ML20067A987
| ML20067A987 | |
| Person / Time | |
|---|---|
| Site: | Brunswick  |
| Issue date: | 01/21/1991 |
| From: | STRUCTURAL INTEGRITY ASSOCIATES, INC. |
| To: | |
| Shared Package | |
| ML19310E585 | List: |
| References | |
| CPL-16Q-306, CPL-16Q-306-R, CPL-16Q-306-R00, NUDOCS 9102080081 | |
| Download: ML20067A987 (70) | |
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SUMMARY
OF TENSILE DATA AT 450-5500F FOR J-TOUGHNESS TESTED FERRITIC PIPING MATERIALS (to)
Material Condition Yield Ultimate (ksi) (ksi) l Base Metal .... 31 - 52 65 - 85 j 34 61
, 70XX SMAW PWHT l 73 - 75 88 l 80XX SMAW PWHT
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SUMMARY
OF AVAILABLE JI DATA FOR FERRITICPIPINGMATERIALSkT 2200 550 F hp) MATERIAL NIMBER J;c 0F TESTS (in-lb/in2) Base Metals! 42 588 - 2300 70XX SMAW As-Welded 3 Avg = 721 PWHT 5 1311 - 1723 80XX SMAW As-Welded - - PWHT 4 345 - 532 SAW As-Welded 3 Avg = 424 PWHT 18 335 - 1350
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SUMMARY
SHEET eE-FT-aco REPORT NO.1 R.2tt o PROJROT N/A meenswa oE-gy.106 nw. O Pu net 5832-3 BRUNSWICK STIAM ELECTMic PLANT memum oE-VT=200 m 2. mm N/A mespwse GE=UT-103 W. 3 Pm m UNIT 1 - 18F90-8N786 N/A l un., RxR ma usmooi O we G!rn G!r w 0n 1 wsw nw 1832RD2 A2-87-FWA33 l m VALVE TO TEE **W TV'88 m ug Q ,,,, N/A l eam T. WALTER /P. WRIONT wt II/II mL 4,est me# C-171/C-173/C-173/C-174 l esa M. GREET 8EERGER WL II 0-175/C-176/C-117 su m W. ARKE8/C. MINOR pgII/I!! masemmam M*AAA 1 DURING TNE ULTRASONIC IXAMINATION OF TNI A90VE REFERENCED WELD, NO INDICATIONS AAffatWnJPVvMASM5%"IG982&EPHH HARH*HYd.""iW4hW" g SYSTEM DID RECCAD TWO (2) NON-0BONETRIC INDICATIONS WHICH MAVE THE FOLLON!NG PARAMETERS 1 DISTANCE FROM THRU-NALL 4THRU- SIDE OF TYPE OF 8EARCH UNITS IERO REFERENCE LENGTH DIM 4N81DM wit t wrte UTTtifED 1 REF4ECTOR
- 1) 7.6" *1.80' .80* 524 UPST " PLANAR 08, 45'8 45'n, 60*E
- 2) 85 7' *1.50" 1.10" 71% UPST ' PLANAR O', 45'8 45'E, 60'E INDICATION 8' IND POINT ON TNE VALVE SIDE CANNOT BE DETERMINED (SEE PLOT 8HIET8).
" AXIALLY ORIENTED s O t., g tj ADDITIONALLit A 0' LONQITUDINAL WAVE SEARCH UNIT WAS UTILI8ED 70 CONFIRM TN2 I
's g PRESENCE AND ORIENTATION OF THE8E INDICATIONS.
Ek lj REDIRECT AND INSIDE SURFACE GECMETS.t FROM THE UPSTREAM!
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{' 4 THE 45' RL SEARCH UNIT RECORDED NON-RELEVANT INDICATIONS, ACCU $ TIC INTERFACE,
%% 7 ROOT AND IN8IDE SURFACE OBONETRY FROM THE UP8TREAN SIDE OF THE _ WELD.
O D. R
}k 3 THE 40' RL SEARCM UNIT RECORDED NON-RELEVANT INDICATICHS,- SNEAR COMPONENT AND INSTDE SURFACE SEONITRY FROM TNE UP8TREAM SIDI 0F TER WELD.
f, A MANUAL EXAMINATION WAS PERFORMED FROM THE DONN87 REAM SIDE OF THE WELD,
~ UTILIBING 48' ENEAR WAVE, 45' AND 60' REFRACTED LONGITUDINAL NAVE SEARCH UNITS. THESE EXAMINATIONS RESULTED IN MO REC 0Fhkaf 2 INDICATONS.
