ML043010481
| ML043010481 | |
| Person / Time | |
|---|---|
| Site: | San Onofre  |
| Issue date: | 10/25/2004 |
| From: | Scherer A Southern California Edison Co |
| To: | Document Control Desk, Office of Nuclear Reactor Regulation |
| References | |
| Download: ML043010481 (111) | |
Text
SOUTHERN CALIFORNIA EDISON An EDISONV INTERN.ATIONALM Company A. Edward Scherer Manager of Nuclear Regulatory Affairs October 25, 2004 U. S. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001
Subject:
Docket Nos. 50-361 and 50-362 Additional Information Supporting Third Ten-Year Inservice Inspection (ISI) Interval Relief Requests ISI-3-11, Revision 1 and ISI-3-12 to Support Potential Pressurizer Heater Sleeve Repairs.
San Onofre Nuclear Generating Station, Units 2 and 3
Reference:
Letter from A. E. Scherer (SCE) to the Document Control Desk (NRC) dated October 15, 2004;
Subject:
Docket Nos. 50-361 and 50-362, Third Ten-Year Inservice Inspection (ISI) Interval Relief Requests ISI-3-1 1, Revision 1 and ISI-3-12 to Support Potential Pressurizer Heater Sleeve Repairs, San Onofre Nuclear Generating Station, Units 2 and 3
Dear Sir or Madam,
As requested, this letter provides the Southern California Edison (SCE) Calculation M-DSC-402, uPressurizer Heater Sleeve J-Groove Weld Flaw Eval-SONGS 2 & 3" to support the SCE Relief Requests ISI-3-11, Revision 1 and ISI-3-12, which were submitted to the NRC by the referenced October 15, 2004, letter.
Should you have any questions, please contact Mr. Jack Rainsberry, Manager, Plant Licensing at (949) 368-7420.
Sincerely, cc:
B. S. Mallett, Regional Administrator, NRC Region IV B. M. Pham, NRC Project Manager, San Onofre Units 2 and 3 C. C. Osterholtz, NRC Senior Resident Inspector, San Onofre Units 2 and 3 P.O. Bo3x 128 San Clemente, CA 92674-0128 949-368-7501 Fax 949-368-7575 c)q,7
CALCULATION TITLE PAGE ICCN NOJ 1PRELIM. CCN NO.
1PAGE OF l CCN CONVERSION:
Catc No. M-DSC-402 DCPJFIDCNJ FCNIECP No. & Rev.
IJ A
CCN NO. CCN-
Subject:
Pressurizer Heater Sleeve J-Groove Weld Flaw Eval -SONGS 2&3 Sheet 1 of 110 System Number/Primary Station System Designators 1201 IBBB SONGS Unit 2 & 3 0-Class I
Tech. SpecJLCS Affecting? 0) NO 0 YES Section No.
Equipment'TagNo.
S2(3)1201ME087 Site Programs/Procedure Impact?
) NO 0 YES. AR No.
10CFR50.59R72.48 REVIEW CONTROLLED COMPUTER PROGRAM/DATABASE Is this calculation revision being issued solely 1
PROGRAM PROGRAM? DATABASE NAME(S)
VERSION? RELEASE NO. (S) to incoporale CCNs?
3 NO Q YES E
DATABASE BIGIF' AR No. 030900690-2 According to SO123-XXIV-5.1 O_ ALSO. LISTED BELOW RECORD OF ISSUES TOTAL PREPARED APPROVED DIC DESRIPIO (Print namrelsign/date)
(Slgnature/date)
DSC DESCRIPTION LAST SHT nita PQS Bioc* - RPoui re, POS 73FN64 Initial POS Block -Repures POS T3e4) 0 INTAISU1 ORIG POS VER. BYn1S FLp-------
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Space for RPE Stamp, Identify use of an alternate Calc., and notes as applicable.
" THE BIGIF COMPUTER PROGRAM (REFERENCE 8) WAS USED BY APTECH TO PERFORM THE STRESS INTENSITY FACTOR AND THE FATIGUE CRACK GROWTH ANALYSES. THE ACCURACY OF THE BIGIF PROGRAM HAS BEEN VERIFIED FOR BOTH ANALYSIS TYPES.
POOR OUALIY DOCUMENT BDSTAVAIABLE COP SIGNED: AP. C/
_A-.!I' II
/z/k DbGUMEET ORIGINATOR DATE SITE FILE COPY This cal. was prepared for the Identified DCP/FCN/ISCO ECP. DCP/FCNIECP completion and turnover acceptance to be verified by receipt of a memorandum directing DCN/ECN Conversion. Upon receipt, this cato. represents the as-built condition. Memo date. -------- by SCIE 26-121-1 REV. 7 2JD4
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CALCULATION CROSS-INDEX ICCN NOJ PREUM. CCN NO.
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Calculation No.
M-DSC-402 Sheet No.
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S023-919-3, PROJECT SPEC FOR PRZ ASSEMBLY SONGS UNITS 2 AND 3 M-DSC-356, EVAL OF MOD PRZ HEATER SLEEVES -
SONGS UNITS 2 AND 3 8
1 DRWG NO. S023-919-79, 0
PRZ GENERAL ARRANGEMENT DRWG NO. S023-919.86, 1
HEATER ARRANGEMENT AND ASSEMBLY SCE26-424 REV. 4 701 IREFERENO:so012SMXvW7.151
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CALCULATION COVER SHEET Calculation No.:
AES-C-5212-2 Client:
Southern California Edison SCE No. M-DSC402, Rev. 0
Title:
Pressurizer Heater Sleeve J-Groove Weld Project No.:
AES 03105212-1Q Flaw Evaluation -SONGS Units 2 and 3 APTECH Office:
Sunnyvale Sheet No.
3 of llO a Uncontrolled 1U Controlled Document Control No.:
1-2
Purpose:
The purpose of this calculation is to evaluate the half-sleeve weld repair for the removal of Alloy 600 heater sleeve. For this repair, any flaws present in the original J-groove weld or sleeve stub shall be acceptable for the remaining service period for the pressurizer. This calculation is based on a fracture mechanics analysis of the repair geometry and conservatively evaluates the significance of flaws that could remain after repair.
Assumptions:
The analysis assumptions are described in Section 3.
Results:
The results of this calculation are summarized in Section 2. The evaluation period covered by this calculation is a 40-year service life considering loading from the original design. The postulated conditions following weld repair, including hypothetical flaws that are assumed to remain, are acceptable to the safety margins of ASME Section XI under IWB-3600 guidelines.
Prepared Checked Verified Approved Revision By By By By Revision Description No.
Date Date Date Date 0
qAmCr "Afc7 Initial Release 11710 (v1-
~
fAPTECHIr ENGINEEIUNG SERVICES. INC.
CAN45 REV. 8196
ENGINEERING SanFiCES. INC Madv br:
Damt aint Calculation No.:
AES-C-5212-2 M
/7lo/ 9 S Ce SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer HeaterSleeve 3-Groove Weld Flaw 5, qrAES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 4oflI0 TABLE OF CONTENTS Section Title Paae CALCULATION TITLE PAGE I
CALCULATION CROSS-INDEX 2
CALCULATION COVER SHEET 3
1.0 INTRODUCTION
6 2.0
SUMMARY
OF RESULTS 9
2.1 Scope and Objectives 9
2.2 Sleeve J-Groove Evaluation Results 9
3.0 ANALYSIS ASSUMPTIONS I I 4.0 METHODOLOGY 12 4.1 Technical Approach 12 4.2 Flaw Acceptance Criteria 13 4.3 Calculation of Flaw Size Parameters 14 4.3.1 Calculation of End-of-Life Flaw Size (ad 14 4.3.2 Calculation of Minimum Critical Flaw Size (a,) for Normal/Upset 14 Conditions 4.3.3 Calculation of Minimum Initiating Flaw Size (as) for Accident 15 Conditions 4.4 Calculation of Stress Intensity Factor 16 4.5 Fracture Toughness Criteria of Appendix K 16 4.6 Definition of Stresses in the J-Groove Region 18 5.0 DESIGN INPUT 23 5.1 Sleeve and Bottom Head Geometry 23 5.2 Design and Operating Conditions 23 5.3 Material Properties 24 5.3.1 Mechanical Strength 24 5.3.2 Fracture Toughness 25 5.3.3 Fatigue Crack Growth Rate for the PZR Bottom Head 26 QAE17 REV 8/96
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ENGINEER INU 5ERVlCES,. INC.
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Calculation No.:
AES-C-5212-2 D
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Proiect No.:
Title:
Pressurizer Heater Sleeve 3-Groove Weld Flaw I.t-t_
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AES 03 105212-1Q Evaluation -
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0 1-2 5ofll0 Section Title Pane
6.0 REFERENCES
37 7.0 NOMENCLATURE 39 8.0 CALCULATIONS 41 8.1 Heater Sleeve Penetration Stresses 41 8.2 Consideration of Weld Residual Stresses 42 8.2.1 Fracture Resistance 42 8.2.2 Fatigue Crack Growth Rate 43 8.3 Definition of Cycle Stresses 43 8.4 Evaluation of Postulated Flaws at the J-Groove Weld 44 8.4.1 Flaw Model 44 8.42 J-Groove Weld Stresses 45 8.4.3 Allowable Flaw Depth Evaluation 45 8.4.3.1 Appendix A Evaluation 45 8.4.3.2 Appendix K Evaluation 46 8.4.4 Fatigue Evaluation 47 8.5 Evaluation of Borated Water Corrosion 48 APPENDIX A-
SUMMARY
OF HEATER SLEEVE CYCLIC STRESSES 54 APPENDIX B-BIGIF COMPUTER OUTPUT FOR J-GROOVE 82 FLAW EVALUATION (UPHILL SIDE)
APPENDIX C-BIGIF COMPUTER OUTPUT FOR J-GROOVE 96 FLAW EVALUATION (DOWNHILL SIDE)
QAE17 REV 8,96
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te7/VI SCE SCE No. M-DSC402, Rev. 0 CCecked by:
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Proiect No.:
Title:
Pressurizer Heater Sleeve 3-Groove Weld Flaw 1Adn--rC-C7 C 5L; AES 03105212-1 Q Evaluation -
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0 1-2 6ofllO
1.0 INTRODUCTION
The pressurizer (PZR) bottom head contains multiple penetrations for instrumentation and heater rod nozzles and sleeves. A schematic illustration of the PZR bottom head is shown in Figure I -I (Ref. 1).
The heater sleeve penetrations are the scope of this calculation.
There are a total of 30 heater sleeves. An illustration of a typical heater sleeve and attachment weld is shown in Figure 1-2 (Ref. 2). The heater sleeves were originally designed to American Society of Mechanical Engineers (ASME)Section III (Ref. 3). An ASME Section XI evaluation (Ref. 4) is performed on the J-groove attachment weld to establish the flaw tolerance of the weld detail, in particular the underlining carbon steel bottom head.
The purpose of this calculation is to evaluate the heater sleeve penetrations with regard to the half-sleeve repair option strategy that removes a portion of the original Alloy 600 sleeve. The assumed cause of flaws in heater sleeves is primary water stress corrosion cracking (PWSCC) due to high surface tensile residual stresses near the J-groove attachment weld. The objective of this calculation is to demonstrate that the half-sleeve repair will satisfy ASME Code Section XI requirements. Since the original nozzle geometry has been restored, ASME Section III Code requirements are satisfied for allowable stress limits and fatigue usage. Therefore, the remaining Code requirements to be evaluated are ASME Section XI acceptance criteria for flaws postulated to exist in the repair. Specifically, the postulated condition assumed to exist after repair is an axially oriented flaw in the corner region within the J-groove weld. This postulated flaw is to address the question of the fracture and flaw growth resistance of the low alloy carbon steel bottom head.
The evaluated conditions addressed in this calculation are pressure, mechanical loads, and design basis transients. The design cycles for a 40-year design life are imposed to justify long-term acceptance. The flaw evaluation procedures, material properties, and acceptance criteria of ASME Section XI, Appendix A and Appendix K, are used as guidance in completing the calculations (Ref. 4).
The half-sleeve repair will allow primary water to come in contact with the carbon steel head.
Therefore, there is a potential for general corrosion or wastage to occur in the annulus between the sleeve and bore hole. This degradation mechanism has been previously evaluated and determined not to be significant for a 40-year service life subsequent to repair (Ref. 5). Therefore, borated water corrosion will not impact the margin requirements of ASME Section XI.
QAE17 REV8196
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Pressurizer Heater Sleeve J-Groove Weld Flaw
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Figure 1 Pressurizer Bottom Head Configuration.
QAE17 REV 8196
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Pressurizer Heater Sleeve J-Groove Weld Flaw
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(-7 LSf AES 03105212-IQ Evaluation -
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0 1-2 8 oflO
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QAE17 REM'8/96
EERPTECHr ENGtNEERING SEllVIX IN Madre by:
Date:
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Calculation No.:
AES-C-5212-2
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SCE SCE No. M-DSC402, Rev. 0 Checked be:
Date:
Proiect No.:
Title:
PressurizerHeater Sleeve J-Groove Weld Flaw Ad4 7TZ..
7 c
(7 AES 03105212-1 Q Evaluation -
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0 1-2 9ofllO 2.0
SUMMARY
OF RESULTS 2.1 Scope and Objectives A fracture mechanics-based evaluation has been performed to justify the long-term acceptance of the weld repair option for heater sleeves in the PZR bottom head. This repair option involves the removal of a portion of the Alloy 600 sleeve and replace it with Alloy 690 sleeve. The Alloy 690 sleeve is attached to the bottom head at the outside surface by a J-groove weld forming a new pressure boundary for the sleeve. The original 3-groove weld at the inside surface remains in service along with a portion of the original Alloy 600 sleeve.
The long-term acceptance of the PZR heater sleeve repair is subject to the acceptance of a postulated condition: the potential existence of axial cracks in the original J-groove attachment weld. The sleeves at the outer position were evaluated since they will be bounding in terms of service stress levels. The flaw evaluation rules and acceptance criteria of ASME Section XI were employed to establish the pressure boundary integrity and allowable service life for the PZR heater sleeve repair.
2.2 Sleeve J-Groove Evaluation Results The flaw postulated to remain in the J-groove attachment weld was conservatively evaluated. The computed stresses for the outer heater sleeves were used to envelop the service conditions for all heater sleeve penetrations subject to repair. A large 1.0-inch depth comer crack, penetrating completely through the sleeve wall and J-groove weld and into the low alloy steel head was conservatively assumed to bound the size of any flaw remaining in the Alloy 600 material. The postulated flaw is illustrated in Figures 4-1 and 8-1. This postulated flaw depth is approximately 25% of the bottom head wall thickness Fracture mechanics and fatigue crack growth (FCG) analyses following the procedures of ASME Section XI, Appendix A, were completed to determine the allowable flaw depths and service life. The calculations for this evaluation are given in Section 8.4. It is assumed that the flaw is surface-connected so that the alloy steel head is exposed to the reactor water. The FCG behavior in a reactor water environment was conservatively assumed. However, pressure loading acting on the crack face was neglected, given the conservative size of the initial flaw assumed in the analysis. In terms of the allowable flaw depth, the limiting flaw location between the uphill and downhill weld locations is the uphill side.
The allowable flaw depth is computed to be 1.45 inches for the uphill side of the penetration. The acceptance criterion is based on maintaining a minimum safety factor of 10O1n on load for normal and upset loading conditions and 2112 on load for emergency and faulted conditions, whichever is limiting.
For the completed evaluation, the limiting service condition is the cooldown transient with flooding for which the smallest allowable flaw depth is calculated (i.e., all10 = 1.42 inches).
QAE17 REV8196
HHRPTSEWC ENGINEERING SERVIES. INQ Made bv:
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Calculation No.:
AES-C-5212-2 9/I 7/O0t SCE SCE No. M-DSC-402, Rev. 0 Checked br.
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Proiect No.:
Title:
PressurizerHeater SleeveJ-Groove WeldFlaw b
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- McStLOB-AES 03105212-lQ Evaluation -
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0 1-2 lOofilO An ASME Section Xl Appendix K toughness evaluation procedure and acceptance criteria was also performed to verify the input parameters and assumptions used for determining allowable flaw depth by Appendix A procedures. The Appendix K procedures are directly applicable given the service temperature (i.e., upper shelf condition) and postulated flaw depth assumptions used in this analysis.
The results from the Appendix K evaluation confirm that the allowable flaw depths fr6m Appendix A are conservative.
The maximum flaw growth for the postulated initial flaw (a,, = 1.0 inches) for a 40-year design life is computed to be 0.21 inch for the uphill side. The final crack depth is therefore calculated to be 1.21 inches and af = 1.21 inches
< aallow
= 1.42 inches The allowable flaw depth is computed to be 1.50 inches for the downhill side of the penetration. For the downhill flaw evaluation, the limiting service condition is again the cooldown transient with flooding for which the smallest allowable flaw depth is calculated (i.e., alaow = 1.52 inches). The maximum flaw growth for the postulated initial flaw (ao = 1.0 inches) for a 40-year design life is computed to be 0.25 inch for the uphill side. The final crack depth is therefore calculated to be 1.25 inches and af
= 1.25 inches
< aallow
= 1.52 inches Therefore, the calculated final flaw depths for both uphill and downhill locations are acceptable for a 40-year design life. Based on this evaluation, any flaws remaining in the J-groove region will be acceptable to the safety margin requirements of ASME Section XI under IWB-3600.
QAE17 REV 8196
ENGiRPTECH:s Madebr.
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Iltle: Pressurizer Heater Sleeve J-Groove Weld Flaw Tr-( 17 5ABZ AES 03105212-lQ Evaluation -
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0 1-2 11 of 110 3.0 ANALYSIS ASSUMPTIONS The following assumptions were made in performing the design analysis calculations:
- 1.
The flaw evaluation was completed using the 1995 Edition of ASME Section XI as guidance. Flaw evaluation procedures given under IWB-3600 and Appendix A of ASME Section XI are generally applicable.
- 2.
Weld residual stresses are considered in the assessment. For elastic-plastic considerations, the maximum stress in the J-groove region is assumed to be limited by the yield strength of the material. A maximum yield strength of 60 ksi is assumed.
- 3.
The hoop stresses at the inside surface of the bottom head due to external sleeve loads are assumed to be negligible (see Ref. 6).
- 4.
Acceptance criteria for normal/upset and accident conditions are considered in the evaluation.
- 5.
Maximum stress conditions for the outermost heater sleeves are assumed for all sleeve locations (bounding for all heater sleeves covered by this calculation).
- 6.
Weld indications are assumed to be crack-like. The crack model is assumed to completely penetrate the J-groove weld and enter the low alloy steel shell.
- 7.
Crack growth rate for reactor water for R = 0.25 is assumed in the evaluation for fatigue crack growth outside the J-groove region. Given the large initial postulated crack and nature of stress cycles (i.e., near zero or negative R ratios), this assumption will be conservative.
- 8.
Cooldown transient with flooding is assumed to occur with each shutdown. This assumption is very conservative given the higher stresses of this transient and that low likelihood of occurrence given current plant operation.
- 8.
Irradiation embrittlement of the PZR bottom head is negligible.
In general, use of the above assumptions will result in a conservative analysis of the flaw for normal operating conditions. Conservative means any condition that will result in a smaller calculated critical flaw size or in accelerated crack growth rates under normal operation.
QAE17 REV 8/96
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Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw A h~r.
-i ce Y-AES 03 105212-1 Q Evaluation -
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0 1-2 12 of 110 4.0 METHODOLOGY 4.1 Technical Approach The evaluation procedures of ASME Section XI, Appendix A, are used to analyze the postulated flaw geometries. The flaw is evaluated as a sharp crack and normal to the maximum principal stress direction (hoop direction) of the bottom head. The flaws are postulated as axially oriented cracks originating in the J-groove, as shown in Figure 4-1. It is conservatively assumed that the flaws will grow radially through the J-groove and into the low alloy steel head/shell material. The initial flaw assumed in the evaluation is a large quarter circular crack that just resides in the low alloy steel. This assumption conservatively ignores any crack growth life through the J-groove material.
The evaluation procedure is described in Article A-5000 of Section XI, Appendix A. Both theoretical solutions and numerical methods are used to evaluate the flaw, given the flaw size and geometry data, material properties, and the transient stresses and temperatures at the penetration location. These methods are used to calculate the following Section XI flaw parameters:
ar -
The maximum size to which the detected flaw is calculated to grow in a specified time period a, -The minimum critical size of the flaw under normal/upset operating conditions ai -The minimum critical size of the flaw under emergency/faulted accident conditions Stress results from a three-dimensional finite element analysis (Ref. 7) are used to define stress distributions at the J-groove weld. The BIGIF computer program (Ref. 8) is used in the stress intensity factor and FCG analyses. The accuracy of the BIGIF program has been verified for both fracture and FCG analyses.
In addition to flaw evaluation procedures under IWB-3600, an alternate evaluation is performed to the procedure of IWB-3730 and Appendix K, which covers the situation of having adequate fracture toughness margins at upper shelf conditions. The methods of Appendix K are used for determining an allowable flaw size where assumptions regarding weld residual stress and concerns for brittle fracture can be more directly addressed. These procedures and acceptance criteria are discussed in Section 4.5 QAE17 REV 8196
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Pressurizer Heater Sleeve 3-Groove Weld Flaw T-t14-r--
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0 1-2 13ofllO 4.2 Flaw Acceptance Criteria Flaws are acceptable if the critical flaw parameters satisfy the criteria of IWB-361 1. These flaw size acceptance criteria are:
af<O.lac (4-1) af <O.5ai (4-2) where as, a,, and a; are defined in Section 4.1.1. Equation 4-1 is the requirement for normal conditions and Eq. 4-2 governs the emergency/faulted conditions.
Alternatively, if the applied stress intensity factor and the flaw size, af, satisfy the following IWB-3612 criteria af <aallow (4-3) where aallow is the minimum value of "a" determined from the following equations:
K, (a) < Kla/10 K, (a)
Klc/NF2 (normallupset)
(emergency/faulted),
(4-4a)
(4-4b) then the flaw is acceptable based on load. For Eq. 4-4a, K1 is the maximum applied stress intensity factor under normal conditions, and Kia is the available fracture toughness based on crack arrest for the corresponding crack tip temperature. For Eq. 4-4b, K, is the maximum stress intensity factor under emergency and faulted conditions, and K1c is the available fracture toughness based on fracture initiation for the corresponding crack tip temperature.
For the case at flange and shell discontinuities, and when the system pressure is less than 20% of the design pressure and the metal temperature exceeds RTNDT + 60TF, the criteria of IWB-3613 states:
K, (a) < KjaAF2, (4-4c) then the flaw is acceptable based on load under these limited service conditions.
QAE17 REV 8/96
l lo ENG!NEERIW3 SERVl:ES, NC Made by Date:
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Calculation No.:
AES-C-5212-2
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Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 177 C( V AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
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0 1-2 14ofl11 Satisfying either the flaw size criteria or the applied load criteria and checking that the appropriate primary stress limits are satisfied will demonstrate acceptance of the flaw to ASME Section XI for the design conditions. It is expected that the acceptance criteria for normal conditions will govern the allowable flaw size because of the higher required safety margins imposed by ASME Section XI.
4.3.
Calculation Flaw Size Parameters 4.3.1 Calculation of End-of-Life Flaw Size (ad)
The expected end-of-life flaw size (af) is computed by a cumulative FCG analysis for normal operating conditions for the remainder of the expected service life of the component, according to Article A-5200 of Section XI, Appendix A. Normal conditions include all transients expected to occur during testing and normal operation. Included in normal operation are upset conditions that are anticipated to occur frequently enough as to warrant their consideration during design.
The FCG rate (daldN) of the shell material is characterized by the following relation:
da/dN=COAKn (4-5) where da/dN is the crack growth rate (i.e., inches per cycle of loading), C0 and n are material constants, and AK1 is the range in stress intensity factor for the load cycle (AK, = Kmx - Kmin).
The material constants for alloy steel head material are given in Appendix A of ASME Section XI. The BIGIF computer program performs the FCG analysis by integrating Eq. 4-5. The number of applied load cycles, N, for the design transients is calculated from N
r da (4-6) o da/dN where ao is the starting crack depth and af is the final crack depth.
4.3.2 Calculation of Minimum Critical Flaw Size (a.) for Normal/Upset Conditions The procedure to compute the minimum critical flaw size for normal operation (a,) as specified by Article A-5200 of Section XI, Appendix A is outlined below:
- 1. Determine the maximum end-of-life irradiation level at the flaw location (embrittlement of the PZR bottom head due to neutron radiation is negligible, i.e., A RTNDT = 0).
