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{{#Wiki_filter: | {{#Wiki_filter:IH AI TENNESSEE VALLEY AUTHORITY BROWNS FERRY NUCLEAR PLANT ExtendedPowe rate -7j].. | ||
* Acoustic Design Relied on Damping Effect-Assumed to eliminate Safety Relief Valve (SRV) resonance* Confirmation of ASB design by 1/8 Scale Model Test (SMT)-Damping effect less than expected-SRV resonance still present* TVA Decided to Cancel ASB Modification | -steam Dryers-- | ||
-No clear advantage to Flow Induced Vibration (FIV)* Requires Stress Analysis to Address EPU-Bump-up factor 4 Decision on Acoustic Side Branches [BFNI With ASBs | October 14, 2008 | ||
_ M SL A Low | |||
____ MSL C Upper MSIS (1 Lower' 10-- -------------------------------- a --- -- ----- -0 50 100 150 200 250 Frequency (Hz)BFN2 With ASBs -MSL A Upper 7 .... .... ....r- | Agenda | ||
,- Data at each strain gage location-Data at CLTP and EPU Mach numbers* Bump-up Factors Calculated as a Function of Frequency by Equation: BF = PSDEPu At each frequency PSDCLTP Applied to Plant CLTP Strain Gage Data to Predict EPU Load PCLTP = CCLTP( | * Status of Unit 1 and 2 Dryer Analyses | ||
= SG Signal -EIC* Additional EIC Signals on Units 1 & 2 EIC now Matched with Companion CLTP and LF Signals PCLTP = CCLTP( | " Decision on Acoustic Side Branches | ||
-- | " Plan to Address SRV Resonance | ||
* Changes in EIC Removal Method | |||
--UECO 2U) BL 0.01 0.001. | * Unit 2 Noise Removal | ||
- | " Submodeling Questions | ||
- | * Review of RAI 19, 20 and 21 Responses | ||
* Schedule 2 | |||
- | Status of Unit 1 and 2 Dryer Analyses * | ||
" TVA Decided not to Install Acoustic Side Branches (ASB) | |||
- No clear advantage | |||
-- | " Unit 1 and 2 Stress Reports (June 2008) Need to be Revised | ||
- SR-a > 2.7 at CLTP | |||
-Weld factor of 1.8 retained-Low level of uncertainty subsumed by bias and uncertainty applied to overall process-20 Review of RAI 19, 20 and 21 Responses I-RA-1* RAI 19-EMCB.147 (Unit 2 only)o New Unit 2 stress analysis o Revised response based on revised analysis-EMCB.192/150 o SRV Resonance EMCB.181 Follow-up o 0- 2 Hz mean filter EMCB.182 Follow-up | - Evaluates CLTP only | ||
-EMCB.181 (Unit 1) & EMCB.147 (Unit 2) Follow-up 0 PSD plot filtering-EMCB.186 & EMCB.187 Follow-up (Unit 1 only)o Sub Modeling* RAI 20-EMCB. 194 (Unit 1 only)o 9% signal coherence-EMCB.195 (Unit 1 only)0 Fan noise 22 Review of RAI | - Unit 2 anomalous low flow (LF) signal (19% power) | ||
-EMCB. 196 (Unit 1 only)o EIC plots-EMCB.197/153 o Strain gage penetration location-EMCB.154 (Unit 2 only)o 9% signal coherence-EMCB.195 0 Extended frequency plots -VFD 23 Review of | - Newer strain gage data now available | ||
" Additional Strain Gage Data | |||
- Unit 1 startup August 2008 | |||
- Unit 2 startup September 2008 | |||
* Unit 1 Stress Report Being Finalized | |||
" Unit 2 Stress Report in Progress 3 | |||
Decision on Acoustic Side Branches | |||
* 24-inch Quad Cities Design Chosen | |||
- Governed by clearance limitations | |||
* Acoustic Design Relied on Damping Effect | |||
- Assumed to eliminate Safety Relief Valve (SRV) resonance | |||
* Confirmation of ASB design by 1/8 Scale Model Test (SMT) | |||
- Damping effect less than expected | |||
- SRV resonance still present | |||
* TVA Decided to Cancel ASB Modification | |||
