

3.3.3 M-536, Sh. 4, Rev.wR.

3.4 ASTM code:

3.4.1 A155, 1977 Ed..

3.4.2 A515, 1977 Ed.

3.5. CC-AA-309-101 1, Revision 3, General Station Piping Analysis.

3.6 Heat Transfer, by J. P. Holman, 1989 Edition.

3.7 ASME Steam Tables, Third Edition.

3.8 MathCad Version 11.2 Professional, Sargent & Lundy LLC Program Number 03.7.548-11.2.

MT q 3.9 WesDyne JWT data Reports:

.3.9.1 A1R14-MT-00r, dated 3-31-09..

3;9.2 AIRI4-MT-003, dated 4-06-09.

S0P0402.DOC

iiiI i*i!

Client: Exelon D7204 Project:. Brabid-wood,.Sta Project No.s:C11a329-121 age 18 Lug Stress: Calculation 4.0 METHODOLO thie in the component lug and stanchion schedule shown in Figures 4.1 and 4.2 were generated-W!,lig Pl¶401 0 PIk3p -ilining the normal stresses on the flaw plane near the lug fillet toe for loa. i in Section 4.2. A cross section of the shear lugs on the same ied in WesDyne +-U data Reports, Reference 3.9, is selected foj kjut' )n is at the filleti(weld toe (1.5" from the nin~e

.. . . . . . . . . . . . . . . .. . . :n,...::,,.

SOP0402, DOC

. . . . .. . . .. . . aM>; --. *..... . ..

Client: Ex.elon Calc. No. 200 9-07 .204:

Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 8 of Page 18 Lug Stress Calculation for 1MS06007S

. E .LEMENTS

.: -. j:

AN:.:

AR10 Z009 MS Lin. a.d 4 Shear Lii::ý F igure 4.2: MS Pipe Cross Section at Support IMS :06007S i

SOP0402 DOC

4

~trgerT~ ~ Ltand~r *.,...+* :. :

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Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 9ofPage 18 Lug Stress Calculation for 1MS06007S 4.2 Description of Load Cases Analyzed:

4.2.1 Axial Force Fa of 100 kips Unit Load Fa is applied at the top of the vertical pipe model as shown in Figure 4.2.1. This model is constrained at the four welding lugs where. the support clamp contact lines (0.5" from the lug top surface).. . . .

ELEMNTSAN .

MS Line and 4 SherLg Figure 4.2. 1: Axial Load Model S0P0402.DOC

L-cirictv.

Client: Exelon aic. No. 2009-07204 Project: Braidwood Station ~ev. No. 0 Project No.: 11329-121 age No. 10 of Page 18 Lug Stress Calculation for 1MS06 007S 4.2.2 Bending Moments Mb of 1,000 in-kips Unit Load Mb is applied at the top of the vertical pipe model as shown in Figure 4.2.2. This model is constrained at the bottom of a vertical pipe model instead of at the weldi~ng lugs to reflect a bending moment applied to a vertical pipe which is restrained at the center: line of the pipe. Note that, if the shear lug is designed to restrain' bending mroments/pipe rotations, then the lug reaction force due to bending moment should be combi1ned with the lug reaction force'due to the pipe axial load in lug stress calculation. In this section,~only stress due to pipe bending moment (no lug reaction) is calculated.

Unit Load Mb. At The Top and Constraints At The Bottom' Figure 4.2.2: Bending Momcnt Model' SON soo402 DOC

LN

. Client: Exe .on Calc. No. 2009-07204 Project: Braidwood Station - Rev. No. 0 Project No.: 11329-121 Page No. 11 of Page 18 Lug Stress Calculation for 1 MS06007S 4.2.3 Pressure Loading P of 1000 psi Unit pressure loading P is applied on the inner surface of the vertical pipe model as shown in Figure 4.2.3. This model is constrained in vertical direction at the four welding lugs where the support clamp contact lines (0.5" from the lug top surface). Pressure load in piping does not require restraint. However, to avoid rigid body motion, vertical restraints were added. This should not affect the lug stress due to pressure.

AN JULN 23 2009 15: 14: 27 Lu-_Lateral Shear Due Unit P u 1000psil ht Figure 4.2.3: Pressure Loading Model SOP0402 DOC

~g~t~4 LiiricI~j" Client: Exelon Caic. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 12 of Page 18 Lug Stress Calculation for 1MS06007S 4.2.4 Thermal Transient Stress due to Fluid Temperature Change of 1 00F/hour Due to the symmetry of the applied loads on the, pipe model only half of the model is used for the thermal analysis. Piping is initially set at 560'F and then cooling off at a rate of 100 0F/hr with heat transfer coefficient hl of 4,000 Btu((hr*ft2 *OF) applied on the inner surface of the vertical pipe model as shown in Figure 4.2.4. This model is constrained in the pipe axial direction at one end of pipe and free at the other end. Symmetry boundary condition is applied at the half model.

AN 3UN 23 2ý009 14:29:37 PLCT NO. i1 Týerial [Ckxdet D

• k Figure 4.2.4: Thermal Transient Model 4.3 Acceptance Criteria None.

S0P0402.DOC

S~nrdnýý Uundl I Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 13 of Page 18 Lug Stress Calculation for 1MS06007S 5.0 CALCULATION The analyses were performed to determine the normal stresses in the MS support lugs using the methodology stated in Section 4. The analysis input are documented in Attachment A and the the analysis, result are discussed in Section 6.

SOP0402. DOC

L.Rta n CI V r Caic. No. 2009_70 ct: Braidwood Station - Rev. No. 0~

ctNo.: 11329-121 Atress. Calculation for 1MS06007S RESULTS / CONCLUSION cross sec WesDync

), is selected for str( :the Fillel irface) and is paral I to ,cc rur fli the and 31~

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Client: Exelon Cabc. N( .2009-07204 Project: Braidwood Station Rev. No Project No.: 11329-121 Page N ,.15 of Page 18 Lug Stress Calculation for 1MS

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Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. 18 of Page 18 Lug Stress Calculation for 1MS06007S 6.2' Conlusions:

Normal stresses on the flaw plane in the lug at the filletweld toe are summarized in Table 6.

Note that, if the shear lug is designed to restrain bending moments/pipe rotations, then the lug reaction force due to the bending moment should be combined with the lug reaction. force due to the pipe axial load in the lug stress calculation.

Table 6: Stress Summary Applied Loading . Normal Stress' Remarks

:  : (psi)

Axial Force of 100 kips 100.685 Assumes 4 lugs in contact.

Double the stress if only, assuming 2 lugs in contact, which

_______________________________ is normally used for design.

Bending moments of 1,000 in-kips 59.158 Excluding Lug Reaction Force' Pressure loading of 1,000 psi 402.500 Thermal transient stress. 225.925 Due to fluid temperature change

___"_____ ____ _ *______ ____ __". ___of lOO1F/hour SOPG402IDOC

SVOr-gý-* LAuWcIV-Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. Al of Page A25 Lug Stress Calculation for 1 MS06007S Attachment A ANSYS Input Data Files File Date Time Lug.txt 4/10/2009 5:03 pm Lug-I.txt 4/13/2009 4:43 pm lFAPostl.txt 4/10/2009 5:03 pm 1BendPostl .txt 4/10/2009 5:03 pm iPPostl.txt 4/10/2009 5:03 pm 1THPost1A.txt 6/23/2009 2:40 pm SOP0402.DOC

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A2 of Page A25 Lug Stress.Calculation for, lMS06007S Filename: LugS.txt

/NOPR Suppress printing of UNDO process

/PMACRO Echo following commands to log FINISH 1 Make sure we are at BEGIN" level

/CLEAR,NOSTART Clear model since no SAVE found

-/PLOPTS,INFO,3.