- 2. Using fracture toughness data, determine the crack-arrest fracture toughness (K12) as a function of temperature.
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0 1-2 15of1lO
- 3. Calculate stress intensity factors, K1, for various geometrically similar crack depths of the assumed flaw.
- 4. Compare the calculated stress intensity factors to the material fracture toughness (Kla) for the appropriate temperature to determine ak for the transient.
- 5. Proceed to the next transient.
The calculated values for the stress intensity factor as a function of crack depth, Kl(a), are utilized in the determination of a, from YK(ac)=Kl.cITRTNDT)
(4-7) where T is temperature at the crack tip and RTNDT is the nil ductility temperature for the shell material.
Equation 4-7, therefore, represents the intersection of the toughness distribution and the applied K1 field.
The smallest value of a, determined by the above procedure after all transients have been considered is the minimum critical flaw size for normal operation. This minimum value of as is checked against the flaw acceptability criteria of IWB-3600 (see Section 4.2).
4.3.3 Calculation of Minimum Initiating Flaw Size (a,) for Accident Conditions The procedure to compute the minimum initiating flaw size (as) for emergency/faulted conditions as specified by Article A-5300 of Section XI, Appendix A, is outlined below:
- 1. Determine the maximum end-of-life irradiation level at the flaw location (embrittlement of the pressurizer bottom head due to neutron radiation is assumed to be negligible, i.e.,
ARTNDT = 0).
- 2. Using fracture toughness data, determine the initiation fracture toughness (Kk,) as a function of temperature.
- 3. Calculate stress intensity factors, K1, for various geometrically similar crack depths of the assumed flaw.
- 4. Compare the calculated stress intensity factors to the material fracture toughness (Kic) for the appropriate temperature to determine a; for the transient.
- 5. Proceed to the next transient.
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0 1-2 16ofllO The calculated values for the stress intensity factor as a function of crack depth, Kl(a), are utilized in the determination of a3 from KI(ai)=KIc(TRTNDT)
(4-8) where T is the temperature at the crack tip and RTNDT is the nil ductility temperature for the shell material. Equation 4-8, therefore, represents the intersection of the toughness distribution and the applied K, field. The smallest value of a; determined by the above procedure after all accident conditions have been considered is the minimum initiating flaw size for emergency/faulted conditions.
This minimum value of a; is checked against the flaw acceptability criteria of IWB-3600 (see Section 4.2).
4.4 Calculation of Stress Intensity Factor The stress intensity factor is defined as KjIFVF-(4-9) where a is the applied stress, F is a function which accounts for flaw geometry and loading mode, "a" is the crack depth, and Q is the flaw shape parameter. The explicit calculation of K] is performed numerically by the BIGIF program.
4.5 Fracture Toughness Criteria of Appendix K For the condition of preventing failure on the upper shelf, adequate toughness is evaluated by demonstrating flaw stability. The equilibrium equation for stable flaw extension is:
J=JR (4-10) where J is the applied J-integral for the applied loads on the flaw and JR is the fracture toughness resistance curve against ductile tearing. The condition for stable ductile tearing is defined by the inequality:
'DJ "C dJR Da da
(
)
where aJIaa is the partial derivative of the applied 3-integral with respect to flaw depth (load held constant), and dJ/da is the slope of the JR curve for the material. Under increasing load, stable flaw extension will continue as long as aJ/aa in Eq. 4-11 remains valid.
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0 1-2 17of 110 For Service Level A and B (normal/upset conditions), adequacy of the upper shelf toughness is confirmed when, for a 1/4t flaw depth plus an additional 0.1 inch in depth to account for crack extension, and a factor of 1.15 on accumulation pressure, and a factor of 1.0 on thermal loads, the Japplied is less than Jo.l, Japplied <~ JDAl (4-12) where Jo., is the JR value at 0.1 inch crack extension. For limiting ductile tearing, flaw extensions at 1.25 times the accumulation pressure and 1.0 on thermal loads, shall remain ductile and stable.
Translating these criteria to flaw evaluation in terms of preventing crack initiation, the structural factors from Eq. 4-12 are equivalent to a factor of 1.4 on operating pressure (accumulation pressure is 1.10 times design pressure and operating pressure is 0.9 times design pressure). Provided that the postulated flaw depth is on the order of 25% of the wall thickness, preventing fracture initiation can be represented by Japplied <JIc (4-13)
In order to maintain the same margin on primary load that ASME Section XI Appendix A requires, the elastic-plastic parameters of Eq. 4-13 can be evaluated for the condition of constrained plasticity based on fracture initiation with the following relationships:
Japplied = 1000(3.16Kp + Kit)2 /E (4-14)
J c =l 000 Ka 2 /E (4-15) a a+1 [Kip +Kit12(16 ae =a KV (4-16) where 3.16 factor is simply 1012 structural factor from IWB-3612 acceptance criteria K1p is the stress intensity factor for pressure loading for crack depth "a" determined from the plastic-zone corrected crack depth a. in Eq. 4-16, QAE17 RE' 5/96
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Pressurizer Heater Sleeve J-Groove Weld Flaw
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0 1-2 IS oflO Kit is the stress intensity factor for thermal loading for crack depth "a" determined from the plastic-zone corrected crack depth a, in Eq. 4-16, ay is the yield strength for the material E is E/(l -v2 ) where E is the modulus of elasticity and v is Poisson's ratio.
Satisfying Eq. 4-13 will be sufficient to meet the criteria of Appendix K in that crack extension is being prevented by the increased structural factor on pressure load (additional factor of 3.16/1.40 or 2.25) and the use of the initiation toughness based on Kia lower bound curve. Therefore tearing stability criterion will automatically be satisfied if Eq. 4-13 is met.
4.6 Definition of Stresses in the J-Groove Region The distribution of hoop stresses at the sleeve penetration and throughout the PZR bottom head was obtained from the results of a three-dimensional finite element analysis (Ref. 7). An illustration of the finite element model is shown in Figure 4-2. Additional views of the model are given in Figures 4-3 and 4-4. This model geometry represents the outermost heater sleeve location (i.e., 52 degree penetration angle). The model represents a 90 degree segment of the PZR lower shell and bottom head. The model includes the surge nozzle and support skirt. The other heater sleeve penetrations are also modeled but the sleeves were omitted from the model to simplify the analysis since they will not affect the local stress results in the area of the outermost sleeve.
Close-up views of the sleeve, original J-groove weld, and repair weld/pad on the outside of the bottom head is shown in Figures 4-3 and 4-4. The results from this analysis will be bounding for sleeves at other locations.
A summary of input stress distributions are given in Appendix A of this calculation. These stress results are used as input to the BIGIF program in the calculation of allowable flaw depth and final flaw depth due to cyclic (fatigue) loading.
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PressurizerHeaterSleeve J-Groove Weld Flaw y
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0 1-2 19ofIlO Heater Element Uphill Side Flaw IBottom Headr Figure 4 Postulated Flaw in Heater Sleeve Weld Region.
Downhill Side Flaw QAE17 REV 8196
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0 1-2 20 of 110 Shell Support Skirt l eater l ISeeve Bottom Head Surge Nozzle Figure 4 Finite Element Model of PZR Bottom Head.
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0 1-2 21ofllO Figure 4 Local View of Heater Sleeve Region.
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0 I-2 22ofI10 l
Original J-groove Weld (Downhill) 8~
l Pad Weld I Heater Sleeve Figure 4 Edge View of Heater Sleeve Region.
QAE17
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0 1-2 23of 10 5.0 DESIGN INPUT 5.1 Sleeve and Bottom Head Geometry The heater sleeve is 1.660-inch nominal outside diameter size. The heater sleeve completely penetrates the PZR bottom head wall. The penetration through the spherical head is vertical. A schematic illustration of the nozzle geometry is shown in Figure 5-la (Ref 2). The components of this penetration are described as follows (Refs. 1, 2, 6):
Sleeve:
Outer radius:
Inner radius:
Wall thickness:
Bottom Head:
Outer radius:
Inner radius:
Wall thickness:
Clad thickness:
Hole diameter:
ro = 0.830 inch (max) rl = 0.6365 inch (min) t = 0.1935 inch (max)
& = 52 5/16 inches R; = 48 7/16 inches (excluding clad) th
= 3 7/8 inches (min, w/o clad )
tc
= 7/16 inch Dh
= 1.672 inches (min) counter bore
= 1.662 inches (min) through hole The half-nozzle repair geometry is illustrated in Figure 5-lb (Ref. 9).
5.2 Design and Operating Conditions The design data for the primary side of the RCS from Refs. 10 and 11 are as follows:
Design pressure Design temperature Operating pressure Operating temperature Hydrotest pressure
= 2500 psia
= 7000F
= 2250 psia
= 653TF
= 1.25PD=3125psia(3110psig)
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0 1-2 24of 10 Thermnal transients are given in Table 5-I (Refs. 1 0 and I11). Seven thermal cases are conservatively assumed that envelop the thermal transients. These are:
I. Isothermal steady-state load of 6530F; corresponding reactor coolant pressure is 2235 psig.
- 2. Heatup/cooldown at a rate of 200'F per hour; corresponding change in reactor coolant of 2235 psig.
- 3. Cooldown with flooding.
- 4. Plant loading/unloading and step changes of +/-201F; corresponding change in reactor coolant of +/-100 psig.
- 5. Reactor trip (loss of load, etc).
- 6. Loss of secondary pressure (emergency condition).
- 7. Leak and hydro test heatup/cooldown at I 000F per hour; corresponding change in reactor coolant pressure is 2235 and 3110 psig.
Except for Case 5, all design basis conditions are classified as normal or upset conditions. Case 5 is classified as emergency condition and is the only accident condition relevant for the bottom head heater sleeve penetrations. The transient temperature conditions for Cases 3, 4 and 5 above are illustrated in Figures 5-2, 5-3 and 5-5. Specified changes in reactor coolant pressure for cooldown with flooding, reactor trips, and loss in secondary pressure are shown in Figures 5-2, 5-4 and 5-6 5.3 Material Properties 5.3.1 Mechanical Strength The materials that comprise the head and sleeves (Refs. 10 and 11) are as follows:
Bottom Head:
Sleeve:
Head Cladding:
Shell/Nozzle Cladding Surge Nozzle Support Skirt:
SA-533, Grade B, Class I SB-I 67, Alloy 600 Alloy 600 Type 304 stainless steel SA-508, Class II SA-516 Grade 70 QAE17 REV 8/96
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0 1-2 25of 10 In the stress analysis, the cladding is included. Ile mechanical strength properties at the design temperature are summarized below (Ref. 3):
l1 MECHANICAL STRENGTH AT 700F I
SleevelWeld Bottom Head (Alloy 600)
(SA-533B-1)
Sm (ksi) 23.3
-26.7 Sy (ksi) 27.0 43.1 S. (ksi) 80.0 80.0 Also, Sy for Alloy 600 at 1000F is 35 ksi. In the assessment of yielding and imposed weld residual stress, a maximum yield strength of 60 ksi is assumed.
5.3.2 Fracture Toughness Definition of fracture toughness at the flaw location as a function of temperature was obtained from Article A-4000 of Appendix A to Section XI (Ref 4).Section XI defines lower-bound behavior for K12 and K10 for SA-533B-1, SA-508-2, and SA-508-3 steels and associated welds, as shown in Figure 5-7.
The equational formats of these reference curves are given below.
Kla
= 26.8 + 12.445 exp[0.0145 (T - RTNDT)]
(5-1)
Klc
= 33.2 + 20.734 exp[0.02 (T - RTND)]
(5-2) where T is the metal temperature in 'F, RTNDT is the reference nil ductility temperature in `F, and K12 and K10 are fracture toughness in ksi in1 2. The toughness parameter, Kl, is based on the lower bound of static initiation critical K1 values measured from specimens tested at several temperatures. Similarly, K1a is based on the lower bound of crack-arrest toughness data. It is assumed that the transition behavior of SA-533B-1 will be such that the normal operation of the PZR bottom head will be on the upper shelf during times when maximum pressure stresses are imposed.
The pressure-temperature (P-T) operation of the RCS will be controlled by the P-T limit curves for the RPV and, therefore, maximum operating stresses will not be experienced by the PZR at lower shelf toughness temperatures. This assumption is justified by the fact that RTNDr of SA-533B3-will be less than +20°F, which is the mean plus two standard deviations (upper bound) reported in Ref. 12. An RTNDT = +20'F will cause the onset of upper shelf conditions at T > 120°F for initiation toughness. For this condition, the upper shelf toughness is 200 ksi in"2, as reflected in Figure 5-7, and is based on data evaluations in Ref. 13.
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0 1-2 26ofI10 5.3.3 Fatigue Crack Growth Rate forthe PZR Boftom Head The reference curve for crack growth rate (da/dN) in a reactor water environment is given in Figure A-4300-2 of ASME Section XI, Appendix A, and is shown in Figure 5-8 for two R-ratio regimes.
The crack growth behavior for the R-ratio range (0* R < 0.25) is used in this evaluation. The equation for crack growth is:
da/dN
=
1.02 x 10-2 AK595 da/dN = 1.01 x 0-7 AK1 95 AK < 17.74 ksi in"2 AK > 17.74 ksi in1/2 (5-3)
(5-4) where AK is in units of ksi in11 and da/dN is in units of inches/cycle. These crack growth rates are used as input to the FCG analysis for the PZR bottom head. The basis for the use of Eqs. 5-3 and 5-4 is discussed in under the analysis assumptions.
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PressurizerHeater SleeveJ-Groove Weld F]aw 1
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0 1-2 27of 110 Table 5-1 THERMAL TRANSIENT CONDITIONS (Refs. 6, 10 & 11)
Symbol Transient Condition Occurrence Al Plant Heatup 200°F/hr 500 BI Steady State 653°F, 2250 psia Cl Cooldown
-200°F/hr 500 CFI Cooldown with Flooding Fig. 5-2
+20°F DI Plant Loading/Step Increase
+2100 psia 1,000,000
-200F El Plant Unloading/Step Decrease
-100 psia Fl Reactor Trip Figs. 5-3 & 5-4 480 GI Loss of Secondary Pressure Figs. 5-5 & 5-6 5
1000F/hr 200 HI Plant Leak Test, Heatup 2250 psia
-1000F/hr 200 H2 Plant Leak test, Cooldown 2250 psia 100°Flhr JI Hydrostatic Test, Heatup 3125 psia 10
-100°F/hr
.11 Hydrostatic Test, Cooldown 3125 psia QAE17 REV 8/96
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0 1-2 28ofII0 Figure 5-1a -
Illustration of the Heater Sleeve Geometry (Original J-Groove Configuration).
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0 1-2 29 of 110 HALF-NOZZLE REPAIR
- (FOR NOZZLE LOCATION SEE TABLE 2)
Figure 5-1 b - Illustration of the Half-Nozzle Repair Configuration.
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0 1-2 3Oof I 0 Cooldown with Floodilng Trndent forth. Lower Pat of Pressurizer 700 -2O f2MO E-,^
-Scous E 3 o0
_10 e
o"Nt pd454ps S
10001 o
os I ts e
s05Ise 10 25
,.Tllm tht)
Noic (1): Tcmpenw conditim an to be hldd wail tbeamal eqilibi mtadicas r add to mimim in Inthe Preir.
Figure 5 Transient Condition-Cooldown with Flooding Transient (Figure 10 of Ref. 10).
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Pressurizer Heater Sleeve J-Groove Weld Flaw 1 7 p-l-.5n L
Lf AES 03105212-1 Q Evaluation -
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0 1-2 31 ofilO0 I.z I
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,I,, or 663ro
!.ItI*
1"F5i r.
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0 1-2 32of110 IE
. IZT r, w W
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'7 EZ5 'O £1 I j-I 0
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Figure 5 Pressure Change in Reactor Coolant During Reactor Trip Transients (Figure 3 of Ref. 11).
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0 1-2 33of110 0
7jUa.= i1.
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-=2700 6aw2 o10 stwoo"
/4000 ^oo zoo oo 77ME-CO0ISD Figure 5 Temperature Change in Reactor Coolant During Loss of Secondary Pressure Transient (Figure 4 of Ref. 11).
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TC-C J7 5 Y.
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0 1-2 34ofII0 0 I v
11 Y515D 1.
g._
I A/lfd L PfR5UPc.
+'?2 Ar5OA a
Za=
J=
- -24 2 6040 7000 eow Ao IXo/o qaoo g2000 77ME- -50CVOD5 Figure 5 Pressure Change in Reactor Coolant During Loss of Secondary Pressure Transient (Figure 4 of Ref. 11).
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Title:
Pressurizer Heater Sleeve J-Groove Neld Flaw 7
T-t7 5g,2!cf AES 03105212-1 Q Evaluation -
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0 1-2 35of110 220 200 180 F-160
- 1 M a
120 e
100 Je 80 3
60 1-KJ, I
I I
-I I
I I
I 40 20 - _
I t
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-80
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40 80 120 160 200 Ir-Tgr7 LF Figure 5 Lower Bound Fracture Toughness from Tests of SA-533B-1, SA-508-2, and SA-508-3 (Figure A-4200-1 from ASME Section Xl, Appendix A, in Ref. 4).
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Pressurizer Heater Sleeve 3-Groove Weld Flaw A
mn 5ftaycf AES 03 105212-1 Q Evaluation -
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0 1-2 36ofI10 i
I 100 101 102 AK, Iksd..A})
Figure 5 Reference Fatigue Crack Growth Curves for Carbon and Low Alloy Ferritic Steels Exposed to Water Environments (Figure A4300-2 from ASME Section Xi, Appendix A, in Ref. 4).
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PressurizerHeater Sleeve J-Groove Weld Flaw IfTc.
(I S/
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0 1-2 37 of 1 10
6.0 REFERENCES
- 1.
Drawing 235-121, Rev. 3, "Pressurizer General Arrangement San Onofre III," S023-919-79-0 (October 10, 1976) (ECD-I1 from Project AES 97103213-1Q).
- 2.
Drawing 235-130, Rev. 4, "Heater Arrangement and Assembly Sa Onofre III," S023-909-86-01 (March 31, 1981) (ECD-12 from Project AES 97103213-IQ)).
- 3.
ASME Boiler and Pressure Vessel Code,Section III, "Rules for Construction of Nuclear Power Plant Components," 1971 Edition through 1971 Summer Addenda.
- 4.
ASME Boiler and Pressure Vessel Code,Section XI, "Rules for Inservice Inspection of Nuclear Power Plant Components," 1995 Edition with 1996 Addenda.
- 5.
"Evaluation of Half-Nozzle Repair for Pressurizer and Steam Generator Instrumentation Nozzles Under Long-Term Service Conditions," Calculation No. AES-C-3247-1, Aptech Engineering Services, Inc. (ICD-2 for Project AES 97123247-1Q) (May 11, 1998)
- 6.
"Analytical Report for Southern California, San Onofre, Unit 2, Pressurizer," CENC-1275, CDCC No. 21986, Combustion Engineering, September 1976 (ECD-5 from Project AES 97103213-lQ).
- 7.
"SONGS 2 and 3 Pressurizer Bottom Head Stress Analysis," ANSYS Results transmitted electronically, Southern California Edison (July 2004) (ECD-2 through 10).
8 Cipolla, R. C., P. M. Besuner, and D. C. Peters, "BIGIF -
Fracture Mechanics Code for Structures," Manual 2, User's Guide, EPRI NP-838 (August 1978).
- 9.
"Half-Nozzle Repair Drawing," DOC No. S023-919-86, Revision 1, Southern California Edison, Transmitted September 15, 2004, (ECD-15).
- 10.
"Project Specification for a Pressurizer Assembly for San Onofre Units Nos. II & No. III,"
Specification No. 01370-PE-130, Revision 10, Combustion Engineering, SCE S023-919-3, Rev. 8 (January 4, 1999) (ECD-]).
- 11.
"General Specification for a Pressurizer Assembly," Specification No. 00000-PE-130, Revision 3, Combustion Engineering, SCE S023-919-4-1, (October 25, 1972) (ECD-2 from Project AES 97103213-1Q).
- 12.
NUREG-0577, "Potential for Low Fracture Toughness and Lamellar Tearing on PWR Steam Generator and Reactor Coolant Pump Supports," Appendix C (October 1979).
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Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 77t.
{7 54/Y§ AES 03105212-IQ Evaluation -
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0 1-2 38of 10
- 13.
"Flaw Evaluation Procedures -Background and Application of ASME Section XI Appendix A," EPRI NP-719-SR, Electric Power Research Institute (August 1973).
- 14.
"Operability Assessment for CEOG Plants with Hypothetical Circumferential Flaw Indications in Pressurizer Heater Sleeves," Draft WCAP-I 6180, Rev. 0, Westinghouse Electric (November 2003).
- 15.
"Evaluation of Modified Pressurizer Heater Sleeves - SONGS Unit 2 and 3," Calculation No.
AES-C-5212-1, Project AES-03105212-1Q, Aptech Engineering Services, (September 17,2004)
(ICD-1).
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Pressurizer Heater Sleeve J-Groove Weld Flaw 7
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0 1-2 39ofII0 7.0 NOMENCLATURE a
aallow a.
ar a;
ao Aa Co D
dh Do E
F 3
Japplied JR K
K1 Kia Kmax Kmin AK n
N P
PD Pmax Pmin
= Flaw depth, inch
= Allowable flaw depth, inch
= Minimum critical crack size for normal/upset conditions, inch
= Final flaw depth, inch
= Minimum critical crack size for accident conditions, inch
= Initial flaw depth, inch
= Change in flaw depth, inch
= Material constant in the reference FCG equation
= Depth of corrosion groove, inch
= Diameter of hole penetration, inch
= Outer diameter, inch
= modulus of elasticity (ksi)
= Flaw correction factor
= J-integral value, in-lbs/in
= Applied J-integral curve, in-lbs/in
= J resistance toughness curve for ductile tearing, in-lbs/in
= Stress intensity factor, ksi in1/2
= Mode I stress intensity factor, ksi inIt2
= Fracture toughness for crack arrest, ksi in1 2
= Static fracture toughness for initiation, ksi in1t2
= Maximum value of K in stress cycle, ksi in12
= Minimum value of K in stress cycle, ksi inln
= Range in stress intensity factor (Kmax - Kmin), ksi infl' 2
= Exponent in the reference FCG equation
= Number of cycles
= Pressure, psi
= Design pressure, psi
= Maximum pressure in transient, psi
= Minimum pressure in transient, psi QAE17 ME' 8196
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Pressurizer Heater Sleeve J-Groove Weld Flaw 7'if 7t..
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0 1-2 40ofI10 AP
= Pressure fluctuation, psi Q
= Flaw shape parameter R
= Radial distance, inch ro
= Outer radius of sleeve, inch ri
= Inner radius of sleeve, inch R
= Mean radius, inch R
= R-ratio (Kmin / Krim)
Ro
= Outer radius of head or shell, inch R;
= Inner radius of head or shell, inch S,
= Allowable stress intensity, psi SI
= Specified minimum ultimate tensile strength, ksi SY
= Specified minimum yield strength, ksi t
= Wall thickness, inch T
= Temperature, TF AT
= Temperature difference, 'F t'
= Clad thickness, inch th
= Head or shell thickness, inch v
= Poisson's ratio ay
= Yield strength, ksi QAE17 REV 8/96
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Pressurizer Heater Sleeve J-Groove Weld Flaw B
y rrz71 2
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0 1-2 41 of llO 8.0 CALCULATIONS 8.1 Heater Sleeve Penetration Stresses The hoop stresses for the heater sleeve penetration were obtained from the finite element analysis contained in Ref. 7. These stress summaries are given in Appendix A of this calculation. The loading conditions and corresponding stress results for the outer heater sleeve penetration are bounding due to the more severe geometric discontinuity between the sleeve and head. Therefore, the stress distributions from this stress analysis are conservatively used to establish the maximum and cyclic stress behavior for all heater sleeve penetrations.
The following load cases from Ref. 7 were used to bound the maximum stresses and stress ranges at the postulated flaw locations:
- 1.
Internal
- 2.
Heatup
- 3.
Cooldown
- 4.
Cooldown with Flooding
- 5.
Isothermal
- 6.
Plant Load/Unload Transient P = 2500 psi AT = 200'F/hr (P = 2235 psig)
Fig. 5-2 T = 6530 F AP = +/-100 psi, AT = +200F)
Figs. 5-3 & 5-4 Figs 5-5 & 5-6 AT = +100°F/hr
- 7.
- 8.
Loss of Secondary Pressure
- 9.
Leak/Hydro Test Weld residual stress was developed from literature results and added to the mechanical and thermal stresses when computing allowable flaw depths.
