Effect of dissimilar metals on fretting fatigue behavior of Ti-6Al-4V

被引:25
作者
Hutson, Alisha [1 ]
Lee, Hyukjae
Mall, Shankar
机构
[1] Univ Dayton, Res Inst, Adv Mat Characterizat Grp, Struct Integ Div, Dayton, OH 45469 USA
[2] USAF, Inst Technol, Dept Aeronaut & Astronaut, ENY, Wright Patterson AFB, OH 45432 USA
关键词
fretting fatigue; titanium; aluminum; nickel-based superalloys; Hertzian contact; FEA;
D O I
10.1016/j.triboint.2006.02.008
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An investigation was conducted to explore fretting fatigue behavior of Ti-6Al-4V specimens in contact with pads of varying composition. Four conditions were selected to provide a range of compositions: Ti-6Al-4V (with two surface finishes), aluminum and nickel. Behavior against each pad condition was evaluated for two pad geometries (cylinder-on-flat, blended flat-on-flat) in two separate test fixtures. Experiments were conducted with varying applied fatigue stresses and contact forces. Applied clamping stresses for the flat-on-flat pads were similar to 200 and similar to 650 MPa. For the cylinder-on-flat geometry, forces were selected to provide Hertzian peak pressures of 292 and 441 MPa. The coefficient of friction, mu, was quantified and pad surfaces were characterized through hardness and composition evaluation. Finite element analyses of the test fixtures were conducted to assess variations in the stress fields. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1187 / 1196
页数:10
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