123 / 2024-10-19 19:23:09
Fatigue Life Extension of Laser Shock Peened 7050 Alumi-num Alloy Manufactured Fillet Structures
fillet structure,laser shock peening,residual stress
全文录用
姜 盎然 / 中国航空制造技术研究院
汝剑 孙 / 中国航空制造技术研究院
Laser shock peening (LSP) is an advanced surface strain strengthening and anti-fatigue manufacturing method. In this paper, LSP was employed to treat 7050 aluminum alloy fillet structures. Residual stress distribution and high cycle fatigue performance were investigated by numerical simulation and experiment, respectively. Further, fatigue life extension was verified with mathematical statistics methods. Results show that by utilizing the following LSP parameters: pulse energy of 25 J, spot size of Φ4.5 mm, overlapping rate of 50%, and peening twice, the average compressive residual stress on the fillet structure surface reached 218.3 MPa, the maximum residual stress in the depth direction located at a depth of 0.9 mm, and the thickness of residual stress affecting layer was 1.6 mm. Besides, the high cycle fatigue life significantly improved after LSP. The average high cycle fatigue life of LSPed side was 160626 cycles, compared to 58606 cycles of the BM side. Further, by using The t-test method of paired comparative experiments, we confirmed that the high cycle fatigue life of LSPed side was 2.18 to 3.36 times higher than that of the BM side at the confidence level of 95%.

 
重要日期
  • 会议日期

    10月18日

    2024

    10月20日

    2024

  • 10月17日 2024

    报告提交截止日期

  • 10月20日 2024

    注册截止日期

  • 11月18日 2024

    初稿截稿日期

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中国机械工程学会表面工程分会
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山东理工大学
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