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0 1-2 42 of 110 The stress combinations for the fatigue stress ranges for the eight plant transient conditions were developed from the load cases. The seven plant transient conditions (Refs. 10 and 11) are listed below:
Pressure (psig)
Plant Condition N
Pmax PmIn AT NlMonth
- 1. Startup/Shutdown 2.. Startup/Shutdown/Flooding
- 3. Plant Load Changes
- 4. Plant Unload Changes
- 5. Reactor Trip
- 6. Loss of Secondary Pressure
- 7. Leak Test
- 8. Hydro Test 500 106 480 2235 2235 2235 2235 2535 0
+/-200F/hr 0
Fig. 5-2 2135
+200F 2135
-207F 1.042 1042 1042 1.00 0.010 0.417 5
2235 1635 Fig. 5-3 135 Fig. 5-5 385
+100IF/hr 200 2235 10 3110 0
+100+/-F/hr 0.021 A stress summary for cyclic stress ranges for each transient is given in Appendix A of this calculation.
These stresses are used as input to the BIGIF computer program.
8.2 Consideration of Weld Residual Stresses The magnitude and distribution of weld residual stress were evaluated to determine if residual stress needs to be explicitly included in the flaw evaluation. The effect of weld residual stress is two-fold.
First, it will increase the stress local to the weld zone, which can affect the critical flaw size. Second, there can be a higher mean stress in the tensile areas of residual stress that can lead to faster FCG rates.
Therefore, the effect of residual stress must be considered and addressed in some format.
8.2.1 Fracture Resistance The weld residual stress can potentially lower the brittle fracture resistance of the ferritic head material.
Because of the ductile nature and austenitic structure of Alloy 600, the nozzle and J-groove weld will not be significantly affected by the presence of high residual stresses. Therefore, the consideration of residual stress on fracture is only an issue for the PZR bottom head.
Calculations that simulate the weld process for the sleeve has been performed for a similar plant design (Ref. 14). Figure 8-2 illustrates the stress contours for the weld residual plus operating stress state local to the J-groove region. This stress contour plot indicates that the peak residual stresses are local to the weld and that the magnitude of stress away from the weld is very low. Further, compressive stresses are also developed local to the weld region.
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Pressurizer Heater Sleeve J-Groove Weld Flaw 1
t7 2
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0 1-2 43ofl10 From these stress analyses, the following considerations was used to construct a residual stress fields in the hoop direction for the uphill and downhill weld regions:
I. Peak residual tensile stress occurs at the surface of the J-groove weld and attenuates with distance from the surface. The magnitude of the tensile residual stress is on the order of the yield strength of the material. The tensile field is contained within the Alloy 600 material.
- 2. Compressive residual stresses are developed at a depth near the clad to base metal region for the uphill side (larger weld prep area), and within the clad for the downhill side (smaller weld prep area). The magnitude of the compressive stresses is on the order of 50% of the yield strength.
- 3. The compressive residual stress attenuates slowly below the clad and becomes near zero within a distance of three times the clad thickness.
- 4. In general, the alloy steel head material will be under compressive residual stress at the clad interface.
On the basis of the stress attenuation and compressive nature of the weld residuals, the effect of weld residual stress on head fracture was included in the analysis for maximum stress intensity factor for the more limiting plant transients.
8.2.2 Fatigue Crack Growth Rate The FCG rate for both Alloy 600 and ferritic pressure vessel steels will exhibit a faster rate when high mean stresses (high R-ratio where R = KmuKma) are present. Since residual stress is not explicitly evaluated in the FCG analysis, the affect of R on growth rate is addressed by assuming an R-ratio equal to 0.25 for all transients and flaw depths. This assumption is judged to be conservative since the combination of residual stress and compressive stresses from thermal stresses will cause R to be more in the range of-1.0 < R < 0.0. This assumption is made in Sections 5.3.3 and the FCG equations were modified accordingly. Therefore, the effect of mean stress is conservatively treated in the FCG analysis.
8.3 Definition of Cycle Stresses The FCG evaluation requires the stress range (cas) for each transient condition. The values for As are developed in Appendix A (Tables A-I and A-2) for the J-groove weld region. The following table of scaling factors was used to define Aa from the eight loading cases:
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0 1-2 44of 10 Load Case Plant Condition PMIN l ISO l HU CD l CDF STEP TRIP l LOSP LTHU LTCD
- 1. Startup/shutdown 0.89410.0 0.0 1.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0
- 2. Startup/Shutdown/Flooding 0.894/0.182 0.0 1.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0
- 3. Steady State Operation 0.894/0.894 1.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
- 4. Plant Load Change 0.934/0.894 0.0 0.0 0.0 0.0 1.0 0.0 0.0 0.0 0.0 S. Plant Unload Change 0.894/0.854 0.0 0.0 0.0 0.0 1.0 0.0 0.0 0.0 0.0
- 6. Reactor Trip 1.014/0.674 0.0 0.0 0.0 0.0 0.0 1.0 0.0 0.0 1.0
- 7. Loss of Secondary Pressure 0.894/0.054 0.0 0.0 0.0 0.0 0.0 0.0 1.0 0.0 0.0
- 8. Leak Test 0.894/0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 1.0 1.0
- 9. Hydro Test 1.243/0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 1.0 1.0 The time step at which the maximum/minimum stress occurs during the transient was determined from the time where the linearized membrane plus bending stress was at maximum or minimum. This was accomplished by an analysis of the transient stress output given in Ref. 7 (see Appendix A).
8.4 Evaluation of Postulated Flaws at the J-Groove Weld 8.4.1 Flaw Model To evaluate the integrity of the heater sleeve repair geometry, it is postulated that an axial flaw(s) remains in the nozzle stub at the original J-groove weld. It is further assumed that the postulated flaw has extended through the weld and clad and penetrated into the low alloy steel base metal. An illustration of the flaw model representing the postulated flaw geometry is shown in Figure 8-1. This represents the worst flaw orientation and size that could develop by stress corrosion cracking.
The initial flaw is conservatively assumed to be located at the comer of the hole and semicircular in shape with a depth of "a." The crack is conservatively assumed to penetrate the sleeve wall as shown in Figure 8-1. The initial flaw depth is assumed to be 1.0-inch (i.e., a0 = 1.0 inch). For this depth, the flaw tip will be well within the low alloy steel since the nominal J-groove prep is approximately 11/32-inch, and the clad thickness is 7/16 inch. A review of the finite element analysis details indicates that the vertical depth of the clad at the outermost sleeve is about 5/8-inch. Hence, it will be conservative to assume a 1.0-inch deep flaw as an initial flaw depth for the evaluation.
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Pressurizer Heater Sleeve i-Groove Weld Flaw
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0 I-2 45 of 110 8.4.2 J-Groove Weld Stresses The stresses at the J-groove weld were obtained from the finite element stress results in Appendix A of this calculation. The stress distribution in two dimensions, i.e., radial and circumferential with respect to the PZR bottom head, was used in the BIGIF program. This program uses linear interpolation within the two-dimensional stress table to calculate K using a weight function solution.
Since the flaw is conservatively modeled to penetrate the sleeve and the weld, the cyclic stress ranges from the finite element analysis are combined accordingly to cover the appropriate flaw area. The tabular input for each transient is listed in the BIGIF output data in Appendices B and C of this calculation.
8.4.3 Allowable Flaw Depth Evaluations 8.4.3.1 Appendix A Evaluation The evaluation of allowable flaw depth following the ASME Section XI Appendix A method requires the solution of K1, and K1a or Kl0 in accordance with Eqs. 4-7 and 4-8. For determining the allowable flaw depth, the fracture toughness acceptance criteria require that K1 <Kla /4i-=2001 0=63.2 ksi in 1 /2 (8-1) for normal, upset, and test conditions, and Ki<Kj,/.Ii=200/,Ii=14l.4 ksi in'/2 (8-2) for emergency and faulted conditions. Since seismic loading will have a negligible effect on stress at the flaw location, the limiting criterion for defining allowable flaw depth is Eq. 8-1.
When defining the maximum stress for computing the allowable flaw depths, the combination of residual plus pressure plus thermal stresses produce stress levels in excess of the specified minimum yield strength. This situation was particularly true for the cooldown with flooding transient where local thermal stresses are high. Therefore, an elastic-plastic consideration was applied where the maximum stress was limited to the yield strength of the material, after all stress sources were elastically combined.
The yield stress assumed as a limit to the stress is 60 ksi. Additional considerations that led to this evaluation with respect to the cooldown/flooding transient are:
I) The cooldown with flooding transient is a less likely event than a normal plant cooldown.
- 2) For toughness considerations, the bottom head will remain on the upper shelf during cooldown transient with flooding transient affording ductile behavior during the transient.
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- 3) Higher stress conditions occur when the RCS pressure is below 20% of the design pressure.
Maximum stress occurs when the RCS pressure is near zero. Therefore, the significant stress conditions for the cooldown/flooding transient when P is less than 20% PD. ASME Section XI flaw acceptance criteria under IWB-3613 permit a relaxation in structural factors from 10112 to 2112 for such a situation.
The solution for K1 for the eight plant transient conditions defined in Section 8.1 was determined with the BIGIF computer program. The semicircular comer crack flaw model (IFI = 303 model in Ref. 8) was used. A listing of the input file and the solution output are given in Appendices B and C.
Appendix B gives the results for the uphill side weld location and Appendix C gives the results for the downhill side.
The highest K1 for all design conditions is computed for the cooldown with flooding transient. A plot of K1 versus flaw depth is given in Figures 8-3 and 8-4 for the case of cooldown/flooding, hydrotest, and loss of secondary pressure. The somewhat irregular shape of K1 is due to the stress distribution behavior in the transition between the weld and the head. The flaw on the uphill side reaches the allowable K1 of Kra 1410 = 63.2 ksi in11 at the smallest depth. The following allowable flaw depths are computed:
Allowable Depth, a8i1, l
Location (inches)
Uphill Side 1.42 Downhill Side 1.52 8.4.3.2 Appendix K Evaluation With regard to the cooldown with flooding transient, an alternate analysis using Appendix K procedures was performed to confirm the assumptions and inputs for the allowable flaw depths computed in Section 8.4.3.1. The purpose of the alternate calculations is to address the uncertainties of weld residual stress and simplified elastic-plastic assumptions used in the Appendix A calculations. The logic used to apply Appendix K methods and acceptance criteria is based on the following:
- 1) The Appendix K procedures use a "postulated" flaw to evaluate margins to failure for upper shelf conditions. This evaluation of the PZR bottom head is similar in that a 1.0 inch flaw is postulated to evaluate material resistance to fracture.
- 2) The Appendix K procedures are applicable since the PZR bottom head will be at upper shelf conditions for all design loads including the cooldown with flooding transient.
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- 3) The 1.0-inch postulated flaw depth is on the order of the postulated depth for the Appendix K analysis (i.e. 25% of the wall thickness). Therefore margins on flaw depth are comparable.
- 4) In the Appendix K analysis, residual stress are not considered since they are not highly influential to upper shelf behavior. Applied stresses are treated as elastic with the structural factors applied separately to pressure and thermal loading (see Section 4.5).
From the analysis procedures for Japplied based on small-scale yielding (Eq. 4-14), the crack tip driving force in terms of K1 are plotted in Figure 8-5. The allowable flaw depth is the depth where K1 exceeds K1a = 200 ksi int 2. From this analysis, the allowable flaw depths are large relative to the postulated flaw depth and exceed the allowable values determined from the Appendix A evaluation. Therefore, the allowable flaw depths from the Appendix A procedure are conservative.
8.4.4 Fatigue Evaluation An FCG analysis was performed to determine the final crack depth (af) after 40 years of service. The following conservative analysis input data and assumptions were used:
- 1. Initial flaw depth equal to 1.0 inch is assumed to exist at the start of service.
- 2. Reference FCG curve for reactor water environment with conservative R-ratio behavior is assumed.
- 3. All plant cooldowns are conservatively assumed to include flooding.
The cyclic stresses were determined on a pure elastic basis (i.e., elastic superposition of pressure and thermal stresses). The stress summaries are given in Appendix A of this calculation. The 40-year service cycles were divided into one-month block loading, as given in Section 8.1. Therefore, 480 blocks equals 40 years of operation. The fatigue life results from the BIGIF program are given in Appendices B and C of this calculation. From these results, the change in crack depth with service time is provided. The FCG is comparable for the downhill and uphill side flaw locations.
The calculated flaw growth and final depths for N = 480 months are summarized below:
I Growth, Aa Final Depth, af Location l
(inches)
(inches)
Uphill Side 0.21 1.21 Downhill Side 0.25 1.25 QAE17 REV 8196
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0 1-2 48ofI10 Therefore, it is determined that ar < aa.low at either weld location. Axial oriented flaws remaining in the heater sleeve J-groove will be acceptable to the ASME Section XI flaw evaluation rules.
8.5 Evaluation of Borated Water Corrosion The potential of borated water corrosion (BWC) of the low alloy steel material was conservatively evaluated in Ref. 5 for the half-nozzle repair geometries for the steam generator and PZR. Local corrosion was modeled as a planar circumferential groove within the hole penetration. The rate for BWC was conservatively established from industry data discussed in Ref. 5. A limit load based analysis determined that the allowable depth of corrosion was large compared to the computed groove depths from BWC. In summary, the total corrosion depths were computed to be less than the allowable corrosion depths established for the PZR bottom head region. Therefore, the ASME Section margins are satisfied based on the previous analysis of the half-nozzle repair design.
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Pressurizer Heater Sleeve J-Groove Weld Flaw
_r__
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0 1-2 49of 10 x
ICladding I Depth
/
Bottom Head (SA 5331B-1)
Postulated Flaw Original Sleeve (Alloy 600)
Y Figure 8 Heater Sleeve J-Groove Flaw Model.
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Pressurizer Heater Sleeve J-Groove Weld Flaw A7 s
c ES 03105212-1Q Evaluation -
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0 1-2 50 of I 10 Figure 8-2 -Weld Residual Stress Distribution at Operating Conditions (Outermost 52° Angle)
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PressurizerHeater Sleeve J-Groove Weld Flaw It TX t7
~5 AES 03105212-lQ Evaluation -
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0 1-2 51 of I10 100 90 80 c
r-0j uL U,
Ui V
to
'BU 70 60 50 40 30 20 -
10 -I-0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 Crack Depth, a (inches)
Figure 8 Stress Intensity FactorVersus Flaw Depth for Corner Flaw in J-Groove Weld Location - Uphill Side.
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lltle: Pressurizer Heater Sleeve J-Groove Weld Flaw etf C7 5E+/- c AES 03105212-IQ Evaluation -
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0 1-2 52of 110 100 90 80 70 I-,C X.
.2.
50 E
,n 40 E 30 x
'ii 20 10 0
0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 Crack Depth, a (inches)
Figure 8 Stress Intensity Factor Versus Flaw Depth for Corner Flaw in J-Groove Weld Location - Downhill Side (Appendix A Evaluation)
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Pressurizer Heater Sleeve J-Groove Weld Flaw By75t$
q
~
e C
AES 03105212-IQ Evaluation -
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0 1-2 53of110 220 200 180 6-160 C
m 140 I-
-P 0
L 120 C,
E 100 0) 0en E 80 E
K
- E 60 40 20 0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 Crack Depth, a (Inches)
Figure 8 Stress Intensity Factor Versus Flaw Depth for Corner Flaw In J-Groove Weld Location (Appendix K Evaluation)
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0 1-2 54of110 Appendix A
SUMMARY
OF HEATER SLEEVE CYCLIC STRESSES A.1 ANALYSIS GEOMETRY The stress results from the three-dimensional finite element analysis of the PZR bottom head penetrations (Ref. 7) were used to define the hoop stress distributions within the J-groove weld. The outermost sleeve is used to define the stresses for all heater sleeve penetrations. Further description of the finite element model is given in Section 4.6 and in Ref. 14.
The finite element model geometry is described in Section 4.6. The node numbers on the Y-Z symmetry plane of the model are used to define the x, y coordinates for input to BIGIF (Ref. 8). Two generic BIGIF models are developed: one for the uphill side and a second for the downhill side. In order to match the rectangular coordinate system of the BIGIF program, the skewed geometry of the ANSYS model was simply mapped to create a rectangular block where 0
- X'
- w and 0
- Y'
- t, where w is the linearized arc length along the inside circumferential surface and t is the wall thickness. For the uphill side, this is accomplished by pivoting the sleeve about Node 3699 until the nozzle aligns along the head radius.
For the downhill side, the nozzle is rotated clockwise about Node 4253 to achieve a radial alignment.
The inside surface circumferential length was selected to be reasonable since the local discontinuity stresses will remain concentrated near the hole penetration at the weld location.
The geometry transformation for the PZR bottom head nodes is shown in the tables. The radial coordinate transformation uses the Y coordinate in the ANSYS model and projects the length to a perpendicular radial line. This creates the "Y" input to the BIGIF program. The circumferential transformation simply uses the element spacing to develop the "X" input to the BIGIF program.
A.2 STRESS
SUMMARY
A.2.1 Finite Element Data The hoop stresses for each load case are summarized in Tables A-I through A-1 I for the nodes within the sleeve/J-groove weld. The ANSYS loading cases are defined as follows:
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0 1
-2 55 fllO Transient Time, t (sec)
Case Description Filename Uphill Downhill (MaxlMin)
(Max)
P Internal pressure, P = 2500 psi hnpres2.p 11 na/na na/na HU Plant heatup, 2000F/hr hnhu.pl 1 10494/na 10495/na CD Plant cooldown, -2000F/hr hncd.pl I 10495/na 10495/na CDF Plant cooldown with flooding hncdf.pl I 4440/na 4440/na SS Isothermal, T=6530F hniso.pl I natna na/na LD Plant loading, AT = +20°F hnstu.p I1 210/na 2101na UNLD Plant unloading, AT = -207F hnstd.pl 1 210/na 210/na TRIP Reactor trip (loss of load) hnlol.pl 1 601/2020 601/2020 LSP Loss of secondary pressure hnlsp.pl 1 400/6200 350/6200 LKHU Leak test heatup,1000F/hr hnltu.pll 10801/na 10801/na LKCD Leak test cooldown, -1000F/hr hnltd.pl I 10801/na 10801/na The coordinates x, y for each reference node are the coordinates established in the transformation shown in Tables A-1 and A-2.
A.3 Cyclic Stress for the PZR Bottom Head The stress ranges for the eight transient loading conditions were obtained by linear combination of the minimum and maximum values of the individual load cases in Tables A-I and A-2. Absolute values of the maximum range is conservatively taken. A description of each transient case and the manner in which the stress range was determined is given below:
- 1. Startup/Shutdown:
The maximum stress during startup/shutdown is the maximum stress from pressure (P=2235 psi) plus heatup, or pressure (P=2235 psi) plus cooldown. The minimum stress state is zero. Therefore, the stress range is Aa = lMAX[(P+ HU), (P + CD)] - [ 0]
- 2. Startup/Shutdown with Flooding: The maximum stress during startup/shutdown with flooding is the maximum stress from pressure (P=2235 psi) plus heatup, or pressure (P=2235 psi) plus cooldown with flooding. The minimum stress state is zero. Therefore, the stress range is Aca = lMAX[(P+IHU),(P+CDF)]-[0]l QAE17 RENV 8/96
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- 3. Plant Loading: The plant loading transient causes a change in stress from a steady-state condition from a +100 psi pressure and +200F temperature change. Therefore, the corresponding stress range is the maximum stress difference between steady-state operation and for an upload condition. Therefore, the stress range is the larger of:
A: =
I[Pss+SS]-[P,,+LOAD]J
- 4. Plant Unloadinm:
The plant unloading transient causes a change in stress from a steady-state condition from a -100 psi pressure and -200F temperature change. Therefore, the corresponding stress range is the maximum stress difference between steady-state operation and a download condition. Therefore, the stress range is:
As =
[PSS
+SS]PUd +UNLAD]1
- 5. Reactor Trip:
The reactor trip causes a major stress cycle from a steady-state operating condition. The cycle associated with a reactor trip assumes a return to steady-state.
Therefore, the stress range for a trip is the maximum of:
=
I[Pm + TRIP.
]
PM. + TRIPMI ]l or Aa = l[Pi + TRIMn]- [PK + TRIPm l
- 6. Loss of Secondary Pressure:
This transient trip causes a stress cycle from a steady-state operating condition to the absolute maximum stress resulting from the thermal transient. The cycle associated with a loss of secondary pressures assumes a return to steady-state conditions. Therefore, the stress range for this transient is:
As =
I[Pss+SS]-[PLsp +LSP]I
- 7. Leak Test:
The plant leak test is performed for a pressure from 0 psig to 223 5 psig and at a temperature change of 4001F. Therefore, the stress range is determined as follows:
Aa MAX[(PL,k+ LKHU), (PL,,k, +LKCD)] - [°0)
- 8. Hydro Test:
The hydro test is performed at 1.25Pd at a temperature change of 400'F.
Therefore, the stress range is calculated as:
A: -
MAX[(PHydro + LKHU), (Pliyd +LKC:D)] - (0]l QAE17 REV 8/96
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0 1-2 57of110 The stress range was computed for each plant condition as described above. The results of the combined cases are given in Tables A-12 and A-13. Linear interpolation with respect to the X' coordinate was used to define the stress values for nodes where stress results were not reported. For the surface nodes along the clad surface, the surface stress was equated to the stress value of the next node into the head (i.e., node at the clad-to-base metal interface). This is a reasonable assumption for pressure load cases and is acceptable for thermal transient cases since peak stresses will be localized only to the surface layer. The stress values in Tables A-12 and A-13, along with the nozzle stresses described in Section A.4 are used as input to the BIGIF program for evaluating the fatigue crack growth in the head material.
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0 1-2 58of110 Table A-la
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Intemal Pressure P = 2500 psi)
Uphill Side Node SX SY SZ SXY J
SYZ l
SXZ 3699
-1863 18970
-4346
-2323
-2271 1472 3682
-2626 31392 7998
-1775
-2663 3785 4385
-1900 29283 17219
-2590
-1041 1606 4366
-2030 22388 11253
-1727
-908
-682 5930
-1964 2874 2791
-812 456
-756 5929
-2416
-1887
-2543
-396 193
-87 3755
-590 13039 2440
-496
-396 5172 3677 6054 22396 14376
-573 647 10878 4578 1571 21493
-5826
-1321
-1747 4131 4553
-1105 25590 2717
-2239
-1327 3014 6972
-111 33704 9182
-2937
-1301 1596 6971 527 35662 12648
-3200
-1175 1244 3745 13970 11332 3693 305 9
5996 4520 2299 14296 6124
-203
-41 6591 4585 2396 15243 5949
-216
-112 7165 4555 1578 15279 5012
-371
-290 5995 7002 2399 16851 6400
-369
-329 5346 6996 3914 16752
.7561
-235
-292.