- No clear advantage to Flow Induced Vibration (FIV) | |||
* Requires Stress Analysis to Address EPU | |||
- Bump-up factor 4 | |||
Decision on Acoustic Side Branches [ | |||
BFNI With ASBs 25 . . . . . . ... | |||
20 ".....MSL S A Upper 20 ------------------------------------ _ M SL A Low er | |||
_MSL B Upper | |||
__ MSL B Lower 15---------- | |||
____ MSL C Upper MSIS (1 Lower | |||
' 10 | |||
-- - - - - - - - - - - - - - - - - - - - - - - - - - - ------ a - -- -- - ---- - | |||
0 50 100 150 200 250 Frequency (Hz) | |||
BFN2 With ASBs - MSL A Upper 7 .... .... .... , ,r- - MSL A Lower | |||
_-- MSL B Upper 6 _ i ------- MSL B Lower 0 -- MSL C Upper | |||
-NISL C Lower 4 ----------I-- ----,-- -------e | |||
--- ---- | |||
0 0 50 100 150 200 250 Frequency (Hz) 5 | |||
Plan to Address SRV Resonance IRA | |||
* 1/8 SMT Performed for each Unit's Configuration | |||
,- Data at each strain gage location | |||
- Data at CLTP and EPU Mach numbers | |||
* Bump-up Factors Calculated as a Function of Frequency by Equation: | |||
BF = PSDEPu At each frequency PSDCLTP Applied to Plant CLTP Strain Gage Data to Predict EPU Load PCLTP = CCLTP(CLTP - EICcLTP) - CLF(LF - EICLF) | |||
PEPU = BF[CCLTP(CLTP- EICCLTP) - CF(LF- EICLF)] | |||
P = Steam line unsteadypressure C = Coherencefactor between upper and lower locations BF = Bump- up factor for SG location EIC = Signal taken wilh zero excitation voltage LF = Low flow signal 6 | |||
Changes in EIC Removal Method SEIC Signal Taken by Removing Strain Gage Excitation Voltage | |||
* Electrical Noise is Removed by Using EIC signal Mechanical Component = SG Signal - EIC | |||
* Additional EIC Signals on Units 1 & 2 EIC now Matched with Companion CLTP and LF Signals PCLTP = CCLTP(CLTP - EICcLTP) - CL,(LF - EICLF) | |||
P = Steam line unsteady pressure C = Coherence factor between upper and lower locations EIC = Signal taken with zero excitation voltage LF = Low flow signal 7 | |||
Changes in EIC Removal Method JiV EIC Signals BFNI A Upper EIC BFNI B Upper EIC | |||
-- *C @lD%,Pm.d FO(2M)AU 0.01 0.0001 Ia 0 50 100 150 200 250 0 50 100 100 200 250 Frqpency (Hz) Fmqumney (Hr) | |||
BFNI A Lower EIC BFNI B Lower EIC 0.1 | |||
-- FHzWO0W(1Bt tfEZ:QeflflPov.m* | |||
0.1I - - U*E. N%Po-4UdZW.D(5M)8L | |||
--UtE @86%Povmrl4*zWIOrO)AL | |||
-- UECO WIk*Oa01*Hz1W0{ | |||
2U)BL 0.01 0.01 I 0001I 0.001 01 a 00001 . .0001 wV-. | |||
000001I 0000001I 0 | |||
ffi2_LL 50 100 Frmoncy (Hz) 150 200 250 0 50 100 F.qmency (Hz) 150 200 250 8 | |||
Changes in EIC Removal Method iRA EIC Signals BFNI C Upper EIC BFNI D Upper EIC 0-1 0.1 | |||
-- -WQet~floVSJUFiZ*WD (TW)OU --U~lECg ewlSS t4HPz WO(736)DU | |||
-- U1E8@o0Po¶.wtvo (2l8,cu 0.01 0.01 0001 0.001 0 0.0001 _ e 0.0001 0.00000_ .... | |||
00l0001 . .. | |||
0 00 100 150 200 250 0 50 100 150 200 250 F-q-n..y (H.) | |||
BFNI C Lower EIC BFN1 D Lower EIC | |||
-- UIEIC@6%P01a11t'4H4 2W0 (1161 C | |||
0.001 0.501 [ | |||
I a 0001 Ia 0, 0001 _______ _ _ _ i _ i ____i i 0 s0 100 150 200 250 50 100 150 200 250 Fmquene (Hz) 9 | |||
Changes in EIC Removal Method IM EIC Signals BFN2 A Upper EIC BFN2 B Upper EIC 0.1 0.1 | |||
-WEC@5%P ýw/HzW(4018U | |||
-WECG$3%POýnHZWO( 2)aU | |||
-WEC@WPOd4HZW(49)BU 0.01 0.001-0.001 | |||
..- | |||
