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首页> 外文期刊>Results in Physics >Effects of scanning path gradient on the residual stress distribution and fatigue life of AA2024-T351 aluminium alloy induced by LSP
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Effects of scanning path gradient on the residual stress distribution and fatigue life of AA2024-T351 aluminium alloy induced by LSP

机译:扫描路径梯度对LSP诱导AA2024-T351铝合金残余应力分布和疲劳寿命的影响

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摘要

Laser shock peening (LSP) is a superficial treatment process employed to induce beneficial residual stress to retard fatigue crack growth, resist corrosion and wear and enhance the mechanical properties of metals. This research study the effects of scanning path gradient on the residual stress and fatigue life of AA2024-T351 aluminum alloy induced by LSP using experiment and 3D FE simulation to optimize the scanning path gradient. The material under study is of great importance in the aerospace industry on fuselage and lugs. Two divergent strategies were used, the scanning path gradient (strategy 1) and the scanning path in advancing direction (strategy 2) both on double-sided dog-bone specimen, and their residual stresses and fatigue life was compared. After LSP, both the LSP treated specimens residual stress and fatigue life were improved. The results showed that the fatigue life of the scanning path gradient was improved by 69.3% while that of the scanning path in advancing direction was improved by 93.5%. In addition, the magnitude of the residual stress on the apex surface was observed to be higher than the bottom surface. Results of the scanning path gradient for the residual stress was calculated by the 3D FE method and it was found to be in good agreement with the experiment results. We observed the presence of tensile residual stresses in between the apex and bottom surfaces after LSP.
机译:激光冲击喷丸(LSP)是一种表面处理工艺,可用来诱导有益的残余应力,以延迟疲劳裂纹的生长,抵抗腐蚀和磨损并增强金属的机械性能。通过实验和3D有限元模拟优化扫描路径梯度,研究了扫描路径梯度对LSP诱导的AA2024-T351铝合金残余应力和疲劳寿命的影响。所研究的材料在航空航天工业中的机身和凸耳上非常重要。使用了两种不同的策略,即双面狗骨头样品的扫描路径梯度(策略1)和前进方向的扫描路径(策略2),并比较了它们的残余应力和疲劳寿命。 LSP处理后,经LSP处理的试样的残余应力和疲劳寿命均得到改善。结果表明,扫描路径梯度的疲劳寿命提高了69.3%,而行进方向的疲劳寿命提高了93.5%。另外,观察到顶点表面上的残余应力的大小高于底表面。残余应力的扫描路径梯度的结果通过3D FE方法计算得出,发现与实验结果非常吻合。我们观察到LSP后在顶点和底面之间存在拉伸残余应力。

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