5387 4509 3436 13155 7572 76 9
7347 4509 3436 13155 7572 76 9
7347 4510 3789 13306 7419 63
-36 7045 4504 3307 13052 7119
-63
-61 6580 6943 2884 14463 7118
-172
-128 6143 6944 3785 15649 7554
-169
-182 5934 6433 7117 13956 10020
-77 60 10637 6433 7117 13956 10020
-77 60 10637 6508 4694 13178 9698
-94 68 9279 6493 3802 12621 9288
-91 58 8555 7252 2853 12033 8338
-77 37 7248 7253 2831 12239 B198
-72 3
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0 1-2 59of110 Table A-lb
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Internal Pressure P = 2500 psi)
Downhill Side Node]
SX J
SY
[
SZ SXY j
_lSXZ 4253
-1583 45446 10012 3014
-3203
-3264 4237
-1224 36726
-3095 2640
-2999
-2953 4461
-216 15383
-5533 1216
-1765 676 6117
-3281
-2143
-2693 141
-119 0
6115
-1635
-2768
-1580 12
-18
-309 4157 6621 24651 19687 541 1174
-15214 4162 10972 32813 23122 619 555
-12694 4737 650 38808 15714 2722
-1828
-3240 6612 1060 38132 11537 3024
-1729
-1889 6611 1228 36607 11512 3100
-1342
-1767 4987 3435 13332 5490 55
-31
-6441 4767 6422 24011 9397
-189
-1088
-9314 4742 2467 22974 7980 700
-1165
-4374 6628 2258 23725 7820 1059
-1100
-3016 6629 2702 23781 8071 1273
-915
-2845 4989 4689 12744 7742
-544 444
-8078 4769 4646 16480 6647
-436
-512
-7022 4744 4667 17057 6737
-194
-491
-6419 6618 4735 17352 6529
-13
-489
-5617 6619 5235 17498 6497 118
-410
-5388 4967 3622 12584 5150
-319 5
-7044 4722 4527 14929 5747
-251
-248
-7206 4727 4793 15246 5870
-173
-276
-6893 6553 5073 15355 5725
-87
-279
-6500 6554 5450 15472 5680 11
-200
-6532 6345 4223 13481 5848
-176 106
-7286 6379 4531 14526 5641
-193
-156
-7295 6525 4872 14629 5535
-160
-212
-7047 7339 5163 14679 5414
-89
-205
-6835 7338 5454 14852 5494 10
-140
-6828 QAE17 REV 8196
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Pressurizer Heater Sleeve J-Groove Weld Flaw j
1 AES03105212-IQ Evaluation -
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0 1-2 60ofllO Table A-2a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Plant Heatup at 10494s)
Uphill Side l
Nodel SX SY SZ SW sYz sxz 3699
-874 5554
-39174
-1684
-3239
-3391 3582
-278
-7665
-49627
-4279
-2976
-2478 4385
-1802
-20432
-44295
-1194
-552
-4120 4366
-1305
-12732
-33842 837
-674
-2852 5930
-1513
-4947
-7708 441 395
-2126 5929
-523
-1536
-5840
-150
-112
-646 3755
-3104
-3337
-25605
-4773
-523
-357 3677
-10942
-14510
-35103
-10033 940
-669 4578
-5859
-712
-37276
-2192
-1363
-1906 4553
-4201
-7415
-40498
-3818 1037
-1992 6972
-5744
-8456
-40261
-2362 1280
-1931 6971
-2896
-6387
-29919 637
-106
-2596 3745
-16359
-4669
-21544
-5459 21 961 4520
-3550
-5731
-24753
-5993 167 133 4585
-4421
-4772
-25006
-6366 149 113 4555
-4353
-2662
-23286
-4696
-93 89 7002
-4879
-1996
-20130
-2650
-42 94 6996
-4743
-391
-15230
-838
-41 166 4509
-4148
-5998
-25673
-4641 50
-12 4509
-4148
-5998
-25673
-4641 50
-12 4510
-4430
-5305
-24380
-3762 58
-40 4504
-4701
-3857
-22406
-3355 49
-9B 6943
-4050
-1732
-18059
-2798 50 48 6944
-4429
-225
-14609
-1167 10 175 6433
-4732
-4790
-28518
-4187
-21
-280 6433
-4732
-4790
-28518
-4187
-21
-280 6508
-3520
-3734
-26568
-3209
-19
-241 6493
-3357
-2362
-23846
-2735
-34
-174 7252
-2928
-231
-17699
-1997
-13
-75 7253
-2832 1259
-13735
-1026
-27 21 QAE17 REV 8196
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Tile: PressurizerHeater Sleeve J-Groove Weld Flaw
[iXt1 (
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0 1-2 61 of 1l0 Table A-2b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Plant Heatup at 10495s)
Downhill Side Node l SX SY [
Sz J
Sxy l
SYz Sxz 4253
-1376
-14349
-75262
-4569 4218 4555 4237
-2066 3455
-60821
-2877 4348 4003 4461
-3304
-2141
-29231
-251 2431 2557 6117 533
-588
-3490 76 340 433 6115
-716
-930 393
-187 107 245 4157
-13724
-27378
-41556
-19854
-2446
-342 4162
-10701
-20256
-42902
-10477
-583 321 4737
-2116
-18050
-50253
-3053 1203 3453 6612
-2408
-6205
-35176
-1139 954 2633 6611
-2062
-3100
-23296
-459 306 1821 4987
-9892
-13466
-31858
-10490
-803
-288 4767
-9911
-12426
-36875
-9243 311
-290 4742
-5014
-6458
-29356
-4483 775 392 6628
-3558
-4063
-21357
-1808 434 658 6629
-2383
-1539
-13800
-707 15 459 4989
-9250
-12707
-26952
-10566
-569
-742 4769
-8153
-9333
-25539
-7755 177
-553 4744
-6793
-7189
-21806
-5927 160
-333 6618
-4347
-3848
-14836
-2987 70
-196 6619
-2602
-1519
-9257
-975
-65
-173 4967
-8874
-11069
-25411
-9929
-165
-430 4722
-7681
-8834
-22366
-7828 33
-339 4727
-6287
-6851
-18730
-6002 44
-262 6553
-4036
-3833
-12533
-3054 14
-182 6554
-2239
-1533
-7563
-699
-32
-167 6345
-9099
-11300
-24854
-10046
-176
-317 6379
-7455
-8657
-21019
-7801
-13
-259 6525
-6129
-6734
-17444
-5997 15
-226 7339
-3830
-3735
-11467
-2972 1
-169 7338
-2043
-1333
-6675
-581
-22
-172 QAE17 REV 8/96
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(
5Xc6LZ AES 03105212-IQ Evaluation -
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0 1-2 62of 10 Table A-3a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Plant Cooldown at 10494s)
Uphill Side Node SX J
SY SZ SXY SYZ
_SXZ 3699 542
-2458 24200 1347 2210 2051 3682 13 5810 28993 2631 1882 1462 4385 1080 12924 25641 710 427 2350 4366 686 7826 18831
-546 447 1627 5930 834 2881 3587
-289
-221 1130 5929 218 717 2973 67 36 250 3755 1951 2678 16128 4193 427 277 3677 6092 9315 20311 6593
-420 361 4578 2648 202 19368 1709 748 1018 4553 2384 4753 21150 2251
-631 960 6972 2943 4488 18765 1163
-732 854 6971 982 2612 11559
-547 51 1151 3745 14475 4888 15494 5093 39
-562 4520 2763 5060 15337 4563
-59 50 4585 2439 3983 14351 4447
-71 53 4555 2009 1988 12145 2904 59 20 7002 2323 1253 9434 1346 21
-10 6996 2055 21 6068 96 21
-70 4509 3868 5951 16131 4514 2
-22 4509 3868 5951 16131 4514 2
-22 4510 3770 4938 14561 3509 12
-2 4504 3073 3228 12176 2499 20 49 6943 1946 1194 8347 1317
-10 7
6944 1898
-7 5841 279
-4
-72 6433 5439 6260 18390 5449 1
224 6433 5439 6260 18390 5449 1
224 6508 4215 5649 17035 4369
-8 204 6493 3648 4450 14849 3496 22 143 7252 1204 268 7694 1203 25 43 7253 1025
.643 5375 224 31
-16 QAE17 REV 8196
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0 1-2 63of110 Table A-3b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Plant Cooldown at 10495s)
Downhill Side l
Node SX SY SZ l
SXY J SYZ J Sxz 4253 873 9485 45925 3024
-2897
-2809 4237 1265
-1379 36211 1822
-2768
-2481 4461 2068 1534 16908 214
-1438
-1654 6117
-393 243 2012
-100
-225
-235 6115 446 666
-174 131
-62
-141 4157 9348 19099 27242 13957 1373 120 4162 7188 13949 26459 7218 300
-282 4737 1205 11586 28790 2079
-786
-2028 6612 873 2860 15825 481
-432
-1299 6611 807 1062 8697 218
-72
-715 4987 6975 9590 20960 7598 374 37 4767 6487 8843 22421 6630
-211 190 4742 2954 4355 16750 3044
-470
-203 6628 1609 2143 9641 855
-177
-343 6629 847 503 4993 297 50
-157 4989 6652 9218 18168 7645 271 357 4769 5695 6884 16297 5687
-113 245 4744 4265 4896 12675 4012
-75 140 6618 1871 1866 6494 1413
-5 65 6619 836 567 3248 304 62 63 4967 6432 8087 17246 7271 21 206 4722 5532 6556 14672 5809
-30 152 4727 3934 4550 1OB97 3963
-14 108 6553 1814 1940 5551 1412 10 61 6554 732 633 2619 76 30 59 6345 6698 8314 17056 7408 52 153 6379 5469 6450 14016 5797
-5 119 6525 3841 4430 10179 3897
-1 95 7339 1746 1902 5088 1354 12 60 7338 681 523 2242
-16 18 68 QAE17 REV8/96
ENGFIEERJ SERCES. WN Madebrv:
Date: /
Client:
Calculation No.:
AES-C-5212-2
/M d a/7/°Q SCE SCE No. M-DSC-402, Rev. 0 Checked by:
- Date, Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw C-4
( 7 S cf c AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.:
Sheet No.:
0 I-2 64ofl10 Table A-4a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Plant Cooldown with Flooding at 4440s)
Uphill Side Node SX SY SZ SXY SYZ SXZ 3699 1248
-5767 70976 5837 7451 6078 3682
-135 23353 86506 8826 6202 4417 4385 2899 43722 76516 2556 2012 7036 4366 2041 27146 56120
-1370 2019 4872 5930 2379 9444 7108
-1015
-467 3219 5929 330 1373 7783 67 77 152 3755 3827 8810 48491 19248 1340 932 3677 16839 31461 59784 24233
-973 1025 4578 6368
-3617 53030 8022 2729 2965 4553 6829 15027 59276 9000
-1821 2146 6972 7986 13546 41529 3330
-2033 1495 6971 80 4345 10265
-2722 328 2124 3745 77251 29324 65674 23775 544
-1763 4520 10783 22105 47631 16466
-103 911 4585 6841 17785 42544 16279
-181 790 4555 5150 10785 35636 11670 290 450 7002 4925 5553 21373 4534 159 234 6996 3055
-423 6376
-932 91
-54 4509 17344 26214 49805 19934 94
-290 4509 17344 26214 49805 19934 94
-290 4510 16619 21042 42734 15496 268
-286 4504 12071 15228 34286 11135 340 3
6943 5296 6699 19405 4487 160 183 6944 2574
-174 6227
-510 37
-28 6433 30720 37168 66064 30839 9
902 6433 30720 37168 66064
.30839 9
902 6508 21089 31461 55508 23570
-10 778 6493 15348 23526 43444 17819 126 505 7252 4963 6796 18636 6664 102 131 7253 1161
-707 5168
-187 153
-39 QAE17 REV 8196
MAPTECH I ENGINER SM3X W
M dE b:
Dac e
Client:
Calculation No.:
AES-C-5212-2
/_ __
'/17/° SCE SCE No. M-DSC-402, Rev. 0 CQecked by.
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 1-t-rc.
(
7 5e.
AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Documenttontrol No.: Sheet No.:
0 1-2 65 of1O Table A-4b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Plant Cooldown with Flooding at 10494s)
Downhill Side Node SX J SY l
SZ SXY_
SYZ l
SXZ 4253 3281 35529 156220 11843
-11466
-9654 4237 4035
-1734 112900 5899
-9173
-8263 4461 6455 5141 45604 470
-3951
-5499 6117
-1304 1211 7015
-256
-778
-785 6115 1343 2278 793 406
-206
-585 4157 38886 81283 104180 60197 4667 233 4162 25497 53513 85567 26931 1135
-1205 4737 3603 42572 83668 7376
-2470
-6289 6612 1029 7742 37482 2275
-1314
-3240 6611 1235 27 8233 514
-148
-937 4987 29864 41757 80240 33550 925
-438 4767 22753 34501 70957 25286
-684 746 4742 8736 15948 48172 10896
-1503
-579 6628 4182 7740 24180 3617
-614
-954 6629 428 173 3706 800 275
-146 4989 28556 39692 70741 33003 727 1005 4769 20082 26404 53299 21388
-295 398 4744 13323 17689 37744 14190
-164 79 6618 5410 7638 17330 5833 41
-99 6619 245 1337 2129 623 279
-56 4967 27328 34773 67935 31281
-160 471 4722 19682 24683 48862 21485
-93 194 4727 13025 16615 33637 14152
-2 49 6553 5780 7924 15355 5761 85
-64 6554 632 1870
.1721
-332 130
-37 6345 28237 35140 67504 31478
-58 326 6379 19658 24118 47254 21327
-42 132 6525 13119 16294 32200 14000 13 59 7339 5857 7748 14341 5442 72
-18 7338 800 1541 1112
-719 78 35 QAE17 REV 8196
WEPTSCHr ENGINEIG SERVCS. INC Made bv:
Dat Client:
Calculation No.:
AES-C-5212-2 0
.IV/7IL el SCE SCE No. M-DSC-402, Rev. 0 Checked br.
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw J'IT C.
2 7..c AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 66of 10 Table A-5a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Steady State Isothermal T = 653°F)
Uphill Side Node Sx SY SZ SXY SYZ SXZ 3699
-355 2664
-14544
-264
-982
-1241 3682
-174
-1297
-18344
-1375
-948
-902 4385
-719
-6229
-16462
-353
-51
-1536 4366
-510
-3811
-12896 329
-119
-1058 5930
-592
-1603
-3757 136 195
-830 5929
-272
-694
-2326
-79
-38
-374 3755
-1347
-724
-9150
-375
-142
-81 3677
-4259
-4267
-13060
-2706 436
-257 4578
-2648
-891
-15193
-178
-425
-737 4553
-1591
-2260
-16168
-1011 384
-895 6972
-2297
-289B
-18018
-919 510
-933 6971
-1687
-2870
-15956 4
14
-1211 3745
-132
,877.
-4891
-292 70 365 4520
-614
-422
-8570
-1351 95 195 4585
-1615
-322
-9226
-1560 76 171 4555
-1821 90
-8988
-1145
-9 120 7002
-2207
-239
-8910
-884 2
91 6996
-2379
-111
-7964
-558
-9 93 4509
-188
-21
-8917
-82 40
-47 4509
-188
-21
-8917
-82 40
-47 4510
-408
-168
-8877
-7D 65
-60 4504
-1125 1
-8649
-357 70
-56 6943
-1658 62
-7943
-961 53 56 6944
-2272 2
-7623
-695 14 102 6433 1163 2009
-8794 1560
-13
-63 6433 1163 2009
-8794 1560
-13
-63 6508 670 1999
-8775 1286
-15
-53 6493 122 1943
-8433 883
.9
-42 7252
-977 1014
-7828
-174 3
-26 7253
-1514 807
-7240
-569 5
10 QAE17 REV 8/96
ENUNEEJ NN ISUMUL. ffM.
Made br.
Dats
/
Client:
Calculation No.:
AES-C-5212-2 71_
/7171W SCE SCE No. M-DSC-402, Rev. 0 aCecked br:
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw I
r r-7 5
t AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 67 ofII Table A-5b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Steady State Isothermal T = 653°F)
Downhill Side Node l SX SY SZ SXY l
SYZJ SXZ 4253
-421
-4163
-25838
-1264 1095 1536
- 4237
-737 1877
-22394
-947 1451 1368 4461
-1164
-873
-11804
-103 931 812 6117 164
-183
-1053 22 101 156 6115
-236
-213 572
-48 43 71 4157
-3415
-6196
-12007
-4382
-904
-207 4162
-3052
-4968
-14693
-2717
-188 34 4737
-834
-4988
-19091
-813 388 1232 6612
-1266
-2572
-15785
-346 379 1132 6611
-1017
-1741
-12523
-181 157 943 4987
-2286
-2968
-9412
-2189
-388
-244 4767
-2978
-2914
-13039
-2216 85
-64 4742
-1823
-1657
-11178
-1181 252 152 6628
-1547
-1303
-9399
-561 164 262 6629
-1348
-820
-7597
-285 40 252 49B9
-2024
-2703
-7698
-2260
-247
-315 4769
-2285
-2125
-8541
-1865 61
-284 4744
-2245
-1824
-8024
-1581 67
-191 6618
-1833
-1161
-6468
-942 42
-129 6619
-1491
-628
-5157
-456
-3
-107 4967
-1991
-2402
-7182
-2144
-122
-201 4722
-2057
-2067
-7260
-1899 4
-180 4727
-1980
-1770
-6754
-1627 22
-151 6553
-1596
-1114
-5390
-986 17
-115 6554
-1219
-559
-4229
-424 l
-4
-101 6345
-2025
-2497
-6928
-2199
-113
-153 6379
-1937
-2047
-6694
-1912
-15
-141 6525
-1874
-1753
-6194
-1646 7
-127 7339
-1464
-1083
-4905
-982 8
-101 7338
-1078
-496
-3799
-408
-5
-94 QAE17 REV 8196
IERPTW CHr ENGERM SIMS.
M Mad:
Datc:
Client:
Calculation No.:
AES-C-5212-2 MDt/
1/0a SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw j7rs.
rS5. td AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document bontrol No.: Sheet No.:
0 1-2 68 of 110 Table A-6a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Plant Loading at 210s)
Uphill Side Node SX SY SZ SXY j
SYZ SXZ 3699
-427 2959
-18713
-634
-1441
-1605 3682
-161
-2850
-23552
-1927
-1337
-1169 4385
-885
-9001
-21065
-519
-186
-1960 4366
-631
-5548
-16246 408
-255
-1353 5930
-733
-2202
-4108 199 217
-1022 5929
-286
-782
-2826
-82
-45
-371 3755
-1568
-1309
-12040
-1616
-226
-143 3677
-5278
-6287
-16667
-4261 487
-319 4578
-2994
-596
-18287
-723
-603
-914 4553
-2015
-3223
-19678
-1601 494
-1009 6972
-2774
-3755
-20275
-1116 629
-1006 6971
-1640
-3097
-16162 194
-13
-1322 3745
-5036
-1006
-8858
-1794 39 466 4520
-1336
-1885
-11454
-2412 96 132 4585
-2059
-1526
-11799
-2615 82 116 4555
-2142
-685
-11140
-1916
-31 86 7002
-2469
-615
-10063
-1164
-10 73 6996
-2509
-79
-8125
-476
-15 93 4509
-1334
-1754
-11892
-1404 33
-25 4509
-1334
-1754
-11892
-1404 33
-25 4510
-1517
-1589
-11446
-1133 45
-38 4504
-1909
-1065
-10703
-1140 45
-53 6943
-1967
-404
-8989
-1239 40 42 6944
-2370 17
-7777
-634 11 100 6433
-858
-474
-12699
-495
-13
-117 6433
-858
-474
-12699
-495
-13
-117 6508
-722
-148
-12074
-326
-13
-100 6493
-925 248
-11060
-364
-16
-74 7252
-1283 517
-8786
-615
-3
-34 7253
-1542 842
-7293
-534
-5 13 QAE17 REV 8/96
"IRPeSCHF ElNEEINES SERVK:ES. MC.
Mada by:
Date-
/I Client:
Calculation No.:
AES-C-5212-2 7&C M /@
74 SCE SCE No. M-DSC402, Rev. 0 Checked bv:
Date:
Proiect No.:
Title:
PressurizerHeaterSleeveJ-Groove WeldFlaw
- j 1
(7 c
1( - AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 jRevision No.:
Document Controi No.: Sheet No.:
0 1-2 69 of 110 Table A-6b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Plant Loading at 21 Os)
Downhill Side Nodel SX SY SZ SXY l
SYZ SXZ 4253
-618
-6348
-35121
-1984 1798 2112 4237
-978 1916
-29089
-1314 2007 1865 4461
-1561
-1154
-14493
-133 1170 1159 6117 243
-259
-1524 39 152 206 6115
-324
-357 506
-71 58 113 4157
-5781
-11203
-18299
-8079
-1175
-210 4162
-4659
-8385
-19920
-4427
-258 112 4737
-1065
-7741
-24213
-1305 547 1621 6612
-1295
-2987
-17855
-488 464 1316 6611
-1055
-1666
-12669
-205 166 977 4987
-4094
-5502
-14202
-4230
-433
-207 4767
-4393
-5103
-17363
-3828 132
-111 4742
-2361
-2690
-14137
-1902 349 189 6628
-1786
-1782
-10767
-791 203 319 6629
-1342
-804
-7612
-326 21 255 4989
-3770
-5139
-11943
-4281
-289
-372 4769
-3544
-3813
-11824
-3226 79
-300 4744
-3102
-2997
-10390
-2524 77
-189 6618
-2153
-1646
-7459
-1318 39
-118 6619
-1464
-687
-5134
-482
-22
-100 4967
-3648
-4513
-11248
-4045
-107
-225 4722
-3302
-3643
-10283
-3269 10
-186 4727
-2832
-2874
-8884
-2572 22
-149 6553
-1952
-1622
-6282
-1358 11
-107 6554
-1223
-655
-4206
-389
-12
-96 6345
-3740
-4634
-10973
-4113
-106
-168 6379
-3185
-3587
-9625
-3273
-12
-144 6525
-2739
-2838
-8248
-2582 7
-127 7339
-1829
-1581
-5744
-1335 3
-97 7338
-1095
-574
-3750
-349
-11
-93 QAE17 REV 8196
ENOtNEERING SERVICES. iC.
MadSyb:
Date:
Client Calculation No.:
AES-C-5212-2
/U7/0Y SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
'iferr-r 7 Afc AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Contro No.:
Sheet No.:
0 1-2 70 ofllO Table A-7a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Plant Unloading at 210s)
Uphill Side Node SX l
SY SZ SXY SYZ_l SXZ 3699
-270 2275
-9865 115
-489
-834 3682
-182 301
-12498
-776
-527
-603 4385
-528
-3242
-11288
-175 87
-1058 4366
-372
-1944
-9099 238 20
-727 5930
-431
-950
-3278 68 165
-610 5929
-249
-588
-1762
-74
-31
-364 3755
-1077
-112
-5939 880
-53
-16 3677
-3092
-2094
-8999
-1057 370
-186 4578
-2209
-1130
-11565 376
-234
-535 4553
-1115
-1215
-1215B
-388 259
-757 6972
-1752
-1981
-15310
-697 370
-839 6971
-1688
-2589
-15356
-186 38
-1071 3745 4772 2729
-755 1223 98 252 4520 131 1061
-5389
-239 90 251 4585
-1111 901
-6331
-445 68 220 4555
-1445 853
-6570
-340 13 148 7002
-1887 126
-7538
-587 14 107 6996
-2187
-152
-7607
-630
-3 90 4509 966 1723
-5632 1248 45
-66 4509 966 1723
-5632 1248 45
-66 4510 715 1270
-6002 998 83
-79 4504
-307 1065
-6338 431 93
-56 6943
-1308 508
-6706
-665 65 68 6944
-2114
-25
-7281
-742 16 101 6433 3154 4434
-4588 3573
-13
-7 6433 3154 4434
-4588 3573
-13
-7 6508 2045 4089
-5177 2863
-16
-3 6493 1165 3573
-5562 2102
-2
-10 7252
-650 1467
-6686 264 10
-19 7253
-1450 739
-7015
-595 14 7
QAE17 RE' 8/96
IMRPTECHIe EMNEER SE5 M
Made br.
. Datej I Cient:
Calculation No.:
AES-C-5212-2 Je 1.
YI i/0 r SCE SCE No. M-DSC402, Rev. 0 Checked by:
Date:
Prolect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 17_
5 5
AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 71 of 110 Table A-7b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Plant Unloading at 21 Os)
Downhill Side Node SX SY SZ SXY l
SYZ SXZ 4253
-209
-1835
-15652
-500 353 906 4237
-470 1767
-14928
-547 843 825 4461
-729
-567
-8721
-71 659 439 6117 79
-100
-557 4
47 102 6115
-140
-62 611
-22 27 28 4157
-928
-974
-5287
-530
-601
-196 4162
-1339
-1386
-8961
-918
-112
-47 4737
-576
-2110
-13409
-293 219 808 6612
-1205
-2103
-13325
-198 286 920 6611
-954
-1778
-12064
-153 146 886 4987
-393
-326
-4275
-66
-328
-272 4767
-1461
-629
-8263
-527 36
-15 4742
-1228
-580
-7882
-422 148 111 6628
-1269
-801
-7798
-321 122 198 6629
-1320
-823
-7392
-239 58 242 4989
-204
-168
-3160
-157
-197
-249 4769
-945
-360
-4948
-435 41
-259 4744
-1321
-599
-5409
-593 56
-188 6618
-1469
-658
-5316
-550 45
-137 6619
-1482
-562
-5051
-423 15
-111 4967
-262
-203
-2840
-164
-133
-170 4722
-738
-415
-3966
-459
-2
-169 4727
-1070
-617
-4410
-634 22
-148 6553
-1203
-590
-4364
-596 23
-120 6554
-1187
-459
-4146
-452 5
-104 6345
-234
-267
-2616
-204
-116
-132 6379
-617
-431
-3507
-480
-18
-133 6525
-954
-618
-3942
-661 8
-124 7339
-1066
-569
-3944
-611 13
-103 7338
-1037
-413
-3752
-461 0
-92 QAE17 REV8196
MiWP CHr ENGIMVWQ SEICES W.
