High Cycle Fatigue Performance in Laser Shock Peened TC4 Titanium Alloys Subjected to Foreign Object Damage

被引:46
作者
Luo, Sihai [1 ]
Nie, Xiangfan [1 ]
Zhou, Liucheng [1 ]
Li, Yiming [1 ]
He, Weifeng [1 ,2 ]
机构
[1] Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, 1st Baling Rd, Xian 710038, Shaanxi, Peoples R China
[2] Xi An Jiao Tong Univ, Inst Aeronaut Engine, Sch Mech Engn, Xian 710049, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
fatigue strength; foreign object damage; laser shock peening; residual stress; TC4 titanium alloy; CRACK GROWTH-PROPERTIES; 6061-T6; ALUMINUM-ALLOY; RESIDUAL-STRESSES; TI-6AL-4V; TEMPERATURES; PREDICTION; INITIATION; AEROFOIL; BLADES;
D O I
10.1007/s11665-018-3172-6
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
During their service, titanium alloys are likely to suffer from the foreign object damage (FOD), resulting in a decrease in their fatigue strength. Laser shock peening (LSP) has been proved to effectively increase the damage tolerance of military engine components by introducing a magnitude compressive residual stress in the near-surface layer of alloys. In this paper, smooth specimens of a TC4 titanium alloy were used and treated by LSP and subsequently exposed to FOD, which was simulated by firing a steel sphere with a nominal velocity of 300 m/s, at 90A degrees with the leading edge of the LSP-treated region using a light gas gun. All impacted specimens were then subjected to fatigue loading. The results showed that LSP could effectively improve the fatigue strength of the damaged specimens. The effect of LSP on the fatigue strength was assessed through fracture observations, microhardness tests and residual stress analyses. The residual stresses due to the plastic deformation caused by LSP and the FOD impact, which were found to play a crucial role on the fatigue strength, were determined using the commercial software ABAQUS.
引用
收藏
页码:1466 / 1474
页数:9
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