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i SENT BYiREClRC PROJECT i 1-17-81 1 16:02 iCP&L BRUNSWICK PLANT
- 40897889841# 2 BNP UNIT 1 RER VALVES 1-311-F0601/.70603 HYDROSTATIC TEST PRESSURE AND TEMPERATURE (ASME XI CRITERIA)
I 1088 TO 1103 PSIG 164'F MIN /Pu*/ 7 MAX NORMAL OPERATING TEMPERATURE AND PRESSURE 532*F/ 1250 PSIG* (SAME AS RECIRC SYSTEM DISCHARGE)
- Based on known suction pressure and pump ourves. No direct I
reading recirculation system discharge pressure gauges. i l puvarcit. pannmTras As mRDoRTED ON CMTRE CHARPY IMPACT TEST RESULTS F060A - FT. LBS . AT ~20
- F 21-18-22 F060B - FT. LBS. \T ~20'F 21-32-31 ULTIMATE TENSILE STRENGTH F060A - 99,100 PSI F0605 - 100,100 PSI YIELD STRENGTH F060A - 81,500 PSI F0605 - 79,900 PSI ELONGATION (4)
F060A - 22.5 F0608 - 22.5 Prepared by: IN,!/~'# Checked by: ^' # # 'b' ' JIM GATES File No.CA'AIA' lib E**' 1/17/'l Pege_/#~# CI
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. - - . _ _ _ -- -- . . - - - . _ . . . ~. . .- - - ._ to pc-CRACK (C) COPYRIGHT 1984, 1988 STRUCTURAL INTEGRITY ASSOCIATES, INC. / ~ C .7, SAN JOSE, CA (408)978-8200 VERSION 2.0 Dato: 18-Jan-1991 Cd9CE /. ~ 4t s t/V G- /*9V4~/f&G-G WM C t Tico: 10:59: 8.33 OF /, 6 T " Ed/f /?FGt ON 0/:' P E p tt C 6 4 TH t C l<f/G7 7, INSTABILITY EVALUATION CP&L bSEP-1 RHR VALVE crock model: AXIAL CRACK IN CYLINDER UNDER INTERNAL PRESSURE MATERIAL PROPERTIES - FLOW STRESS (SIGMAf)= 81.4500 YIELD STRESS (SIGMAo)= 62.8000 YIELD STRAIN (EPSILONo)= 2.317E-03 YOUNG MODULUS = 2.710E+04 POISSON RATIO = 0.3000 l l RAMBERG-OSGOOD STRESS-STRAIN LAW:- l ALPHApl= 0.3520 l Nple 8.4900 GEOMETRIC PROPERTIES:- OUTSIDE DIAMETER = 12.2950 WALL THICKNESS (t)= 1.6950 OTHER CONDITIONS - PLANE STRAIN <1) OR PLANE STRESS <2)= 1 dA= 1.695E-02 LOADING CONDITIONS:- PRESSURE: 1.0000
-CRACK DEPTH (a): 1.1000 i (a/t): 0.6490 c/t(a/b) F_ H 0.0000 1.1220 38.7137 0.1250 1.1853 16.1976 0.2500 1.3515 10.6242 0.3750 1.6641- 6.6517 0.5000 1.9766 2.6793 0.6250 2.4176 1.6100 Prepared by: I8CI~/9~7/
0.7500 2.8586 0.5408 g ,jyj,, File No.CPe-//+ru. Itov: o Page C-A ci C -J'
pc-CRACK VERSION 2.0 PAGE 2' HATERIAL J-R CURVE CPLRHRVL i Ja 1.8657 * (da)^ 0.2862 /' C' ~2 0.3500
~
J1c= Jeax= 2.0000 INCREMENTATION:- PRESSURE INCREMENT = 0.2500 NUMBER OF INCREMENTS = 100 INCREMENT PRESSURE WITH CRACK SIZE ADJUSTHENT FROM MATEllIAL R-CURVE STRESS Andj Jappl Tappl Tmat dA 1.0000 1.1000 0.0130 0.1395 522514.8725 0.0000 1.2500 1.1000 0.0204 0.2199 169317.1298 0.0000 1.5000 1.1000 0.0296 0.3200 67070.6710 0.0000 1.7500 1.1000 0.0406 0.4408 30498.7427- 0.0000 2.0000 1.1000 0.0535 0.5833 15335.2663 0.0000 2.2500 1.1000 0.0683' O.7484 8323.6917 0.0000 2.5000 1.1000 0.0852 0.9372 4798.0118 0.0000 2.7500 1.1000 0.1042 1.1507 2903.3481 0.0000 3.0000 1.1000 0.1255 1.3896 1828.7059 0.0000 3.2500 1.1000 0.1490 1.6548 1191.2933 0.0000 3.5000 1.1000 0.1749 1.9468 798.6976 0.0000 3.7500 1.1000 0.2033 2.2663 548,9717 0.0000 4.0000 1.1000 0.2342 2.6136 385.6303 0.0000 4.2500 1.1000 0.2678 2.9892 276.1507 0.0000 4.5000 1.1000 0.3040 3.3936 201.1703 0.0000 4.7500 1.1000 0.3431 3.8274 148.8190 0.0000 5.0000 1.1040 0.3892 4.3177 108.6527 0.0042 5.2500 1.1062 0.4371 4.8310 81.3661 0.0063 5.5000 1.1091 0.4896 5.3869 61.3100 0.0093 5.7500 1.1133 0.5481 5.9964 46.2792 0.0138 6.0000 1.1196 0.6144 6.6727 34.8122 0.0206 6.2500 1.1313 0.6961 7.4767 25.4945 0.0319 6.5000 1.1518 0.8042 f ~'S7 17.7902 0.0529 6.7500 1.2100 1.0198 1 - 7 9.8370 0.1212 BY INTERPOLATION Jerita 0.9995 4 Tcrits 10.5866 PRESSUREcrits 6.7264 w= 1.2830 MATERIAL J-R CURVE: CPLRHRVL da Jaat Tmat 0.0020 0.3500 184.1541 0.0026 0.3500 152.1712 0.0034 0.3671 125.7428 0.0045 0.3963 103.9044 Prepared by: E '# # 0.0058 0.4278 85.8588 use f/af/g/ 0.0076 0.4618 70.9473 Checked by,. _ Flto N3. Cf&NA ~lN RCV; 9- -- Pege C ~T c .G.f-.- .