/PLOPTS,LEGI, 1

/PLOPTS,LEG2,1

/PLOPTS,LEG3,l

/PLOPTS,FRAME, 1

/PLOPTS,TITLE,,

/PLOPTS,MINM,l

/PLOPTS,FILE,0 iPLOPTS,LOGO, 1

/PLOPTS,WINS,l

/PLOPTS,W?,00

/PLOPTS,DATE,2

/TRIAD,RBOT

/REPLOT

/NOPR

/PMETH,OFF,0 KEYW,PR SET,l KEYW,PRSTRUC,1 KEYW,PRTHERM, 0 KEYW,PRFLUID,0.

KEYW;PRMULTI,0

/GO

/prep7

• ET, I,SOLIDI85BS TREF, 70, '

temp=550 TUNIF,temp, DEFINE MATERIALS ************* * ****** *****DEFINE MATERIALS MATERIAL 1i PIPE & REDUCER MPTEMP,,,,,,,,

MPTEMP, 1,0.,

MPDATA;EX,1l,:,26.93e6 MPDATA,PRXY, ,0 .3 MPDATA, DENS,1,,0. 283/386. 4 SPECIFY PARAMETERS .. ************..***....... ***SPECIFY PARAMETERS OD=32+3/4 PipeTk1l.344 Llug=16 ..

• Wlug-5 HLug"-2.5 SOP0402.DOC

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A3 of Page A25 Lug Stress Calculation for 1MS06007S CREATE GEOMETRY ********** *.* ***CREATE GEOMETRY k, 1000,0,0,0 k,1001,0,0,OD/2 CYL4,0,0,OD/2,0,OD/2-PipeTk,180 WPSTYLE,,,,,,, 1 wpro, 45.000000,,

SAVE

/PNUM, KP, 0

/PNUM, LINE, 0

./PNUM, AREA, 0

/PNUM, VOLU, 1

/PNUM,NODE,0

/PNUM,TABN,0

/PNUM,SVAL,O

/NUMBER,O

/PNUM,ELEM,0

!REPLOT BLC5,0,0,1.5*OD,Wlug BLC5,0,0,Wlug,1.5*OD.

FLST,2, 2, 5,ORDE, 2 FITEM,2,2 E'ITEM, 2,-3 ASBL,P51X, 1 FLST,2,2,5,0RDE,2 FITEM,2,5 FITEM,2,-6 ADELE,P51X, , .1

• KWPAVE, .14 wpoff,Hlug,0,0 wpro, ,,90.000000 ASBW, 4 ADELE, 2, , ,1 KWPAVE, 16 wpoff,0,H1ug,0 wpro,,90.00o0000, ASBW, 7 ADELE, 2, ,

VOFFST,4, LIlug,,

APLOT

• VOFFST,3,Llug, ,

VOFFST,1,Liug, ,q SOP0402.DOC

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A4 of Page A25 Lug Stress Calculation for 1 MS06007S VOFFST,14,2*OD, VOFFST,1,-2*OD, VADD, ALL WPCSYS,-1 VSBW, 6 wpoff,0,0,Llug VSBW, 2 wpoff,0,0,Llug/2 VSBW, 3 wpoff, 0,0,-Llug*2 VSBW, 1 FLST,8,3,4 FITEM,8,68

-FITEM,8,33 FITEM, 8,76 ADRAG, 59,,,,,, P51X VSBA, 4, 27 ADELE, 27, , ,.

KWPLAN,-1, 1000, 14, 1001.

VSBW, 8 KWPLAN,-I, 1000, 13, 1001 VSBW,. . 4 KWPLAN,-1, 1000, 15, 1001 VSBW, 9 KWPLAN,-I, 1000, 16, 1001 VSBW, 11 SAVE GENERATE MESH ***************** GENERATE MESH I**********************4*4* ******** ..

DEFINE NUMBER OF LINE DIVISION Pipe thickness FLST, 5,12,4,ORDE,12 FITEM,5,2 FITEM,5,4 FITEM 5,30

• FITEM 5,32 FITEM,5,38 FITEM, 5,40 FITEM 5,46 FITEM, 5,48 FITEM, 5,61 FITEM,5,64 FITEM,5,69 FFITEM,5,12 CM, Y,LINE LSEL. . . . P5IX CM, YI,L1NE EMSEL,, Y SOP0402.DOC

E enr 4,. LLsncIVW Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A5 of Page A25 Lug Stress Calculation for 1MS06007S LESIZE,_YlI ,.,3,,,,, 1 From Ext-Lug to outer radial FLST,5,4,4,ORDE,2 FITEM,5,55 FITEM,5,-58 CM, _Y, LINE LSEL, , , ,P51X CM, YI,LINE CMSEL,, Y LESIZE, YI, , ,8, , , , 1I Between lugs FLST,5,2,4,ORDE,2 FITEM, 5,53 FITEM,5,-54 CM,_Y,LINE LSEL .I I P51X CM, YI,LINE CMSEL,,_Y LESIZE,_Y, ,1,16,, ,,

From lug to outer axial FLST,5,12,4,ORDE,8 FITEM,5,50 FITEM,5,-51 FITEM,5,65 FITEM, 5,-68 FITEM,5,73 FITEM,5,-76 FITEM,5,80 FITEM,5,-81 CM,_Y,LINE LSEL,. P51X CM, YI,LINE.

CMSEL,, Y LESIZE, YI, , , .. . . . 1 Lug Width FLST, 5,8,4,ORDE, 7 FITEM,5,6 FITEM, 5,-8 FITEM, 5,14 FITEM, 5,-15 FITEM, 5,20 FITEM, 5, 22, FITEM, 5,24 CM, Y,LINE LSEL, ... P51X CM, YI,LINE CMSEL,,_Y SOP0402.DOC

L~arncJIy Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A6 of Page A25 Lug Stress Calculation for 1MS06007S LESIZE, _Y1, , .5,

! Lug Length FLST, 5,8,4,ORDE, 4 FITEM, 5,16 FITEM, 5,-19 FITEM, 5,25 FITEM, 5,-28 CM, Y,LINE LSEL, , , ,PSIX CM, _Y1,LINE CMSEL,,_Y 1*

LESIZE, Y1, , ,15, , , ,i 1*

Lug Height FLST, 5,8, 4,ORDE, 5 FITEM,5,5 FITEM,5,9 FITEM, 5,-13 FITEM, 5,21 FITEM, 5,23 CM,.Y,LINE LSEL, , , ,P51X CM, _Y1,LINE CMSEL,,_Y LESIZE,_YI, , ;5, , , 1