S 0.00001 0.00001 0.~0l00 00.001 0 so 100 ISO 200 250 FBAquency (H.) Fmq-.ney (Hz) | |||
BFN2 A Lower EIC BFN2 B Lower EIC 0.t 0.1 001 | |||
_ -- EEG | |||
* (228q | |||
%Poý4536Hz'VFO TO 0.01 0.001 1 0.001 ul 0.0001 : :: | |||
0000 0*00001-0.000001 * - * - . --- | |||
0,000001 ' | |||
0 50 100 10S 200 250 0 00 100 150 200 250 Frequency (Hz) Frequency (H1) 10 | |||
Changes in EIC Removal Method EIC Signals BFN2 C Upper EIC BFN2 D Upper EIC 0.1-0.01 -- ____ _ 0.01 001 0.00001 0 0 1.0 1.020 210 100 150 200 250 Freqency (Hr) | |||
BFN2 C Lower EIC 01 | |||
--L EC (ie)c | |||
@81%,Pov,fOe'6$HzWD | |||
-WEI@1,po.4S ztFD(4)O. | |||
0.01 0.0001 0.00001 _______ | |||
0 so 100 150 200 250 Fmq.mnmy (Hz) 11 | |||
Unit 2 Noise Removal | |||
* Additional Data Taken on Unit 2 to Confirm Signal Behavior | |||
- Electrical noise on Unit 2 varies with recirculation pump speed (VFD frequency) | |||
- Relationship is not well understood | |||
- 19% power signal originally used for noise removal was atypical | |||
- Composite 19% & 30% power signals replaced | |||
* New LF signal at 5% Power and Companion 5% EIC Signal | |||
- All strain gages -on MSL D lower damaged | |||
- Substituting MSL A for MSL D due to strain gage failures | |||
- CLTP signal and companion EIC signal unchanged 12 | |||
Unit 2 Noise Removal PSD Signals BFN2 A UPoer BFN2 B Uppe 1.0E-01 1.0E-01 14 0 | |||
50 100 150 200 250 50 150 200 250 100 Fq y(z Fre.n1y (.z) | |||
BFN2 A Lo BFN2 B Lower 1.0E-01 1.0E-02 F1.00E-03 1.0E-03 1*- | |||
1 0-04 I. 01 .00-04 I.0E-05 1.00-00 1.00-06 50 100 150 200 250 Freqency (Hz) Froequcy (Hz) 13 | |||
Unit 2 Noise Removal PSD Signals BFN2 C LpW BFN2 D Upep 1.00E01 10E-02 1.00-03 0 | |||
(0 .00-04 1.00-06 50 100 150 200 250 Freq-y (Hz) | |||
BFN2 C Loý BFN2 D tow 1.0E-01 1.0E-02 1.0E-03 0 | |||
l.E-05 I .00-00 250 so 100 150 200 250 FM.weoy (Ftz) Frequey (Hz) 14 | |||
Submodeling Questions Is the Stress Reduction Factor (SRF) accurate and unique? | |||
Would a different analyst get the same solution? | |||
- Limited, Specific Purpose o Avoid excess conservatism of shell model o Based on mechanistic behavior along weld line | |||
- CDI Shell Model => SIA Shell Submodel o Characteristic load matches CDI stress along the weld line Drain Channel-to-skirt: Bending thru the joint - See Figure 1 Hood Stiffener-to-Hood: Membrane in stiffener - See Figure 2 | |||
- SIA Shell Submodel => SIA Solid Submodel o Incorporates weld geometry o Applies characteristic loads o Accurately captures load transfer mechanism and stress distribution through weld | |||
- Submodel attributes (loads & boundary conditions) are not unique, but SRF is unique & accurate. So a different analyst would get the same result. | |||
15 | |||
S ubmodeling Questions IRAI Submerged Skirt - Figure 1 Node 98156, Skirt 1000 800 CL 600 C | |||
U) 4-400 200 0 | |||
50 50.1 50.2 50.3 50.4 50.5 Time [ s ] | |||
16 | |||
Submodeling Questions Inner Hood Stiffener - Figure 2 Node 104843, Hood Support 5000 [ | |||
4 0 00 .... ... .............. - - - | |||
3000-- -- | |||
CD | |||
.-U) 2000oo ..... Ci | |||
.......... .. .. | |||
-.-Surface : | |||
0)0 10 0 0 -m id dle .. . . . . . .-- | |||
.. . --. . . . . . .. . . . . . . . .. . . .. . . ... . . . .. . . . | |||
bottom 50 50.1 50.2 50.3 50.4 50.5 Time [s ] | |||
17 | |||