, _ , ~ ._. ,,
pc-CRACK -VERSION 2.0 - PAGE 3 0.0099 0.4985 5806255 0.0130 0.5381 48.4437 0.0170. 0.6809 40.0302 /g C - y. 0.0222 0.6271 33.0780 0.0290 0.6769 27.3332 0.0378 0.7308 22.5861 1 0.0494 0.7888 18.6634 l 0.0646 0.8516 15.4221 0.0843 0.9193- 12.7436 O.1102 0.9924 10.5304 0.1439 1.0712 8.7015 i 0.1881 1.1564 7.1903 0.2457 1.2484 5.9415 0.3209 1.3476 4.9096 0.4193 1.4547- 4.0569 ' O.5477 1.5704 3.3523 ! 0.7156 1.6953 2.7701 1 0.9348 1.8300 2.2890 8 1.2212 1.9755 1.8915 END OF pc-CRACK - 1 l . l l l Prepared by: TYNf-W Checked by: *' e /A//.9/ Fue No, CA-/40-704 Rovi D -- Page C- F ef_C_-P
'I
to p3-CRACK $ C-f" (C) COPYRIGHT 1984, 1988 1 I STRUCTURAL INT 5:0RITY ASSOCIATES, INC. SAN JOSE, CA (408)978-8200 VERSION 2.0 Dato: 18-Jan-1991 C All* 3'* ~ l'l3 /WG- /?VNN??llM W/14-L , Tico: 10:49:48.47 A I SR /~l0N A M /, $~7f /:44
/tC'"GIOIV C/* Ad5DMCdb 7~WQHQ INSTABILITY EVALUATION ! CP&L BSEP-1 RHR VALVE l crack model: AXIAL CRACK IN CYLINDER UNDER INTERNAL PRESSURE MATERIAL PROPERTIES:-
FLOW STRESS (SIONAf)= 81.4500 YIELD STRESS (SIONAo)= 62.8000 YIELD STRAIN (EPSILONo)= 2.317E-03 YOUNG MODULUS = 2.710E+04 POISSON RATIO = 0.3000 RANDERG-05000D STRESS-STRAIN LAW:- ALPilApl= 0.3520 Np1= 8.4900 OEOMETRIC PROPERTIES:- OUTSIDE DIAMETER = 12.2950 WALL THICKNESS (t)= 1.5350 OTHER CONDITIONS:- PLANE STRAIN <1) OR PLANE STRESS <2>= 1 dA= 1.635E-02 LOADING CONDITIONS - PRESSURES 1.0000 CRACK DEPTH (a)= 1.1009 (a/t)= 0.716d c/t(a/b) F H 0.0000 1.1220 37.7045 0.1250 1.1860 15.8513 0.2500 1.3561 10.4580 0.3750 1.6762 6.5798 1 0.5000 1.9963 2.7016 ! 0.6250 2.4626 1.6309 j 0.7500 2.9289 0.5602 ! Prepared by: M['/ f" U Checked by: ^'d c '/3d8/ File No._Cr#WN 'JM Rev: 0 -l Pege C'[- of C ~P l I l
pc-CRACK VERSION 2.0 PA0E 2 NATERIAL J-R CURVE:CPLRHRVL Ja 1.8657 * (da)* 0.2862 [$' C ~ b J1c= 0.3500 Jooxa 2.0000 INCREMENTATION - PRESSURE INCREMENT = 0.2500 NUMBER OF INCREMENTS = 100 INCREMENT PRESSURE WITH CRACK SIZE ADJUSTMENT FROM MATERIAL R-CURVC STRESS Andj Jappl Tappi -Tant dA 1.0000 1.1000 0.0194 0.2144 191977.1739 0.0000 1.2500 1.1000 0.0306 0.3391 61806.4586 0.0000 1.5000 1.1000 0.0445 0.4952 24305.4611 0.0000 1.7500 1.1000 0.0612 0.6839 10966.8747 0.0000 2.0000 1.1000 0.0808 0.9066 5470.7578 0.0000 2.2500 1.1000 0.1036 1.1642 2946.3047 0.0000 2.5000 1.1000 0.1296 1.4573 