Made ps:
Date-/
Client:
Calculation No.:
AES-C-5212-2 1
DaY
/-/Oy CiSCE SCE No. M-DSC-402, Rev. 0 Checked br.
Date:
Proiect No.:
Title:
PressurizerHeaterSleeveJ-Groove Weld Flaw rt-5! 5 AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No_
Document Control No.:
Sheet No.:
0 1-2 72 of 110 Table A-8a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Reactor Trip at 601s)
Uphill Side Nodel Sx SY 0Sz l
SXY SYz sxz 3699
-126 1552
-2594 620 228
-197 3682
-172 2528
-3280 128 107
-135 4385
-223 1238
-3104 95 273
-301 4366
-143 882
-3013 94 216
-201 5930
-168 59
-2348
-28 119
-240 5929
-196
-422
-821
-60
-10
-319 3755
-606 772
-1007 2515 72 77 3677
-1173 1184
-2538 1344 241
-69 4578
-1383.
-1345
-5441 1117 58
-202 4553
-357 376
-5440 529 63
-489 6972
-795
-415
-9954
-289 144
-634 6971
-1511
-1847
-12984
-432 84
-770 3745 11003 5003 4935 3178 128 78 4520 1161 3028
-501 1332 76 306 4585
-284 2546
-1714 1158 51 269 4555
-770 1883
-2567 829 44 176 7002
-1234 713
-4809
-68 32 120 6996
-1696
-116
-6301
-631 9
79 4509 2467 3995
-587 2978 48
-86 4509 2467 3995
-587 2978 48
-86 4510 22D7 3184
-1449 2403 98
-98 4504 877 2501
-2503 1513 114
-50 6943
-664 1174
-4238
-131 76 80 6944
-1677 18
-6020
-691 21 91 6433 5603 7366 1607 6023
-13 66 6433 5603 7366 1607 6023
-13 66 6508 3755 6601 261 4784
-17 62 6493 2509 5525
-1058 3617 6
34 7252
-73 2089
-4302 918 17
-5 7253
-1188 683
-5869
-517 27 4
QAEI7 REV 8/96
MAPTMF ENGINEIERW SERVCES. RC.
Madz bv:
Date:
mient:
Calculation No.:
AES-C-5212-2
/
Date:_
1/ 7/c c/
SCE SCE No. M-DSC-402, Rev. 0 Checed by:
Date:
Project No.:
Title:
PressurizerHeater Sleeve J-Groove Weld Flaw
(
-) S!in N $f' AES 03105212-l Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Documeit Control No.:
Sheet No.:
0 1-2 73 of 110 Table A-8b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Reactor Trip at 601s)
Downhill Side Node' Sx SY Sz SXY SYz Sxz 4253 98 1493
-380 592
-695
-34 4237
-68 1432
-3437 61
-63 12 4461
-86
-249
-3815
-36 219
-112 6117
-38 48 219
-11
-28 21 6115 13 198 805 27 11
-26 4157 2548 6291 4372 4800
-140
-174 4162 1172 3812
-250 1671 13
-153 4737
-211 2167
-4387 447
-35 144 6612
-978
-1094
-8470 59 124 528 6611
-707
-1516
-10040
-62 111 707 4987 2211 3292 3047 2820
-225
-291 4767 773 2608
-1002 1860
-39 65 4742
-285 1021
-2611 670
-14 44 6628
-746 72
-4718 79 44 86 6629
-1152
-671
-6277
-105 73 202 4989 2294 3306 3238 2724
-110
-132 4769 977 2107 406 1564 6
-201 4744 74 1180
-1295 835 31
-167 6618
-792 199
-3100 102 42
-137 6619
-1288
-304
-4294
-272 39
-110 4967 2105 2795 3278 2535
-136
-113 4722 1125 1890 890 1551
-12
-137 4727 282 1059
-760 799 18
-133 6553
-506 286
-2418 59 27
-118 6554
-967
-161
-3510
-389 16
-101 6345 2207
- 2773 3447 2511
-110
-93 6379 1231 1819 1156 1514
-21
-110 6525 401 1024
-465 761 7
-109 7339
-366 286
-2130 15 17
-97 733B
-807
-157
-3214
-434 7
-82 QAE17 REV 8196
ENGINEERI SEMACES. W.
Made-y Date/
0 Client:
Calculation No.:
AES-C-5212-2 e
Date:9
//y C/l SCE SCE No. M-DSC-402, Rev. 0 Checked br.
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw r
(7. 5%t
§ AES 03105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Docume&t Control No.: Sheet No.:
0 1
1-2 74of110 Table A-9a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Loss of Secondary Pressure at 350s)
Uphill Side Nodel Sx SY l
SZ SXY SYZ l
SxZ 3699
-433 2814
-19377
-800
-1580,
-1671 3682
-141
-3588
-24456
-2085
-1450
-1220 4385
-895
-9894
-21837
-577
-256
-2030 4366
-645
-6143
-16715 415
-318
-1404 5930
-749
-2388
-3889 216 202
-1049 5929
-265
-752
-2864
-76
-52
-331 3755
-1545
-1571
-12620
-2228
-254
-170 3677
-5404
-6987
-17289 4832 471
-328 4578
-2928
-347
-18452
-1004
-661
-939 4553
-2079
-3553
-20119
-1833 507
-1001 6972
-2847 4104
-20208
-1163 633
-977 6971
-1483
-3127
-15137 294 40
-1296 3745
-7594
-2087
-10429
-2544 15 477 4520
-1671
-2628
-12144
-2844 86 78 4585
-2153
-2157
-12288
-3032 75 68 4555
-2164
-1173
-11546
-2245
-43 51 7002
-2452
-903
-10108
-1290
-19 52 6996
-2400
-142
-7710
-421
-20 85 4509
-1925
-2664
-12604
-2099 25
-10 4509
-1925
-2664
-12604
-2099 25
-10 4510
-2078
-2334
-11979
-1707 28
-20 4504
-2239
-1678
-11095
-1563 24
-47 6943
-2027
-761
-9073
-1365 28 28 6944
-2245
-55
-7395
-584 6
90 6433
-2003
-1929
-13914
-1701
-11
-135 6433
-2003
-1929
-13914
-1701
-11
-135 6508
-1503
-1437
-13001
-1280
-10
-117 6493
-1504
-842
-11802
-1121
-17
-86 7252
-1427 50
-8932
-903
-6
-37 7253
-1475 696
-7016
-527
-11 10 QAE17 REV' 8196
rr....._
ENGINEERING SERVICES, INC.
Made by:
Date 0clint:
Calculation No.:
AES-C-5212-2
-ACX
_ t 7/0 5 SCE SCE No. M-DSC402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
PressurizerHeaterSleeveJ-GrooveWeld Flaw 1.T-r-AES 03105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Documenftontrol No.: Sheet No.:
0 1-2 75 of 110 Table A-9b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Loss of Secondary Pressure at 350s)
Downhill Side Node SX SY sz SXY SYZ Sxz 4253
-676
-7036
-37191
-2230 2052 2248 4237
-1023 1753
-30165
-1412 2142 1976 4461
-1634
-1108
-14581
-129 1204 1253 6117 262
-287
-1689 39 166 214 6115
-349
-440 272
-88 55 121 4157
-6671
-13235
-20335
-9593
-1216
-180 4162
-5209
-9776
-21135
-5072
-284 151 4737
-1067
-8802
-25070
-1478 598 1712 6612
-1223
-3082
-17720
-559 480 1324 6611
-1041
-1552
-11807
-228 157 924 4987
-4801
-6521
-15646
-5070
-409
-157 4767
-4841
-5985
-18207
-4456 151
-138 4742
-2479
-3115
-14612
-2173 382 196 6628
-1791
-1985
-10748
-893 216 330 6629
-1214
-754
-7009
-353 10 235 4989
-4485
-6151
-13255
-5118
-286
-372 4769
-3969
-4486
-12574
-3744 86
-280 4744
-3346
-3473
-10828
-2882 78
-170 6618
-2184
-1874
-7469
-1477 35
-100 6619
-1333
-732
-4713
-492
-31
-86 4967
-4315
-5376
-12520
-4824
-87
-216 4722
-3734
-4259
-11011
-3786 15
-171 4727
-3091
-3316
-9300
-2925 21
-133 6553
-2025
-1867
-6314
-1513 7
-92 6554
-1147
-735
-3856
-362
-16
-84 6345
-4428
-5496
-12252
-4887
-91
-160 6379
-3625
-4181
-10351
-3779
-8
-131 6525
-3013
-3266
-8663
-2926 6
-115 7339
-1922
-1821
-5780
-1475 1
-85 7338
-1047
-640
-3413
-307
-12
-85 QAE17
-REV 8196
IftRPWECH ENGMERrM SERV ES. INC.
Made by:
Date:
/C liernt:
Calculation No.:
AES-C-5212-2 L
C
/I 710 0 SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Project No:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
.21 Lz rf7 5c; AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
DocumentControl No.: Sheet No.:
0 I-2 76of110 Table A-1 Da
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Leak Test Heatup at 10801s)
Uphill Side Node Sx S
SY SZ SXY SYZ sXZ 3699
-443 2838
-198D6
-827
-1620
-1708 3682
-147
-3717
-24991
-2134
-1485
-1247 4385
-917
-10158
-22309
-590
-263
-2075 4366
-658
-6316
-17067 426
-325
-1436 5930
-765
-2478
-3968 220 206
-1075 5929
-272
-814
-2971
-78
-56
-340 3755
-1573
-1634
-12916
-2309
-260
-175 3677
-5512
-7175
-17675
-4950 480
-337 4578
-2988
-390
-18867
-1034
-677
-963 4553
-2116
-3685
-20651
-1878 515
-1039 6972
-2919
-4325
-21022
-1204 636
-1026 6971
-1541
-3379
-15974 294
-50
-1366 3745
-7922
-2204
-10761
-2652 12 488 4520
-1713
-2737
-12449
-2929 88 76 4585
-2189
-2246
-12581
-3114 78 66 4555
-2209
-1247
-11864
-2310
-43 48 7002
-2541
-1013
-10535
-1360
-19 52 6996
-2504
-240
-8138
-471
-20 89 4509
-1991
-2799
-12953
-2192 27
-9 4509
-1991
-2799
-12953
-2192 27
-9 4510
-2134
-2445
-12289
-1768 30
-21 4504
-2299
-1766
-11412
-1608 27
-49 6943
-2098
-855
-9467
-1436 29 28 6944
-2334
-142
-7808
-641 6
93 6433
-2141
-2083
-14409
-1838
-11
-140 6433
-2141
-2083
-14409
-1838
-11
-140 6508
-1599
-1554
-13425
-1372
-11
-119 6493
-1556
-884
-12162
-1181
-18
-87 7252
-1497
-23
-9340
-975
-6
-39 7253
-1528.
643
-7415
-576
-12 10 QAE17 REV 8196
MEAPTECHE ENGINEERINS SERW1ES~ IN Calculaton No.:
AES-C-5212-2
_by:
Date:9 Client:
SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiec* No.:
Title:
PressurizerHeater SleeveJ-Groove Weld Flaw (7 S44.
AE S 03A105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Doctnnetr ControJ No.: Sheet No.:
0 I-2 77 of 110 Table A-l0b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Leak Test Heatup at 10801s)
Downhill Side Nodel SX SY SZ SXY SYZ_l SXz 4253
-689
-7152
-37858
-2278 2095 2289 4237
-1042 1783
-30676
-1432 2177 2013 4461
-1665
-1148
-14834
-133 1222 1275 6117 267
-291
-1745 38 170 220 6115
-350
-448 247
-91 55 124 4157
-6834
-13571
-20754
-9842
-1236
-181 4162
-5295
-9958
-21480
-5181
-291 152 4737
-1067
-8995
-25521
-1492 606 1747 6612
-1277
-3228
-18307
-578 487 1366 6611
-1079
-1657
-12388
-235 161 983 4987
-4920
-6694
-15927
-5202
-413
-157 4767
-4934
-6130
-18478
-4544 153
-144 4742
-2533
-3195
-14862
-2202 390 199 6628
-1844
-2068
-11076
-915 223 338 6629
-1275
-830
-7355
-363 12 243 4989
-4586
-6289
-13410
-5235
-289
-380 4769
-4042
-4577
-12705
-3810 90
-289 4744
-3400
-3541
-10950
-2920 82
-179 6618
-2245
-1955
-7670
-1511 39
-109 6619
-1392
-804
-4931
-510
-30
-96 4967
-4415
-5501
-12632
-4931
-90
-222 4722
-3793
-4336
-11077
-3844 16
-178 4727
-3127
-3376
-9355
-2954 23
-141 6553
-2070
-1941
-6454
-1546 9
-100 6554
-1189
-805
-4024
-378
-15
-92 6345
-4520
-5612
-12335
-4988
-94
-165 6379
-3670
-4247
-10378
-3830
-8
-137 6525
-3036
-3315
-8680
-2951 8
-121 7339
-1956
-1890
-5892
-1506 2
-92 7338
-1081
-701
-3554
-321
-10
-93 QAE17 REV 8196
NItHAPTWC ENGINEEM SUM=CE IM Mad-by:-
Date-Cl/ ient:
Calculation No.:
AES-C-5212-2 A
//0 Ci SCE SCE No. M-DSC-402, Rev. 0 Checked br.
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw T
-7 5e{
40 ARS 03105212-1 Q Evaluation -
SONGS Units 2 and 3.
Revision No.:
Document Control No.: Sheet No.:
0 1-2 78fllO Table A-11 a
SUMMARY
OF STRESSES FOR UPHILL J-GROOVE (Leak Test Cooldown at 10801s)
Uphill Side Node SX SY SZ l
SXY SYZ 1
SXZ 3699 200
-1119 9746 575 895 842 3682 32 2499 12166 1131 789 614 4385 426 5521 10811 321 196 1001 4366 305 3446 8116
-201 215 692 5930 354 1289 1489
-124
-84 490 5929 91 317 1254 24 19 98 3755 683 1022 6501 1793 154 107 3677 2567 3990 8549 2866
-193 157 4578 1229 41 8487 804 348 444 4553 993 2033 9224 1078
-264 411 6972 1283 1977 8138 528
-306 362 6971 400 1132 4883
-248 34 496 3745 6689 2318 6820 2149 29
-240 4520 1144 2135 6338 1858
-31 30 4585 1060 1768 6102 1901
-34 29 4555 922 995 5381 1347 29 12 7002 983 585 4100 630 14
-2 6996 858 27 2569 64 11
-28 4509 1589 2464 6600 1851
-3
-14 4509 1589 2464 6600 1851
-3
-14 4510 1585 2088 6019 1449 2
-6 4504 1387 1460 5196 1093 7
18 6943 862 594 3679 649 1
3 6944 794 23 2478 139 0
-28 6433 2484 2871 7905 2421 3
91 6433 2484 2871 7905 2421 3
91 6508 1760 2402 7031 1864 2
79 6493 1364 1663 5870 1415 12 53 7252 701 415 3592 667 8
19 7253 443
-223 2283 122 13
-5 QAE17 REV 8196
M SAPTECHr ENGN9EM~NO SSW= IMVW Made by:
Datr:
Client:
Calculation No.:
AES-C-5212-2 ICY6a
-/
- 710, SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 1
( -r-r 1
c5 AES 03 105212-l Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document 0ntrol o.: Sheet No.:
0 1-2 79 of 110 Table A-11b
SUMMARY
OF STRESSES FOR DOWNHILL J-GROOVE (Leak Test Cooldown at 10801s)
Downhill Side Node SX l
SY l
SZ SXY SYZ SXZ 4253 383 4035 19663 1330
-1261
-1201 4237 525
-629 15135 751
-1150
-1044 4461 842 569 6770 58
-576
-680 6117
-153 168 884
-22
-92
-104 6115 180 268
-8 54
-25
-65 4157 4184 8556 11936 6280 612 61 4162 3004 5966 11053 3039 147
-117 4737 521 4914 11875 865
-309
-846 6612 398 1303 7101 293
-200
-559 6611 372 440 3803 95
-44
-312 4987 3132 4324 9194 3429 165 13 4767 2738 3758 9351 2788
-82 85 4742 1229 1826 6920 1264
-193
-84 6628 742 997 4385 456
-92
-146 6629 356 209 2164 142 16
-71 4989 2965 4100 7937 3409 120 160 4769 2352 2882 6758 2370
-43 103 4744 1728 2022 5246 1649
-31 54 6618 908 953 3060 735
-6 24 6619 368 276 1420 163 27 24 4967 2848 3593 7550 3228 13 88 4722 2261 2717 6056 2387
-10 60 4727 1633 1914 4571 1653
-6 41 6553 874 967 2613 736 4
23 6554 333 312 1153 63 13 23 6345 2937 3650 7447 3259 22 64 6379 2227 2658 5772 2374 0
45 6525 1613 1879 4302 1643
-1 37 7339 846 944 2401 703 5
24 7338 315 262 990 21 8
27 QAE17 REV 8196
ENGIrNEEJUN SERYWES. I.
Made, br.
Date:
Cl/
ient:
Calculation No.:
AES-C-5212-2 By7 D
//a7te O SCE SCE No. M-DSC402, Rev. 0 Checked bv:
Date:
Proiect No.:
Title:
PressurizerHeaterSleeveJ-Groove Weld Flaw 3.tt-rc..
7 So AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.:
Sheet No.:
0 1-2 8oofllI Table A-12
SUMMARY
OF CYCLIC STRESSES FOR UPHILL J-GROOVE Cyclic Stres es, Aa (ksl)
Startup!
Loss of X
Y, Startup/
Shutdown Plant Plant Reator Secondary Leak Hydro Node J
.nn)
Shutdown Lwt~
odin Loading UnLoading Trip Pressure Test Test 3899 0.000 0.0O r 20.31 70.19 4.52 5.03 r
21.84 5.07 r
5.S6 4.35 3682 o.ooo 0.47 r
36.14 87.96 r
4-57 521 18.37 s.es 19.32 2210 4385 O.OW0
- 0.
41.03 79.64 3.23 3.80 9.64 4.45 26.20 32.20 4366 O.ooo 0.7S2 28.89 58.16 245 Z90 8.72 3.21 18.18 22.09 5930 O.OW 1.744 6.08 7.61 0.13 0.26 ZOS 0.02 3.98 4,S6 5929 O.ooo 2.697 0.70 7.32 0.70 0.77 4.48 0.68 1.02 1.So 3755 0.14 o.ooo 18.31 48.93 2.70 3.02 10.60 3.34 8.68 9.53 3677 0.194 0.476 33.16 82.39 Z46 2.91 7.09 3.45 21A0 26.40 4578 0.194 0.634 14.16 51.97 3.56 4.09 21.97 3.57 3.28 1.25 4553 0.194 0.792 23.58 59.77 3.29 3.79 17.66 3.80 11.85 12.60 6972 0.194 1.744 26.97 43.20 1.52 1.97 13.36 1.e9 16.35 19.54 6971 0.194 Z697 22.87 12.56 0.81 0.41 6.39 1.50 16.19 20.59 3745 0.735 0.000 18.80 66.34 3.67 3.84 7.32 5.34 10.12 11.41 4520 0.735
_0.476 20.81 48.74 2.39 2.69 7.57 3.24 11.81 13.94 4585 0.735 0.634 19.67 43.62 2.10 2.42 7.87 2.74 11.A2 13.49 4555 0.735 0.792 16.63 38.55 1.75 2.02 7.72 2.29 9.86 11.61 7002 0.735 1.744 15.16 22.54 0.64 0.86 5Ao 0.85 9.82 12.05 6996 0.735 2.697 12.83 7.75 0.44 0.25 2.43 0.66 9.33 11.96 4509 1.304 0.000 22.90 51.18 Z37 2.68 7.04 328 13.37 16.00 4509 1.304 0.476 22.90 51.18 2.37 2.68 7.04 3.28 13.37 16.W 4510 1.304 0.634 21.19 44.08 1.98 2.28 6.56 2.70 12.65 1523 4504 1.304 0.792 18.54 35.58 1.As 1.74 6.86 Z06 11.56 14.04 6943 1.304 1.744 14.71 20.70 0.48 0.67 3.89 0.75 10.04 12.52 6944 1.304 2.697 12.59 7.80 0.45 0.26 2.11 0.64 9.23 11.86 6433 3.276 0.000 27.33 67.88 3.10 3.40 6.54 4.58 16.86 20.35 6433 3.276 0.476 27.35 67.88 3.10 3.40 6.54 4.58 16.86 20.35 6508 3.276 0.634 2S.70 57.27 2.52 2.82 5.92 3.70 15.70 19.08 6493 3.276 0.792 23.15 45.13 1.88 2.13 4.98 2.87 14.17 17.41 7252 3.276 1.744 15.15 20.15 029 0.47 2.84 0.65 11.05 13.95 7253 3.276 2.697 12.70 6.58 0.60 0.43 1.21 0.67 9.61 12A7 QAE17 REV 8196
OINPTECHS ENGINFERING SERtVICES. INCG Madeb Date-aet Calculation No.:
AES-C-5212-2 1C Z
_qj 7/0 I eE:
SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 7
AES 031052l2-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.:
Sheet No.:
0 1-2 81 of 110 Table A-13
SUMMARY
OF CYCLIC STRESSES FOR DOWNHILL SIDE
-Cyclic Stresses, Ac (ksl_
statuplJ Loss of XN j
Startup/
Shutdown Plant Plant Reator Secondary Leak Hydra Node on)_
(in)
Shutdown (wLFlcIng U Loading UnLoading Trip Pressure Test Test 4253 0.000 0.000 54.88 165.17 8.48 9.39 29.44 19.76 28.61 32.10 4237 0.000 0.266 33.44 110.13 6.94 7.71 31.62 5.17 12.37 1129 4461 0.000 0.565 11.96 40.6 3.13 3.53 18.16 1.87 1.82 0.11 6117 0.000 1.660 OAO 4.61 0.69 0.71 3.40 1.63 1.52 2.46 6115 0.000 2.756 1.02 0.62 0.19 0.17 0.86 1.03 1.17 1.72 4157 0.194 0.000 44.84 121.78 4.72 5.15 6.21 24.87 29.54 36AO 4162 0.194 0.266 47.13 10624 3.38 3.88 4.93 25.86 31.72 39.78 4737 0.194 0.565 42.84 97.72 3.86 4.42 13.80 19.18 25.92 31.40 6612 0.194 1.660 26.14 47.80 1.15 1.54 9.56 11.63 17.42 21.44 6611 0.194 2.756 18.99 18.52 0.77 0.46 4.04 8.95 14.09 18.11 4987 0.619 0.000 25.87 85.15 4.35 4.70 11.37 10.85 14.10 16.02 4767 0.619 0.266 30.82 79.36 3.57 4.02 11.43 13.06 17.75 21.03 4742 0.619 0.565 23.88 55.31 2.32 2.86 8.85 10.14 14.05 16.83 6628 0.619 1.660 16.63 31.17 0.74 0.98 5.24 7.92 11.38 14.10 6629 0.619 2.756 1221 10.92 0.63 0.44 1.63 6.19 9.38 12.19 4989 1.301 0.000 25.09 77.66 3.63 3.92 7.57 12.06 14.86 17.56 4769 1.301 0.266 22.24 59.24 2.75 3.06 7.77 9.62 12.70 15.02 4744 1.301 0.565 18.70 43.77 1.83 2.08 6.01
.8.46 11.27
' 13.62 6618 1.301 1.660 12.33 23.17 0.47 0.63 2.92 6.49 8.90 11.17 6619 1.301 2.756 9.06 7.94 0.54 0.41 0.41 5.01 7.23 9.49 4967 1.985 0.000 21.85 72.54 3.65 3.93 8.61 9.66 12.15 13.95 4722 1.985 0.266 19.81 54.00 2.56 2.83 6.87 8.58 11.19 13.20 4727 1.985 0.565 16.14 38.88 1.66 1.57 5.13 7.48 9.82 11.86 6553 1.985 1.660 10.67 20.47 0.43 0.57 2.35 5.73 7.73 9.73 6554 1.985 2.756 7.70 6.80 0.48 0.37 0.11 4.40 6.23 8.21 6345 2.491 0.000 22.28 72.73 3.58 3.84 7.89 10.24 12.67 14.71 6379 2.491 0.266 19.06 52.30 2A8 2.74 6.31 8.40 10.81 12.78 6525 2.491 0.565 15.13 37.15 1.61 1.81 4.74 7.12 925 11.18 7339 2.491 1.660 9.93 19.18 0.41 0.53 2.05 5.42 724 9.13 7338 2.491 2.756 7.15 6.02 0.49 0.39 020 4.23 5.90 7.82 QAE17 REV8/6
MMRPITCHS MIGNEERING SERVCES. ItC Madepr.
