ML18059A424
ML18059A424 | |
Person / Time | |
---|---|
Site: | Palisades |
Issue date: | 12/01/1992 |
From: | Woodman B ABB COMBUSTION ENGINEERING NUCLEAR FUEL (FORMERLY, ASEA BROWN BOVERI, INC. |
To: | |
Shared Package | |
ML18059A421 | List: |
References | |
NUDOCS 9310120438 | |
Download: ML18059A424 (16) | |
Text
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CORRELATION BETWEEN
- YIELD STRENGTH AND TIME TO PWSCC FOR ALLOY 600 PRESENTED AT THE 1992 EPRI WORKSHOP ON PWSCC.OF ALLOY 600 IN PWR'S ORLANDO,FLORIDA DECEMBER 1-31992 BRIAN W. WOODMAN r CONSUL TING ENGINEER ABB-COMBUSTION ENGINEERING NUCLEAR SERVICES
- 'I
- I ALLOY600 r *9a1012043a 9a1007-.,- :\
i PDR ADDCK 05000255 I1 : .
S. *
- PDR L.
FIGURE 11 CHRONOLOGY OF RECENT PWSCC EVENTS 1986 INDUSTRY EXPERIENCES 600 PWSCC (HIGH YIELD STRENGTH MATERIAL)
(MANUFACTURING DEVIATIONS}
1987 YGN SPECIFICATION REQUIRES LOW YIELD STRENGH AND RESISTANT METALLURGY -
1991 CEOG DEVELOPS INITIAL RANKING FOR*.* PWSCC SUSCEPTABILITY:
50 KSI MAX YIELD STRENGTH 1850 °F MIN ANNEALING TEMP SEPT '91 EdF CEDM NOZZLE CRACKING NOV '91 - PALO VERDE REMOVES NOZZLES:
FEB '92 HOT LEG NOZZLES (72 KSI)
PZR NOZZLES (52 KSI)
MAR '92 SONGS REPLACEMENT NOZZLE CRACKS LOW YIELD STRENGTH (38 KSI)
APR'92 YGN NOZZLE DATA RECEIVED FO-R REVIEW APR'92 PROBABALISTIC FAILURE MODEL DEVELOPED AND CORRELATED TO CRACK DATA (MORE RESTRICTIVE CRITERIA)
APR'92 ABB-CE DECISION TO REPLACE
CORRELATION ANALYSIS
- PRESSURIZER NOZZLES
- TUBE MATERIAL
- THEORETICAL MODEL
- I ALLOY600
FIGURE III.2 TIME TO FIRST FAILURE SURFACE FOR ALLOY 600 FORGINGS 1.20 1.00 Cl..
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I-590 20 . 600 0
OPERATING TE_MPERATURE 650 YIELD STRENGTH - KSI OEGF 76
TIME TO FIRST CRACKING VS YIELD STRENGTH CE PRESSURIZER NOZZLES Fitted Actual
.100 80 .......................... ;......................................................:............................ .
Cl) a:
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36 46 56 66 76 A600 BAR 653 OEGF YIELD STRENGTH
TIME TO CRACK INITIATION VS YIELD STRENGTH - NORRING DATA Fitted Actual 20 ----:****-***-****** **************-******-**-*-~*-****-***-** *******--*************---**-!**-****-******- *-****** **-**-****-*-****r***-****************-*-**--*--************* *******-**-************* *****-********-*****
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35 40 45 50 55 60 YIELD STRENGTH - KSI 365 OEGC
- TIME TO FIRST CRACKING VS YIELD STRENGTH CE PRESSURIZER NOZZLES 1.00 ****:-*****-*** ............ L......................L.......................i .......................L......................i.......................i....................... i.......................i. ...................... t ...
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60 65 55 70 75 80 (Zl~t,i,pA YIELD STRENGTH - KSI 653 OEGF
Theoretical Model
Creep Rupture
!/!, = C2 t
c
=_1...
I C.
£ = c3 exp( ~~)exp(~;)
where exp(~;) is approximated by (JN Nln (j = V<J RT Ina =-v-=CONSI'ANT a NRT Regression Analysis 35 ~a ~ 60 KSI N =3.75 Constant Activation Volume Constant Temperature
WEIBULL FAILURE
- MODEL
- EST/MA TION OF PARAMETERS
- SHAPE - EST/MA TED FROM 61 KS/HEAT (ALL CRACKED) : 6.0
- SCALE - EST/MA TED FROM 36 KS/HEAT
( 1 CRACK) : 119 X1a3 EFPH
- FOR OTHER HEATS - SCALE ADJUSTED BY SIGY 3*5
- DEVELOPMENT OF EXTREMAL MODEL
- PARAMETERS OF EXTREME VALUE DISTRIBUTION OBTAINED BY SIMULATION
- MINIMUM FAILURE TIMES FOR GROUPS OF 7
- EST/MA TION OF FAILURE BOUNDS FOR MN M FIRST CRACKS
- I ALLOY600
EXTRE l~E VALUE DI S-l HI BUT \oN SIN-I HES!S BASR L r-l\1LURE MODEL P;(t) " I - FXP(- C-b)ri,)
. -R N\OKfE -CR RLO SIMUU\TOR
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EXTREM.E VRLUE.
01.s\R\ \3ll110\'l t
i &T FA\ LUR.£. 11f\i\ES FOR PORIU\TIOI'{ OF SJlE N
- TIME TO FIRST CRACKING VS YIELD STRENGTH CE PRESSURIZER NOZZLES 200 ............................. *****************=* .........................................******* .. .... ..... . .......... ******.* ............ *- ****************** .... **!** ...................... ***** ********-**. -~*-**
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30 40 50 60 70 80 653 OEGF YIELD STRENGTH - KSI
APPL/CATION TO CRDMLIFE PREDICTION ANALYSIS
- ASSUMPTIONS
- 25 NOZZLES AT RELATIVELY EQUAL RISK
- APPLIED STRESS APPROX/MA TEL Y 125% OF YIELD
- WEIBULL FAILURE MODEL
- 50 KCAUMOLE ACTIVATION ENERGY
- 50 KS/ MATERIAL
- 36 KS/ MATERIAL
- I ALLOY600
TIME TO FIRST FAILURE FOR CROM NOZZLES WITH 45 KSI OPERATING STRESS BASAL EXTREME
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CHRlVGt. JN t PWSc.c FOR.
UN I FORM DE~O RM~TlON TESTS C HAN()E IN tPhJSCC FDf\ VNIFOR[\\ APPLIED STR t.SS TES'fS .
(}'! = J( TA.UNEl\L ) G~RIN Sltof_ .
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