Simulation and analysis of residual stress in 17-7 PH stainless steel welded joints using laser shock peening technology

To investigate the effect of power density on the residual stress distribution on the surface of 17-7 PH stainless steel welded joints during laser shock process, we utilized ABAQUS finite element software for analyzing its distribution under different laser shock power densities. The material was tested for residual stress using an X-ray stress diffractometer to verify the accuracy of the simulation results and lay the foundation for finding the optimal process parameters. The simulation results show that when the laser power density is 2.79 GW/cm 2 , the maximum residual compressive stress value on the surface of the sample after laser shock peening is −37.2 MPa; When the laser power density is 2.79 GW/cm 2 , the maximum residual compressive stress value on the surface of the sample is −94.1 MPa; When the power density reaches 5.17 GW/cm 2 , the maximum residual stress value on the surface of the laser shock peening sample is −144.8 MPa, and residual stress cavity is formed. The experimental results show that when the laser power density is 2.79 GW/cm 2 , the maximum residual compressive stress on the surface of the sample is −37.3 MPa; When the power density is 3.98 GW/cm 2 , the uniformity of compressive stress distribution on the surface of the sample is optimal, with a maximum residual compressive stress value of −99.0 MPa; When the power density is 5.17 GW/cm 2 , the maximum residual compressive stress value is −146.1 MPa, and residual stress cavity is formed on the material surface. The simulation results are close to the experimental results, and the model error ranges from 0.2% to 4.9%. The simulation results are accurate and reliable.

Authors

Institutions

Publication Details

Journal
Frontiers in Materials
Published
2024-11-27
DOI
https://doi.org/10.3389/fmats.2024.1484792
Primary Topic
Surface Treatment and Residual Stress
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Simulation and analysis of residual stress in 17-7 PH stainless steel welded joints using laser shock peening technology

Kangwen Li, Yaping Li, Weichen Yu, Guangran Guo
Frontiers in Materials
Surface Treatment and Residual Stress
article

Simulation and analysis of residual stress in 17-7 PH stainless steel welded joints using laser shock peening technology

Kangwen Li, Yaping Li, Weichen Yu, Guangran Guo
article en

Abstract

To investigate the effect of power density on the residual stress distribution on the surface of 17-7 PH stainless steel welded joints during laser shock process, we utilized ABAQUS finite element software for analyzing its distribution under different laser shock power densities. The material was tested for residual stress using an X-ray stress diffractometer to verify the accuracy of the simulation results and lay the foundation for finding the optimal process parameters. The simulation results show that when the laser power density is 2.79 GW/cm 2 , the maximum residual compressive stress value on the surface of the sample after laser shock peening is −37.2 MPa; When the laser power density is 2.79 GW/cm 2 , the maximum residual compressive stress value on the surface of the sample is −94.1 MPa; When the power density reaches 5.17 GW/cm 2 , the maximum residual stress value on the surface of the laser shock peening sample is −144.8 MPa, and residual stress cavity is formed. The experimental results show that when the laser power density is 2.79 GW/cm 2 , the maximum residual compressive stress on the surface of the sample is −37.3 MPa; When the power density is 3.98 GW/cm 2 , the uniformity of compressive stress distribution on the surface of the sample is optimal, with a maximum residual compressive stress value of −99.0 MPa; When the power density is 5.17 GW/cm 2 , the maximum residual compressive stress value is −146.1 MPa, and residual stress cavity is formed on the material surface. The simulation results are close to the experimental results, and the model error ranges from 0.2% to 4.9%. The simulation results are accurate and reliable.

Frontiers in MaterialsVol. 11
Commercial Aircraft Corporation of China (China) (CN), Nantong University (CN)
Openalex Percentile: Top 78%
Surface Treatment and Residual Stress
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

Simulation and analysis of residual stress in 17-7 PH stainless steel welded joints using laser shock peening technology — Kangwen Li, Yaping Li, et al. · Frontiers in Materials (2024) | TGRS Research Map | TGRS