ML092930135
| 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
Exelkn.
Nudear ATTACHMENT 1 Design Analysis Major Revision Cover Sheet Page I of I CC-AA-309-1001 Revision 4 Design Analysis (Major Revision)
Last Page No. 18 & A25 (Page i)
Analysis No.:'
2009-07204 Revision:
0
Title:
Lug Stress Calculation for 1 MS06007S 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-1 01-106 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 1 MS06007S 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 Print Name (See page l)
Siqn Name 07-13-2009 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 M r V.,
U r 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 Page I of I (FP4'a i i)
DESIGN ANALYSIS NO.
100?- 07ZO9 REV:
0
- 1.
Do assumptions have sufficient rationale?
- 2.
Are assumpiions compatible with the way the plant is operated and with the licensing basis?
- 3.
Do the design inputs have sufficient rationale?
- 4.
Are design inputs correct and reasonable?
- 5.
Are design inputs compatible with the way the plant is operated and with the licensing basis?
- 6.
Are Engineering Judgments clearly documented and justified?
Are Engineering Judgments compatible with the way the plant is operated and with the licensing basis?
Do the results and conclusions satisfy the purpose and objective, of the Design Analysis?
Are the results and conclusions compatible with the way the plant is operated and with the licensing basis?
i0 Does the Design Analysis include the applicable design basis documentation?
Have any limitations on the use of the results been identified and transmitted to the appropriate organizations?
- 12.
Are there any unverified assumptions?
Do all unverified assumptions have a tracking and closure mechanism in place?
1 4.
Have all affected design analyses been documented on the Affected Documents List (ADL) for the associated Configuration Change?
Do the sources of inputs and analysis methodology used meet current technical requirements and regulatory commitments? (If the 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 Print /Sign 7
Yes 0
No El 5]
[]
[]
[]
[]
[]
N/A El
[]
[]
[]
5]
5]
5]
5][
5]
55
[
5][
[]
5]
5]
5]
5]
5:
59 51ý-c DATE: C?7-/r-Y?.
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..................
g.....
I........................................................................................
Page 13 6.0 Results / Conclusion......................................................................
Page 14 ATTACHMENTS:
A ANSYS Input..................................................................
I
............................ 25 Pages SOP0402.DOC
L~ArlncIv Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S 1.0 PURPOSE AND SCOPE Calc. No. 2009-07204 Rev. No. 0 Page No. 3 of Page 18 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 1 00 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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. 4 of Page 18 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 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 r0 f
L~Asn dVI' Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. 5 of Page 18
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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. 6 of Page 18
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.
3.6 CC-AA-309-101 1, Revision 3, General Station Piping Analysis.
Heat Transfer, by J. P. Holman, 1989 Edition.
3.7 ASME Steam Tables, Third Edition.
3.8 MathCad Version 11.2 Professional, Sargent 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.
& Lundy LLC Program Number S0P0402.DOC
Client: Exelon Project:. Brabid-wood,.Sta Project No.s:C11a329-121 Lug Stress: Calculation 4.0 METHODOLO D7204 age 18 iiiI i*i!
thie in the component lug and stanchion schedule shown in Figures 4.1 and 4.2 were generated-
-ilining the normal stresses on the flaw plane i in Section 4.2. A cross section of the shear ied in WesDyne +-U data Reports, Reference
)n is at the filleti(weld toe (1.5" from the nin~e W!,lig Pl¶401 0
PIk3p near the lug fillet lugs on the same 3.9, is selected foj
- n,...: :,,.
toe for loa.
kjut' SOP0402, DOC
Client: Ex.elon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S aM >;
Calc. No. 200 9-07.204:
Rev. No. 0 Page No. 8 of Page 18 F
E
.LEMENTS AN:.:
j:
AR10 Z009 MS Lin.
a.d 4 Shear Lii::ý igure 4.2: MS Pipe Cross i
Section at Support I MS :06007S SOP0402 DOC
4
~trgerT~ ~
Ltand~r
- .,...+* :. :
7"!..........
Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. 9ofPage 18 4.2 4.2.1 Description of Load Cases Analyzed:
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
Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06 L-cirictv.
007S aic. No. 2009-07204
~ev. No. 0 age No. 10 of Page 18 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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204
- Rev. No. 0 Page No. 11 of Page 18 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
ht 1000psil Figure 4.2.3: Pressure Loading Model SOP0402 DOC
~g~t~4 Lii ricI~j" Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Caic. No. 2009-07204 Rev. No. 0 Page No. 12 of Page 18 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 1000F/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
Figure 4.2.4: Thermal Transient Model 4.3 Acceptance Criteria None.
