ML020520687

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Meeting Handouts for Meeting Held on 01/27/02 to Discuss RCS Piping Inspection Plans for Their Next Refueling Outage
ML020520687
Person / Time
Site: Summer South Carolina Electric & Gas Company icon.png
Issue date: 01/17/2002
From:
NRC/NRR/DLPM
To:
Assa R,NRR/DLPM,415-1391
References
TAC MB3839
Download: ML020520687 (35)


Text

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Presentation to USNRC Refuel 13 Plans for RC S Hot-L eg Nozzles V. C. Summer Nuclear Station January 17, 2002

Meeting Objective

"*Refuel 12

- Commitments -Inspect B/C Hot Legs

- WCAP 15615, Integrity Evaluation

- Safety Evaluation Report

"*Refuel 13

- Inspect to Demonstrate Continued Integrity

- Apply Stress Improvement to Mitigate

"*Be Proactive

- Expectations

- Communications

Meeting Overview

  • Existing Condition-Gary Moffatt
  • Inspection Techniques-Terry McAlister
  • Mitigation Techniques-Gary Moffatt
  • Summary/Discussion mIwIff I

SCA vc Summer RF 12 Relevant Indications A LOOP HOT LEG - New weld w/IAlloy 690 material A, B, & C COLD LEGS- WCAP 15615 > 25 years HOT LEG LOOP LOCATION/ LENGTH ORIENTATION (EDDY CURRENT)

C 309/CIRC 0.5 B 35/CIRC 0.6 B 200.8/AXIAL 0.25 B 348/AXIAL 0.25

Automated UT/ECT Exam Plans for the V.C. Summer R.V.

Nozzle to Pipe Examinations, Spring 2002

RF-12 And Post RF- 12 Experience

  • UT Capability Demonstrated Via Exam of EPRI Block
  • ET Capability Demonstrated Via Exam of EPRI Block

"* Both Demonstrations Witnessed by Station, ANII and NRC Representatives

ET was Used (For First Time in USA) to Complement UT in Screening for Surface and Near Surface Indications

"* ET Has Been Extensively Used for Screening Purposes in RPV Head Penetration Exam with Positive Results

RF- 13 Hot Leg NDE Strategy

  • UT Using Wesdyne Enhanced Process

- Satisfy Post RF-12 Commitments

- Demonstrate Integrity of Welds

- To Provide Basis for Performance of MSIP

  • ET Using Wesdyne Enhanced Process

- Compliment UT Exam

- Screening for Indications for Further Investigation

- Address Post RF-12 Communications

"7' A CA'A Examination Strategy Edd Current Exams Ultrasonic Exams Evaluate data and measure I criteria Apply screening any relevant indications. Correlate ECT with UT and I evaluate inconsistencies, if Perform ASME Section XI present.

assessment of recorded indications.

Further investigate any indication exceeding MSIP acceptance criteria.

Present results to Utility MSIP Team

A 6CANA C'MPANY Ultrasonic Examinations Technique Improvements

  • Transducer Optimization and Size Reduction (30 x 30mm reduced to 22x22mm Probe Size)

"* Improvements in the Transducer Sled

( Floating Probes Within a Frame )

"* Addition of C-scan Analysis Display (Depth Gate Developed Plan View) ioVI;i; 1

  • A UT Transducer Size Reduction i

Fri Shown: V.C Summer ECT Indication 1 in actual surface geometry. Lack of contact for 30x30mm Probe and probable contact scenario for 22x22mm probe

4SANACONIFANY V . C. Summer A Nozzle data - Through-Wall Crack, 70 degree L Data, 2.0 MHz Inconel weld/buttering seen in sweeps 5-8 i.0 MHz Probe should improve imaging

A SCANA COMPANY Vc 309 V.C. Summer 2002 Examinations - Bore Sled I

4

11 INA Ultrasonic C-Scan display for Paragon Analysis Software Depicted: Developed plan view of 360 degree scan with artificial circ oriented defects 5

  • SCEd*&G, Ultrasonic Technique Plan for Probe Use / Acquisition
  • 70' 1.0 MHz 4 directionally Dual element construction - ( 7.6 x 14.2mm x2)

Incremental distance. 125"circ., .125" Axial

° Conservative 57% overlap of one element

  • ASME Code calibration / characterization 9 0.08 to .1 Inter Pulse Period Other techniques available if needed 6 0).