Submodeling Questions I-- | |||
ft-A-1 | |||
* Are the submodel loads statically equivalent to the CDI model? | |||
- No - not statically equivalent, nor required | |||
- Limited objective is to capture stress along weld line | |||
- Simple Example: | |||
REAL BEAM EQUIVALENT BEAM Objective: Design Connecting Weld (For FEA Model) | |||
For Real Beam Using FEA | |||
,=-- M= | |||
M k-ft I k , ,M 10k-ft 10k+ | |||
~ILZ Z 0M = 10 k-ft | |||
-21 18 | |||
Submodeling Questions Are the times used the ones which yield the largest stress intensity after application of the SRF? | |||
Refer again to Figures 1 & 2 | |||
- Alternating stress defined by either membrane or bending extrema | |||
- Extrema states produce maximum strain (i.e., fatigue usage) | |||
- SRF should be based on the extrema stress state | |||
- At other points in time, the product of stress intensity and SRF would have a lower value; i.e., be less conservative 19 | |||
Submodeling Questions Demonstrate that the uncertainty in calculating the SRF is small | |||
- Approach produces high certainty that bounding stress of weld line is captured | |||
- Solid submodel mesh sensitivity study demonstrated convergence | |||
- Weld factor of 1.8 retained | |||
- Low level of uncertainty subsumed by bias and uncertainty applied to overall process | |||
- 20 | |||
Review of RAI 19, 20 and 21 Responses I-RA-1 | |||
* RAI 19 | |||
- EMCB.147 (Unit 2 only) o New Unit 2 stress analysis o Revised response based on revised analysis | |||
- EMCB.192/150 o SRV Resonance EMCB.181 Follow-up (Unit 1 only) o 0- 2 Hz mean filter EMCB.182 Follow-up (Unit 1 only) 0 EIC removal | |||
- EMCB.183 Follow-up (Unit 1 only) 0 SR-P values in table 21 | |||
Review of RAI 19, 20 and 21 Responses ITVA_ | |||
" RAI 19 (continued) | |||
- EMCB.181 (Unit 1) & EMCB.147 (Unit 2) Follow-up 0 PSD plot filtering | |||
- EMCB.186 & EMCB.187 Follow-up (Unit 1 only) o Sub Modeling | |||
* RAI 20 | |||
- EMCB. 194 (Unit 1 only) o 9% signal coherence | |||
- EMCB.195 (Unit 1 only) 0 Fan noise 22 | |||
Review of RAI 19Y20 and 21 Responses I-R-A-1 RAI 20 (continued) | |||
- EMCB. 196 (Unit 1 only) o EIC plots | |||
- EMCB.197/153 o Strain gage penetration location | |||
- EMCB.154 (Unit 2 only) o 9% signal coherence | |||
- EMCB.195 0 Extended frequency plots - VFD 23 | |||
Review of RAI 19 20 and 21 Responses | |||
* RAI 21 | |||
- EMCB.198 (Unit 1 only) o EIC removal | |||
- EMCB.155 (Unit 2 only) 0 EIC removal 24 | |||
Schedule I Item Date TVA response to RAI 21 on Channel Bow 10/17/08 TVA submit Unit 1 stress analysis & Unit 2 status 10/31/08 TVA submit Unit 2 stress analysis 11/14/08 Tentative ACRS meetings 2/09-3/09 Unit 2 outage begins 4/09 NRC issue EPU Amendment for Units 1, 2, and 3 4/09 Unit 2 startup at EPU 5/09 Unit 1 implement EPU 6/09 Unit 3 implement EPU Spring 2010 25}} |
Revision as of 12:06, 14 November 2019
ML082890206 | |
Person / Time | |
---|---|
Site: | Browns Ferry |
Issue date: | 10/14/2008 |
From: | Tennessee Valley Authority |
To: | Division of Operating Reactor Licensing |
Brown, E, NRR/DORL, 415-2315 | |
Shared Package | |
ML083030525 | List: |
References | |
TAC MD5262, TAC MD5263 | |
Download: ML082890206 (25) | |
Text
IH AI TENNESSEE VALLEY AUTHORITY BROWNS FERRY NUCLEAR PLANT ExtendedPowe rate -7j]..