1685.7285 0.0000 2.7500 1.1000 0.1590 1.7863 1013.0642 0.0000 3.0000 1.1000 0.1918 2.1512 634.1657 0.0000 3.2500 1.1000 0.2283 2.5520 410.9066 0.0000 3.5000 1.1000 0.2685 2.9891- 274.2345 0.0000 3.7500 1.1000 0.3125 3.4633 187.7712 0.0000 4.0000 1.1032 0.3637 3.9923 128.7034 0.0033 4.2500 1.1053 0.4185 4.5617 90.6521 0.0054 4.5000 1 ;085 0.4797 5.1911 64.5174' O.0087 4.7500 1.1133 0.5490 5.9035 46.0917 0.0139 5.0000 1.1211 0.6296 6.7452 32.7498 0.0225 5.2500 1.1374 0.7355 7.8710 22.2262 0.0387 5.5000 1.3912 0.9441 9.1252 11.9226 0.0926 5.7500 1.1926 1.0629 10.5339 8.8731 0.1401 BY INTERPOLATION Jerita 1.0187 Torita 10.0091 PRESSUREcrits 5.6569 ws 0.8668 MATERIAL J-R CURVE: CPLRHRVL-da Jaat Taat 0.0020 0.3500 184.1541 0.0026 0.3500 152.1019-0.0034 0.3672 125.6283 0.0045 0.3965 103.7626 0.0058 0.4281 85.7026 0.0076 0.4622 70.7859 0.0100 0.4990 58.4655 0.0130 0.5388 48.2895 0.0171 0.5817 39.8847 + l 0.0223. 0.6281 32.9427 Prepared by:- MC/~Od/ Checked by: _me </w/s/ File No. cA-M#-JM Rev: 0 , Page C -/A of= C d l 1
-1
pc-CRACK VERSION 2.0 PAGE 3 0.0291 0.6782 27.2090 0.0381 0.7322 22.4732 o g7 0.0498 0.7906 18.5617 /f 0.0651 0.8536 15.3310 0.0851 0.9216 12.6626 0.1112 0.9951 10.4587 0.1454 1.0744 8.6383 0.1901 1.1600 7.1348 . 0.2485 1.2525 5.8930 O.3249 1.3523 4.8673 0.4247 1.4601 4.0202 0.5551 1.5764 3.3204 0.7257 1.7021 2.7425 0.9486 1.8377 2.2652 1.2401 1.9842 1.8709 END OF pc-CRACK i Prepared by: MS/f-/ f- 9/ Checked by: "'c /h //3/ File No'.MV49-106 gey: 0 _ PageC-7 ef C -f _
CPL-16Q PCCRACK EPFH AXIAL FLAW PRESSURE VS. HOOP STRESS Ro(IN): 12.295 Ro(IN): 12.295 SIONAha t(IN): 1.695 t(IN): 1.535 (2*p*Ro*2)/ Ri(IN): Ri(IN): 10.76 (Ro*2-Ri'2) 10.6 HOOP HOOP PRESS. STRESS PRESS. STRESS (KSI) (KSI) (KSI) (KSI) 1.00 7.791 1.00 8.543 1.25 9.738 1.25 10.679 1.50 11.686 1.50 12.815 1.75 13.634 1.75 14.950 2.00 15.581 2.00 17.088 2.25 17.529 2.25 19.222 2.50 19.477 2.50 21.358 2.75 21.424 2.75 23.493 3.00 23.372 3.00 25.629 3.25 25.320 3.25 27.765 3.50 27.267 3.50 29.901 3.75 29.215 3.75 32.036 4.00 31.163 4.00 34.172 4.25 33.110 4.25 36.308 4.5G 35.058 4.50 38.444 4.75 37.006 4.75 40.580 5.00 38.954 0.00 42.715 5.25 40.901 5.25 44.851 5.50 42.849 5.50 46.987 5.75 44.797 5.75 49.123 6.00 46.744 6.00 51.258 6.25 48.692 6.25 53.394 6.50 50.640 6.50 55.530 6.75 52.587 6.75 57.666 7.00 54.535 7.00 59.801 7.25 56.483 7.25 61.937 7.50 58.430 7.50 64.073 7.75 60.378 7.75 66.209 8.00 62.326 8.00 68.344 8.25 64.273 8.25 70.480 8.50 66.221 8.50 72.616 8.75 68.169 8.75 74.752 9.00 70.116 9.00 76.888 i 9.25 72.064 9.25 79.023 9.50 74.012 9.50 81.159 I 9.75 75.959 9.75 83.295 10.00 77.907 10.00 85.431- ! 