摘要
研究了用激光冲击强化的方法提高均压孔部位疲劳寿命的可行性。使用流水约束层和铝箔涂层,利用波长为1 064 nm,脉宽为20 ns,能量为35 J,光斑直径为5 mm的YAG激光器对试样进行了激光冲击强化处理。实验结果表明,该方法可以有效提高均压孔部位疲劳寿命。利用扫描电镜对试样断口进行了观察和分析,并对疲劳寿命提高机制进行了讨论。
To improve the fatigue life of the symmetrical pressure hole, a new laser shock processing technology is investigated. Symmetrical pressure hole specimens are processed with YAG laser. The laser peening parameters are as follows: the wavelength of 1 064 nm; the pulse duration of 20 ns and output energy of 35 J. The laser is focused on a spot of 5 mm. Results indicate that the fatigue life is effectively increased by laser shock processing. The fractographs of the specimen are analyzed by scanning electron microscopy(SEM), and the improvement mechanism of the fatigue life is discussed.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
2010年第3期379-382,共4页
Journal of Nanjing University of Aeronautics & Astronautics
基金
国防预研基金(5132701)资助项目
关键词
激光冲击强化
疲劳寿命
残余应力
显微组织
laser shock peening
fatigue life
residual stress
microscopic texture