-steam Dryers--
October 14, 2008
Agenda
- Status of Unit 1 and 2 Dryer Analyses
" Decision on Acoustic Side Branches
" Plan to Address SRV Resonance
- Changes in EIC Removal Method
- Unit 2 Noise Removal
" Submodeling Questions
- Review of RAI 19, 20 and 21 Responses
- Schedule 2
Status of Unit 1 and 2 Dryer Analyses *
" TVA Decided not to Install Acoustic Side Branches (ASB)
- No clear advantage
" Unit 1 and 2 Stress Reports (June 2008) Need to be Revised
- SR-a > 2.7 at CLTP
- Evaluates CLTP only
- Unit 2 anomalous low flow (LF) signal (19% power)
- Newer strain gage data now available
" Additional Strain Gage Data
- Unit 1 startup August 2008
- Unit 2 startup September 2008
- Unit 1 Stress Report Being Finalized
" Unit 2 Stress Report in Progress 3
Decision on Acoustic Side Branches
- 24-inch Quad Cities Design Chosen
- Governed by clearance limitations
- Acoustic Design Relied on Damping Effect
- Assumed to eliminate Safety Relief Valve (SRV) resonance
- Confirmation of ASB design by 1/8 Scale Model Test (SMT)
- Damping effect less than expected
- SRV resonance still present
- TVA Decided to Cancel ASB Modification
- No clear advantage to Flow Induced Vibration (FIV)
- Requires Stress Analysis to Address EPU
- Bump-up factor 4
Decision on Acoustic Side Branches [
BFNI With ASBs 25 . . . . . . ...
20 ".....MSL S A Upper 20 ------------------------------------ _ M SL A Low er
_MSL B Upper
__ MSL B Lower 15----------
____ MSL C Upper MSIS (1 Lower
' 10
-- - - - - - - - - - - - - - - - - - - - - - - - - - - ------ a - -- -- - ---- -
0 50 100 150 200 250 Frequency (Hz)
BFN2 With ASBs - MSL A Upper 7 .... .... .... , ,r- - MSL A Lower
_-- MSL B Upper 6 _ i ------- MSL B Lower 0 -- MSL C Upper
-NISL C Lower 4 ----------I-- ----,-- -------e
--- ----
0 0 50 100 150 200 250 Frequency (Hz) 5
Plan to Address SRV Resonance IRA
- 1/8 SMT Performed for each Unit's Configuration
,- Data at each strain gage location
- Data at CLTP and EPU Mach numbers
- Bump-up Factors Calculated as a Function of Frequency by Equation:
BF = PSDEPu At each frequency PSDCLTP Applied to Plant CLTP Strain Gage Data to Predict EPU Load PCLTP = CCLTP(CLTP - EICcLTP) - CLF(LF - EICLF)
PEPU = BF[CCLTP(CLTP- EICCLTP) - CF(LF- EICLF)]
P = Steam line unsteadypressure C = Coherencefactor between upper and lower locations BF = Bump- up factor for SG location EIC = Signal taken wilh zero excitation voltage LF = Low flow signal 6
Changes in EIC Removal Method SEIC Signal Taken by Removing Strain Gage Excitation Voltage
- Electrical Noise is Removed by Using EIC signal Mechanical Component = SG Signal - EIC
- Additional EIC Signals on Units 1 & 2 EIC now Matched with Companion CLTP and LF Signals PCLTP = CCLTP(CLTP - EICcLTP) - CL,(LF - EICLF)
P = Steam line unsteady pressure C = Coherence factor between upper and lower locations EIC = Signal taken with zero excitation voltage LF = Low flow signal 7
Changes in EIC Removal Method JiV EIC Signals BFNI A Upper EIC BFNI B Upper EIC
-- *C @lD%,Pm.d FO(2M)AU 0.01 0.0001 Ia 0 50 100 150 200 250 0 50 100 100 200 250 Frqpency (Hz) Fmqumney (Hr)
BFNI A Lower EIC BFNI B Lower EIC 0.1
-- FHzWO0W(1Bt tfEZ:QeflflPov.m*
0.1I - - U*E. N%Po-4UdZW.D(5M)8L
--UtE @86%Povmrl4*zWIOrO)AL
-- UECO WIk*Oa01*Hz1W0{
2U)BL 0.01 0.01 I 0001I 0.001 01 a 00001 . .0001 wV-.
