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Application of Laser Shock Processing to Improving the Fatigue Performance of Compressor Blade

机译:激光冲击加工在提高压缩机叶片疲劳性能下的应用

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The vibration strength under allowable value leads to the failure of compressor blade of certain aeroengine. In order to solve the problem, laser shock processing on blade was studied. First, the processed part of blade as well as the laser shock processing (LSP) parameters was established. Second, the influence of LSP and tumbling to the vibrate fatigue capability of blades were researched according to the application of the project. Third, the strengthening mechanism of LSP on improving the fatigue performance of the blade was studied. The results show that, LSP is consistently dependable and can prolong the vibration fatigue life of the blade efficiently. LSP can be placed after tumbling or directly replace it during the manufacturing of blade. The grain refinement, higher hardness and compressive residual stress are the three main reasons that enhance the fatigue capability of blade.
机译:允许值下的振动强度导致某些航空发动机的压缩机叶片的失效。为了解决问题,研究了刀片上的激光冲击处理。首先,建立了刀片的加工部分以及激光冲击处理(LSP)参数。其次,根据该项目的应用,研究了LSP和翻滚到叶片振动疲劳能力的影响。第三,研究了LSP改善叶片疲劳性能的强化机理。结果表明,LSP始终可靠,可以有效地延长刀片的振动疲劳寿命。在翻滚后可以放置LSP,或者在制造刀片期间直接更换它。晶粒细化,更高的硬度和压缩残余应力是增强叶片疲劳能力的三个主要原因。

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