机械工程

飞机受损件激光喷丸残余应力调控研究

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  • 1.华南理工大学 机械与汽车工程学院,广东 广州 510640;
    2.广州民航职业技术学院 飞机维修工程学院,广东 广州 510403
张俊豪(1992-),男,博士生,主要从事塑性成形、模具及装备技术研究。E-mail:415709826@qq.com

收稿日期: 2021-05-17

  修回日期: 2021-06-21

  网络出版日期: 2021-07-05

基金资助

国家自然科学基金资助项目(51575117), 广东省基础与应用基础研究基金项目(2021A1515011074)

Study on Residual Stress Control of Damaged Aircraft Component Based on Non-uniform Overlap Ratio Laser Shock Peening

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  • 1. School of Mechanical and Automobile Engineering, South China University of Technology, Guangzhou 510640, Guangdong, China; 
    2.Aircraft Maintenance Engineering College, Guangzhou Civil Aviation College, Guangzhou 510403, Guangdong, China
张俊豪(1992-),男,博士生,主要从事塑性成形、模具及装备技术研究。E-mail:415709826@qq.com

Received date: 2021-05-17

  Revised date: 2021-06-21

  Online published: 2021-07-05

Supported by

Supported by the National Natural Science Foundation of China(51575117), Guangdong Basic and Applied Basic Research Fund Project (2021A1515011074)

摘要

论文基于残余压应力-激光喷丸搭接率的拟合关系式,设计出非均匀搭接率下的激光光斑位置路径;基于ABAQUS软件建立了7075-T6铝合金受损件激光喷丸有限元模型,实现了非均匀搭接率下激光喷丸有限元数值模拟并获得残余应力场的分布情况。结果表明,采用非均匀搭接率的激光喷丸方法可使试样表面在打磨或受到拉伸载荷后仍处于应力均匀分布的状态;通过增加搭接率调控残余应力值的大小,还可实现修复件表面在受到拉伸载荷时处于均匀压应力状态,从而抑制疲劳裂纹的萌生和扩展。试验结果与模拟结果一致,验证了模型的可靠性。

本文引用格式

张俊豪, 程秀全, 夏琴香, 等 . 飞机受损件激光喷丸残余应力调控研究[J]. 华南理工大学学报(自然科学版), 2022 , 50(3) : 73 -79 . DOI: 10.12141/j.issn.1000-565X.210309

Abstract

Based on the fitting relationship between residual compressive stress and overlap ratio, the laser spot path was designed under non-uniform overlap ratio. A laser shock peening finite element (FE) model for laser shock peening damaged 7075 aluminum alloy component was established based on ABAQUS software. The non-uniform overlap ratio laser shock peening simulation was realized and the distribution of residual stress was obtained. The results show that the non-uniform overlap ratio laser shock peening can keep the surface of the specimen in a state of uniform stress after grinding or under tensile load. By increasing the overlap ratio to control residual stress, the surface of the repaired component can be kept in a state of uniform compressive stress under tensile load, so as to inhibit the initiation and propagation of fatigue cracks. The experimental results are consistent with the simulation results, which verifies the reliability of the model.
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