激光冲击工艺对GH742镍基高温合金疲劳性能的影响Effects of laser shock processing on fatigue property of GH742 Ni-based superalloy
何卫锋,李应红,周章文,张永康,汪诚
摘要(Abstract):
对两组镍基高温合金(GH742)试样进行激光冲击强化后,分别进行拉-拉疲劳试验和振动疲劳试验,并和未进行强化处理的试样进行对比,分析了强化试件的疲劳断口特征。结果表明激光冲击强化能提高镍基高温合金拉-拉疲劳寿命3.6倍以上,提高振动疲劳寿命2.4倍;强化后残余压应力影响层深度达1.0mm。
关键词(KeyWords): 镍基高温合金;激光冲击强化;疲劳;残余压应力;断口金相
基金项目(Foundation): 国防预研基金(513270103)
作者(Author): 何卫锋,李应红,周章文,张永康,汪诚
参考文献(References):
- [1]马壮.航空发动机构件激光冲击强化研究[D].西安:空军工程大学,2008.
- [2]张永康.激光冲击强化提高航空材料疲劳寿命的研究[D].南京:南京航空航天大学,1995.
- [3]王华明,李晓轩,孙锡军.激光冲击处理不锈钢及镍基合金后表面力学性能的研究[J].中国激光,2000,27(8):756-760.WANG Hua-ming,LI Xiao-xuan,SUN Xi-jun,et al.Study of surface mechanical properties of laser shock processed austenitic steel and Ni-based superalloy[J].Chinese Journal of Lasers,2000,27(8):756-760.
- [4]Gomez-Rosas G,Rubio-Gonzalez C,et al.High level compressive residual stresses produced in aluminum alloys by laser shock processing[J].AppliedSurface Science,2005,252:883-887.
- [5]Shepard M J.Laser shock processing induced residual compression for improved damage tolerant design[D].University of Dayton,2004.
- [6]Chu J P,Rigsbee J M,et al.Laser shock processing effects on surface microstructure and mechanical properties of low carbon steel[J].Materials Science andEngineering A,1999(260)260-268.
- [7]GB3075-82,金属轴向疲劳试验方法[S].国家标准局,1982.
- [8]美国金属学会.金属手册(第八版).断口金相与断口图谱(第九卷)[M].北京:机械工业出版社,1983.
文章评论(Comment):
|
||||||||||||||||||
|
||||||||||||||||||