-It Pipe ends FLST,5,8,4,ORDE,8 FITEM,5,1 FITEM, 5,29 FITEM, 5,41 FITEM, 5,-42 FITEM, 5,44

• FITEM,5,60 FITEM,5,62 FITEM,5,70 CM,_Y,LINE LSEL, , . , P51X CM, _YI,LINE CMSEL,,_Y LESIZE,_YI, , ,15,0 2, , ,

MSHAPE, 0,3D MSHKEY, I It CM, Y.VOLU VSEL, , , , 9 CM, Y1,VOLU CHKMSH, 'VOLU CMSELS,_Y VMESH, Y1 SOP0402.DOC

S-qrge~aif*i LA-t-IrCIV Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A7 of Page A25 Lug Stress Calculation for 1MS06007S CMDELE, Y CMDELE, YI CMDELE, Y2 FLST,5,6,6,ORDE,6 FITEM,5,1 FITEM,5,4 FITEM,5, 7 FITEM, 5, -8 FITEM, 5,10 FITEM, 5, 12 CM, _Y,VOLU VSEL ... . P51X CM, _Y1,VOLU CHKMSH, 'VOLU' CMSEL, S, _Y VMESH,_-1 CMDELE, Y CMDELE, CMDELE, Y1 CMDELE, _Y2 FLST, 5,2, 6,ORDE,2 FITEM,5,5 FITEM, 5, -6 CM, Y,VOLU VSEE .... P51X CM, Y1,VOLU CHKMSH, 'VOLU' CMSEL,S, Y 1*

VSWEEP, Y1 CMDELE, Y CMDELE, _Y CMDELE, Y2 FLST,5,2,6 ORDE,2 FITEM,5,2 FITEM,5,-3 CM, _Y,VOLU VSEL, , , P51X CM, Yl,VOLU CHKMSH, 'VOLU' CMSEL,S, Y VMESH _Yl-CMDELE, Y CMDELE, Y1 CMDELE, Y2 C*** Top Constraint for AppliedLoad N, , 0,0, kz (30) ,,,

N, 0,0,kz(30)+l ...

.ET, 2, BEAM4:

SOP0402DOC

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Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A8 of Page A25 Lug Stress Calculation for 1MS06007S R,1, 1,1, 1,1, 1, RMORE, , .

Type, 2 Mat,1 Real, 1 E, 10937,10938 LoadNode=10937 allsel,all*

VSYMM,Y,all,., , ,0,0 NUMMRG,ALL, , , , LOW NSEL,S,LOC, Z,kz(29)

CERIG,10937,ALL,ALL, I I I allsel,all C** Constrains at the lug contact points FLST,2,24,1,ORDE, 16 FITEM, 2,1175 FITEM, 2,1336 FITEM,2,1405 FITEM, 2,-1408 FITEM, 2,2295 FITEM, 2,2456 FITEM, 2,2525 FITEM, 2,-2528' FITEM,2,11041 FITEM,2,11202.

.FITEM,2,11271 FITEM, 2,-11274 FITEM, 2,19651 FITEM, 2,19812 FITEM, 2,19881 FITEM,2,-19884

./GO D, P51X,I I .I ,

IUX, UY,UZ, I I allsel,all

/GO' D,P5!X, ,0, , , ,UZ, . . . .

SAVE FINISH Filename: Lug-l.txt

/NOPR Suppress printing of. UNDO process

/PMACRO Echo following commands to log FINISH Make sure we are at BEGIN level

/CLEARNOSTART. Clear model since no SAVE found

/PLOPTS, INFO, 3

/PLOPTS,LEGi,1

/PLOPTS, LEG2,1

/PLOPTS,LEG3,1

/PLOPTS, FRAME, 1

/PLOPTS,TITLE, 1

/EPLOPTS,MINM,1

/PLOPTS,FILE,O

/PLOPTS, LOGO, 1

/PLOPTS, WINS, 1 SOP0402.DOC

E3~tvg~ru1~ L~arcIV~

$1 Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A9 of Page A25 Lug Stress Calculation for 1MS06007S

/PLOPTS.,WP, 0

/PLOPTS, DATE, 2

/TRIAD, RBOT

/REPLOT

/NOPR

/PMETH,OFF, 0 KEYW,PR_SET,1 KEYW,PR_STRUC,1 KEYW,PR_THERM,0 KEYW,PRFLUID,0 KEYW,PRMULTI,0

/GO

/prep7 ET,1, SOLIDS SOLID5 UX,UY,UZTEMP DOF SET TREF, 70, temp=550 TUNIF,temp,

• SET,DenSTL,0.283

• SET,FFcc, (144*12*DenSTL)

DEFINE MATERIALS********* ........... ***** **********. DEFINE MATERIALS 1* Carbon Steel MPTEMP,1,0 MPDATA, PRXY, I,,.3 MPDATA, DENS,1,,DenSTL MPTEMP,,,,,,,,

MPTEMP, 1,70 MPTEMP, 2,100 MPTEMP, 3,200 MPTEMP, 4,300 MPTEMP, 5,400 MPTEMP, 6, 500 MPTEMP, 7,600 MPTEMP, 8,700 MPDATA, KXX, 1,,31.5/12 IBTtU/hr-in-F MPDATA,KXX,I,,31.0/12

.MPDATA, KXX, 1,,30.0/12 MPDATA, KXXi, ,29.i/12 MPDATA,KXX,1I,,28.1/12 MPDATA,KXX,1,,27.2/12 MPDATA,KXX,1I,,26.2/12 MPDATA,KXX, 1,,25.3/12 MPDATA,C,1,,55.34/(FFcc) !BTU/in^3-F.

• MPDATrA,C,1, ,56,27/ (FFcc)

MPDATA,C-,I,,57;19/(EF'cc)

MPDATA,C,1,,59.05/(FFcc)

MPDATA,C, 1,, 60. 88/(FFcc)

MLPDATA, C, ,,62. 70/ (FFcc)

MPDATA,C-,1,,64.52/(F'Fcc)

MPDATA, C, 1,,67.23/ (F1'cc)

S0P0402.DOC

ý4rgfrI LA-mci'1-Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A10 of Page A25 Lug Stress Calculation for 1MS06007S MPDATA,EX,1,,29.90E÷6 For > .3%C MPDATA,EX,I,,29.81E+6 MPDATA,EX,1,,29.50E+6 MPDATA, EX,1,,29.00E+6 MPDATA,EX,I,,28.30E÷6 MPDATA,EX,1,,27.40E+6 MPDATA,EX,1,,26.70E+6 MPDATA,EX,1,,25.40E+6 MPDATA,ALPX,1,,6.07E-6 MPDATA,ALPX, 1;,6.13E-6 MPDATA,ALPX,1,,6.38E-6 MPDATA, ALPX, 1,,6.60E-6 MPDATA,ALPX,1,,6.82E-6 MPDATA, ALPX, 1,,7.02E-6 MPDATA,ALPX,1,,7.23E-6 MPDATA,ALPX, 1,,7.44E-6 SPECIFY PARAMETERS ********************* .*****.***.,******'***.SPECIFY'PARAMETERS OD=32+3/4' PipeTk=1.344 Llug=16 Wlug=5 HLug=2.5 ID=OD/2-PipeTk CREATE GEOMETRY *********************

• CREATE GEOMETRY k,1000,0'D,0 k,1001,0, 0, OD/2 CYL4,0,0,OD/2,0,OD/2-PipeTk,180 WPSTYLE .... ",,,I' wpro,45.000000,,

SAVE

/PNUM,KP,0

/PNUM, LINE, 0

/PNUM,AREA,0

/PNUM,VOLU,l

/PNUM,NODE, 0

/PNUM, TABN, 0

/PNUM, SVAL, 0

/NUMBER, 0 1*

/PNUM,ELEM, 0

/REPLOT BLC5,0,0,1.5*OD,Wlug BLC5,0,0,Wiug, 1.5*OD FLST, 2, 2, 5, ORDE,2 FITEM, 2,2 FITEM,2,-3 SOP0402.DOC

I..,uriv Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. Al1 of Page A25 Lug Stress Calculation for 1MS06007S ASBL, P51X, 1 FLST, 2,2,5,ORDE,2 FITEM,2,5 FITEM, 2,-6 ADELE,P51X, , ,.