Dat er i
Cent:
Calculation No.:
AES-C-5212-2 9
/
6cte7/
/_
°i SCE SCE No. M-DSC-402, Rev. 0 Chedced by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw A
fCiSf.5c[ AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Documen(Control No.: Sheet No.:
0 1-2 82ofll0 Appendix B BIGIF COMPUTER OUTPUT FOR J-GROOVE FLAW EVALUATION (UPHILL SIDE)
QAE17 REV 8196
NRHAPTECHr E-N~GNEENG SERVCES, IN.
Maev Date:
ICQient:
Calculation No.:
AES-C-5212-2 9 / 7/0
~_eSCE SCE No. M-DSC402, Rev. 0 Checked bv:
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw rt Sf4j S° AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
DocumentControl No.: Sheet No.:
0 1-2 83of110 SONG5 VZR HEAUTR SLZCW RZPMR EVLATION WITCHSMAD lMA UPHILL SUE sLcIrs E
SDA?
INUTCAL tOIA¶ON 11 PC VERSION REV. 0 -
SEPTEMR 23. 1985 CENIRPTID 2ttN::
2WCTIONS rOR Usr IN rACTURE HICHANICS PAOSLAsS ANALYSIS SELECTION 1IrAT) 1 rASIGUT ANALYSIS CRACK CrOtMTRY HODEL INDEX W12RPB JIM!)
303 S50RACr 1/4 CIRCULAR CRACK VARZJSE THICONESS IPCIT1CA0MON INTH)
O CONSTANT SCDS THICKNESS CRACK oRtm RATE RIzL JIDAMN 2 INSUT TABULAR DA/DN, DELTA-X DATA SNTECRATION !WCEMNS SCHOM CIM 3 REFINED SINGLE OR MULT INTEGRATION SCHMS CINCL)
O SINGLE INCREHsEKTS USED TO DOUBME CRACK S12E 0N3UB)
USER SPECIFlED NDUB 30 QAE17 REV 8/96
MMAPTCH-E RGEnING SERACES NC Made br.
Date,,Cl{
ient:
Calculation No.:
AES-C-5212-2
__/_
710_
SCE SCE No. M-DSC-402, Rev. 0 Checked bv:
Date.
Proiect No.:
Title:
Pressurizer Heater Sleeve l-Groove Weld Flaw
' iTt.
7 sf AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document tontrol No.: Sheet No.:
0 1-2 84of 110 CEOHESRY AND NXTfR1AL CPACKR ROW T INPUS NUMR or DEGRESs OF FEDCH -
I SONGS PER HEATER SErVE RrPAXR tVALUATION BOSTTO NM 17" UPHILL SIDE INITIAL A-fLUZS FOR EACH DEMME Or fe0DT CRAx LESSN AX II) -
1.0000 CZGOETR? TACTORS On1) 2.7000 0(2)
.00000 0(3)
.00000 G (4
.00000 0 (5)
.00000 G(6)
.00000 0(7)
.00000 C (8)
.00000 BODY WIDTH X-COORD.
TO CEnAC CENTER 1XC)
Y-COORD. TO CRAZ CENTER M)
CRac 0RIZNSATION ANjILE (PRI, VZG Z S
DA/DN OPSION4 SELEcTD:
2 ICI 1000.0 FRACTURE TOHenSS THEMR ARM SETS Or INPUT DATA FOR 1 R-RATOS R-RATIO -
.25000 DELTA-K DA/DN 1.0000 1.020000-12 17.740 2.730000-05 100.00 9.02000E-04 3 POINTS DNPUT QAE17 REV 8/96
ENGINEER1NG SEMCES. NC Made byg Date:
IC/lient:
Calculation No.:
AES-C-5212-2 MaCL
-//
71j SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 1V( TCC J7S AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 85 fllO LOAD TR1WSIENTS:
8 TANSIINTI4)
IN PR=L SONGS PZR MATER S2VE IMPAR EVALUATION BOTTOM READ r IIPSZLL SIDE N14MWR OT CSCIZS NUMBER AWER BL SPE cIrIER AGLD 2PSRD IPLD iWM IWO M
PX NPY 1
STARTUP/SHUTDOWN
.00000 1
1.0000 2
5 0
0 5
6 SYARIATE STRESS TABLE X
r BIW4AIX,)
.oooe
.00000 20.310
.00000
.47C00 36.140
.00000
.63400 41.030
.00000
.79200 2s.es0
.00000 1.7140 6.0800
.00000 2.6970
.70000
.19400
.00000 1.310
.19400
.47600 33.160
.19400
.63400 24.160
.19400
.79200 23.SSO
.19400 1.7440 26.970
.19400 2.6970 22.870
.73500
.0000 18:.00
.73500
.47600 20.810
.73500
.63400 19.670
.73500
.79200 1i.s30
.73500 1.7110 151.60
.73500 2.6970 12.830 1.3040
.00000 22.g00 1.3040
.47600 22.900 1.3040
.63400 21.190 1.3040
.79200 18.540 1.3040 1.7440 14.710 1.3040 2.6970 12.590 3.2760
.00000 27.350 3.27 0
.47600 27.350 3.2760
.63400 25.700 3.2760
.79200 23.150 3.2760 1.7440 15.100 3.2760 2.6970 12.700 THE DATA rOR TIM ST7RSS rFILL HAS SN RWAO CORFPCTLY 2
.00000 3
0 0
0 0
0 2
STARTUfSPjUTDOWN/FLOOello 1.0420 1
1.0000 2
6 0
0 s
6 BIVAATAE STRESS TABLE X
r SIMKAIX T)
.00000
.00000 70.190
.00000
.47600 17.960
.00000
.63400 79.640
.00000
.79200
- 9.160
.00000 1.7440 7.6100
.00000 2.6970 7.3200
.19400
.00000 48.931
.19400
.47600 62.390
.19400
.63400 51.970
.19400
.79200 59.770
.19400 1.7440 43.200
.19400 2.6970 12.560
.73500
.09000 66.340
.73500
.47600 48.740
.73500
.63400 13.620
.73500
.79200 36.550
.73500 1.7440 22.540
.73500 2.6970 7.7500 1.3040
.00000 51.1eo 1.3040
.47600 31.080 1.3040
.:3400 44.080 1.3040
.79200 35.s5o 1.3040 2.7440 20.700 1.3040 2.6970 7.so00 3.2760
.00000 67.980 3.2760
.47600 67.800 3.2760
.63400 57.270 QAE17 REV 8196
MRAPTECHF EN3S EERJ SE3MC.
INC.
Made bvr Date:
Client:
Calculation No.*
AES-C-5212-2
/
G 7 /10 SCE SCE No. M-DSC-402, Rev. 0 OCecked bv:
Date:
Proiect No_
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
_1-L 3.f..
4 AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Dociument Control No.: Sheet No.:
0 I-2 86 of 110 3.2760
.79200 45.130 3.2760 1.7440 20.150 3.2760 2.6970 6.6602 TIM DATA TOR THE STRESS FTELD MAS SEER F CORRECTLY 2
.00000 3
0 C
0 0
0 3
PLANTS LOAD/SYUP 1042.0 1
1.0000 2
5 0
0 5
6 TIVAREATE STRESS SABIX X
S SIGdXTY)
.00000
.00000 4.5200
.00000
.47600 4.5700
.00000
.63400 3.2300
.00000
.79200 2.4500
.00000 1.7440
.13000
.00000 2.6970
.70000
.11402
.00000 2.7000
.19400
.47600 2.4600
.19400
.63400 3.5600
.19400
.79200 3.2900
.19400 1.7440 1.5200
.19400 2.6970
.1000
.73500
.00000 3.6700
.73500
.47600 2.3900
.73500
.63400 2.1000
.73500
.79200 1.7500
.73500 1.7440
.64000
.73500 2.6970
.44000 1.3040
.00000 2.3700 1.3040
.47600 2.3700 1.3040
.63400 1.9800 1.3040
.79200 1.4800 2.3040 1.7440
.48000 2.3040 2.6970
.45000 3.2760
.00000 3.1000 3.2760
.41600 3.1000 3.2760
.63400 2.5200 3.2760
.79200 1.9800 3.2760 1.7440
.29000 3.2760 2.6970
.60000 THE DATA 5
THE STRESS zL5 SEEN READ Cw
=cTLY 2
.00000 3
0 0
0 0
0 4
PLRT WLQAD/STEP 1042.0 1
1.0000 2
5 0
0 5
6 BrVAR.ATE STRESS TABLE.
X Y
S!MIAIX.YI
.00000
.00000 5.0300
.00000
.47600 5.2100
.00000
.63400 3.9000
.00000
.79200 2.9000
.00000 1.7440
.26000
.00000 2.6970
.77000
.19400
.00000 3.0200
.19400
.47600 2.9:00
.19400
.63400 4.0900
.19400
.79200 3.7900
.19400 1.7440 1.9700
.19400 2.6970
.41000
.13500
.00000 3.9400
.73500
.47600 2.6900
.73500
.63400 2.4200
.73500
.79200 2.0200
.73500 1.7440
.96000
.73500 2.6970
.25000 1.3040
.00000 2.69800 1.3040
.47600 2.6800 1.3040
.63400 2.2800 1.3040
.79200 1.7400 1.3040 1.7440
.67000 1.3040 2.6970
.26000 3.2760
.00000 3.4000 3.2760
.47600 3.4000 QAE17 REV 8196
F4MMAPTECHr ENTEIR SERMES. NC Made~br Date, n Cient:
Calculation No.:
AES-C-5212-2 Date: / /°Y SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Project No.:
TItle: PressurizerHeater Sleeve J-Groove Weld Flaw
-7 5e2 AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document ContkoJ No.:
Sheet No.:
0 1-2 87of110 3.2760
.63400 2.9200 3.2760
.79200 2.1300 3.2760 1.7440
.47000 3.2760 2.6970
.43000 mc DAT0. tOR THC S7INSS rILO RAS BEEN B
AD CORRECTLY 2
.00000 3
0 0
0 0
0 5
REACTOR TRIP 1.0000 I
1.0000 2
5 0
0 5
6 SDVAATE STRESS SAC x
r 120AXY?
.00000
.00000 21.340
.00000
.47600 18.370
.00000
.63400 9.6400
.00000
.79200 0.7200
.00000 1.7440 2.0500
.00000 2.6970 4.4BOO
.29400 00000 20.600
.19400
.47600 7.0900
.19400
.63400 21.970
.19400
.79200 17.660
.19400 1.7440 13.360
.19400 2.6970 6.3900
.73500
.00000 7.3200
.73500
.47600 7.5700
.73500
.43400 7.8700
.73500
.79200 7.7200
.73500 1.7440 5.4000
.73500 2.6970 2.4300 1.3040
.00000 7.0400 1.3040
.47600 7.0400 1.3040 63400 6.5600 1.3040
.79200 s.9600 1.3040 1.7440 3.8900 1.3040 2.6970 2.1100 3.2760
.00000 6.5400 3.2760
.47600 6.5400 3.2760
.63400 3.9200 3.2760
.79200 4.9800 3.2760 1.7440 2.8400 3.2760 2.6970 1.2100 THE DATA IMR TIM STRE55 FICI HAS BEN READ CNORECTLY 2
.00000 3
0 0
0 0
0 6
1.058 OF SEMA9 PRCSSURC 1.050002-02 1
1.0000 2
5 0
0 5
6 311VARIATZ STRESS TABLt X
I S10A1XYI
.00000
.00000 5.0700
.00000
.47.00 5.6o00
.00000
.63400 4.4500
.00000
.79200 3.2100
.00000 1.7440 2.00000K-02
.00000 2.6970
.60OO0
.19400
.00000 3.3400
.19400
.47600 3.4500
.19100
.63400 3.5700
.19400
.79200 3.8000
.19400 1.7440 1.6900
.29400 2.6970 1.5000
.73500
.00000 5.3400
.73500
.47600 3.2400
.73500
.63400 2.7400
.73500
.79200 2.2900
.73500 1.7440
.93000
.73500 2.6970
.66000 1.3040
.00000 3.2800 1.3040
.47600 3.2800 1.3040
.43400 2.7000 1.3040
.79200 2.0600 1.3040 1.7440
.75000 1.3040 2.6970
.64000 3.2760
.00000 4.5800 3.2760
.47000 4.5800 QAE17 REV 819G
ENAHRPTECHI ENGWNERMN SERVtCES MN Madrbv:
Date:/
Cl/ ient:
Calculation No.:
AES-C-5212.2 c
Date/q7/0/
QiCE SCE No. M-DSC-402, Rev. 0 Checked br.
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 1-11 T.7 5 q6 Y
AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Documeent Control No.: Sheet No.:
0 1-2 880fllO 3.2760
.63400 3.7000 3.2760
.79200 2.8700 3.2760 1.7440
.65000 3.2760 2.6970
.67000 2T1 DATAOR tlC STRESS YIELD RS BEEN 2r0 COSCTLY 2
.00000 3
0 0
0 0
0 7
PLKWT LEAK 7TST
.41700 1
1.0000 2
5 a
0 a
6 arVARIAT2 STRESS TABLE X
I SIQAXMY)
.00000
.00000 5.9600
.00000
.47600 19.320
.00000
.63400 26.200
.00000
.79200 18.10O
.00000 1.7440 3.9800
.00000 2.6970
.1.0200
.19400
.00000 8.4800
.19400
.47600 21.400
.19400
.63400 3.2800
.1940D
.79200 11.650
.19400 1.7440 16.350
.19400 2.6970 26.190
.73500
.00000 10.120
.73500
.47600 11.810
.73500
.63400 11.420
.73500
.79200 9.8600
.73500 1.7440 9.8200
.73500 2.6970 9.3300 1.3040
.00000 13.370 1.3040
.47600 13.370 1.3040
.63400 12.630 1.3040
.79200 11.560 1.3040 1.7440 10.040 1.3040 2.6970 9.2300 3.27C0
.00000 16.860 3.27C0
.47600 16.860 3.2760
.63400 15.700 3.2760
.79200 14.170 3.2760 1.7440 11.050 3.2760 2.6970 9.6200 THE DIATA FOR T12 STRESS FrLE RAS III RA m
cOncTLY 2
.00000 3
0 0
0 0
0 8
RYDROTSST 2.100001-02 1
1.0000 2
5 0
0 5
6
'OVARIATE STRESS TALE X
S SIMCMYX)
.00000
.00000 4.3S00
.00000
.47600 22.100
.00000
.63400 32.200
.00000
.79200 22.090
.00000 1.7440 4.9600
.00000 2.6970 1.9000
.19400
.00000 9.5300
.19400
.47600 26.400
.19400
.63400 1.2500
.19400
.79200 12.600
.19400 1.7440 19.540
.19400 2.6970 20.590
.73500
.00000 11.410
.73500
.47600 13.940
.73500
.63400 13.490
.73500
.79200 11.610
.73500 0.7440 12.050
.73500 2.6970 11.960 1.3040
.00000 16.000 1.3040
.47600 16.000 1.3040
.63400 15.230 1.3040
.79200 14.040 1.3040 1.7440 12.520 2.3040 2.6970 11.940 3.2760
.00000 20.350 QAE17 REV 8/96
EHRIPN ECHE ENC71NEER G SERVlCES NC Made by:
Date aiCent Calculation No.:
AES-C-5212-2
/
9/ 7/0/
SCE SCE No. M-DSC402, Rev. O checked br.
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
(
2f4 IC AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Cbntrol No.:
Sheet No.:
0 1-2 89ofll0 3.276C
.47600 20.350 3.2760
.63400 19.00e 3.2760
.79200 17.410 3.2760 1.7440 13.950 3.2760 2.6970 12.470 THE DATA FMO THE STRESS TEEM HAS 8119 READ COSrMLY 2
.00000 3
0 0
0 0
0 DETAILED CUTPUT n3R AML LAO 79R310N7 IS) AND CR201 Drc8EE Im OF TR1tDOM lT=4ATA1N VREJWP
- R1
....v*...
s04s r1R mAmR xItEvE REPAIR tvALm om w0 m rIA bb UnhILL SIDE 71 3INT DEGREE or eCCS Nad=R 1TZ10r
/sL=
IO.X TRASSIINT VA/W naN KIlAN DEL.C R-RAT (PER CT=S) sor DA/Dx cR20 (PER 31L.)
SIZE H
1 1
.0000 28.45 2
1 1.042 70.02 3
1 1042.
3.56 4
1 1042.
4.03 5
1 1.000 13.50 6
1 1.0500E-02 4.60 7
1
.4170 15.66 a
1 2.10001-02 18.07 1
1
.0000 28.69 2
1 1.042 70.30 3
1 2042.
3.57 A
1 1042.
4.03 5
1 1.000 13.56 6
1 1.05001-02 4.61 7
1
.4170 15.83 8
3 2.100O0-02 19.29 1
1
.0000 28.93 2
1 1.042 70.57 3
1 1042.
3.57 4
1 1042.
4.04 5
1 1.000 13.61 6
1 1.05000-02 4.62 7
1
.4170 16.00 a
1 2.1000E-02 18.50 1
I
.0000 29.16 2
1 1.042 70.80 3
1 1042.
3.57 4
1 1042.
4.04 5
1 1.000 13.66 6
1 1.05000-02 4.62 7
1
.4170 16.16 8
1 2.1000I-02 18.70 2
1
.0000 29.41 2
1 1.042 71.03 3
1 1042.
3.57 4
1 1042.
4.05 S
I 1.000 13.71 6
1 1.05OOE-02 C.6 7
1
.4170 16.34 8
1 2.1000E-02 18.93 1
1
.0000 29.66 2
1 1.042 71.23 3
1 1042.
3.57 4
1 1042.
4.05 5
1 1.000 13.77 6
1 1.0500E-02 4.62 7
1
.4170 16.52 8
1 2.1000E-02 19.16
.00 14.23 28.45
.00 35.01 70.02
.00 1.76 3.56
.00 2.01 4.03
.00 6.75 13.50
.00 2.30 4.60
.00 7.63 15.66
.00 9.04 1e.07
.000 6.9096s-05
.000 4.0021E-04
.000 1.95540-09
.000 4.04610-09
.000 5.40460-06
.000 8.87211-09
.000 1.3102E-05
.000 2.e520r-05
.00 14.35 28.69
.000 7.02331.05
.00 35.15 70.30
.000 4.033e8-04
.00 1.7C 3.57
.000 1.9720E-09
.00 2.02 4.03
.OD 4.09600-09
.00 6.76 13.56
.000 5.53731-06
.00 2.31 4.61
.0OD 9.0650E-09
.00 7.91 15.83
.000 1.3949C-05
.00 9.24 18.28
.000 2.91620-05
.00 14.47 28.93
.000 7.1384E-05
.00 35.28 70.57
.000 4.0634t-o0
.00 1.79 3.57
.000 1.9el8e-09
.00 2.02 4.04
.000 4.1325C-09
.00 6.81 13.61
.000 5.685SS-06
.00 2.31 4.62
.000 9.1362Z-09
.00 8.00 16.00
.000 1.4867Z-05
.00 9.25 18.50
.000 2.9e37r-05 4.347t-04 1.00 4.386E-04 1.02 4.4232-04 1.05
.0000 53.53 107.8
.00 14.58 29.16
.00 35.60 70.80
.00 1.79 3.57
.00 2.02 4.04
.00 6.83 13.66
.00 2.31 4.62
.00 8.08 16.16
.00 9.55 18.70
.00 14.71 29.41
.00 35.52 71.03
.00 1.79 3.57
.00 2.02 4.05
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RAPTNCH %
ENGINEERUG SERVICES INC.
Made by:
Date: ;
Client-Calculation No.:
AES-C-5212-2 M
Ca1 7/0
_SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
- f 7
t tc.
AES 0310S212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
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HNIHRNPTECH.
MI~NEERING SERYME, Ur-Maje bir:
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Calculation No.:
AES-C-5212-2 SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 17AfCi 58 AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Documen(Contrgi No.: Sheet No.:
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.00 9.81
.00 11.61
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WEIPTECHr EMN~EERNG SERVCMINQ Mad by:
Date: /
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Calculation No.:
AES-C-5212-2
/_ _
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/
/
SCE SCE No. M-DSC-402, Rev. 0 Checked by.
Date:
Project No.:
Title:
PressurizerHeater Sleeve J-Groove Weld Flaw
_ LC J 7
-- AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
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.000 5.5072E-09
.000 4.19032-05
.000 5.990s9-05 4.7872-04 1.74 4.7942-04 1.78 4.79se-04 1.82 4.799E-04 1.87 4.7972-04 1.91 4.798E-04 1.95 4.79S2-04 2.00 4.7892-04 2.05 4.7812-04 2.09 1594.
1679.
1764.
8355.
1946.
2039.
2134.
2232.
2332.
QAE17 REN 8196
ER"PICHE ENGINEERM SERVICES. INC.
Made by:
Date:
Client:
Calculation No.:
AES-C-5212-2 qllf Oz SCE SCE No. M-DSC402, Rev. 0 Checked br.
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
- 1-f A1J-( 7 AES 03105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 93of110 1
1
.0000 26.64 2
1 1.042 72.74 3
1 1042.
3.24 4
2 1042.
3.63 s
1 1.000 13.36 6
1 1.05000-02 4.23 7
1
.4170 22.24 a
1 2.10000-02 26.73 1
1
.0000 36.90 2
1 1.042 72.68 3
1 1042.
3.13 4
1 1042.
3.63 5
1 1.000 13.30 6
1 1.0500E-02 4.22 7
1
.4170 22.48 e
1 2.1000Z-02 27.08 1
1
.0000 37.18 2
1 1.042 72.62 3
1 1042.
3.11 4
1 1042.
3.61 3
I 1.000 13.26 6
1 1.03000-02 4.22 7
1
.4170 22.72 8
1 2.1000E-02 27.41 1
1
.0000 27.45 2
1 1.042 72.57 3
1 1042.
3.1o 4
1 1042.
3.59 5
1 1.000 13.22 6
1 1.05000-02 4.22 7
1
.4170 22.96 8
1 2.10000-02 27.74 1
1
.0000 37.72 2
1 2.042 72.50 3
1 1042.
3.09 4
1 1042.
3.57 s
1 1.000 13.18 6
1 1.03000-02 4.22 7
1
.4170 23.20 8
1 2.10000-02 2e.06 1
1
.0000 38.00 2
1 1.042 72.39 3
1 1042.
3.08 4
1 1042.
3.55 s
1 1.000 13.13 6
1 1.05000-02 4.21 7
1
.4170 23.46 8
1 2.1000E-02 28.41 1
1
.0000 38.28 2
1 1.042 72.25 3
1 1042.
3.07 4
1 1042.
3.53 5
1 1.000 13.03 6
1 1.0500E-02 4.21 7
1
.4170 23.72 a
1 2.10000-02 28.77 1
1
.0000 38.56 2
1 1.042 72.08 3
1 1042.
3.06 1
1042.
3.51 1
1.000 12.s8 6
1 1.0500t-02 4.21 7
1
.4170 23.88 8
1 2.10000-02 29.13 1
1
.0000 38.84 2
1 1.042 71.88 3
1 1042.
3.05 4
1 2042.