- k S0P0402.DOC
S~nrdnýý Uundl I
Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. 13 of Page 18 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 V
CI r
Caic. No. 2009_70 Rev. No. 0~
ct: Braidwood Station ctNo.: 11329-121 Atress. Calculation for 1 MS06007S RESULTS / CONCLUSION cross sec WesDync
- the Fillel
,cc rur fli
), is selected for str(
irface) and is paral I to the and 31~
Lmirid~,
- i*!.:*.
Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1MS Cabc. N(
Rev. No Page N
.2009-07204
,.15 of Page 18 AN AR13 2ý009 09:46: 16 NO
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- 47. 904 SOP0402 DOG
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PCýSTI SUJRFACESD VALU-E=
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'AN APR 10 2009 15:35:11 i
-1128,.
-957.772'
-787./738S
.617.704
-447. r7M 7 636 462
.325 LUU--
essure of 1,000 psi S(
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Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. 18 of Page 18 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 lOO1 F/hour SOPG402IDOC
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LAuWcIV-Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. Al of Page A25 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?,0 0
/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 1 MS06007S 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 F FITEM,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 1 MS06007S 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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A6 of Page A25 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 Project: Braidwood Station Project No.: 11329-121 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, Y1
- 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:
Calc. No. 2009-07204 Rev. No. 0 Page No. A7 of Page A25 SOP0402DOC
E~are~iILuari civ-,
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 1 MS06007S 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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S
/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 Calc. No. 2009-07204 Rev. No. 0 Page No. A9 of Page A25 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 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 IBTtU/hr-in-F 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 1 MS06007S 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 1 MS06007S 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
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Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A12, of Page A25 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 FLST,5,4,4,ORDE, 2 FITEM, 5,55 FITEM,5,-58 CM, Y,LINE LSEL,..
. P51X CM, YI,LINE CMSEL,,_Y outer radial 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 1 MS06007S 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 Project: Braidwood Station Project No.: 11329-121 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, Calc. No. 2009-07204 Rev. No. 0 Page No. A14 of Page A25 MSHAPE, 0,3D MSHKEY,1 CM,_Y,VOLU
- VSEL, 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, 9
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.
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LIarlcEv Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S 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 Calc. No. 2009-07204 Rev. No. 0 Page No. A15 of Page A25 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, SUCR, LugI,CPLANE,40,-
CSWPLA,11,1,1,1, RSYS,11 19806 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 P LOT 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 1 MS06007S 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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for I MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A19 of Page'A25 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
- Time, 0.00001 NSUBST, I,1,1 CMSEL,S,HFACE SFA,ALL,
,CONV,htc,560 ALLSELALL SOLVE
- Time, 1.0 Nsub, 60,100,60 CMSEL, S,HFACE SFA,ALL,
,CONV,htc,460 ALLSELALL SOLVE
- Time, 3.0 Nsub,20,100,20 CMSEL, S,HFACE SFA, ALL,
,CONV, htc,260 ALLSEL, ALL
!SOLVE
- Time, 5.0 Nsub, 10,100, 0
!h= 4000 BTU/hr-ft^2-F LS=2 LS-3 LS-4 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 1 MS06007S 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 Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A21 of Page A25 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 11/08/2007 08/31/2007 06/22/2007 08/31/2007 08/31/2007 09/05/2007 08/31/2007 03/31/2006 11/08/2007 08/31/2007 08/31/2007 08/31/2007 02/21/2007 01/20/2002 08/31/2007 08/31/2007 11/08/2007 11/08/2007 09/19/2002 03/30/2006 08/31/2005 08/30/2007 10/05/2000 11/08/2007 04/12/2006 09/24/2002 11/23/2004 09/24/2002 09/19/2002 09/24/2002 08/17/2004 01/26/2006 10/23/2000 09/20/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 09/20/2006 11/04/2006 11/04/2006 11/04/2006 10/20/2004 06/12/2007
.03/07/2002 03/18/2003 10/03/2006 09/20/2006 09/20/2006 09/20/2006 10/03/2006 10/03/2006 10/03/2006 10/03/2006 10/03/2006 08/31/2007 05/07/1999 03/25/2005 SOP0402.DOC 11:16 AM 11:16 AM 12:04 AM 03:04 PM 12:21 AM 12:21 AM 10:26 AM 03:37 AM 03:03 AM 10:42 AM 12:21 AM 12:20 AM 12:21 AM.
