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The Effects of Laser Shock Peening on Fatigue Life in Ni-based Superalloy

机译:激光冲击强化对镍基高温合金疲劳寿命的影响

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The goal of this work was to determine effects of laser shock peening (LSP) on the fatigue life of the nickel-based superalloy, as well as the mechanism including the residual stress-depth profile (both depth of compression and magnitude) and the microstructure. The vibration fatigue performance of the standard test coupons made by Ni-based superalloy K417 with and without laser shock peening is researched. The residual stress distribution and microscopic structure after LSP are tested and analyzed by X-ray diffraction, SEM and TEM. The results indicated that the compress residual stress is up to 1.0mm in the test coupons after LSP, and the maximum residual compressive stress is about 660MPa under the surface. At the same time, the high pressure shock wave caused by laser propagate into the material which formed high density dislocation in the surface of the samples, and the γ' is divided leading to increase the sub-grain. Because of the deep residual compressive stress, high density dislocation and much more sub-grains, the vibration fatigue strength is improved about 180MPa by LSP. It is very instructive in the structure design and applying LSP to Ni-based superalloy.
机译:这项工作的目的是确定激光冲击喷丸(LSP)对镍基高温合金疲劳寿命的影响,以及包括残余应力-深度分布(压缩深度和大小)以及显微组织在内的机理。 。研究了含镍和不含激光冲击喷丸的镍基高温合金K417制成的标准试样的振动疲劳性能。通过X射线衍射,SEM和TEM测试和分析了LSP后的残余应力分布和微观结构。结果表明,LSP处理后试样的压缩残余应力最大为1.0mm,表面最大残余压缩应力约为660MPa。同时,由激光引起的高压冲击波传播到在样品表面上形成高密度位错的材料中,并且γ'被分割,导致亚晶粒增加。由于深的残余压应力,高密度位错和更多的亚晶粒,LSP将振动疲劳强度提高了约180MPa。这对结构设计以及将LSP应用于镍基高温合金具有很大的指导意义。

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