S A4 CRt ¶C'-

A O;M hNA Eddy Current Technique Plan for Probe Use/Acquisition Two Probes, Plus Point normal orientation and Plus Point Off-axis orientation for detection of flaws in all possible orientations.

Identical to 2000 examination configuration

"* Increment size -.125"

"* Operating frequency - 100, 250 and 500 KHz for each probe

  • Data IPP ( distance between pulses, scan direction) = 0.025

>I/

0.025"

.125" 7 t."pi 'I

A S%

Mechanical Stress Improvement Process (MSIP)

1=164 M&C. .0,.

Mechanical Stress Improvement Process - MSIP MSIP

"* Invented, developed, and first used in 1986

"* Displacement controlled - verifiable by measuring pipe hoop contraction oPermanently removes weld residual tensile stresses and generates compressive residual stresses

° Mitigates stress related cracking in nuclear reactor plant piping weldments

A SCANA COMPANY MSIP PRINCIPLE (a)AS WELDED (b) AFTER MSIP Removal of Tension Provides Permanent Protection of Weldments Against Stress Related Cracking 2

SCANA COPIIIPANY BASIC CONCEPT OF MSIP TOOL

a. Application of Pressure to CL,

,b O..Z Contract Pipe T O.D. I'D*

APPLIED PRESSURE

b. Schematic of Permanent b.

Deformation after MSIP

c. Mechanism of Compression ZONE Generation in Axial and Hoop Directions
  • Deformation in pictures are exaggerated for viewing purposes 3

MSIP APPLICATION TO NOZZLE/SAFE END WELD INBWR PLANT k ]

Vt-:

41

ASMMMWM2---_

REDISTRIBUTION OF STRESS IN 28" WELDMENT APdat Hoop Before MSIP After MSIP Before MSIP After MSIP 20ksi

-- 10ksi 20ksi

- -- 20ksi

- Weldment ID 00 ID OD ID OD ID 00 5

Argonne National Laboratory 12" and 28" Straight-To-Straight Tests "MSIPTREATED 12" AND 28" WELDMENTS EXAMINED TO:

DETERMINE RESIDUAL STRESS STATE PRODUCED BY MSIP COMPARE MEASUREMENTS WITH FINITE ELEMENT ANALYSIS INVESTIGATE POSSIBILITY OF ANY UNDESIRABLE SIDE EFFECTS

"* RESIDUAL STRESSES MEASURED ON INNER SURFACE AND THROUGHWALLS:

INNER SURFACE AXIAL AND HOOP STRESSES HIGHLY COMPRESSIVE

(-30 KSI TO -50 KSI IN HAZ FOR 12" AND

-22 KSI TO -50 KSI IN HAZ FOR 28")

THROUGHWALL AXIAL RESIDUAL STRESS DISTRIBUTIONS ALMOST LINEAR ACROSS THICKNESS 0 COMPRESSIVE STRESSES IN HAZ PERSIST THROUGH 50% OF PIPE WALL MEASUREMENTS COMPARE FAVORABLY WITH ANALYTICAL RESULTS AND ARE, IN FACT, BETTER NO UNDESIRABLE SIDE EFFECTS

MSIP Experience

  • Used Since 1986 on Over 1300 Welds Including more than 500 Nozzle and Safe-End Welds in Over 30 BWR Units Worldwide 0 Applied to Welds Without and With Stress Corrosion Cracks 0 No Indications Found in Treated Welds 0 Pre-existing Cracks Arrested; No Crack Growth after MSIP During Subsequent Fuel Cycles
  • Verified by Argonne National Laboratory and EPRI for Pipe Specimens and Nozzle Specimens Without and With Cracks 9 NRC Acceptance NUREG-0313

A SIANA COM'PANY MSIP FOR BWR vs. PWR

  • Similar Materials

- Nozzle SA508 CIil1

- Weld 82/182

- Safe-end SST

"* Similar Configuration

- Nozzle to Safe-end / Pipe Welds

"° Similar Geometry

- Comparable D/t

"*Analysis shows similar Post-MSIP results

"° Application

- Similar Tooling

- Similar Procedures

- Same Verification Parameters S"!oI - -

9

A CYA COMPANY EPRI BWR RECIRCULATION SYSTEM NOZZLE (N2), FN2-1-1, FN2-1-3 1.121 3-15088,0 1.87

.137

.887 11.50 DIA 13.56 DIA 9.90 DIA It.OD DIA 14.00 OIA 10-- ----- --- -- --- -- -

10t

H-. I

> u

-LI

- .."~ ?i1

/ N*

N .W... .N

--.-- 4 ' i*

  • w I I-,oC U

V SrCAEAe Qrv V.C.Summer Process Qualification EPRI BWR NOZZLE TO SAFE-END V.C. SUMMER NOZZLE TO SAFE-ENDIPIPE Nominal OD = 14" Average OD = 33.93" Nominal ID = 11.6" Average Wall Thickness t = 2.42" Mean Dia. DM = 12.8" Mean Dia. DM = 31.51" Wall Thicknesst = 1.2" DM= 12.8 = 10.67 DM = 31.51 = 13.02 t 1.2 t 2.42 The BWR Safe-end DM is less than V.C. Summer.