KWPAVE, 14 wpoffH1ug, 0,0 wpro,,, 90.000000 ASBW, 4 ADELE, 2, , ,4 KWPAVE, 16 wpoff,0,Hlug,0 wpro,,90.000000, ASBW, 7 ADELE, 2, , .1 VOFFST, 4, Llug, APLOT VOFFST,3,Llug, VOFFST,I,Llug,-

VOFFST,14,2*OD, VOFFST,I,-2*OD, VADD,ALL WPCSYS,-"

VSBW, 6 wpoff, 0,0,Llug VSBW, 2 wpoff, 0,0,Llug/2 VSBW, 3 wpoff, 0,0,-L1ug*2 VSBW, 1 FLST,8,3,4 FITEM,8,68 L'ITEM,8,33 FITEM,8,76 ADRAG, 59 ...... P51X.

VSBA, 4, 27 ADELE, 27,, ,I KWPLAN,-I, 1000,. 14, 1001 VSBW, 8 KWPLAN,-1, 1000, 13, i001 VSBW, 4 KWPLAN,-I, 1000, 15, 1001 VSBW, 9 KWPLAN,-I, 1000, 16, 1001 SOP0402.DOC

AM!,rt~ ~r~~

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A12, of Page A25 Lug Stress Calculation for 1MS06007S SAVE GENERATE MESH ** ********* *********** GENERATE MESH DEFINE NUMBER OF LINE DIVISION Pipe thickness FLST,5,12,4,ORDE,12 FITEM,5,2 FITEM,5,4 FITEM, 5,30 FITEM,5,32 FITEM, 5,38 FITEM,5,40 FITEM, 5,46 FITEM, 5,48 FITEM, 5,61 FITEM, 5,64 FITEM, 5,69 FITEM,5,72 CM, Y,LINE LSEL, .,. . P51X CM, _Y,LINE CMSEL,,_Y LESIZE,_YI, , 3, , , , 1 From Ext-Lug to outer radial FLST,5,4,4,ORDE, 2 FITEM, 5,55 FITEM,5,-58 CM, Y,LINE LSEL, .. . P51X CM, YI,LINE CMSEL,,_Y LESIZE,_Y, ,,,8,.... 1 Between lugs FLST,5,2,4,ORDE,2 FITEM, 5, 53 FITEM,5,-54 CM, Y,LINE LSEL, .,. . P51X CM, YI,LINE CMSEL, Y LESIZE,_Yl , ,16..,, .1 From. lug to outer axial FLST,5,12,4,0OROE,8 FITEM, 5,50 FITEM5,-551 FITEM, 5,65 FITEM, 5, -68 FITEM,5,73 SOP0402.DOC

S~aroLunrclil-Client: Exelon Caic. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A13 of Page A25 Lug Stress Calculation for 1MS06007S FITEM,5,-76 FITEM,5, 80 FITEM, 5,-81 CM, _Y, LINE LSEL, P51X CM, _YI,LINE CMSEL,,_Y LESIZE,_YI, , ,6 .... 1 Lug Width FLST,5,8,4,ORDE,7 FITEM,5,6 FITEM,5,-8 FITEM, 5,14.

FITEM,5,-15 FITEM,5,20 FITEM, 5,22 FITEM, 5,24.

CM,_Y,LINE LSEL, , , .P51X CM, _YI,LINE CMSEL,, Y LESIZE,_Y,, ,,5, .., 1 1*

Lug Length FLST,5,8,4,ORDE,4 FITEM,5,16 FITEM;5,-19 FITEM, 5,25 FITEM,5,-28 CM, Y,LINE LSEL .... P5lx CM, YI,LINE CMSEL,, _Y 1*

LESIZE,_YI, ,., 15 . . .. 1 Lug Height FLST, 5,8,4,ORDE, 5 FITEM,5,5 FITEM,5,9 FýITEM,5,-13 FITEM,5,21 FITEM,5,23 CM, _Y,LINE LSEL .... PS5X CM, YI,LINE*

CMSEL,,,_Y LESIZE, Y!, , , , ,, ,1 0Pipe ends F*LST, 5,8,4,ORDE 8 SOP0402.DOC

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A14 of Page A25 Lug Stress Calculation for I MS06007S FITEM, 5,.1 FITEM, 5,29 FITEM, 5, 41 FITEM,5,-42 FITEM, 5,.44 FITEM, 5, 60 FITEM, 5, 62 FITEM,5,70 CM, _Y, LINE LSEL, , , , P51X CM, _YI,LINE CMSEL,, _Y" LESIZE, _Yi, , ,15,0.2, ,- "

MSHAPE, 0,3D MSHKEY,1 CM,_Y,VOLU VSEL, , , 9 CM, Y1,VOCLU CHKMSH,'VOLU' CMSEL,S, _Y.

VMESH, YI CMDELE, _Y CMDELE, Y1 CMDELE, _Y2 FLST,5,6,6,ORDE, 6 FITEM,5,1 FITEM,5,4 FITEM,5,7.

FITEM,5,-8 FITEM,5,10 FITEM,5,12 CM, Y,VOLU VSEL. .,. . Pi5X CM, Y1,VOLU CHiKMSH, 'VOLU' CMSEL,S, _Y VMESH,_Y'1, CMDELE, _Y CMDELE, 7 Li CMDELE, _Y2 FLST, 5, 2,6OD, FITEM, 5,5.

FI'rEM*5,-6,

• CM, Y,VOLU VSEL, , P51X C-M, Y1,VOLJ CI-IMSH, 'VOLU.

CMSELC,S, _Y VSWEEP, Y1i S0P0402.DOC.