3.48 5
1 1.000 12.89 6
1 1.05000-02 4.21 7
1
.4170 24.23 8
1 2.1000Z-02 2.350
.00 18.32 36.64
.00 36.38 72.76
.00 1.57 3.14
.00 1.82 3.63
.00 6.68 13.36
.00 2.11 4.23
.00 11.12 22.24
.00 13.37 26.73
.00 18.43 36.80
.00 36.34 72.68
.00 1.56 3.13
.00 1.81 3.63
.00 6.65 13.20
.00 2.21 4.22
.00 11.24 22.48
.00 13.54 27.08
.00 18.59 37.18
.00 36.31 72.62
.00 1.56 3.11
.00 1.8o 3.61
.00 6.63 13.26
.00 2.21 4.22
.00 11.36 22.72
.00 15.70 27.41
.00 18.73 37.45
.00 36.2s 72.57
.00 1.55 3.10
.00 1.79 3.59
.00 6.61 13.22
.00 2.11 4.22
.00 11.48 22.96
.00 13.87 27.74
.00 18.e6 37.72
.00 36.25 72.50
.00 1.51 3.09
.00 1.79 2.57
.00 6.59 13.19
.00 2.21 4.22
.00 11.60 23.20
.00 14.03 28.06
.00 18.00 38.00
.00 36.19 72.39
.00 1.54 3.08
.00 1.78 3.55
.00 6.56 13.13
.00 2.11 4.21
.00 11.73 23.46
.00 14.20 28.41
.00 18.14 38.28
.00 36.12 72.25
.00 2.34 3.07
.00 1.76 3.53
.00 6.53 13.05
.00 2.11 4.21
.00 11.86 23.72
.00 14.30 28.77
.00 18.28 38.56
.00 36.01 72.08
.00 1.53 3.06
.00 1.75 3.51
.00 6.49 12.98
.00 2.11 4.21
.00 11.99 23.98
.00 14.57 29.13
.00 19.42 38.84
.00 35.94 71.38
.00 1.52 3.05
.00 1.74
.3.48
.00 6.45 12.89
.o0 2.11 4.21
.00 12.12 24.25
.00 14.75 29.50
.000 1.1316E-04
.000 4.312DE-04
.000 9.2650E-10
.000 2.25010-09
.000 5.09710-06
.000 5.43290-09
.000 4.27260-05
.000 6.12230-05
.002 1.1474Z-04
.000 4.3039t-04
.000 B.98322-10
.000 2.17150-09
.000 4.9566"-06
.000 5.3733E-09
.000 4.36260-03
.000 6.2728E-03
.000 1.1644E-04
.000 4.2976E-04
.000 8.7810Z-10
.000 2.10489-09
.000 4.8672t-06
.000 5.33620-09
.000 4.45650-05
.000 6.42480-05
.000 1.18110-04
.000 4.29160-04
.000 8.6193E-10
.000 2.0463Z-09
.000 4.7898E-06
.000 5.32898-09
.000 4.5489z-05
.000 6.57440-05
.000 1.19772-04
.000 4.28272-04
.000 8.4544Z-10
.000 1.8848e-09
.000 4.6993t-06
.000 5.32180-09
.000 4.64300-05
.000 6.7274t-05
.000 1.21472-04
.000 4.27010-04
.000 8.27660-10
.000 1.91810-09
.000 4.58040-06
.000 5.31280-09
.000 4.7417Z-OS
.000 6.8s90z-05
.000 1.2325E-04
.000 4.25450-04
.000 8.0948t-10
.000 1.84810.09
.000 4.4351E-06
.000 5.30760-09
.000 4.8462r-05
.000 7.06070-OS
.000 1.2501t-04
.000 4.2349Z-04
.000 7.91310-10
.000 1.7761Z-09
.000 4.27920-06
.000 5.30270-09
.000 4.95220-05
.000 7.2358E-05
.000 1.26760-04
.000 4.21170-04
.000 7.7384E-10
.000 1.70398-og
.000 4.11820-06
.000 5.30050-09
.000 5.05809-05
.000 7.41320-05 4.769E-04 2.14 4.761Z-04 2.19 4.757C-04 2.24 4.754Z-04 2.30 4.7470-04 2.35 4.7360-04 2.41 4.722Z-04 2.46 4.7040-04 2.52
.6820-04 2.58 2434.
2539.
2647.
2737.
2870.
2986.
3105.
3227.
3353.
QAEI17 REVS/96
MAPTECHF ENGINEERFNG SERVICES. INC Made bvr.
Date:
c l r
ient:
Calculation No.:
AES-C-5212-2 4& 4Ž.
SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date Proiect No.:
Title:
PressurizerHeaterSleeveJ-GrooveWeldFlaw it.
127 5e, C4e AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Documcnt Control No.: Sheet No.:
0 1-2 94ofl10 I2 3
S4 6
7II 1
.0000 39.11
.00 19.55 39.11
.000 1.28511-04 4.656E-04 2.64 1
1.042 71.64
.00 35.82 71.64
.000 4.18431-04 1
1042.
3.04
.00 1.52 3.04
.000 7.5624Z-10 1
1042.
3.46
.00 1.73 3.46
.000 1.6302E-09
- 1.
1.000 12.20
.00 6.40 12.10
.000 3.9498E-06 1
1.0500E-02 4.21
.00 2.11 4.21
.000 5.2960E-09 1
.4170 24.51
.00 12.26 24.51
.000 5.16170-05 1
2.1000E-02 2.916
.00 14.93 29.86
.000 1.5636E-05 CRACK SIZE 0r 1Sl DOF WILL ZX1D gm WI1, Gm1),
0)3 )XT I21RATIOt.
rROCuSim ?Z321K4E0.
3462.
QAE17 REV 896
NONI APTECH.
ENGNEERNG SD8=E& N Madubr.
Date:
Client:
Calculation No.:
AES-C-S212-2 11 Dat ey///
QsCE SCE No. M-DSC-402, Rev. 0 Clecked by:
Date:
Proiect No.:
Title v
Pressurizero eater S 2neeJ-GroovevWeldi Faw N:
or7 SC AES 031o05212-1 Q Evaluadon - SONGS Units 2 and 3 ReGlsion No.:
DocumeAt Control No.: Sheet No0 0
1-2 95of110 Y.£rnoD o£RLWP S0rs PZR HEAER SUrVE-RSpAIR 2VAWMATION 80?TM NU FLM UPOILL Smr FATIRJi: CER= GROMI AXALYSIS SUMMS CQACl DIbMl CZOS)
AC)
Al 1.000 1.023 1.047 1.072 1.097 1.122 1.149 1.176 1.203 1.231 1.260 2.2e9 1.320 1.350 1.382 1.414 1.447 1.481 1.316 1.531 1.587 1.625 1.662 1.701 1.741 1.7e2 1.023 1.866 1.910 1.954 2.000 2.047 2.095 2.144 2.194 2.245 2.297 2.351 2.406 2.462 2.320 2.579 2.639 Kaxnme sREss ixSNsiTy rmw~s)
FOR WORST INPUT LOAD TRANSIINT 70.019 70.304 70.567 70.801 71.C27 71.234 71.421 71.589 71.729 71.835 71.925 72.036 72.135 72.238 72.329 72.423 72.492 72.570 72.624 72.635 72.718 72.802 72.870 72.916 72.973 73.017 73.042 73.040 73.020 73.016 72.988 72.933 72.859 72.7s6 72.679 72.624 72.574 72.493 72.386 72.250 72.079 71.376 71.636 TOTAL CRACN GROWTH RATE CS)
DADN I )
DADNI 4.34741-04 4.3864Z-04 4.42291-04 4.4558E-0O 4.4885E-04 4.51922-04 4.54741-04 4.57352-04 4.39611-0 4.61451-04 4.63101-04 4.65171-04 4.66891-04 4.6834t-04 4.6962t-04 4.70931-04 4.7190Z-04 4.72953-04 4.73712-04 4.74101-04 4.7499£-04 4.76191-04 4.77171-04 4.77861-04 4.7869s-04 4.79331-04 4.7977E-04 4.79s6C-04 4.797L1-04 4.79771-04 4.7953s-04 4.78941-04 4.78101-04 4.7691Z-04 4.76131-04 4.75721-04 4.75381-04 4.74681-04 4.73611-04 4.72221-04 4.7040E-04 4.6e211-04
.0000 53.53 107.8 163.0 219.0 275.9 333.8 392.7 432.6 513.7 S73.9 639.4 704.0 770.0 837.3 906.0 976.1 1048.
1121.
1196.
1272.
1330.
1430.
1311.
1394.
1679.
1786.
1835.
1946.
2039.
2134.
2222.
2332.
2434.
2539.
2647.
2757.
2870.
2986.
3105.
3227.
3353.
3482.
QAE17 REV 8/96
MMAPT £CHr ENsGMERIIN3
- SERVICES, Madeiby:
ate-o C / iene Calculation No.:. AES-C-5212-2 B
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7 1 /
SCE SCE No. M-DSC402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
-b y
r-75m c
AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Docurn-t Control No.: Sheet No.:
0 1-2 96 of 110 Appendix C BIGIF COMPUTER OUTPUT FOR J-GROOVE FLAW EVALUATION (DOWNHILL SIDE)
QAE17 REV 8196
ENGINEERINO SERIWCES.
INC.
Madq by.
Datec Client Calculation No.:
AES-C-5212-2 01%
at2/ 7
¢ CSCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 7 5 AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Cntrol No.: Sheet No.:
0 1-2 97of110 BMWl~ PM~ REATER SULV RZPMR ZVACATCION MTTW4 ELMf n)
DOCWNWLL SIMr BIGMr BOUNDARY Z=XGRAL ZVJTIONf IBM PC VERSION StV. 0 -SEPTEMBER
- 23. 1915 GENERATED ZNF2UrNCE rUNCTIOtS FR USE IN F9AC-Tm WCRAMICS PROBLEMS ANALYSIS SELECTION MIA?)
I FAIW!E XAXXLSIS CRACK GEMER MEL I)DZX NUMBER (UT) 303 SU9I7CE 114 CIRCULAR CRUXK VARIABLE THICRNSS "ECrrZCALTION (MlN o CONSTANT BODYTHt~ICKNESS CRACK GROSMI PATE ROLE (WIMM) 2 INPUT !AKILAR DA/DN. DELTA-K DATA INTIGRATTON INCREMENT SCREWf 4INrM) 3 PEnINZD SINGILE OR KIL1T TINTEGRATIONl SCHEMES (U"L o SINGLE INCRZEfNTS WSED TO DOEmLE CRACIC SIZE IPMKB)
USER SPECITED MinUB -
30 QAE17 REV 8196
ENGINEERM SMACES. INC.
Made br.
Date:
Cl aient:
Calculation No.:
AES-C-5212-2 Jx§z. -
L *7 I SCE SCE No. M-DSC402, Rev. 0 Checked by:
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
-f t7 co AES 03105212-IQ Evaluation-SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 98of110
=ClWTRY AMD HATERAL CPAK CROWTH IN7UT NaLMR oF DEG=S or FU1DOH.
1 SONS PMR MEATEC StMVE RE7ASR MVALTO0 WOITCH NZAD FUN DOrSILS SHI DNITMAL A-VArs oR SALk DEGMRE OF 37ZEDON CRAMC LrNGT AS1C)
.87500 CGETSRY FACTORs
- (1) 2.5000 8O WIDTH C (2)
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EAPTECH.
NEENUNG SERV CS, W MadebDr.
Date:
-ai 0nt:
Calculation No.:
AES-C-5212-2 9
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SCE SCE No. M-DSC-402, Rev. 0 Cbecked by:
Date:
Proiect No.:
Title:
PressurizerHeaterSleeveJ-GrooveWeldFlaw 7rCld yC AES 03105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 99of110 LOAD TRNlSINS:
8 ?RANSISNrT(S IN PROSZrM SCOS PZR N1EATER SLZVC PRZPAIR VYA tLIOC DOTTo BEUD rLAN DOWNHILL SIDE N8CEZR or CYCLES NUMBER NAME PR SZC11rR AD
- SPSRD, SPL KA0z IWOD NPX I
NPT 1
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.00000 1
1.0000 2
5 0
0 6
5 BIVARLATE STRESS TASLE X
I S1CM.tX,}T
.00000
.00000 34.880
.00000
.26600 33.440
.000
.56300 31.960
.00000 1.6600
.40000
.00000 2.7560 1.0200
.19400
.00000 44.840
.19400
.26600 47.130
.19400
.53500 42.840
.19400 1.6600 26.140
.19400 2.7360 18.900
.61900
.00000 25.870
.61900
.26600 30.820
.61900
.56500 23.080
.61900 1.6600 16.630
.61900 2.7560 12.210 1.3010
.00000 25.090 1.3010
.26600 22.240 1.3010
.56500 18.700 1.3010 1.6600 12.330 1.3010 2.7560 9.0600 1.9s50
.00000 21.850 1.9850
.26600 29.810 1.9850
.56500 16.140 1.9850 1.6600 10.670 1.9850 2.7560 7.7000 2.4910
.00000 22.280 2.4910
.26600 19.060 2.4910
.56500 15.130 2.4910 1.6600 9.9300 2.4910 2.7560 7.1500 TUE DATA ION TIM STRESS FIEX =AS KSEN M
EAD CORRECTLT 2
- 00000 3
0 0
0 0
0 2
STARTUP/sjTJDowN/ruOclNG 1.0420 1
1.0000 2
5 0
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.00000 165.20
.00000
.26600 110.30
.00000
.56300 40.660
.00000 1.6600 4.6100
.00000 2.7560
.62000
.19400
.00000 121.80
.19400
.26600 106.20
.19400
.56500 97.720
.19400 1.6600 47.800
.19400 2.7560 18.520
.61900
.00000 83.130
.61900
.26600 79.360
.61910
.56500 55.310
.61900 1.6600 31.170
.61910 2.7560 10.920 1.3010
.00000 77.660 1.3010
.26600 39.240 1.3010
.56500 43.770 1.3010 1.6600 23.170 1.3010 2.7560 7.9400 1.9850
.00000 72.540 1.9850
.26600 54.000 1.9850
.36500 38.eeo 1.8eso 1.6600 20.470 QAE17 RE' 8196
£H1APSCH ENGINEERMN SEVM tM Made ty:.
Date:
/
aient:
Calculation No.:
AES-C-5212-2
/ce-4:V
/1.
/0.
SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve l-Groove Weld Flaw
-P-4 -r..
(7
__f___
AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 100of 10 1.9950 2.7560 6.8000 2.4910
.00000 72.730 2.4910
.26600 52.300 2.4910
.56500 37.150 2.4910 1.6600 19.180 2.4910 2.7560 6.0200 Slli DATA TMR TIM 62SS 2FIELD IIAS Bl:JN REM2 CORRECTLY 2
.00000 3
0 0
0 0
0 3
PLANS 1=/ST0 P
1042.0 1
1.0000 2
5 0
0 6
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.00000
.00000 6.4800
.00000
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.00000
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.00000 1.6600
.69000
.00000 2.7560
.29000
.19400
.00000 4.7200
.19400
.26600 3.3800
.19400
.56500 3.1600
.19400 1.6600 1.1500
.19400 2.7560
.77000
.61900
.00000 4.3500
.61900
.26600 3.5700
.61900
.56500 2.3200
.61900 1.6600
.74000
.61900 2.7560
.63000 1.3010
.00000 3.6300 1.3010
.26600 2.7500 1.3010
.56500 1.8300 1.3010 1.6600
.47000 1.3010 2.7560
.54000 1.9850
.00000 3.6500 1.9850
.26600 2.5600 1.9850
.56500 1.6600 1.9850 1.6600
.43000 1.9850 2.7560
.48000 2.4910
.00000 3.5800 2.4910
.26600 2.4800 2.4910
.56500 1.6100 2.4910 1.6600
.41000 2.4910 2.7560
.49000 TIM DATA FMR THE STRZSS TFELD KllS BEEN READ CORRECTLY 2
.. 00000 3
0 0
0 0
0 4
PLANT IUNL=/STEP 2042.0 1
1.0000 2
5 0
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.00000
.00000 9.3900
.00000
.26600 7.7100
.00000
.56500 3.3300
.00000 1.6600
.71000
.00000 2.7560
.17000
.19400
.00000 5.1500
.19400
.26600 3.8800
.19400
.56500 4.4200
.19400 1.6600 1.5400
.23300 2.7560
.46000
.61900
.00000 4.7000
.61900
.26600 4.0200
.61900
.56500 2.6600
.61900 1.6600
.98000
.61900 2.7560
.44000 1.3010
.00000 3.9200 1.3010
.26600 3.0600 1.3010
.56500 2.0800 1.3010 1.6600
.63000 1.3010 2.7560
.41000 1.9850
.00000 3.9300 1.9850
.26600 2.8300 1.9850
.56500 1.8700 QAE17 REV 8/96
HZiSH3PSECHR ENGINEERING SVTRICE5 INC.
Mad bir.
Date:
Claient-Calculation No.:
AES-C-5212-2 M7.
/,
SCE SCE No. M-DSC402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
PressurizerHeaterSleeveJ-Groove Weld Flaw lte-_
(7 Sf4 AES 03105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 101 of 110 1.9850 1.6600
.57000 2.9950 2.7560
.37000 2.4910
.00000 3.8400 2.4910
.26600 2.7400 2.4910
.56500 1.3100 2.4910 1.6600
.53000 2.4910 2.7560
.39000 THE DATA FOR THE STRESS VEtM RAS BEEN RUMAD CORRECTLY 2
.00000 3
0 0
a 0
0 S
ZACT0R TRIP 1.0000 1
1.0000 2
5 0
0 8
5 D!VARIAT? STRESS tAS X
Y ssW.AMxY!
.00000
.00000 29.440
.00000
.26560 31.620
.00000
.56510 18.160
.00000 1.6600 3.4000
.00000 2.7557
.66000
.19400
.00000 6.2100
.29400
.26560 4.9300
.19400
.56510 13.800
.19400 1.6600 9.5600
.19400 2.7557 4.0400
.61900
.00000 11.370
.61900
.26560 11.430
.61900
.56510 3.e500
.61900 1.6600 5.2400
.61900 2.7557 1.6300 1.3010
.00000 7.5700 1.3010
.26560 7.7700 1.3010
.56510 6.0100 1.3010 1.6600 2.9200 1.3010 2.7557
.41000 1.9950
.00000 8.6100 1.9950
.26560 6.6700 1.9850
.56510 5.1300 1.9850 1.6600 2.3500 1.9850 2.7s57
.11000 2.4910
.00000 7.0900 2.4910
.26560 6.3100 2.4910
.56510 4.7400 2.4910 1.6600 2.0500 2.4910 2.7557
.20000 THE DATA rOR THE STRESS rIZW HAS 921N lPA0 CORRECTLY 2
.00000 3
0 0
0 0
0 6
LOSS or sEsxuAT PRESStE 1.0500CS-02 1
2.0000 2
5 0
0 6
5 B1VARIATE STRESS TASLE X
T SI4hCfxiT)
.00000
.00000 29.760
.00000
.26600 5.1700
.00000
.56500 1.9700
.00000 1.6600 1.6300
.00000 2.7560 1.0300
.29400
.00000 24.870
.19400
.26600 25.960
.29400
.56500 19.390
.19400 1.6600 11.630
.19400 2.7360 9.9500
.61900
.o0000 10.850
.61900
.26600 13.060
.61900
.56500 20.140
.61900 1.6600 7.9200
.61900 2.7560 6.1900 1.3010
.00000 12.060 1.3010
.26600 9.6200 1.3010
.56500 s.o600 1.3020 1.6600 6.4900 1.3010 2.7560 5.0100 1.9851
.00000 9.6600 1.9850
.26600 e.5900 QAE17 REV 8/96
ENERPTEC.
1ENGINESUIXI SERYN:ES. WG Madekr.
Date:,,
Cient:
Calculation No.:
AES-C-5212-2
?7/71/T SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve i-Groove Weld Flaw 7
E7 Sf42 1
AES 03105212.1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Contiol No.: Sbeet No.:
0 1-2 1020fllO 1.9850
.56500 7.4800 1.9850 1.6600 5.7300 1.9e50 2.7560 4.4000 2.4910
.00000 10.240 2.4910
.26600 8.4000 2.4910
.56500 7.1200 2.4910 1.6600 5.4200 2.4910 2.7560 4.2300 T)E WA7A MR TUC STflSS FULD MS BEE NA0 CYMCThY 2
.00000 3
0 0
0 0
0 7
PLANT LE TS
.41700 1
1.0000 2
5 0
0 6
5 SlVAR2AS STnSS TABLE X
SlQtX,Yj
.00000
.00000 28.110
.000000
.26600 2.370
.00000
.56500 1.9200
.00000 1.6600 1.5200
.00000 2.7560 1.1700
.19400
.00000 29.540
.19400
.26600 31.720
.19400
.56500 25.920
.19400 1.6600 17.420
.19400 2.7560 14.090
.61900
.00000 14.100
.61900
.26600 17.730
.61900
.56300 14.050
.61900 1.6600 11.390
.61900 2.7560 9.3800 1.3010
.00000 14.860 1.3010
.26600 12.700 1.3010
.56500 11.270 1.3010 1.6600 8.6000 1.3010 2.7560 7.2300 1.9850
.00000 12.150 1.9850
.26600 11.190 1.9850
.56500 9.8200 1.9850 1.6600 7.7300 1.9850 2.7560 6.2300 2.4910
.00000 12.670 2.4910
.26600 10.810 2.4910
.56500 9.2500 2.4910 1.6600 7.2400 2.4910 2.7560 5.9000 THY DASA MR 58S STRESS fW SAS SEEN R1EA0 CORRCTLY 2
.00000 3
0 0
0 0
0 S
HYDAZEST 2.10000E-02 1
1.0000 2
5 0
0 6
5 IVAR2IAT ST1RE55 STAZt X
Y S1A (X Y)
.00000
.00000 32.100
.00000
.26600 11.290
.00000
.56500
.10000
.00000 1.6600 2.4600
.00000 2.7560 1.7200
.19400
.00000 36.390
.19400
.26600 39.770
.19400
.56500 31.390
.19400 1.6600 21.430
.19400 2.7560 18.100
.61900
.00000 16.010
.61900
.26600 21.020
.61900
.56500 16.830
.61900 1.6600 24.100
.61900 2.7560 12.190 1.3010
.00000 17.550 1.3010
.26600 15.010 1.3010
.56500 13.610 1.3010 1.6600 11.170 1.3010 2.7560 9.4900 1.9850
.00000 13.950 QAE17 REV 8196
EASPTECH1 ENG SMMERVScEs Mc Made by:
Date clint:
Calculation No.:
AES-C-5212-2
/
W//7/° /
SCE SCE No. M-DSC-402, Rev. 0 Checked bvy Date Proiect No.:
Title:
Pressurizer Heater Slceve J-Groove Weld Flaw t
-i'rC.
7 5
e AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No:
0 1-2 1030fllO 1.985C
.26600 13.190 1.9850
.56500 11.660 1.9850 1.4600 s.7200 1.9850 2.7560 9.2100 2.4910
.00000 14.710 2.4910
.26600 12.780 2.4910
.56500 11.100 2.4910 1.6600 9.1200 2.4910 2.7560 7.8100 THEDATA IcR THE rsR5s rLD wAs BEEN HEAD CORRECTLY 2
.00000 3
0 0
0 0
0 QAE17 REV 8/96
6FEIREAPTECH.
ENGINEERIN3 SERVg:ES. INC.
Madeby:
Date-a Cient:
Calculation No.:
AES-C-5212-2 e--
/__/_
_/_
SCE SCE No. M-DSC-402, Rev. 0 Checked bv:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 1-T (7 2f
-t2 c AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 I-2 104 ofllO DZ7A2UD OUTPUT rOR ALL CAnD AJ3NSUNTp3) AD C2tACK DtMl(S OF FR1EDO4 Il(T1TR&TICH 82ZAKUP
- RPrnD BONCS KR RIATCR SLEEVE REPAIR I LUAION BOTTOM READ rLR DOWNHILL SIDE TRAP.xSflT Dz92 or CC=s KUMBER REEDG:M
/BLOCK I
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 8
1 2.10001-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.0500-02 7
1
.4170 8
1 2.10001-02 1
2
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.0500E-02 7
1
.4170 1
2.1000-02 1
1
.0000 2
1 1.042 3
1 1042.
A 1
1042.
