针对K24 镍基铸造合金材料表面粗糙度大引起吸收保护层贴合不紧密的问题，提出采用无保护层激光冲击(LSPwC)方法对K24合金进行强化，利用高周疲劳实验验证其强化效果，并从残余应力、微观组织方面讨论疲劳性能改善机理。实验结果表明：相对于原始叶片，LSPwC 后的模拟叶片的疲劳强度提高16%，保温后疲劳强度提高11%。LSPwC 在试样表层诱导产生高幅值残余压应力和高密度位错，从而提高模拟叶片的疲劳性能；保温后，大部分残余压应力发生松弛，位错结构具有较好的热稳定性，这是保温后模拟叶片疲劳性能提高的主要原因。

Protective layers can not fit well with the surfaces of the materials due to the surface roughness of the K24 nickel based alloy is high. So the laser shock processing without coating (LSPwC) is carried out on the K24 alloy and the high cycle fatigue tests are conducted to verify the reinforcement effect. The mechanisms of the residual stress and microstructures to fatigue performances are discussed. The results show that, compared with the untreated specimen, the fatigue strength of the specimen treated by LSPwC is improved by 16% and that after heat preservation is improved by 11%. Under the effects of the compressive residual stress and high density dislocations that induced by LSPwC, the fatigue performances of the specimens are improved. After heat preservation, the majority of compressive residual stress release, the dislocations have great stability, and this is the main cause of the high cycle fatigue performance improvement.