~rgEEtt~ LIarlcEv Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A15 of Page A25 Lug Stress Calculation for 1MS06007S CMDELE, _Y CMDELE, _Yl CMDELE, Y2 FLST, 5,2,6, ORDE, 2 FITEM, 5,2 FITEM, 5, -3 CM, _Y,VOLU VSEL . . . P51X CM, _Y!,VOLU CHKMSH, 'VOLU' CMSEL,S, _Y VMESH, _Yl CMDELE, Y CMDELE, Y1 CMDELE, Y2 FLST,5,9,5,ORDE,9 FITEM, 5,15 FITEM, 5,23 FITEM, 5,35 FITEM,5,40 FITEM, 5,50 FITEM, 5,53 FITEM, 5,-54 FITEM, 5,58 FITEM, 5,61 ASEL,S, , . P51X CM, HFACE,AREA Filename: IFAPostl.txt

/INPUT,'lugS','txt'

/SOL ANTYPE,0 C*** Unit load of IE6 in-lbf F,10937,FZ,100000 SOLVE FINISH

/POSTI SET,1 NWPLAN,-1, 19811, 19652, 19806 SUCR, LugI,CPLANE,40,-

CSWPLA,11,1,1,1, RSYS,11 STJMAP, sz, S, Z SIIMAP,Syz S,YZ SUMAP, Sxz, S, Xl

/RGB, INDEX, 100,100, 100, 0

/RGB,IND1EX, 80, 80, 80,13 SOP0402.DOC

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A16 of Page A25 Lug Stress Calculation for 1.MS06007S

/RGB,INDEX, 60, 60, 60,14

/RGB,INDEX, 0, 0, 0,15

/REPLOT

/SHOW, PNG PNGR, COMP, 1, -1 PNGR, ORIENT, HORIZ PNGR, COLOR, 2 PNGR,TMOD,I

/GFILE,800,

/VIEW,l ,,1

/UDOC,1,CNTR,RIGH SET, FIRST

/TITLE,Lug Normal Stress Due to Unit Axial Load 1E+05 lbf SUPL,LUGI;SZ,0

/TITLE,Lug Vertical Shear Due to Unit Axial Load 1E+05 lbf SUPL, LUGI,SYZ, 0

/TITLE,Lug Lateral Shear Due to Unit Axial Load 1E+05 lbf SUPL,LUG1,SXZ,0

/SHOW,CLOSE

/DEVICE,VECTOR-,0

/RGB,INDEX, 0, 0, 0, 0

/RGB,INDEX, 60, 60, 60,13

/RGB,INDEX, 80, 80, 80,14

/RGB, INDEX, 100,100,100,15

/REPLOT Filename: lMendPostl.txt

/INPUT,'lugs., 'txt

/SOL 1*

ANTYPE,0 C*** Unit load of 1E6 in-lbf F,10937,MY,707000 F,10937,MX,707000 SOLVE FINISH

/POSTI SET, 1 NWPLAN,-I, 19811, 19652, 19806-SUCR, Lugl,CPLANE, 40, CSWPLA, 11,1, 01, 1 RSYS,!I SUMAP,sz,S,Z SUMAP,SyzS,YZ SUMAP, Sxz, S, XZ

/RGB,INDEX,100,100,100, 0

/RGB, INDEX, 80, 80, 80,13

/RGB, INDEX, 60, 60, 60, L4

/RGB, INDEX, 0, 0, 0,15

/ RE PLOT SOP0402.DOC

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. Al 7 of Page A25 Lug Stress Calculation for 1 MS06007S

/SHOW,iPNG PNGR,COMP,I,-i PNGR,ORIENT,HORIZ "PNGR,COLOR,2 PNGR,TMOD,.

/GFILE,800,

/VIEW, I,,I

/UDOC, 1,CNTR,RIGH SET, FIRST

/TITLE,Lug Normal Stress Due to Unit Bending Moment 1E+06 in-lbf SUPL,LUG1,SZ,0

/TITLE,Lug Vertical Shear Due to Unit Bending Moment IE+06 in-lbf SUPL, LUGI,SYZ, 0

/TITLE,Lug'Lateral Shear Due to Unit Bending Moment 1E+06 in-lbf SUPL,LUG1,SXZ,0

/SHOW, CLOSE

/DEVICE,VECTOR, 0 .i

/RGB,INDEX, 0, 0, 0, 0.

RGB, INDEX, 60, 60, 60,13

/RGB,INDEX, 80, 80, 80,14

/RGB, INDEX, 100,100,100,15 IREPLOT Filename: lPPostl.txt

/INPUT,'IlugS', txt b

"/SOL ANTYPE,O C*** Unit load of 1000 p si FLST,2,18,5,ORDE,17 FITEM, 2,15 FITEM,2,23" FITEM,2,35 .

FITEM,2, 40 FITEM,2,50 FITEM,2,53 - "

FITEM,2,-54 FITEM,2,58 FITEM,2,61 FITEM,2, 67 FITEM,2,15 FITEM,2,78 FITEM, 2, 87b FITEM,2,92 FITEM, 2,ý108 FITEM,2,112 FITEM,2,-14

,/GO SFA, P51X,1,PRES, 1000

• DDELE,ALL,UX DDELE, ALL,UY SOLVE SOP0402.DOC

"W Lianrciv Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A18 of Page A25 Lug Stress Calculation for 1MS06007S FINISH

/1OST1 SET, 1 NWPLAN,-i, 19811, 19652, 19806 SUCRLugl,CPLANE, 40, CSWPLA, 11, 1, i, 1, RSYS, 11 SUMAP, sz, S, Z SUMAP, Syz, S,.YZ SUMAP,Sxz,S,XZ

/RGB,INDEX,100,100,100, 0

/RGB,INDEX, 80, 80, 80,13

/RGB,INDEX, 60, 60, 60,14

/RGBINDEX, 0, 0, 0,15

/REPLOT

/SHOW, PNG PNGR,COMP,I,-i PNGR,ORIENT,HORIZ PNGR,COLOR,2 PNGR,TMOD,1

/GFILE, 800,

/VIEW, 1, , 1

/UDOC,1,CNTR;RIGH SET, FIRST.

/TITLE,Lug Normal Stress Due to Unit Pressure of 1000 psi SUPL,LUG1,SZ,0

/TITLE,Lug Vertical Shear Due to Unit Pressure of 1000 psi SUPL,LUG1,SYZ,0

/TITLE, Lug Lateral Shear Due to Unit Pressure of 1000 psi SUPL,LUG1,SXZ,0

/SHOW,CLOSE

/DEVICE,VECTOR,0

/RGB,INDEX, 0, 0, 0, 0

/RGBINDEX, 60, 60, 60,13

/RGB,INDEX, 80, 80, 80,14

/RGB,INDEX, 100,100,100,15

./REULOT Filename: ITHPostlA.txt

!/INPUT,'Lug-l','txt','.\MS-Lug\',, 0!

/PSF,CONV,HCOE,2,0,1

/PBF,DEFA', l1

/PIC,DEFA, ,I

/PBC,ALL,,1 FLST, 2, 5, 5,OR.DE, 5 FITEM,2,14 FITEM,2, 16 FITEM, 2,22 FITEM, 2, 34 FITEM, 2" 39 SOP0402.DOC

S4%getvQA LurLacv, Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A19 of Page'A25 Lug Stress Calculation for I MS06007S DA,251X,SYMM FLST,2,5,5,ORDE, 5 FITEM, 2,18 FITEM, 2,20 FITEM, 2,32 FITEM, 2,36 FITEM, 2,41 DA, P51X SYMM DA, 19, SYMM FLST,2,1,5,ORDE, I FITEM, 2,19 DA,,P51X, UZ,._

ALLSEL, ALL

!KEYW,PR_STRUC,0

!KEYWPR_THERM,I FINISH

/SOL ANTYPE,4 TRNOPT,FULL LUMPM,0 AUTO, on OUTPR, ALL, ALL, OUTres,ALL, ALL, KBC,0 TIMINT,0,STRUCT TIMINT,1,THERM TUNIF, 560.0, IC,ALL,Temp, 560.0 htc=4000/144 !h= 4000 BTU/hr-ft^2-F Time, 0.00001 NSUBST, I,1,1 CMSEL,S,HFACE SFA,ALL, ,CONV,htc,560 ALLSELALL SOLVE Time, 1.0 LS=2 Nsub, 60,100,60 CMSEL, S,HFACE SFA,ALL, ,CONV,htc,460 ALLSELALL SOLVE Time, 3.0 LS-3 Nsub,20,100,20 CMSEL, S,HFACE SFA, ALL, ,CONV, htc,260 ALLSEL, ALL

!SOLVE Time, 5.0 LS- 4 Nsub, 10,100, 0 SOP0402-DOC

3Strir ft Lkin cNv Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A20 of Page A25 Lug Stress Calculation for 1MS06007S CMSEL, S, HFACE SFAALL, ,CONV,htc,60 ALLSEL, ALL

!SOLVE FINISH

/POST!