10.25 79.855 10.25 87.566 Prepared by: @b i Checked by: - * '/* M# ' 0 A c-f File No.C84 ~/AUfM Rev: Page_ C~I d - -
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l 1 to J pc-CRACK ! (C) COPYRIGHT 1984, 1988 l STRUCTURAL INTEGRITY ASSOCIATES. INC. I SAN JOSE, CA (408)978-8200-VERSION 2.0 Dato: 18-Jan-1991 Tico: 11:26:26.65 LEAST SQUARE-CURVE FIT OF STRESS PROFILE s CPL RHR PRESSURE STRESSES AT 1.636" SECTION (1260 - PSI, SF=3 ) TERN COEFFICIENT l C0 4.473E+01 4 C1 -6.757E+00. C2 4.039E+00 C3 -1.408E+00 COEFFICIENT OF DETERMINATION R*2= 0.9998 CORRELATION COEFFICIENTS 0.9996 X VALUE Y VALUE Y CALC DIFF 0.000E+00 4.474E+01 4.473E+01 1.300F-02 2.700E-01 4.313E+01 4.317E+01 -4.246E-02 5.500E-01 4.204E+01 4.200E+01 4.148E-02 8.300E-01 4.110E+01 4.109E+01 5.239E-03 1.100E+00 4.027E+01 4.031E+01 -3.163E-02 1.380E+00 3.941E+01 3.939E+01 1.918E-02 1.535E+00 3.877E+01 3.878E+01 -4.801E-03 END OF pc-CRACK-i i Prepared by: JT<//-/ P-t/
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to pc-CRACK i (C) COPYRIOHT 1984, 1988 l STRUCTURAL INTEGRITY ASSOCIATES, INC. I SAN JOSE, CA (408)978-8200 VERSION 2.0 Dato: 18-Jan-1991 Tico: 11:39:50.75 LEAST SQUARE CURVE FIT OF STRESS PROFILE-CPL RHR THERMAL STRESSES AT 1.535" SECTION (632 F, SFal) TERM COEFFICIENT
; CO 1.319E+01 C1 -3.456E+00 C2 7.880E-01 C3 -1.097E+00 COEFFICIENT OF DETERMINATION R*2= 0.9995 CORRELATION COEFFICIENT = 0.9990 X VALUE Y VALUE Y CALC DIFF 0.000E+00 1.322E+01 1.319E+01 3.419E-02 2.700E-01 1.220E+01 1.229E+01 -8.856E-OP.
5.500E-01 1.138E+01 1.134E+01 3.910E-02 8.300E-01 1.029E+01 1.023E+01 5.703E-02. 1.100E+00 8.860E+00 8.878E+00 -1.762E-02 1.380E+00 6.960E+00 7.034E+00 -7.422E-02 1.535E+00 5.820E+00 5.770E+00 5.008E-02 END OF pc-CRACK
.L Prepared by: 7FC// -/ F-9/
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i to pr-CRACK (C) COPYRICHT 1984, 1988 STRUCTURAL INTEGRITY ASSOCIATES, INC.
/j )b -4 SAN JOSE, CA (408)978-8200 VERSION 2.0 Datot 18-Jan-1991 C/1se h - L//9 = x (MA= era'nno) .