t Therefore, VC Summer is bounded by the existing applications.

A SCANA LOMPANY V. C. SUMMER HOT LEG NOZZLE WELD REGION AN DEC 28 2001 11:17:12 PLOT NO. I ELEMENTS PowerGraphics EFACET:1 MAT NUM V C Surmaer RPV Hot Leg Nozzle Assembly 13

A SCANA COMPANY V. C. SUMMER HOT LEG NOZZLE AS-WELDED RESIDUAL STRESS (AXIAL)

SJ DEC 28 2001 11:20:58 PLOT NO. 3 NODAL SOLUTION STEP=2 SUB =6 TIME=2 SY (AVG)

RSYS=0 PowerOraphics EFACET-I AVRES=AII DMX = .009322 SMN =-34307 SMUX -56039

-34307

-24268

-14230

-4192 5847 15885 25924 35962 46000 No 56039 V C Sununer RPV Hot Leg Assembly As-Welded Stresses 14


A SCANA 0GOFANY V. C. SUMMER HOT LEG NOZZLE AS-WELDED RESIDUAL STRESS (HOOP)

J DEC 28 2001 11:21:34 PLOT NO. 4 NODAL SOLUTION STEP=2 SUB =6 Tfl4E:2 SZ (AVG)

RSYS=O PowerGraphics EFACET=

AVRES=All DMX =.009322 SNvN =-32227 SSMX :64541

-32227

-21475

-10723 28.645

- 10781 21533 32285 43037 53789 64541 IV C S.unuer RPV Hot Leg Assembly As-We.lded Stresses 15-

A SCANA O0PVy V. C. SUMMER HOT LEG NOZZLE WELD POST- MSIP RESIDUAL STRESS (AXIAL)

AN DEC 28 2001 12:34:52 PLOT NO. 1 NODAL SOLUTION STEP=9 SUB -4 TIME:9 SY (AVG)

RSYS:0 PowerGraphics EFACET=1 AVRES=All MX :.251796 SMN =-46788 SmX =42978 46788

-36814 S-26840 IKE -16866

-6892

. 3082 13056 23030 33004 42978 VC Summer RPV HL Nozzle Assembly Post MSIP Stresses 16

A SCANA (,OMP3ANY V. C. SUMMER HOT LEG NOZZLE WELD POST- MSIP RESIDUAL STRESS (HOOP)

J'N DEC 28 2001 12:35:19 PLOT NO. 2 NODAL SOLUTION STEP=9 SUB =4 Tfl4E=9 Sz (AVG)

RPSYS=O PowerGraphics EFACET=

AVRES=AI1 DAX -=.251796 SN*A=-52831 SlY =36508

-52831 S&D-42904

= -32978 ff--1 -23051 fm -13124 6729

-3198 16655

  • 26582 36508 VC Sununer RPV HL Nozzle Assembly Post MSIP Stresses

MSIP Conclusions

"*MSIP at V. C. Summer is Bounded by Existing Qualification Testing

- Similar Materials

- Similar Configuration / Geometry

- Comparable D/t

"*MSIP FEA for V. C. Summer

- Axial compressive stresses - 50% wall

- Hoop compressive stresses - 50% wall

"*NUREG 0313 - 0.3t Acceptance Criteria

"*Operating experience on over 500 nozzle and safe-end welds

  • MSIP has been demonstrated to be effective in mitigating SCC

A AA.'P, VC Summer RF 13 Repair Contingencies e Localized ID Repair MSIP

  • Localized Repair From OD - MSIP 0 Spool Piece Replacement J

Summary

"* Demonstrate Continued Integrity Through Inspection

"° Apply Mitigating Process

- Proven To Be Effective

- Qualification Applies To VC Summer

- Accomplished Via 10CFR50.59

"* Inspection/Evaluation Results Provided To NRC To Support SER Revision