NWPLAN,-I, 2455, - 2296, 2450 SUCR, Lugl, CPLANE, 40, CSWPLA, 11,1,1,1, RSYS, 1i SET, 2, 40, 1 SUMAP, sz, S, Z SUMAPSyz,S,YZ SUMAP,Sxz,S,XZ

/RGB, INDEX,100,100,100, 0

/RGB,INDEX, 80, 80, 80,13

/RGB,INDEX, 60, 60, 60,14

/RGB,INDEX, 0, 0, 0,15

/REPLOT

/SHOW, PNG PNGR, COMP, 1, -1 PNGR, ORIENT, HORIZ PNGR, COLOR, 2 PNGR, TMOD,.1

/GFILE, 800,

/VIEW, i, , 1

/UDOC, i, CNTR, RIGH

/TITLE,Lug Normal Stress Due to Cool Down Thermal Transient 100F/hr SUPL,LUG1, SZ, 0

/TITLE,Lug Vertical Shear Due to Cool Down Thermal Transient 10OF/hr SUPL,LLUG1,SYZ,0

/TITLELug Lateral Shear Due to Cool Down Thermal.Transient 100/hr SUPL.LUG1, SXZ, 0

/SHOW,CLOSE

/DEVICE,VECTOR,0

/RGB, INDEX, -0, 0, 0, 0

/RGB,INDEX, 60, 60, 60,13

/RGB,INDEX, 80, 80, 80, 14

/RGB, INDEX, 100, 100, 100, 15

/ REPLOT S0P0402.oOC

~tvgerI1L& LiridyI Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A21 of Page A25 Lug Stress Calculation for 1MS06007S ANSYS Program File Listing (PC ANSYS64-1)

Volume in drive C has no label.

Volume Serial Number is 84E4-E259 Directory Of C:\Program Files\ANSYS Inc\vll0\ANSYS\bin\winx64 11/08/2007 11:16 AM <DIR>

11/08/2007 11:16 AM <DTR>

08/31/2007 12:04 AM 19,968 acon.exe 06/22/2007 03:04 PM 158,208 animate.exe 08/31/2007 12:21 AM 1,571.anstclshllO.bat 08/31/2007 12:21 AM 1,580 answishllO*bat 09/05/2007 10:26 AM 71,350,272 ANSYS.exe 08/31/2007 03:37 AM 31,744 ANSYS1IO.exe 03/31/2006 03:03 AM 7,048 ansysll0.ver 11/08/2007 10:42 AM <DI:R>, ANSYSLM 08/31/2007 12:21 AM 739 ansysservllO.bat.

08/31/2007 12:20 AM 19,813 ansystsllO 08/31/2007 12:21 AM. 323 ansystsllO.bat, 02/21/2007 03:53 PM 61,440 ans admin.exe 01/20/2002 12:57 PM 671,744 asmutils.dll 08/31/2007 03:36 AM 64,512 binlib.dll 08/31/2007 12:52 AM 16,461,312 cadoe.dll 11/08/2007 10:42 AM <DIIR> DANSYSMPICH 11/08/2007 10:42 AM <DI)R> DANSYSMSMPI 09/19/2002 04:28 PM 2,142,277 DataViz370-dll 03/30/2006 12:56 PM 462,848 DFORMD.dll 08/31/2005 04:13 PM 126,976 dispinfo.exe 08/30/2007 05:25 PM 466,944 DisplayW.exe 10/05/2000 04:54 PM 438,342 DSGStreamN.dll 11/08/2007 11:14 AM 204 file.err 04/12/2006 10:02 AM 36,864 gus.exe 09/24/2002 02:48 PM 196,679 HardCopy370.dll 11/23/2004 04:03 PM 283,136 ifdlglOO.dll 09/24/2002 02:49 PM 4,833,365 Inv3ll.dll 09/19/2002 04:28 PM 98,304 Invr31l.dll 09/24/2002 02:49 PM 442,454 Invw311.dll 08/17/2004 01:36 PM 150,528 jpeg62.dll 01/26/2006 11:06 AM 45,056 lauricherllO.exe 10/23/2000 09:00 PM 217,600 libcpepcf9Omd.dll 09/20/2006 05:49 PM 243,200 libguide40.dll 11/04/2006 07:47 AM 328,192 libguide40.stats.dll 11/04/2006 07:48 AM 757,760,libifcoremd.dll 11/04/2006 07:48 AM 757,760 libifcoremdd.dll 11/04/2006 07:48 AM 746,496 libifcorert.dll 11/04/2006 .07:48 AM 746,496 libifcorertd.dll 11/04/2006 07:49 AM 147,968 libifportmd..dll 09/20/2006 .08:22 PM 6,144 libimalloc.dll 11/04/2006 07:50 AM 2,192,896 libmmd.dll 11/04/2006 07:51 AM 2,213,888 libmmdd.dll 11/04/2006 07:47 AM 108,544 libompdb.dll 10/20/2004 03:12 PM 396,288 libtiff.dll 06/12/2007 12:45 PM 71,832,576 is971_MPPDP.exeSave

.03/07/2002 12:47 PM 65 machines 03/18/2003 10:20 PM 1,060,864 mfc7l.dll.

10/03/2006 04:26 PM 4,129,792 mkl def.dll 09/20/2006 08:10 PM 940,544 mkl ias.dll 09/20/2006 08:10 PM 2,648,064 mkl_lapack32.dll 09/20/2006 08:10 PM 2,703,872 mkllapack64.dlI 10/03/2006 04:27 PM 4,938,752 mklmc.dll 10/03/2006 04:26 PM 5,784,576 mkl_p4n.dll 10/03/2006 04:06 PM 2,392,576 mkl-vml-def.dll 10/03/2006 04:20 PM 3,043,840 mkl vml-mc.dll 10/03/2006 04:12 PM 3,021,312 mkl vmlp4n.dll 08/31/2007 01:05 AM 388,096 mnflib.dll 05/07/1999 12:00 AM 645,616 MSCOMCT2.OCX 03/25/2005 08:00 AM 941,568 msvcp60.dll SOP0402.DOC

V" NI~

Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A22 of Page A25 Lug Stress Calculation for 1MS06007S 03/30/2006 12:56 PM 348,160 msvcr7l.dll 08/31/2007 12:20 AM 1,587 nlhistllO.bat