Tico 11:59t48.95 i LINEAR ELASTIC FRACTURE NECHANICS EVALUATION CPL RHR VALVE, 1.535" SECTION (A), SF=3 ON PRESSURE, SF=1 ON THERNAL crock model ELLIPTICAL LONGITUDINAL CRACK IN CYLINDER (T/R=0.1,A/L=0.5) i WALL THICKNESS (t)= 1.5350 STRESS COEFFICIENTS CASE ID CO C1 C2 03 PRESSA 44.7250 -6 7567 4.0393 -1.4076 THERHA 13.1858 -3.4559 0.7880 -1.0970 , CRACK ---------------STRESC INTENSITY FACTOR--~~------------ l SIZE CASE CASE PRESSA THERHA 0.0246 7.858 2.312 0.0491 11.105 3.261 0.0737 13.590 3.983 0.0982 15.682 4.586. 0.1228 17.522 5.113 0.1474 19.183 5.586 0.1719 20.707 6.017 0.1965 22.123 6.414 0.2210 23.452 6.783 0.2456 24.708 7.130 0.2702 25.903 7.456 0.2947 27.043 7.766 0.3193 28.141 8.061-- 0.3438 29.202 8.343 I 0.3684 30.227 8.613
- 0.3930 31.220 8.871 >
0.4175 32.183- 9.119 0.4421 33.120 9.358-0.4666 -34.032 9.587 0.4912 34.916 9.806 0.5158 35.780 10.017 0.5403 36.625 10.220 0.5649 37.453 10.416 0.5894 38.263 10.605 0.6140 39.059 10.788 0.6386 39.847 .10.'966 Prepared by: MCM-/7 -7/ Checked by: we '/w/s/ File No.CA-/4c ,74 Revt O Page_2)-I of b//-
l pc-CRACK ' VERSION 2.0 1 PA@E 2' 0.6631 40.623 11o138 l 0.6877 41.38b 11.304 jg y) . 7 i 0.7122 42.137 11.463 l 0.7368 42.877 11.618 : O.7614 43.606 11.766 ' J.7859 44.329 11.909 0.8105 45.043 12.046 l 0.8350 45.747 12.177 0.8596 46.444 12.302 0.8842 47.131 12.422 0.9087 47.811 12.536 0.9333 48.487 12.646 0.9578 49.158 12.751 i 0.9824 49.823 -12.850-1.0070 50.481 12.944 1.0315 51.132 13.032 8 1.0561 51.776 13.114 j 1.0806 52.413 13.190 1.1052 53.038 13.259 1.1298 53.658 13.322 { 1.1543 54.271 13.379 l 1.1789 54.879 13.430 1.2034 55.481 13.475 1.2280 56.077 13.513 ; 1 END OF pc-CRACK-l I 1 l l Prepbred by:
-/ 7 - Y / _
Checked by: _we e/"/s/_ File No,, CAW 4f-706 Rev:_9 Page:D-7 of D-// ' 4 r-% '+
s_r s > 3 )) ( pc-TRACK (1,,h[~f[ (C) 00PYRIAHT 1984, 1988 STRUCTURAL INTEOR'TY AEUOCIATES, INC. SAN JO2E, C,i (408)978-8200 V'ahs10N 2.0 Date: 18-Jan-1991 Tice: 11:50:54.86 C N % * ~~ 4[8 * ' LINEAR ELASTIC FRACTURE MECHANICS EVALUATION CPL RHR VALVE, 1.535" SECTION (A), SF=3 ON PRESSURE, SF=1 ON THERMAL vrack modeltELLIPTICAL LONOITUDINAL CRACK IN CYLINDER (T/R=0.1.A/L*0.2) WALL THICKNESS (t)= 1.5350 STRESS COEFFICIENTS CASE ID CO C1 02 C3 PRESSA 44.7250 -6.7567 4.0393* -1.4076 THERNA 13.1858 -3.4559 0.7880 -1.0970 1 CRACK ---------------STRESS INTENSITY FACTOR---------------- ' SIZE CASE CASE PRESSA THERMA 1 0.0246 10.771 3.170 ! 0.0491 15.294 4.493 ! 0.0737 18.807 5.515 0.0982 21.806 6.382 0.1228 24,481 7.151 0.1474 26.929 7.851 0.1719 29.204 8.498. 0.1965- 31.347 9.104 0.2210 33.383 9.676 0.2450 35.332 10.220 0.2702 37.208 10.740 0.2947- 39.022 11.240~ 0.3193 40.810 11.730 0.3438 42.581 12.212 0.3684 44.315 12.681 0.3930 46.017 13.138 0.4175 47.690 13.584 0.4421 49.338 14.020-0.4666 50.966 14.448 0.4912 52.580 14.868 0.5158 54.176- 15.281 0.5403 55.757 15.687 0.5649 57.324 -16.085-0.5894- 58.878 16.477 0.6140 60.421 16.862-0.63C6 61.945 17.238 Prepared by: #C/-/ P- t/ Checked by: me _ e/ai/sf
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File No. cit-/Sc-yy p,7~o '~ ' Page J -/ __ot.L-y
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seu e-pc-CRACK VERSION 2.0 PAGE 2 0.6631 63.459 17.608 O.6877 64.965 17.973 y,._c ' 0.7122 66.462 18.331 0.7360 67.962 18.684 0.7614 69.436 19.031 0.7859 70.988 19.392 O.8105 72.561 19.754 0.8350 74.132 20.111 0.8596 75.701 20.463 0.8842 77.26' 20.810 9 0.9087 78.838 21.151 1 0.9333 80.392 21.485 0.9578 81.942 21.812 s 0.9824 83.492 22.133 ! 1.0070 85.041 22.449 ' 1.0315 86.589 22.758 1.0561 88.136 23.062 ' 1.0806 89.686 23.361 1.1052 91.245 23.656 1.1298 92.805 23.946 , 1.1543 94.365 24.229 j 1.1789 95.924 24.505 j 1.2034 97.484 24.775 ! 1.2280 99.044 25.038 ) END OF pc-CRACK 3 l 1 Prepared by: M'c//-/f- t/ Checked.by: ase </4 e/,f File No.CA-NF-fee Rev: -- O Pege3- P _ oL@ - ff 3 3
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' pc-CRACK - /3 )$ -- / p - J (C)_COPYRISHT- 1984,-1988 STRUCTURAL INTEORITY; ASSOCIATES, INC.
