Residual Stress

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Proactive Residual Stress Management Craig Stover Technical Leader EPRI - Advanced Nuclear Technology

ILWR MRP Conference August 4, 2016 Chicago, IL © 2016 Electric Power Research Institute, Inc. All rights reserved.

What if we could prevent cracks up front... Could we save ourselves from costly inspections and repairs...

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Objectives  Review EPRI Report: – 3002005402 - Guidance for ALWR Primary System Component Residual Stress Management

 Review ongoing EPRI research on residual stress modeling

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Residual Stress Guidelines Purpose: Optimize performance and life-cycle management of Residual Stress (RS) related degradation and failures in advanced nuclear plants  Currently, nuclear industry uses Chemistry, Inspection, & Repair to manage material degradation  Opportunity to create another “tool” to strategically & proactively manage material degradation – Residual Stress – Non-prescriptive, asset management tool that quantifies RS risk and provides guidance on mitigation techniques

– Allows the utility to identify susceptible locations & determine which tool is the best solution

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Core Shroud 304L/316L SCC

Methodology – ALWRs Developed Residual Stress Guidelines for ALWRs  FMEA methodology for identifying & quantifying RS risk – Screen out low risk locations, focus on higher risk welds

– Insight on value of mitigation

 Guidance on management strategies – Mitigation options: technical basis & critical factors – How to choose appropriate technique

 Significant review and input from industry – WRTC advisors, industry experts – Hosted three TAGs (project meetings) 5 © 2016 Electric Power Research Institute, Inc. All rights reserved.

Methodology – SMRs Updated RS Guidelines for SMRs  Partnered with NuScale to review current methodology

 Made minor changes, documented light water SMR applicability, included a worked example (nozzle to safe end DMW) – Minimal changes due to very similar operating environments and materials, biggest difference is “inspectability” i.e. access concerns

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Process for Determining if RSM Technique Should be Applied - Simplified 1. Select components / locations for evaluation 2. Screen out low risk items – Functionality, replaceability, “as-manufactured”, degradation mechanism

3. Collect data – Material, environment, fabrication & welding process, geometry, repair?

4. Assess RS risk (FMEA) – – – –

Influence of RS on initiation and crack growth Surface RS & Thru-wall RS (configuration and fabrication) Weighting factors on occurrence and severity IASCC (if applicable)

– Factor of Improvement (how much impact from RS mitigation?)

5. Integrity Risk – ISI + Flaw tolerance 7 © 2016 Electric Power Research Institute, Inc. All rights reserved.

Example Application – Advanced PWR: DVI Piping Weld 1. Location – weld joining DVI nozzle safe end to SS piping 2. Does NOT screen out –

Passive, long lived, shop & field welds, SCC & thermal fatigue applicable

3. Data assumed, not specific to design or vendor 4. Assess Risk – Assumed GTAW, standard single V groove, etc… – RPN: 161 x FOI 1.6 = 190 – Integrity Category: 4 – RSM Category: C Assume deep OD weld repair: – RPN x FOI = 1856 – RSM Category: B

5. Evaluate RSM Technologies –

Heat sink welding, dry ID compression welding, induction heat stress improvement, Mechanical Stress Improvement (MSI), shot peening, laser jet peening, etc….

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Interpreting Results

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RSM Guidelines Summary Advanced Light Water Reactors

Small Modular Reactors

 Methodology for identifying and quantifying risk of residual stress (FMEA)

 Partnered with SMR vendor to review current methodology  Expanded scope, documented light water SMR applicability, documented a worked example (nozzle to safe end DMW)

– Screen out low risk locations, focus energy on higher risk welds

– Insight on value of mitigation

 Guidance on management strategies – Mitigation options: technical basis and critical factors – Technique selection (e.g. different welding techniques, mechanical stress improvement process, weld overlay, peening, and polishing

– Minimal changes due to very similar operating environments and materials, biggest difference is “inspectability” i.e. access concerns

See EPRI report 3002005402, ANT: Guidance for ALWR Primary System Component Residual Stress Management

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Residual Stress Modeling Measuring & Modeling  How can we incorporate Residual Stress into the design phase?  Need improved modeling & measurement, lack of confidence and raw data to benchmark (Gap identified in Report)  Partnering with WRTC to fabricate mock-ups for modeling and measuring RS – WRTC fabricating several ALWR mock-ups

– ANT fabricating an SMR mock-up (partnership with SMR Vendor)

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Modeling Project Methodology  Fabricating 4 RPV Nozzle mockups – Mockups will simulate both long and short nozzles – Nozzles will be welded to safe-ends utilizing both narrow and wide groove welds – WRS finite element modeling conducted to predict stresses – Residual Stresses will be measured and benchmarked against the stresses predicted by the model

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FEA Preliminary Results - PWHT As-Welded at 70 F

 First step shows significant aswelded residual stress buildup

End of Hold Time at 1100 F

 Second step shows the majority of the residual stresses are relieved at the end of PWHT  Thirst step shows residual stress re-appear – Since the stress relieving occurs at a high temperature, “new” residual stresses are created when the materials are cooled – The stainless steel cladding wanted to shrink more than the vessel during cooling resulting in tensile RS in the cladding

End of PWHT at 70 F

Cooling 100°F/hr Hold time 1.5 hrs

Air cool from 800 F

Heating 100°F/hr

ksi

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FEA Preliminary Results – Dissimilar Metal Welds (DMW) HOOP STRESS

 DMWs result in extensive compressive hoop residual stresses in the weld roots

Long nozzle Wide Groove Long nozzle

Short nozzle Wide Groove Short nozzle

Narrow Groove

Narrow Groove Max

Max

 DMWs result in insignificant tensile axial residual stress in the weld roots  This is a reverse trend from a typical butt AXIAL STRESS weld. – The reason for the reverse trend is because the nozzle has a very thick wall. Therefore, the R/t ratio becomes smaller leading to compressive residual stresses on the ID

Max

HOOP STRESS

Max

ksi

Long nozzle Wide Groove

Short nozzle Wide Groove Max

Max

 The most susceptible crack initiation location is from the nozzle OD surface near the DMW and buttering interface

AXIAL STRESS ksi

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Mockup Status  Mockups are going through final machining – Safe-ends will be welded by the end of August.

 Residual Stress measurements and benchmarking against the model will be completed by the end of 2016  A final report will be published by the end of first quarter of 2017

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Together…Shaping the Future of Electricity

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