.09/01/2004 03:22 PM 120,832 png.dll 09/24/2002 02 :49 PM 3,751,936 qt-mt305.dll 09/22/2003 11:28 AM 3,129,344 splash.exe 11/04/2006 07:53 AM 286,720 svml -dispmd.dll 12/22/2006 05:02 AM 17,944,576 sxpost.exe 12/09/2004 03:50 PM 627,200 tc183.dll 10/03/2006 01:55 PM 859,648 tc184.dll 07/18/2005 09:30 AM 17,408 tclddel2.dll 12/09/2004 03:50 PM .13,824 tcldde83.dll 12/09/2004 03:50 PM 27,136 tclpip83.dll 07/18/2005 09:30 AM 6,656 tclpip84.dll 07/18/2005 09:30 AM 18,944 tclregll.dll 12/09/2004 03:50 PM 15,360 tclreg83.dll 10/03/2006 01:55 PM 11,776 tclsh.exe 10/03/2006 01:55 PM 11,776 tclsh84.exe' 04/17/2003 02:58 PM 915,968 tiff.dll 12/09/2004 04:04 PM 924,160 tk83.dll 03/14/2005 03:24 PM 1,374,208 tk84.dll 03/14/2005 03:24 PM 16,896'wish.exe 03/14/2005 03:24 PM 16,896 wish84.exe" 04/20/1998 12:08 PM 125,440 wntshell.exe 09/01/2004 03:21 PM 55,808 zlib.dll 80 File(s) 242,531,855 bytes Directory of C:\Program Files\ANSYS Inc\vllo\ANSYS\bin\winx64\ANSYSLM 11/08/2007 10 :42 AM <DIR>

11/08/2007 10:42 AM <DIR>.

09/05/2007 01:50 PM 70,265,856 ANSYS.exe 01/20/2002 12:57 PM 671,744 asmutils.dll 08/31/2007 03:36 AM 64,512 binlib.dll 08/31/2007 12:52 AM 16,461,312 cadoe.dll 09/19/2002 04:28 PM 2,142,277 DataViz370.dll 03/30/2006 12:56 PM 462,848 DFORMD.dll .

10/05/2000 04:54 PM 438,342 DSGStreamN.dll 09/24/2002 02:48 PM 196,679 HardCopy370.dll 11/23/2004 04:03 PM 283,136 ifdlgloo.dll 09/24/2002 02:49 PM 4,833,365 Inv3ll.dll 09/19/2002 04:28 PM 98,304 Invr3ll.dll 09/24/2002 02:49 PM 442,454 Invw3ll.dll 08/17/2004 01:36 PM 150,528 jpeg62.dll 10/23/2000 09:00 PM 217,600 libcpepcf90md.dll 09/20/2006 05:49 PM 243,200 libguide40.dll 11/04/2006 07:47,AM 328,192 libguide4ostats;dll 11/04/2006 07 48 AM .757,760 libifcoremd.dll 11/04/2006 07.48 AM 757,760 libifcoremdd.dll 746,496 11/04/2006 07 48 AM libifcorert.dll 11/04/2006 07 48 AM 746,496 libifcorertd.dll 11/04/2006 07:49 AM 147,968 libifportmd.dll 09/20/2006 08:22 PM 6,144 libimalloc.dll 11/04/2006 07:50 AM 2,192,896 libmnmd.dll 11/04/2006 07:51 AM 2,213,888 libmmdd.dll 11/04/2006 07:47 AM 108,544 libomp_db.'dll 10/20/2004 03:12 PM 396,288 -libtiff.dll.

03/18/2003 10:20 PM 1,060,864 mfc71.dll .

10/03/2006 04:26 PM 4,129,792 mkl def.dll 08/21/2005 06:58 PM 6,816,256 mkl~i2p.dll' 09/20/2.006 08:10 PM 940,544 mkl ias.dll 09/20/2006 08:10 PM 2,648,064 mkl-lapack32.dll 09/20/2006 .08:10 PM 2,703,872 mkl-lapack64.dll 10/03/2006 04:27 PM 4,938,752 mkl-mc.dll 10/03/2006 04:26 PM 5,.784,576 mkl~p4n.dll 10/03/2006 04:06 PM 2,392,576 mkl vmlndef.dll 08/11/2005 02:31 PM 1,562,112 mkl vml i2p.'dll 10/03/2006 04:20 PM 3,043,840 mkl vml mc.dll 10/03/2006 04:12 PM 3,021,312 mkl-vm1lp4n.dll 08/31/2007 01:05 AM 388,096 mnflib.dll SOP0402.DOC

4,r.aJlndv-Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A23 of Page A25 Lug Stress Calculation for 1MS06007S 03/25/2005 08:00 AM 941,568 msvcp6O.dll 03/30/2006 12:56 PM 348,160 msvcr7l.dll 09/01/2004 03:22 PM 120,832 png.dll 09/24/2002 02:49 PM 3,751,936 qt-mt305.dll 11/04/2006 07:53 AM 286,720 svml_dispmd.dll 12/09/2004 03:50 PM 627,200 tc183.dll 10/03/2006 01:55 PM 859,648 tc184.dll 07/18/2005 09:30 AM 17,408 tclddel2.dll 12/09/2004 03:50 PM .13,824 tcldde83.dll 12/09/2004 03:50 PM 27,136 tclpip83.dll 07/18/2005 09:30 AM 6,656 tclpip84.dll 07/18/2005 09:30 AM 18,944 tclregll.dll 12/09/2004 03 50 PM 15,360 tclreg83.dll 10/03/2006 01:55 PM 11,776 tclsh.exe 10/03/2006 01:55 PM 11,776 tclsh84.exe 04/17/2003 02:58 PM 915,968 tiff.dll 12/09/2004 04:04 PM 924,160 tk83.dll 03/14/2005 03:24 PM 1,374,208 tk84.dll 09/01/2004 03:21 PM 55,808 zlib.dll 58 File(s) 155,134,333 bytes Directory of C:\Program Files\ANSYS Inc\vllO\ANSYS\bin\winx64\DANSYSMPICH 11/08/2007 10:42 AM <DIR>

11/08/2007 10:42 AM <DIR>

09/05/2007 01:46 PM 77,097,984 ANSYS.exe 01/20/2002 12:57 PM 671,744 asmutils.dll 08/31/2007 03:36 AM .64,512 binlib.dll 08/31/2007 12:52 AM 16,461,312 cadoe.dll 09/19/2002 04:28 PM 2,142,277 DataViz370.dll 03/30/2006 12:56 PM 462,848 DFOPMD.dll 10/05/2000 04:54 PM 438,342 DSGStreamN.dll 09/24/2002 02:48 PM 196,679 INardCopy370.dll 11/23/2004 04:03 PM 283,136 ifdlglOO.dll 09/24/2002 02:49 PM 4,833,365 Inv3ll.dll 09/19/2002 04:28 PM 98,304 Invr3ll.dll 09/24/2002 02:49 PM 442,454 Invw3ll.dll 08/17/2004 01:36 PM 150,528,jpeg62.dll 10/23/2000 09:00 PM 217,600 libcpepcf9Qmd.dll 09/20/2006 05:49 PM 243,200 libguide40.dll 11/04/2006 07:47 AM 328,192 libguide40_stats.dll 11/04/2006 07:48 AM 757,760 libifcoremd.dll 11/64/2006 07:48 AM 757,760 libifcoremdd.dll-11/04/2006 07:48 AM 746,496 libifcorert.dll 11/04/2006 07:48 AM 746,496 libifcorertd.dll 11/04/2006 07:49 AM 147,968 libifportmd.dll 09/20/2006 08:22 PM 6,144 libimalloc.dll 11/04/2006 07:50 AM 2,192,896 libmmd.dll 11/04/2006 07:51 AM 2,213,888 libmmdd.dll 11/04/2006 07:47 AM 108,544 libomp_db.dll 10/20/2004 03:12 PM 396,288 libtiff.dll 03/18/2003 10:20 PM 1,060,864 mfc7l.dll 10/03/2006 04:26 PM 4,129,792 mkl def.dll 09/20/2006 08:10 PM 940,544 mkl ias.dll.