03:53 PM 12:57 PM 03:36 AM 12:52 AM 10:42 AM 10:42 AM 04:28 PM 12:56 PM 04:13 PM 05:25 PM 04:54 PM 11:14 AM 10:02 AM 02:48 PM 04:03 PM 02:49 PM 04:28 PM 02:49 PM 01:36 PM 11:06 AM 09:00 PM 05:49 PM 07:47 AM 07:48 AM 07:48 AM 07:48 AM
.08:22 PM 07:50 AM 07:51 AM 07:47 AM 03:12 PM 12:45 PM 12:47 PM 10:20 PM 04:26 PM 08:10 PM 08:10 PM 08:10 PM 04:27 PM 04:26 PM 04:06 PM 04:20 PM 04:12 PM 01:05 AM 12:00 AM 08:00 AM
<DIR>
<DTR>
<DI:
<DII
<DI) 19,968 acon.exe 158,208 animate.exe 1,571.anstclshllO.bat 1,580 answishllO*bat 71,350,272 ANSYS.exe 31,744 ANSYS1IO.exe 7,048 ansysll0.ver R>,
ANSYSLM 739 ansysservllO.bat.
19,813 ansystsllO 323 ansystsllO.bat, 61,440 ans admin.exe 671,744 asmutils.dll 64,512 binlib.dll 16,461,312 cadoe.dll R>
DANSYSMPICH R>
DANSYSMSMPI 2,142,277 DataViz370-dll 462,848 DFORMD.dll 126,976 dispinfo.exe 466,944 DisplayW.exe 438,342 DSGStreamN.dll 204 file.err 36,864 gus.exe 196,679 HardCopy370.dll 283,136 ifdlglOO.dll 4,833,365 Inv3ll.dll 98,304 Invr31l.dll 442,454 Invw311.dll 150,528 jpeg62.dll 45,056 lauricherllO.exe 217,600 libcpepcf9Omd.dll 243,200 libguide40.dll 328,192 libguide40.stats.dll 757,760,libifcoremd.dll 757,760 libifcoremdd.dll 746,496 libifcorert.dll 746,496 libifcorertd.dll 147,968 libifportmd..dll 6,144 libimalloc.dll 2,192,896 libmmd.dll 2,213,888 libmmdd.dll 108,544 libompdb.dll 396,288 libtiff.dll 71,832,576 is971_MPPDP.exeSave 65 machines 1,060,864 mfc7l.dll.
4,129,792 mkl def.dll 940,544 mkl ias.dll 2,648,064 mkl_lapack32.dll 2,703,872 mkllapack64.dlI 4,938,752 mklmc.dll 5,784,576 mkl_p4n.dll 2,392,576 mkl-vml-def.dll 3,043,840 mkl vml-mc.dll 3,021,312 mkl vmlp4n.dll 388,096 mnflib.dll 645,616 MSCOMCT2.OCX 941,568 msvcp60.dll
V" NI~
Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A22 of Page A25 03/30/2006 08/31/2007
.09/01/2004 09/24/2002 09/22/2003 11/04/2006 12/22/2006 12/09/2004 10/03/2006 07/18/2005 12/09/2004 12/09/2004 07/18/2005 07/18/2005 12/09/2004 10/03/2006 10/03/2006 04/17/2003 12/09/2004 03/14/2005 03/14/2005 03/14/2005 04/20/1998 09/01/2004 12:56 PM 12:20 AM 03:22 PM 02 :49 PM 11:28 AM 07:53 AM 05:02 AM 03:50 PM 01:55 PM 09:30 AM 03:50 PM 03:50 PM 09:30 AM 09:30 AM 03:50 PM 01:55 PM 01:55 PM 02:58 PM 04:04 PM 03:24 PM 03:24 PM 03:24 PM 12:08 PM 03:21 PM 80 File(s) 348,160 msvcr7l.dll 1,587 nlhistllO.bat 120,832 png.dll 3,751,936 qt-mt305.dll 3,129,344 splash.exe 286,720 svml -dispmd.dll 17,944,576 sxpost.exe 627,200 tc183.dll 859,648 tc184.dll 17,408 tclddel2.dll
.13,824 tcldde83.dll 27,136 tclpip83.dll 6,656 tclpip84.dll 18,944 tclregll.dll 15,360 tclreg83.dll 11,776 tclsh.exe 11,776 tclsh84.exe' 915,968 tiff.dll 924,160 tk83.dll 1,374,208 tk84.dll 16,896'wish.exe 16,896 wish84.exe" 125,440 wntshell.exe 55,808 zlib.dll 242,531,855 bytes Directory of C:\\Program Files\\ANSYS Inc\\vllo\\ANSYS\\bin\\winx64\\ANSYSLM 11/08/2007 11/08/2007 09/05/2007 01/20/2002 08/31/2007 08/31/2007 09/19/2002 03/30/2006 10/05/2000 09/24/2002 11/23/2004 09/24/2002 