SAN JOSE,:CA-(408)978-8200 VERSION 2.0 Dsto1 18-Jan-1991 C//56 7, - dpff * /d [M/#EC//04/V0)' Tics 12:40:31.88 , LINEAR ELASTIC FR/.CTURE NECHANICS EVALUATION CPL RHR VALVE, 1.535" SECTION-(A), SF=3 ON PRESSURE, S?=1-OH THERNAL crack sodel: ELLIPTICAL LONOITUDINAL-CRACK lIN= CYLINDER (T/R=0.1,A/L=0.1) , WALL THICKNESS (t)= 1.5350 STRES8 COEFFICIENTS 1 CASE ID CO C1 -C2 C3 i PRESSA 44.7250 -6.7567 4.0393 -1.4076 THERNA 13.1858- l
-3.4559 0.7880 .0970 1 C RACK --------------- STRES S I NTENS I TY FACTOR----------------
SIZE CASE CASE PRESSA THERNA 0.0246 11.706 3.445 0.0491 16,696 4.905 0.0737 20.621 6.047 0.0982 24.013 7.029 0.1228 27.071 - 7.910 0.1474 20.902 8.721 0.1719 :32.566 9.480 0.1965 35.161- 10.199 0.2210 37.536 -10.886 0.2456 39.889 11.546 0.2702 42.175 12.184 0.2947 44.406 12.803 0.3193 46.713 13.441 0.3438 49.119 14.105-0.3684 51.508 14.761 0.3930 53.885- 15.410 0.4175 56.252 -16.053 0.4421 58.612 16.691 0.4666 60.967 17.324 Oi4912 63.319 17.953 0.5158 65.670 18.578: l G.5403- 68.021- 19.200-0.5649 70.374 19.818 0.5894 72.730- 20.433 0.6140 75.089- 21.045 f Prepared by: N//~4-W 0.6386 77.452 21.654 Checked by: **c_/h/h/ File No.CW /(# -Fe% Rev: O Page .b-/0 of b ~/f
po-CRACK VERSION 2.0 PACE: 2 0.6631 '<9.820 - 22.260 - 0.6877
.0.7122 82.193 84.572 22.864 f. M
- 23.465 - -
0.7368- 86.958 24.063
-0.7614 89.351 - 24.658 0.7859 92.088 25.345 0.8105 94.958 26.062 0.8350 97.847 26.779 0.8596 100.756 27.495 0.8842 103.686- 28.211 0.9087 106.636 28.926 0.9333 109.610 29.641 3
0.9578 112.611 30.357 - 0.9824 115.631 31.072 1.0070 118.670 31.784 ' 1.0315 121.729 32.494 1.0501 124.807 ._ 33.202 -j 1.0806 127.900 ?3.906 1 1.1052 131.004 34.604-1.1258 134.125 35.299 j 1.1543 137.265 35.989 1,1789 -140.422 36.676 l 1.2034 143.596 - 37.358 1.2280 146.788 -38.036 END OF pc-CRACK l l l 1 Prepared by: T M */P-9/ , checked by: pe e du/s/ File No CA-M9-Pos Rev: C Page D-l/ of_E-W e _
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(=Lt9W /IV 7W/CK C&c Tl0Af C/~ VA t VE., i i 1 l 1 Revision C Preparer /Date 7M.f p.sy/ l Checker /Dete ac o/atfy-File No. C/04-/sG4 -Pos Page E-- / of 5- 7 l
to pc-CRACK (C). COPYRIGHT- 1984, 1988 STRUCTURAL INTEORITY-ASSOCIATES,1INC. SAN ~ JOSE, CA (408)978-8200 VERSION 2.0 D:to 18-Jan-1991 ' Tito: 14:39:35.48 LEAST SQUARE CURVE FIT OF STRESS PROFILE CPL RHR PRESSURE STRESSES AT 2.988" SECT 10N'(1250 PSI, SF=3)
'TERH COEFFICIENT CO 2.510E+01 C1 -2.763E+00 C2 -1.131E+00 C3 2.766E-01 COEFFICIENT OF DETERMINATION R'2= 0.9996 CORRELATION COEFFICIENT = -0.9992 X VALUE Y VALUE- Y CALC DIFF 0.000E+00 2.505E+01 2.510E+01 -5.171E-02 4.970E-01 2.362E+01 2.348E+01 1.417E-01' 9.970E-01 2.141E+01 2.150E+01 -8.464E-02 1.497E+00 1.931E+01 1.936E+01 -4.742E-02.