000001I 0000001I 0
ffi2_LL 50 100 Frmoncy (Hz) 150 200 250 0 50 100 F.qmency (Hz) 150 200 250 8
Changes in EIC Removal Method iRA EIC Signals BFNI C Upper EIC BFNI D Upper EIC 0-1 0.1
-- -WQet~floVSJUFiZ*WD (TW)OU --U~lECg ewlSS t4HPz WO(736)DU
-- U1E8@o0Po¶.wtvo (2l8,cu 0.01 0.01 0001 0.001 0 0.0001 _ e 0.0001 0.00000_ ....
00l0001 . ..
0 00 100 150 200 250 0 50 100 150 200 250 F-q-n..y (H.)
BFNI C Lower EIC BFN1 D Lower EIC
-- UIEIC@6%P01a11t'4H4 2W0 (1161 C
0.001 0.501 [
I a 0001 Ia 0, 0001 _______ _ _ _ i _ i ____i i 0 s0 100 150 200 250 50 100 150 200 250 Fmquene (Hz) 9
Changes in EIC Removal Method IM EIC Signals BFN2 A Upper EIC BFN2 B Upper EIC 0.1 0.1
-WEC@5%P ýw/HzW(4018U
-WECG$3%POýnHZWO( 2)aU
-WEC@WPOd4HZW(49)BU 0.01 0.001-0.001
..-
S 0.00001 0.00001 0.~0l00 00.001 0 so 100 ISO 200 250 FBAquency (H.) Fmq-.ney (Hz)
BFN2 A Lower EIC BFN2 B Lower EIC 0.t 0.1 001
_ -- EEG
- (228q
%Poý4536Hz'VFO TO 0.01 0.001 1 0.001 ul 0.0001 : ::
0000 0*00001-0.000001 * - * - . ---
0,000001 '
0 50 100 10S 200 250 0 00 100 150 200 250 Frequency (Hz) Frequency (H1) 10
Changes in EIC Removal Method EIC Signals BFN2 C Upper EIC BFN2 D Upper EIC 0.1-0.01 -- ____ _ 0.01 001 0.00001 0 0 1.0 1.020 210 100 150 200 250 Freqency (Hr)
BFN2 C Lower EIC 01
--L EC (ie)c
@81%,Pov,fOe'6$HzWD
-WEI@1,po.4S ztFD(4)O.
0.01 0.0001 0.00001 _______
0 so 100 150 200 250 Fmq.mnmy (Hz) 11
Unit 2 Noise Removal
- Additional Data Taken on Unit 2 to Confirm Signal Behavior
- Electrical noise on Unit 2 varies with recirculation pump speed (VFD frequency)
- Relationship is not well understood
- 19% power signal originally used for noise removal was atypical
- Composite 19% & 30% power signals replaced
- New LF signal at 5% Power and Companion 5% EIC Signal
- All strain gages -on MSL D lower damaged
- Substituting MSL A for MSL D due to strain gage failures
- CLTP signal and companion EIC signal unchanged 12
Unit 2 Noise Removal PSD Signals BFN2 A UPoer BFN2 B Uppe 1.0E-01 1.0E-01 14 0
50 100 150 200 250 50 150 200 250 100 Fq y(z Fre.n1y (.z)
BFN2 A Lo BFN2 B Lower 1.0E-01 1.0E-02 F1.00E-03 1.0E-03 1*-
1 0-04 I. 01 .00-04 I.0E-05 1.00-00 1.00-06 50 100 150 200 250 Freqency (Hz) Froequcy (Hz) 13
Unit 2 Noise Removal PSD Signals BFN2 C LpW BFN2 D Upep 1.00E01 10E-02 1.00-03 0
(0 .00-04 1.00-06 50 100 150 200 250 Freq-y (Hz)
BFN2 C Loý BFN2 D tow 1.0E-01 1.0E-02 1.0E-03 0
l.E-05 I .00-00 250 so 100 150 200 250 FM.weoy (Ftz) Frequey (Hz) 14
Submodeling Questions Is the Stress Reduction Factor (SRF) accurate and unique?
Would a different analyst get the same solution?
