华南理工大学学报(自然科学版) ›› 2022, Vol. 50 ›› Issue (3): 73-79.doi: 10.12141/j.issn.1000-565X.210309

所属专题: 2022年机械工程

• 机械工程 • 上一篇    下一篇

飞机受损件激光喷丸残余应力调控研究

张俊豪1 程秀全2 夏琴香1† 程思竹2   

  1. 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
  • 收稿日期:2021-05-17 修回日期:2021-06-21 出版日期:2022-03-25 发布日期:2022-03-01
  • 通信作者: 夏琴香(1964-),女,博士,教授,主要从事塑性成形、模具及装备技术研究。 E-mail:meqxxia@scut.edu.cn
  • 作者简介: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
  • 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

ZHANG Junhao1 CHENG Xiuquan2 XIA Qinxiang1 CHENG Sizhu2   

  1. 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
  • Received:2021-05-17 Revised:2021-06-21 Online:2022-03-25 Published:2022-03-01
  • Contact: 夏琴香(1964-),女,博士,教授,主要从事塑性成形、模具及装备技术研究。 E-mail:meqxxia@scut.edu.cn
  • About author: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
  • 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。

关键词: 7075铝合金, 受损件, 激光喷丸, 非均匀搭接, 残余应力调控

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.

Key words: 7075 aluminum alloy, damaged component, laser shock peening, non-uniform overlap, residual stress control

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