5 1
1.000 6
1 1.0500E-02 7
1
.4170 a
1 2.10001-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 8
1 2.1000Z-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 8
1 2.200OE-02 t=
l0t1F KMEAN tIL-X 37.83 95.37 4.15 4.73 13.68 16.69 22.18 26.45 37.92 95.41 4.15 4.73 13.72 16.72 22.25 26.53 38.03 95.49 4.14 4.72 13.75 16.77 22.33 26.64 38.16 95.59 4.14 4.72 13.77 16.84 22.44 26.78 38.28 95.68 4.13 4.71 13.78 16.91 22.54 26.91 38.41 95.75 4.13 4.71 13.79 16.97 22.64 27.05
.00 18.91 37.83
.00 47.69 95.37
.00 2.08 4.15
.00 2.37 4.73
.0o 6.84 13.68
.00 8.34 16.69
.00 11.09 22.18
.00 13.22 26.45 0W 18.96
.00 47.71
.00 2.07
.00 2.36
.00 6.86
.00 8.36
.00 11.12
.00 21.1.2
.00 13.27
.00 19.01
.00 47.74
.00 2.07
.00 2.236
.00 6.87
.00 8.39
.00 11.17
.00 13.32
.00 19.08
.00 47.80
.00 2.07
.00 2.36
.00 6.88
.00 8.42
.00 11.22
.00 13.39
.00 19.14
.00 47.84
.00 2.07
.00 2.36
.00 6.89
.00 8.45
.00 11.27
.00 13.46
.00 19.20
.00 47.88
.00 2.06
.00 2.35
.00 6.90
.00 8.49
.00 11.32
.00 13.52
.00 19.18
.00 47.79
.00 2.06
.00 2.35
.00 6.92
.00 8.47
.00 21.31
.00 13.51 37.92 95.41 4.15 4.73 13.72 16.72 22.25 26.53 38.03 95.49 4.14 4.72 23.73 16.77 22.33 26.64 38.16 S5.59 4.14 4.72 13.77 16.84 22.44 26.78 38.28 95.68 4.13 4.71 13.78 16.91 22.54 26.91 TSJMIZNT WA/ON R-PAT tITR CYCLE)
.000 1.20431-04
.000 7.31181-04
.000 4.8654Z-09
.000 1.05801-08
.000 5.86531-06
.000 1.91161-05
.000 4.25261-05
.000 5.9931E-05
.000 1.2091-04
.000 7.318O0-04
.000 4.83911-09
.000 1.0531t-08
.000 5.96201-06
.000 1.9352Z-05
.000 4.27741-05
.000 6.03071-05
.000 1.2167E-04
.000 7.32961-04
.000 4.81071-09
.000 1.04801-08
.000 6.0372Z-06
.000 1.97041-05
.000 4.3094z-OS
.000 6.0797Z-05
.000 1.22491-04
.000 7.3453Z-04
.000 4.77661-09
.000 1.04191-08
.000 6.0972z-06
.000 2.0177I-05
.000 4.34851-05
.000 6.14001-05
.000 1.2328t-04
.000 7.358E1-04
.000 4.71322-09
.000 1.0341t-08
.000 6.1279E-06
.000 2.06481-05
.000 4.3873E-05
.000 6.20031-05 Dor A/OK CRACK (PER LOCK)
SJZE 8.0301-04
.875 8.03SE-04
.P95 N
.0000 25.46 8.0521-04
.916 8.0691-04
.938 8.0s94-04
.960 8.096E-04
.982 8.0671-04 1.01 8.033E-04 1.03 51.47 78.05 105.2 232.9 161.3 190.5 38.41
.000 1.24041-04 95.75
.000 7.36931-04 4.13
.000 4.68281-09 4.71
.000 1.02401-08 13.79
.000 6.1505E-06 16.97
.000 2.11261-05 22.64
.000 4.42621-05 27.05
.0oo 6.2610Z-05 1
1
.0000 38.39 2
1 1.042 95.58 3
1 1042.
4.12 4
1 1042.
4.70 5
1 2.000 13.84 6
1 1.05001-02 16.94 7
1
.4170 22.63 s
1 2.1000E-02 27.03 38.38 85.58 4.12 4.70 13.84 1.94 22.63 27.03 38.34 95.37 4.11 4.68 13.8s 16.90 22.60
.000 1.2388-04
.000 7.34261-04
.000 4.6282Z-09
.000 1.01161-08
.000 6.27042-06
.000 2.0904Z-05
.000 4.4199E-Os
.000 6.25141-05
.000 1.23631-04
.000 7.31131-04
.000 4.56511-09
.000 9.9747E-09
.000 6.3785t-06
.000 2.06411-05
.000 4.41091-05 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
I 1.000 6
1 I 05OOZ-02 7
1
.4170 38.34 95.37 4.11 4.68 13.88 16.90 22.60
.00
.00
.00
.00
.00
.00
.00 19.27 47.68 2.OS 2.34 6.94 8.45 11.30 QAE17 RE' 8/96
ljGHAPTECH.
ENGINEERM~ SERM ES. M:
Madcbyr Date:
Cli ent:
Calculation No.:
AES-C-5212-2 7
D 9 /11:/°7 SCE SCE No. M-DSC-402, Rev. 0 QCecked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw
-1.4 7 (7
(7Szgs('(
AES 03105212-IQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Docurnent Control No.
Sheet No.:
0 1-2 105 of 110 a
2.1000t-02 27.00
.00 13.50 27.00 I
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 1
2.10001-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.0500E-02 7
1
.4170 S
1 2.10001-02 1
1
.0000 2
1 1.042 3
1 1D42.
4 1
1042.
5 1
1.000 6
1 1.0500X-02 7
1
.4170 a
I 2.10001-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.0500E-02 7
1
.4170 S
1 2.1000E-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.0500E-02 7
1
.4170 1
2.10004-02 1
1
.0000 2
1 1.042 3
1 1042.
A 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 a
1 2.10002-02 1
1
.0000 2
1 1.042 3
1042.
4 1
1042.
5 1
1.000 6
1 1.0500t-02 7
1
.4170 B
1 2.10001-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 8
1 2.1000t-02 1
1
.0000 2
1 1.042 3
1 1062.
4 1
1042.
5 1
1.000 6
1 1.05001-02 7
1
.4170 a
1 2.1000t-02 38.28 95.12 4.10 4.67 13.91 16.66.
22.57 26.96 30.26 34.91 4.08 4.66 13.93 16.84 22.56 26.35 38.24 34.74 4.07 4.65 13.95 16.83 22.57 26.96 38.22 94.52 4.06 4.63 13.96 16.62 22.57 26.97 38.18 94.27 4.04 4.62 13.36 16.80 22.56 26.96 38.13 93.99 4.03 4.60 13.96 16.78 22.55 26.96 38.06 93.68 4.01 4.53 13.95 16.76 22.53 26.94 37.99 93.32 3.98 4.55 13.93 16.73 22.51 26.32 37.39 S2.93 3.96 4.53 13.91 16.69 22.48 26.89
.00 19.14
.00 47.56
.00 2.05
.00 2.34
.00 6.935
.00 6.43
.00 11.29
.00 13.46
.00 19.13
.00 47.46
.00 2.04
.00 2.33
.00 6.g7
.00 0.42
.00 11.28
.00 13.68
.00 19.12
.00 47.37
.00 2.04
.00 2.32
.00 6.98
.00 6.42
.00 11.28
.00 13.48
.00 19.11
.00 47.26
.00 2.03
.00 2.32
.00 6.36
.00 6.41
.00 11.28
.00 13.46
.00 19.09
.00 47.14
.00 2.02
.00 2.31
.00 6.38
.00 8.40
.00 11.28
.00 13.46
.00 13.06
.00 47.00
.00 2.01
.00 2.30
.00 6.93
.00 6.38
.00 21.28
.00 13.48
.00 13.03
.00 46.84
.00 2.00
.00 2.29
.00 6.98
.00 6.38
.00 11.27
.00 13.47
.00 18.99
.00 46.66
.00 1.99
.00 2.28
.00 6.97
.00 8.36
.00 11.25
.00 13.46
.00 18.95
.00 46.46
.00 1.98
.00 2.26
.00 6.95
.00 8.35
.00 21.24
.00 13.45 38.28 35.12 4.10 4.67 13.31 16.e6 22.57 26.96 38.26 94.91 4.06 4.66 13.93 16.84 22.36 26.39 38.24 94.74 4.07 4.65 13.93 16.83 22.57 26.96 38.22 94.52 4.06 4.63 13.96 16.62 22.57 26.37 38.18 34.27 4.04 4.62 13.96 16.80 22.56 26.96 38.13 93.9S 4.03 4.60 13.96 16.78 22.55 26.96 38.06 33.68 4.01 4.58 13.95 16.76 22.53 26.94 37.99 93.32 3.96 4.55 13.93 26.73 22.51 26.92 37.83 92.93 3.96 4.53 13.91 16.69 22.48 26.89
.000 6.23804-05
.000 1.2328-44
.000 7.2739Z-04
.000 4.48921-00
.000 3.80991-09
.000 6.46821-06
.000 2.03381-05
.000 4.39871-05
.000 6.2202E-05
.000 1.231OE-04
.000 7.2437E-04
.000 4.41431-09
.000 9.65451-09
.000 6.5S362-06
.000 2.0166E-05
.000 4.39541-05
.000 6.2165K-05
.000 1.2303E-06
.000 7.21711-04
.000 4.33721-09
.000
. 9.50052-09
.000 6.58371-06
.000 2.02271-05
.000 4.39781-05
.000 6.221SE-05
.000 1.22862-04
.000 7.28534-44
.000 4.2496-09
.000 9.32711-09
.000 6.61221-06
.000 2.00361-05
.000 4.39784-05
.000 6.22401-05
.000 1.22621-04
.000 7.1483E-04
.000 4.15281-09
.000
.31331E-09
.000 6.62231-06
.000 1.S9141-05
.000 4.3953E-05
.000 6.22298-05
.000 1.22311-04
.000 7.10741-04
.000 4.04741-09
.000 8.92781-09
.000 6.6159S-06
.000 1.97641-05
.000 4.3910t-05
.000 6.21934-05
.000 1.21911-06
.000 7.06072-04
.000 3.93151-09
.000 e.68431-09
.000 6.5831Z-06
.000 1.2358r-05
.000 4.3845Z-05
.000 6.21321-05
.000 1.2141t-04
.000 7.00861-04
.000 3.807S6-09
.000 0.4221t-09
.000 6.532B8-06
.000 1.93811-05
.000 4.37511-05
.000 6.2031Z-05
.000 1.2093E-04
.000 6.39121-04
.000 3.67661-09
.000 8.14331-09
.000 6.46341-06
.000 1.91301-05
.000 4.3631E-CS
.000 6.1294E-05 7.9921-01 12.0 7.2585-94 1.08 7.3231-04 1.10 7.893X-04 1.13 7.852E-04 1.15 7.806E-04 1.18 1.7521-04 1.21 7.693E-04 1.24 7.62BE-04 1.27 220.5 251.4 283.1 315.6 349.1 383.6 419.1 455.7 493.5 QAE17 REV8196
ENGINEERING SERVICES. INC.
Made by:
Date:
Cient:
Calculation No.:
AES-C-5212-2 AAYL 9/_ 7/0__
SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw jc C7 5
q ABS 03105212-1Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.: Sheet No.:
0 1-2 106 ofilO I
1
.0000 2
1 1.042 3
I 1042.
4 2
2042.
S 1
1.000 6
1 1.oSOO-02 7
1
.4170 1
2.10002-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 1.0500E-02 7
1
.4170 a
1 2.10001-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 2
1.000 6
1 1.05002-02 7
1
.4170 8
1 2.2000Z-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
S 1
1.000 6
1 1.05002-02 7
1
.4170 8
1 2.1000C-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
s 1
1.000 6
1 1.0500Q-02 7
1
.4170 a
1 2.10002-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
S 1
1.000 6
1 1.05002-02 7
1
.4170 8
1 2.1000E-02 1
1
.0000 2
1 1.042 3
1 1042.
4 1
1042.
5 1
1.000 6
1 2.05001-02 7
1
.4170 e
1 2.10002-02 1
1
.0000 2
1 1.042 5
1 1042.
4 1
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O 1
1.000 6
1 2.05002-02 7
1
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1 2.10001-02 1
1
.0000 2
1 2.042 3
2 1042.
4 2
1042.
5 1
1.000 6
1 1.03002-02 7
1
.4170 8
1 2.10002-02 37.78 92.50 3.94 4.50 13.88 16.65 22.44 26.85 37.67 92.06 3.91 4.47 13.84 16.61 22.40 26.82 37.62 91.74 3.89 4.44 13.80 16.61 22.41 26.84 37.56 91.38 3.86 4.42 15.76 16.60 22.41 26.85 37.49 91.01 3.63 4.39 13.71 16.59 22.41 26.06 37.41 92.62 3.80 4.36 13.66 16.58 22.40 26.87 37.32 90.21 3.77 4.31 13.60 16.57 22.40 26.88 37.22 89.76 3.74 4.29 13.54 16.55 22.38 26.88 37.11 89.28 3.71 4.25 13.48 16.52 22.36 26.07
.O0 18.89 37.78
.00 46.25 92.50
.00 1.97 3.94
.00 2.23 4.50
.00 6.94 13.88
.00 8.33 16.65
.00 11.22 22.44
.00 13.43 26.85
.00 18.84 37.67
.00 46.03 92.06
.00 1.95 3.91
.00 2.24 4.47
.00 6.92 13.84
.00 8.31 16.61
.00 11.20 22.40
.00 13.41 26.82
.00 18.81 57.62
.00 45.87 91.74
.00 2.94 3.89
.00 2.22 4.44
.00 6.90 131.0
.00 8.30 16.61
.00 11.20 22.41
.00 13.42 26.84
.00 18.78 37.56
.00 45.69 91.38
.00 1.93 3.86
.00 2.21 4.42
.00 6.88 13.76
.00 8.30 16.60
.00 11.20 22.41
.00 13.43 26.85
.00 18.74 37.49
.00 45.51 91.01
.00 1.92 3.83
.00 2.19 4.39
.00 6.85 13.71
.00 e.30 16.59
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.00 13.43 26.86
.00 18.70 37.41
.00 45.31 90.62
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.00 6.83 13.66
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.00 11.20 22.40
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.00 18.66 37.32
.00 45.11 90.21
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- 1. 8 175t-05 4.327s2-05 6.1840l-03 1.1604t-04 6.42882-04 2.480694-09 5.62482-09 5.36172-06 1.8029s-OS 4.3208t-05 6.1814z-OS 7.109E-04 1.52 7.032C-04 1.56 842.0 893.2 QAE17 REV 8/96
ENOINEERH SSWCES. INC.
Madeb Date:
/Client.
Calculation No.:
AES-C-5212-2
/_______f 710 i
SCE SCE No. M-DSC402, Rev. 0 Ohecked by:
Date:
Project No.:
Title Pressurizer Heater Sleeve J-Groove Weld Flaw
- 47 e
7 AES 03105212-2Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Lontrol No.:
Sheet No.:
0 1-2 107 of 110 1
1
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1 1.042 3
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2 2.20001-02 37.00 88.79 3.69 4.22 13.41 16.50 22.35 26.87 36.87 88.27 3.64 4.18 13.34 16.47 22.32 26.85 36.72 87.70 3.60 4.14 13.25 16.44 22.29 26.83 36.58 87.23 3.56 4.09 13.17 16.40 22.25 26.80 36.44 86.56
-3.53 4.05 13.09 36.37 22.22 26.78 36.29 83.97 3.49 4.01 13.00 16.33 22.18
- 26. 7S 36.16 e5.42 3.46 3.97 12.91 16.31 22.16 26.74 36.09 84.95 3.42 3.93 12.82 16.31 22.18 26.78 36.02 84.48 3.39 3.90 12.72 26.32 22.19 26.83
.00 18.50 37.00
.00 44.40 88.79
.00 1.84 3.68
.00 2.11 4.22
.00 6.71 13.41
.00 3.25 16.50
.00 11.17 22.35
.00 13.43 26.87
.00 18.44 36.87
.00 44.13 88.27
.00 1.82 3.64
.00 2.09 4.18
.00 6.67 13.34
.00 8.24 16.47
.00 11.16 22.32
.00 13.43 26.95
.00 28.36 36.72
.00 43.83 87.70
.00 1.80 3.60
.00 2.07 4.14
.00 6.63 13.25
.00 8.22 16.44
.00 11.14 22.29
.00 13.41 26.83
.00 18.29 36.53
.00 43.56 87.13
.00 1.78 3.56
.00 2.05 4.09
.00 6.59 13.17
.00 8.20 16.40
.00 11.13 22.25
.00 13.40 26.80
.00 18.22 36.44
.00 43.20 86.56
.00 1.76 3.53
.00 2.03 4.05
.00 6.55 13.09
.0O 9.18 16.37
.00 11.21 22.22
.00 13.39 26.78
.00 18.25 36.29
.00 42.89 85.97
.00 1.75 3.49
.00 2.01 4.00
.00 6.50 13.00
.00 8.17 16.33
.00 11.09 22.18
.00 13.37 26.75
.00 18.08 36.26
.00 42.71 85.42
.00 1.73 3.46
.00 1.99 3.97
.00 6.46 12.91
.00 8.15 16.31
.00 11.08 22.16
.00 13.37 26.74
.00 18.05 36.00
.00 42.48 84.95
.00 1.71 3.42
.00 1.97 3.93
.00 6.41 12.82
.00 8.16 16.31
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.00 13.39 26.78
.00 18.01 36.02
.00 42.24 84.48
.00 1.70 3.39
.00 2.95 3.90
.00 6.36 12.72
.00 6.16 16.32
.00 11.10 22.19
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1113.
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QAE17 REV S196
MAPITCHF ENGINEERIN3 SERVICES. I=C Mad: blr Date: f Claient:
Calculation No.:
AES-C-5212-2
/b D
t/ 71//
SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Project No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 7ft Tt7....
AES 03105212-] Q Evaluation -
SONGS Units 2 and 3 Revision No.:
Documefo Control No.: Sheet No.:
0 1-2 108 of 110 I
1
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1 1.042 3
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4 1
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1 2.1000t-02 35.95 84.01 3.36 3.86 12.63 16.33 22.21 26.87 35.88 83.51 3.33 3.82 12.53 16.34 22.23 26.92 35.80 82.99 3.30 3.79 12.42 16.34 22.25 26.96 35.72 82.45 3.27 3.75 12.30 16.35 22.26 27.00 35.64 81.89 3.24 3.71 12.17 16.36 22.28 27.05 35.35 81.30 3.21 3.67 12.04 16.36 22.29 27.09 35.47 80.71 3.18 3.63 11.91 16.37 22.31 27.14 35.39 80.13 3.15 3.60 11.78 16.38 22.33 27.19 35.31 79.50 3.13 3.56 11.64 16.38 22.35 27.23
.00 17.98 35.95
.00 42.00 84.01
.00 1.68 3.36
.00 1.93 3.86
.00 6.31 12.63
.00 8.17 16.33
.00 11.11 22.21
.00 13.44 26.87
.00 17.94 35.88
.00 41.76 83.31
.00 1.67 3.33
.00 1.91 3.82
.00 6.26 12.53
.00 8.17 16.34
.00 11.12 22.23
.00 13.46 26.92
.00 17.90 35.80
.00 41.50 82.99
.0 1.65 3.30
.00 1.89 3.79
.00 6.21 12.42
.00 8.17 16.34
.00 11.12 22.25
.00 13.40 26.96
.00 17.86 35.72
.00 41.22 82.45
.00 1.63 3.27
.00 1.87 3.75
.00 6.15 12.30
.00 8.17 16.35
.00 11.13 22.26
.00 13.30 27.00
.00 17.82 35.64
.00 40.94 81.89
.00 1.62 3.24
.00 1.86 3.71
.00 6.09 12.17
.00 8.19 16.36
.00 11.14 22.28
.00 13.52 27.05
.00 17.77 35.55
.00 40.6s5 81.30
.00 1.60 3.21
.00 1.84 3.67
.00 6.02 12.04
.00 8.18 16.36
.00 11.35 22.29
.00 13.55 27.09
.00 17.74 35.47
.00 40.36 80.71
.00 1.59 3.18
.00 1.82 3.63
.00 5.95 11.91
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.00
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.00 40.06 80.13
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.00 5.89 11.78
.00 8.19 16.38
.00 11.17 22.33
.00 13.59 27.19
.00 17.65 35.31
.00 39.75 79.50
.00 1.56 3.13
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.00 5.82 11.64
.00 8.19 16.38
.00 11.17 22.35
.00 13.62 27.23
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1259.
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- 8. 9954-10 1.94301-09 2.24042-06 1.72351-05 4.31374-05 6.344 6E-05 5.756E-04 2.26 s.6751-04 2.31 5.589Z-04 2.36 1996.
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2184.
QAE17 REV 8196
ENGINEERING SERVICES. INC.
Ma4 Y
Date
/a ient:
Calculation No.:
AES-C-5212-2 MZ '
Dateq //0t SCE SCE No. M-DSC402, Rev. 0 Cledced br:
Date:
Proiect No.:
Title:
Pressurizer Heater Sleeve J-Groove Weld Flaw 1
(7 Sf ge54 AES 03105212-lQ Evaluation -
SONGS Units 2 and 3 Revision No.:
Document Control No.:
Sheet No.:
0 1
-2 109ofllO 1
1
.0000 35.22
.00 17.61 35.22
.000 1.0475Z-04 2
1 1.042 78.06
.00 39.43 79.86
.000 5.04621-04 3
1 1042.
3.10
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.000 2.54990-10 4
1 1042.
3.52
.00 1.76 3.52
.000 1.62322-09 s
I 1.000 11.49
.00 5.75 11.49
.000 2.0781Z-06 6
1 2.050o0-02 16.39
.00 6.19 16.39
.000 1.7163r-05 7
1
.4170 22.36
.00 11.11 22.36
.000 4.31le9-os 8
1 2.1000t-02 27.28
.00 13.64 27.2!
.000 6.36502-05 5.502E-04 2.42 2284.
2387.
1 1
.0000 35.12
.00 17.56 35.12
.000 1.04181-04 5.410E-04 2.47 2
1 1.042 78.17
.00 39.09 78.17
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1 1042.
3.07
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1 1042.
3.48
.00 1.74 3.48
.000 1.7074t-09 5
1 l.000 21.34
.00 5.67 11.34
.000 1.91320-06 6
1 1.050oo-02 16.39
.00 8.19 16.39
.000 1.7165-05 7
1
.4170 22.37
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22.37
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s 2.1000o-02 27.32
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MA=K sssr or 1O T DOF WILL ZXCE0D 5=Y WIDTH, CCI, ON =XI 2T0RATIT1.
WOCSSSXIG nTr141MD.
QAE17 REV 8196
HNOHRIPTECHS ENGMRING SMICES.
W Made by:
Datt
~
C~lient:
Calculation No.:
AES-C-5212-2
/A e//
0 9 SCE SCE No. M-DSC-402, Rev. 0 Checked by:
Date:
Project No.:
Title:
Pressurizer Heater Sleeve Ji-Groove Weld Flaw 7 Tf f 7 d AES 03105212-1 Q Evaluation -
SONGS Units 2 and 3 Revision No-DocumenFControl No.: Shect No.:
0 1-2 110 of I 10 3ri3 nxm=
SCNGS 9 VAR 3SIV 21MMR 2VA T2ION BOTTOM HZ rLAD DOWNSILU SlE FATIOM CRACK GROWTH )=TSIS SOMPM CRAeK 0DNRStO2(S)
H4X19E04 JtRESS flZNSIY rACOR IS) 5OR W0R2S.
r190 LOAD r72A13 At!)
r0Ox TOTAL CRACK GROrWT PAE IS) wm2 41)
Al
.875
.895
.216 938
.960
.982 1.005 1.029 1.053 1.077 1.1C2 1.128 1.155 1.182 1.209 1.237 1.266 2.296 1.326 1.357 1.389 1.421 1.455 1.499 1.523 1.559 2.596 1.633 1.671 1.710 1.750 1.791 1.833 1.876 2.919 1.964 2.010 2.057 2.105 2.154 2.205 2.256 2.309 2.363 2.410 2.475 95.371 s5.412 95.4s9 95.595 9S.684 95.754 95.976 9s.387 95.117 94.914 94.735 94.5221 94.271 93.994 93.677 93.322 92.930 92.503 92.061 91.735 91.383 91.014 900.23 90.2S1 89.759 89.280 88.793 88.267 87.695 87.129 86.362 85.974 85.415 84.950 84.477 84.009 83.511 82.990 82.447
- 81. 887 81.295 90.714 80.126 79.502 78.t56 78.170 8.03042-04 8.03821-04 8.03172-04 9.06945-04 8.0844Z-04 9.09572-04 e.06692-04 8.03292-04 7.9917Z-04 7.9583t-04 7.92 88E-04 7.8933E-04 7.8516E-04 7.8053E-04 7.75243-04 7.6933-04 7.;627PE-04 7.5572E-04 7.4842r-04 7.4302E-04 7.3722Z-04 7.3119Z-04 7.24 81-04 7.21333-04 7.10962-04 7.03202-04 6.95472-04 6.8717Z-04 6.78233-04 6.69433-04 6.6076E-04 6.51612-04
- 6. 43393-04 6.36U3£-04 6.29413-04 6.2254Z-04
- 6. 1521Z-04 6.0773E-04 5.9996E-04
- s. 92013-04
- 5. 83 6S3-04 5.755S£-04 5.6747£-04 5.5894E-04 5.50213-04 5.4102E-04 "m=R or cT=S oft ORt TO GRCW CRACK 1RCH 2NITM 3?ZZ N
.0000 25.46 31.47 78.05 105.2 132.9 161.3 190.5 220.5 251.4 283.1 315.6 349.1 383.6 419.1 455.7 493.5 532.4 572.7 614.3 657.2 701.4 747.0 794.2 842.8 893.2 945.3 999.3 1055.
1113.
1173.
1236.
1300.
1367.
1436.
1508.
1582.
1659.
1739.
1821.
1907.
1996.
2088.
2184.
2284.
2387.
QAE17 REV 8/96