- Limited, Specific Purpose o Avoid excess conservatism of shell model o Based on mechanistic behavior along weld line
- CDI Shell Model => SIA Shell Submodel o Characteristic load matches CDI stress along the weld line Drain Channel-to-skirt: Bending thru the joint - See Figure 1 Hood Stiffener-to-Hood: Membrane in stiffener - See Figure 2
- SIA Shell Submodel => SIA Solid Submodel o Incorporates weld geometry o Applies characteristic loads o Accurately captures load transfer mechanism and stress distribution through weld
- Submodel attributes (loads & boundary conditions) are not unique, but SRF is unique & accurate. So a different analyst would get the same result.
15
S ubmodeling Questions IRAI Submerged Skirt - Figure 1 Node 98156, Skirt 1000 800 CL 600 C
U) 4-400 200 0
50 50.1 50.2 50.3 50.4 50.5 Time [ s ]
16
Submodeling Questions Inner Hood Stiffener - Figure 2 Node 104843, Hood Support 5000 [
4 0 00 .... ... .............. - - -
3000-- --
CD
.-U) 2000oo ..... Ci
.......... .. ..
-.-Surface :
0)0 10 0 0 -m id dle .. . . . . . .--
.. . --. . . . . . .. . . . . . . . .. . . .. . . ... . . . .. . . .
bottom 50 50.1 50.2 50.3 50.4 50.5 Time [s ]
17
Submodeling Questions I--
ft-A-1
- Are the submodel loads statically equivalent to the CDI model?
- No - not statically equivalent, nor required
- Limited objective is to capture stress along weld line
- Simple Example:
REAL BEAM EQUIVALENT BEAM Objective: Design Connecting Weld (For FEA Model)
For Real Beam Using FEA
,=-- M=
M k-ft I k , ,M 10k-ft 10k+
~ILZ Z 0M = 10 k-ft
-21 18
Submodeling Questions Are the times used the ones which yield the largest stress intensity after application of the SRF?
Refer again to Figures 1 & 2
- Alternating stress defined by either membrane or bending extrema
- Extrema states produce maximum strain (i.e., fatigue usage)
- SRF should be based on the extrema stress state
- At other points in time, the product of stress intensity and SRF would have a lower value; i.e., be less conservative 19
Submodeling Questions Demonstrate that the uncertainty in calculating the SRF is small
- Approach produces high certainty that bounding stress of weld line is captured
- Solid submodel mesh sensitivity study demonstrated convergence
- Weld factor of 1.8 retained
- Low level of uncertainty subsumed by bias and uncertainty applied to overall process
- 20
Review of RAI 19, 20 and 21 Responses I-RA-1
- RAI 19
- EMCB.147 (Unit 2 only) o New Unit 2 stress analysis o Revised response based on revised analysis
- EMCB.192/150 o SRV Resonance EMCB.181 Follow-up (Unit 1 only) o 0- 2 Hz mean filter EMCB.182 Follow-up (Unit 1 only) 0 EIC removal
- EMCB.183 Follow-up (Unit 1 only) 0 SR-P values in table 21
Review of RAI 19, 20 and 21 Responses ITVA_
" RAI 19 (continued)
- EMCB.181 (Unit 1) & EMCB.147 (Unit 2) Follow-up 0 PSD plot filtering
- EMCB.186 & EMCB.187 Follow-up (Unit 1 only) o Sub Modeling
- RAI 20
- EMCB. 194 (Unit 1 only) o 9% signal coherence
- EMCB.195 (Unit 1 only) 0 Fan noise 22
Review of RAI 19Y20 and 21 Responses I-R-A-1 RAI 20 (continued)
- EMCB. 196 (Unit 1 only) o EIC plots
- EMCB.197/153 o Strain gage penetration location
- EMCB.154 (Unit 2 only) o 9% signal coherence
- EMCB.195 0 Extended frequency plots - VFD 23
Review of RAI 19 20 and 21 Responses
- RAI 21
- EMCB.198 (Unit 1 only) o EIC removal
- EMCB.155 (Unit 2 only) 0 EIC removal 24
Schedule I Item Date TVA response to RAI 21 on Channel Bow 10/17/08 TVA submit Unit 1 stress analysis & Unit 2 status 10/31/08 TVA submit Unit 2 stress analysis 11/14/08 Tentative ACRS meetings 2/09-3/09 Unit 2 outage begins 4/09 NRC issue EPU Amendment for Units 1, 2, and 3 4/09 Unit 2 startup at EPU 5/09 Unit 1 implement EPU 6/09 Unit 3 implement EPU Spring 2010 25