09/19/2002 09/24/2002 08/17/2004 10/23/2000 09/20/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 09/20/2006 11/04/2006 11/04/2006 11/04/2006 10/20/2004 03/18/2003 10/03/2006 08/21/2005 09/20/2.006 09/20/2006 09/20/2006 10/03/2006 10/03/2006 10/03/2006 08/11/2005 10/03/2006 10/03/2006 08/31/2007 10 :42 AM 10:42 AM 01:50 PM 12:57 PM 03:36 AM 12:52 AM 04:28 PM 12:56 PM 04:54 PM 02:48 PM 04:03 PM 02:49 PM 04:28 PM 02:49 PM 01:36 PM 09:00 PM 05:49 PM 07:47,AM 07 48 AM 07.48 AM 07 48 AM 07 48 AM 07:49 AM 08:22 PM 07:50 AM 07:51 AM 07:47 AM 03:12 PM 10:20 PM 04:26 PM 06:58 PM 08:10 PM 08:10 PM
.08:10 PM 04:27 PM 04:26 PM 04:06 PM 02:31 PM 04:20 PM 04:12 PM 01:05 AM
<DIR>
<DIR>.
70,265,856 671,744 64,512 16,461,312 2,142,277 462,848 438,342 196,679 283,136 4,833,365 98,304 442,454 150,528 217,600 243,200 328,192
.757,760 757,760 746,496 746,496 147,968 6,144 2,192,896 2,213,888 108,544 396,288 1,060,864 4,129,792 6,816,256 940,544 2,648,064 2,703,872 4,938,752 5,.784,576 2,392,576 1,562,112 3,043,840 3,021,312 388,096 ANSYS.exe asmutils.dll binlib.dll cadoe.dll DataViz370.dll DFORMD.dll DSGStreamN.dll HardCopy370.dll ifdlgloo.dll Inv3ll.dll Invr3ll.dll Invw3ll.dll jpeg62.dll libcpepcf90md.dll libguide40.dll libguide4ostats;dll libifcoremd.dll libifcoremdd.dll libifcorert.dll libifcorertd.dll libifportmd.dll libimalloc.dll libmnmd.dll libmmdd.dll libomp_db.'dll
-libtiff.dll.
mfc71.dll mkl def.dll mkl~i2p.dll' mkl ias.dll mkl-lapack32.dll mkl-lapack64.dll mkl-mc.dll mkl~p4n.dll mkl vmlndef.dll mkl vml i2p.'dll mkl vml mc.dll mkl-vm1lp4n.dll mnflib.dll SOP0402.DOC
4,r.aJlndv-Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A23 of Page A25 03/25/2005 03/30/2006 09/01/2004 09/24/2002 11/04/2006 12/09/2004 10/03/2006 07/18/2005 12/09/2004 12/09/2004 07/18/2005 07/18/2005 12/09/2004 10/03/2006 10/03/2006 04/17/2003 12/09/2004 03/14/2005 09/01/2004 08:00 AM 12:56 PM 03:22 PM 02:49 PM 07:53 AM 03:50 PM 01:55 PM 09:30 AM 03:50 PM 03:50 PM 09:30 AM 09:30 AM 03 50 PM 01:55 PM 01:55 PM 02:58 PM 04:04 PM 03:24 PM 03:21 PM 58 File(s) 941,568 msvcp6O.dll 348,160 msvcr7l.dll 120,832 png.dll 3,751,936 qt-mt305.dll 286,720 svml_dispmd.dll 627,200 tc183.dll 859,648 tc184.dll 17,408 tclddel2.dll
.13,824 tcldde83.dll 27,136 tclpip83.dll 6,656 tclpip84.dll 18,944 tclregll.dll 15,360 tclreg83.dll 11,776 tclsh.exe 11,776 tclsh84.exe 915,968 tiff.dll 924,160 tk83.dll 1,374,208 tk84.dll 55,808 zlib.dll 155,134,333 bytes Directory of C:\\Program Files\\ANSYS Inc\\vllO\\ANSYS\\bin\\winx64\\DANSYSMPICH 11/08/2007 11/08/2007 09/05/2007 01/20/2002 08/31/2007 08/31/2007 09/19/2002 03/30/2006 10/05/2000 09/24/2002 11/23/2004 09/24/2002 09/19/2002 09/24/2002 08/17/2004 10/23/2000 09/20/2006 11/04/2006 11/04/2006 11/64/2006 11/04/2006 11/04/2006 11/04/2006 09/20/2006 11/04/2006 11/04/2006 11/04/2006 10/20/2004 03/18/2003 10/03/2006 09/20/2006 09/20/2006 09/20/2006 10/03/2006 10/03/2006 10/03/2006 10/03/2006 10/03/2006 08/31/2007 08/31/2007.
