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GH4169D高温合金喷丸强化残余应力场仿真与参数化建模

罗健鑫 张伟 雷力明 谭靓 姚倡锋

航空材料学报2026,Vol.46Issue(8):84-92,9.
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航空材料学报2026,Vol.46Issue(8):84-92,9.DOI:10.11868/j.issn.1005-5053.2026.000122

GH4169D高温合金喷丸强化残余应力场仿真与参数化建模

Simulation and parametric modeling of residual stress field in shot peening of GH4169D superalloy

罗健鑫 1张伟 1雷力明 1谭靓 2姚倡锋2

作者信息

  • 1. 太行国家实验室,成都 610213
  • 2. 西北工业大学 航空发动机高性能制造工业和信息化部重点实验室,西安 710072
  • 折叠

摘要

Abstract

Residual compressive stress is a critical factor affecting the performance and service life of components.The active introduction and precise control of residual compressive stress have become one of the core technical approaches to improve component reliability and extend service life.Aiming at the difficulties in optimizing shot peening process parameters and insufficient prediction accuracy of residual stress fields for GH4169D superalloy,this work adopts a combined simulation and experimental method for investigation.A multi-shot peening simulation model considering the random distribution characteristics of shot particles is established to analyze the material strain rate as well as the correlation between residual stress and plastic strain under various process conditions,and the accuracy of the random shot peening residual stress model is verified.Shot peening strengthening experiments are carried out based on the response surface methodology.The influence laws of different shot peening intensities and coverage rates on the depth distribution of the residual stress-affected layer are compared,and parametric modeling is performed for the depth distribution of the residual stress-affected layer.The results reveal that the cosine attenuation function can realize parametric modeling of residual stress fields of GH4169D superalloy under diverse shot peening processes,with the fitted determination coefficient R2 greater than 0.95.These findings provide an effective method for rapid optimization of shot peening strengthening processes and accurate modeling of residual stress fields of GH4169D superalloy.

关键词

高温合金/喷丸强化/残余应力/有限元模拟/参数化建模

Key words

superalloy/shot peening/residual stress/finite element simulation/parametric modeling

分类

航空航天

引用本文复制引用

罗健鑫,张伟,雷力明,谭靓,姚倡锋..GH4169D高温合金喷丸强化残余应力场仿真与参数化建模[J].航空材料学报,2026,46(8):84-92,9.

基金项目

太行国家实验室自主立项项目(BK133) (BK133)

国家自然科学基金项目(92360309) (92360309)

航空材料学报

1005-5053

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