09/20/2006 08:10 PM -2,648,064 mkllapack32.dll 09/20/2006 08:10 PM 2,703,872 mkllapack64.dll 10/03/2006 04:27 PM 4,938,752 mkl mc.dll 10/03/2006 04:26 *PM 5,784,576 mkl~p4n.dll 10/03/2006 04:06 PM 2,392,576 mkl-vml-def.dll 10/03/2006 04:20 PM 3,043;840 mkl vmlmc.dll 10/03/2006 04:12 PM 3,021,312 mkl vml p4n.dll 08/31/2007 01:05 AM 388,096 mnflib.dll 08/31/2007. 03:44 AM 5,632 mpitestmpich.exe 03/25/2005 08:00 AM 941,568 msvcp60.dll 03/30/2006 12:56 PM 348,160 msvcr7l.dll 09/01/2004 03:22 PM 120,832. png.dll 09/,24/2002 02:49 PM 3,751,936 qt-mt305.dll 11/04/2006 07-53 AM 286,720 svml_dispmd.dll 12/09/2004 03: 50 PM 627,200 tc183.dll SOP0402.DOC

BSlfgftrit"\ LEL~rIdJV' Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A24 of Page A25 Lug Stress Calculation for 1MS06007S 10/03/2006 01:55 PM 859,648 tc184.dll 07/18/2005 09:30 AM 17,408 tclddel2.dll 12/09/2004 03:50 PM 13,824 tcldde83.dll 12/09/2004 03:50 PM 27,136 tclpip83.dll 07/18/2005 09:30 AM 6,656 tClpip84.dll 07/18/2005 09:30 AM 18,944 tclregll.dll 12/09/2004 03:50 PM 15,360 tclreg83.dll 10/03/2006 01:55 PM 11,776 tclsh.exe 10/03/2006 01:55 PM 11,776 tclsh84.exe 04/17/2003 02:58 PM 915,968 tiff.dll 12/09/2004 04:04 PM 924,160 tk83.dll 03/14/2005 03:24 PM 1,374,208 tk84.dll 09/01/2004 03:21 PM 55,808 zlib.dll 57 File(s) 153,593,725 bytes Directory of C:\Program Files\ANSYS Inc\vllO\ANSYS\bin\winx64\DANSYSMSMPI 11/08/2007 10:42 AM <DIR>

11/08/2007 10:42 AM <DIR>

09/05/2007 01:44 PM 77;097,984 ANSYS.exe 01/20/2002 12:57 PM 671,744 asmutils.dll 08/31/2007 03:36 AM 64,512 binlib.dll, 08/31/2007 12:52 AM 16,461,312 cadoe.dll 09/19/2002 04:28 PM 2,142,277 DataViz370.dll 03/30/2006 12:56 PM 462,848 DFORMD.dll 10/05/2000 04:54 PM 438,342 DSGStreamN.dll 09/24/2002 02:48 PM 196,679 HardCopy370.dll 11/23/2004 04:03 PM 283,136 ifdlglOO.dll.

09/24/2002 02:49 PM 4,833,365 Inv3ll.dll 09/19/2002 04:28 PM 98,304 Invr3ll.dll 09/24/2002 02.:49 PM 442,454 Invw3ll.dll 08/17/2004 01:36 PM 150,528 jpeg62.dll 10/23/2000 09:00 PM 217,600 libcpepcf9Omd.dll 09/20/2006 05:49 PM 243,200 libguide40.dll 11/04/2006 07:47 AM 328,192 libguide40_stats.dll 11/04/2006 07:48 AM 757,760 libifcoremd.dll 11/04/2006 07:48 AM 757,760 libifcoremdd.dll 11/04/2006 07:48 AM 746,496 libifcorert.dll 11/04/2006 07:48 AM 746,496 libifcorertd.dll 11/04/2006 07:49 AM 147, 968 libifportmd.dll 09/20/2006 08:22 PM 6,144 libimalloc.dll 11/04/2006 07:50 AM 2,192,896 libmmd.dll 11/04/2006 07:51 AM 2,213,888 libmmdd.dll 11/04/2006 07:47 AM 108,544 libompdb.dll 10/20/2004 03 :12 PM 396,288 libtiff.dll 03/18/2003 10:20 PM 1,060,864 mfc7l.dll 10/03/2006 04:26 PM 4,129,792 mkl def.dll 09/20/2006 08:10 PM 940,544 mkl ias.dll 09/20/2006 08:10 PM 2,648,064 mkl lapack32.dll 09/20/2006 08:10 PM 2,703,872 mkl_lapack64.dll 10/03/2006 04:27 PM 4,938,752 mkl-mc.dll 10/03/2006 04:26 PM 5,784,576 mkl-p4n~dll 10/03/2006 04:06 PM 2,392,576 mklvmldef.dll 10/03/2006 04:20 PM 3,043,840 mklvmlmc.dll 10/03/2006 04:12 PM 3,021,312 mkl vmlp4n.dll.

08/31/2007 01:05 AM 388,096 mnflib.dll

• 08/31/2007 03:43 AM 5,632 mpitestmsmpi.exe 03/25/2005 08:00 AM 941,568 msvcp6O.dll 03/30/2006 12:56 PM 348,160 msvcr7l.dll 09/01/2004 03:22 PM 120,832 png.dll .

09/24/2002 02:49 PM 3,751,936 qt-mt305.dll 11/04/2006 07:53 AM 286,720 svmldispmd.dll 12/09/2004 03:50 PM 627,200 tc183.dll 10/03/2006 01:55 PM 859;648 tc184.dll 07/18/2005 09:30 AM 17,408 tclddel2..dll 12/09/2004 03:50 PM 13 , 824' tcldde83.dll 12/09/2004 03:50 PM 27, 136 tclpip83.dll 07/18/2005 09:30 AM 6,656 tclpip84.dll S0P0402.DOC

LtmincIVI Client: Exelon Calc. No. 2009-07204 Project: Braidwood Station Rev. No. 0 Project No.: 11329-121 Page No. A25 of Page A25 Lug Stress Calculation for 1MS06007S 07/18/2005 09:30 AM 18,944 tclregll.dll 12/09/2004 03:50 PM 15,360 tclreg83.dll 10/03/2006 01:55 PM 11,776 tclsh.exe 10/03/2006 01:55 PM 11,776 tclsh84 ;exe 04/17/2003 02:58 PM 915,968 tiff.dll 12/09/2004 04:04 PM 924,160 tk83.dll 03/14/2005 03:24 PM 1,374,208 tk84.dll 09/01/2004 03:21 PM 55,808 zlib.dll 57 File(s) 153,593,725 bytes Total Files Listed:

252 File(s) 704,853,638 bytes 11 Dir(s) 97,437,290,496 bytes free S0P0402.DOC