Research Progress and Prospect of Laser Shock Peening Technology in Aero-engine Components

被引:0
|
作者
Nie, Xiangfan [1 ,2 ]
Li, Yinghong [1 ]
He, Weifeng [1 ]
Luo, Sihai [1 ]
Zhou, Liucheng [1 ]
机构
[1] Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an,710038, China
[2] School of Mechanical and Power Engineering, East China University of Science and Technology, Shanghai,200237, China
关键词
Aero-engine - Aero-engine components - Anti-fatigue - Application of laser - Blade turbine - High cycle fatigue - Laser shock peening - Research outlook - Research progress - Service environment;
D O I
10.3901/JME.2021.16.293
中图分类号
学科分类号
摘要
Because of hostile service environment and complicated working loads, aero-engine components are apt to high-cycle fatigue fracture, which seriously affects security and reliability of aero-engine. Laser shock peening, LSP, is a novel surface plastic-strengthening technology. High-cycle fatigue performance can be improved effectively under the action of compressive residual stress and microstructural modification. LSP has been widely applied in the batch production and maintenance of aero-engine components. Research status, application situation and problems to be resolved of laser shock peening on fan/compressor blade, turbine blade, turbine disk, cartridge receiver, hydraulic actuator, pipe, gear and so on were discussed deeply. The development tendency of laser shock peening research on aero-engine components in recent years was analyzed and concluded. The future work on equipment, technique, mechanism and application of laser shock peening on aero-engine components was taken an outlook. In future, hope that the large-scale industrial application of laser shock peening on aero-engine components could be realized under the synergistic action of the whole industry and the whole technology chain. © 2021 Journal of Mechanical Engineering.
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页码:293 / 305
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