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Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening

机译:激光震动Peening改善GH3039高温合金的疲劳寿命

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摘要

In order to improve fatigue life of GH3039 superalloy, GH3039 superalloy sheets were treated by laser shock peening (LSP). The microstructure of GH3039 superalloy before and after LSP was characterized using an optical microscope, transmission electron microscope (TEM), and X-ray diffractometer. The fatigue life of the samples with and without LSP was investigated by fatigue experiments. Moreover, surface profile and residual stress were also examined. Experimental results indicated that the grains in the surface layer of the LSP sample were remarkably refined and reached the nanometer scale. The average surface roughness increased from 0.024 μm to 0.19 μm after LSP. The average fatigue life of the laser treated samples was 2.01 times larger than that of the untreated specimens. Additionally, mathematical statistical analysis confirms that LSP has a significant influence on the fatigue life of GH3039 superalloy. The improvement of fatigue life for the laser processed GH3039 superalloy was mainly attributed to compressive residual stress and grain refinement generated by LSP.
机译:为了提高GH3039高温合金的疲劳寿命,通过激光冲击喷丸(LSP)处理GH3039超合金片。使用光学显微镜,透射电子显微镜(TEM)和X射线衍射仪表征GH3039高温合金的微观结构。通过疲劳实验研究了具有和不含LSP的样品的疲劳寿命。此外,还检查了表面轮廓和残余应力。实验结果表明,LSP样品的表面层中的晶粒显着精制并达到纳米级。在LSP之后,平均表面粗糙度从0.024μm增加到0.19μm。激光处理样品的平均疲劳寿命比未处理的样品大的2.01倍。另外,数学统计分析证实LSP对GH3039超合金的疲劳寿命产生了显着影响。激光加工GH3039高温合金的疲劳寿命的改善主要归因于LSP产生的压缩残余应力和晶粒细化。

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