03/25/2005 03/30/2006 09/01/2004 09/,24/2002 11/04/2006 12/09/2004 SOP0402.DOC 10:42 AM 10:42 AM 01:46 PM 12:57 PM 03:36 AM 12:52 AM 04:28 PM 12:56 PM 04:54 PM 02:48 PM 04:03 PM 02:49 PM 04:28 PM 02:49 PM 01:36 PM 09:00 PM 05:49 PM 07:47 AM 07:48 AM 07:48 AM 07:48 AM 07:48 AM 07:49 AM 08:22 PM 07:50 AM 07:51 AM 07:47 AM 03:12 PM 10:20 PM 04:26 PM 08:10 PM 08:10 PM 08:10 PM 04:27 PM 04:26 *PM 04:06 PM 04:20 PM 04:12 PM 01:05 AM 03:44 AM 08:00 AM 12:56 PM 03:22 PM 02:49 PM 07-53 AM 03: 50 PM
<DIR>
<DIR>
77,097,984 ANSYS.exe 671,744 asmutils.dll
.64,512 binlib.dll 16,461,312 cadoe.dll 2,142,277 DataViz370.dll 462,848 DFOPMD.dll 438,342 DSGStreamN.dll 196,679 INardCopy370.dll 283,136 ifdlglOO.dll 4,833,365 Inv3ll.dll 98,304 Invr3ll.dll 442,454 Invw3ll.dll 150,528,jpeg62.dll 217,600 libcpepcf9Qmd.dll 243,200 libguide40.dll 328,192 libguide40_stats.dll 757,760 libifcoremd.dll 757,760 libifcoremdd.dll-746,496 libifcorert.dll 746,496 libifcorertd.dll 147,968 libifportmd.dll 6,144 libimalloc.dll 2,192,896 libmmd.dll 2,213,888 libmmdd.dll 108,544 libomp_db.dll 396,288 libtiff.dll 1,060,864 mfc7l.dll 4,129,792 mkl def.dll 940,544 mkl ias.dll.
-2,648,064 mkllapack32.dll 2,703,872 mkllapack64.dll 4,938,752 mkl mc.dll 5,784,576 mkl~p4n.dll 2,392,576 mkl-vml-def.dll 3,043;840 mkl vmlmc.dll 3,021,312 mkl vml p4n.dll 388,096 mnflib.dll 5,632 mpitestmpich.exe 941,568 msvcp60.dll 348,160 msvcr7l.dll 120,832. png.dll 3,751,936 qt-mt305.dll 286,720 svml_dispmd.dll 627,200 tc183.dll
BSlfgftrit"\\
LEL~rIdJV' Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A24 of Page A25 10/03/2006 07/18/2005 12/09/2004 12/09/2004 07/18/2005 07/18/2005 12/09/2004 10/03/2006 10/03/2006 04/17/2003 12/09/2004 03/14/2005 09/01/2004 01:55 PM 09:30 AM 03:50 PM 03:50 PM 09:30 AM 09:30 AM 03:50 PM 01:55 PM 01:55 PM 02:58 PM 04:04 PM 03:24 PM 03:21 PM 57 File(s) 859,648 tc184.dll 17,408 tclddel2.dll 13,824 tcldde83.dll 27,136 tclpip83.dll 6,656 tClpip84.dll 18,944 tclregll.dll 15,360 tclreg83.dll 11,776 tclsh.exe 11,776 tclsh84.exe 915,968 tiff.dll 924,160 tk83.dll 1,374,208 tk84.dll 55,808 zlib.dll 153,593,725 bytes Directory of C:\\Program Files\\ANSYS Inc\\vllO\\ANSYS\\bin\\winx64\\DANSYSMSMPI 11/08/2007 11/08/2007 09/05/2007 01/20/2002 08/31/2007 08/31/2007 09/19/2002 03/30/2006 10/05/2000 09/24/2002 11/23/2004 09/24/2002 09/19/2002 09/24/2002 08/17/2004 10/23/2000 09/20/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 