1.987E+00 1.732E+01 1.732E+01 6.118E-03 2.487E+00 1.556E+01 .1.549E+01 6.925E 2.988E+00 1.410E+01 1.413E+01 -3.328E-02 END 0F pc-CRACK Prepared by: N//-/ P-v Checked by: v4e e/A//3/ , FUe No. cA-//q-706 Rev: O Page A ~% ci &~? g g-x 1
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to \ pc-CRACK- 1 (C) COPYRIGHT 1984, 1988 { STRUCTURAL-INTEGRITY-ASSOCIATES, INC. SAN JOSE,--CA (408)978-8200 i VERSION 2.0 Dato: 18-Jan-1991 ' Tito 14:49:56.80 LEAST SQUARE CURVE FIT OF STRESS PROFILE CPL RHR THERMAL FTRE.1SES AT 2.988" SECTION (532 F, SF=1) TERM COEFFICIENT C0 3.005E+00 C1 -6.115E-01 ! C2 l
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C3 1.274E-01 1 I COEFFICIENT OF DETERMINATION R*2= 0.9995 CORRELATION COEFFICIENT = 0.9989 l X VALUE Y VALUE Y CALC DIFF 0.000E+00 2.990E+00 3.005E+00 -1.508E-02 4.970E-01 2.640E+00- 2.601E+00 3.872E , l 9.970E-01 2.040E+00 2.057E+00 -1,683E-02 1 1.497E+00_ _1.450E+00 -1.469E+00 -1.913E-02 1.987E+00 9.400E-01 9.434E-01 -3.357E-03 2.487E+00 5.8002-01 5.520E-01 2.797E-02 2.988E+00 3.900E-01 4.023E-01 -1.229E END OF pc-CRACK ' i Prepared by: 78Y/-/ f -P/ Checked by: ac dads / FBe No.CA-/GO-706 Rev: O Page 5-7_ cf.f-7 8' 8 ~
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y 1 to-pc-CRACK (C) COPYRIGHT 1984 1988 STRUCTURAL INTEGRITY ASSOCIATES. INC.
-g* g _ g SAN JOSE, CA (408)978-8200 4 VERSION 2.0 Dato: 18-Jan-1991 Tics: 15: 1:20.79 i i
LINEAR ELASTIC FRACTURE HECHANICS EVALUATION CPL RHR VALVE, 2.988" SECTION (C), SF=3 ON PRESSURE, SF=1 ON_ THERMAL-crack model: LONGITUDINAL CRACK IN CYLINDER (T/R=0.1) WALL THICKNESS (t)= 2.9880 STRESS COEFFICIENTS CASE ID CO C1 C2 C3-PRESSC 25.1017 -2.7628 -1.1305 0.2766 ! THERMC 3.0051 -0.6115 '- 0.4677 0.1274 CRACK ---------------STRESS INTENSITY _ FACTOR---------------- l SIZE CASE CASE PRESSC THERMC-0.0478 10.313 1.231 0.0956 14.858 1.768 0.1434 18.530 -2.198 0.1912 21.778 2.575 0.2390 24.771 2.919 O.2868 27 594 3.239 0.3347- 30.420 3.557-0.3825 33.216- 3.869 0.4303 35.962 4.172 0.4781 38.673 4.467 0.5259 41.356 4.757 0.5737 44.019 5.041 0.6215 46.775 5.332 0.6693 49.640 5.632 l 0.7171 52.510 5.928 I 0.7649 55.386 6.221 0.8127' 58.268 6.512 , 0.8605 61.159 6.799. I :0.9084 64.223 _7.101 0.9562 67.811 7.457 1.0040 71.435 7.813 i , 1.0518 _75.094 8.167 1-l'% $5b9
- 1.1952 86.2 9.219 1.2430 99 832 9.655 Prepared by: MT-P/
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Fue No.M gey: g Page M _::f_ E 1 _ ________,
pc-CRACK VERSION 200 PAGE 1.2908~ 95e456 10.091-P.C~2 1.3386 100.131 10.527 1.3864 104.855 10.963 1.4342' 109.625 11.397 ! 1.4820 114.441 11.831 l 1.5299 120.609 12.409 1.5777 127.295 13.039 1.6255 134.067 13.671 1.6733 140.921 14.304 1.7211 147.853 14.938 1.7689 154.862 16.573 1.8167 162.583 16.275 1.8645 171.034 17.043 1.9123 179.576 17.812 1.9001 188.207 18.581 2.0079 196.923 -19.349 2.0557 205.720 20.116 2.1036 214.912 20.911 2.1514 225.133 21.793 2.1992 235.444 22.674 2.2470 245.842 23.551 2.2948 256.323 24.426 2.3426 266.884 25.297 2.3904 277.522 26.165 END OF pc-CRACK Prepared by: f/<-//-/ P -r/ Checked by: # 4c //a//s/
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