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Effect of dissimilar metals on fretting fatigue behavior of Ti–6Al–4V
Authors:Alisha Hutson   Hyukjae Lee  Shankar Mall
Affiliation:aAdvanced Materials Characterization Group, Structural Integrity Division, University of Dayton Research Institute, Dayton, OH 45469-0128, USA;bDepartment of Aeronautics & Astronautics, Air Force Institute of Technology (AFIT/ENY), Wright-Patterson Air Force Base, OH 45433-7765, USA
Abstract: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 not, vert, similar200 and not, vert, similar650 MPa. For the cylinder-on-flat geometry, forces were selected to provide Hertzian peak pressures of 292 and 441 MPa. The coefficient of friction, μ, 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.
Keywords:Fretting fatigue   Titanium   Aluminum   Nickel-based superalloys   Hertzian contact   FEA
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