11/04/2006 09/20/2006 11/04/2006 11/04/2006 11/04/2006 10/20/2004 03/18/2003 10/03/2006 09/20/2006 09/20/2006 09/20/2006 10/03/2006 10/03/2006 10/03/2006 10/03/2006 10/03/2006 08/31/2007 08/31/2007 03/25/2005 03/30/2006 09/01/2004 09/24/2002 11/04/2006 12/09/2004 10/03/2006 07/18/2005 12/09/2004 12/09/2004 07/18/2005 10:42 10:42 01:44 12:57 03:36 12:52 04:28 12:56 04:54 02:48 04:03 02:49 04:28 02.:
49 01:36 09:00 05:49 07:47 07:48 07:48 07:48 07:48 07:49 08:22 07:50 07:51 07:47 03 :12 10:20 04:26 08:10 08:10 08:10 04:27 04:26 04:06 04:20 04:12 01:05 03:43 08:00 12:56 03:22 02:49 07:53 03:50 01:55 09:30 03:50 03:50 09:30 AM AM PM PM AM AM PM PM PM PM PM PM PM PM PM PM PM AM AM AM AM AM AM PM AM AM AM PM PM PM PM PM PM PM PM PM PM PM AM AM AM PM PM PM AM PM PM AM PM PM AM
<DIR>
<DIR>
77;097,984 ANSYS.exe 671,744 asmutils.dll 64,512 binlib.dll, 16,461,312 cadoe.dll 2,142,277 DataViz370.dll 462,848 DFORMD.dll 438,342 DSGStreamN.dll 196,679 HardCopy370.dll 283,136 ifdlglOO.dll.
4,833,365 Inv3ll.dll 98,304 Invr3ll.dll 442,454 Invw3ll.dll 150,528 jpeg62.dll 217,600 libcpepcf9Omd.dll 243,200 libguide40.dll 328,192 libguide40_stats.dll 757,760 libifcoremd.dll 757,760 libifcoremdd.dll 746,496 libifcorert.dll 746,496 libifcorertd.dll 147, 968 libifportmd.dll 6,144 libimalloc.dll 2,192,896 libmmd.dll 2,213,888 libmmdd.dll 108,544 libompdb.dll 396,288 libtiff.dll 1,060,864 mfc7l.dll 4,129,792 mkl def.dll 940,544 mkl ias.dll 2,648,064 mkl lapack32.dll 2,703,872 mkl_lapack64.dll 4,938,752 mkl-mc.dll 5,784,576 mkl-p4n~dll 2,392,576 mklvmldef.dll 3,043,840 mklvmlmc.dll 3,021,312 mkl vmlp4n.dll.
388,096 mnflib.dll 5,632 mpitestmsmpi.exe 941,568 msvcp6O.dll 348,160 msvcr7l.dll 120,832 png.dll.
3,751,936 qt-mt305.dll 286,720 svmldispmd.dll 627,200 tc183.dll 859;648 tc184.dll 17,408 13, 824' 27, 136 6,656 tclddel2..dll tcldde83.dll tclpip83.dll tclpip84.dll S0P0402.DOC
LtmincIVI Client: Exelon Project: Braidwood Station Project No.: 11329-121 Lug Stress Calculation for 1 MS06007S Calc. No. 2009-07204 Rev. No. 0 Page No. A25 of Page A25 07/18/2005 12/09/2004 10/03/2006 10/03/2006 04/17/2003 12/09/2004 03/14/2005 09/01/2004 09:30 AM 03:50 PM 01:55 PM 01:55 PM 02:58 PM 04:04 PM 03:24 PM 03:21 PM 57 File(s) 18,944 tclregll.dll 15,360 tclreg83.dll 11,776 tclsh.exe 11,776 tclsh84 ;exe 915,968 tiff.dll 924,160 tk83.dll 1,374,208 tk84.dll 55,808 zlib.dll 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