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Adhesive wear of a Ti6Al4V tribopair for a fast friction contact

Friction tests at high sliding velocity are carried out by subjecting specimens to an apparent normal pressure of 110MPa in the range of 40–64m/s to reproduce severe conditions of contact between the rotating blades and the rotor in aircraft engines. Therefore, impacts of a projectile against a fixe...

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Bibliographic Details
Published in:Wear 2014-12, Vol.320, p.25-33
Main Authors: Chassaing, G., Faure, L., Philippon, S., Coulibaly, M., Tidu, A., Chevrier, P., Meriaux, J.
Format: Article
Language:English
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Summary:Friction tests at high sliding velocity are carried out by subjecting specimens to an apparent normal pressure of 110MPa in the range of 40–64m/s to reproduce severe conditions of contact between the rotating blades and the rotor in aircraft engines. Therefore, impacts of a projectile against a fixed sample are carried out for the investigation of a pair of Ti6Al4V materials. A mean coefficient of friction has been ascertained by two types of method: a tribometer device and an energetic approach. A slight sensitivity of the coefficient of friction with respect to the sliding velocity is observed. Postmortem analyses of samples reveal a decomposition of the frictional subsurface in multiple distinct layers: initial microstructure, severe plastic deformation (shear strain up to 16), phase transformation (T>980°C) and material transfer. A scenario of the adhesive wear mechanism is proposed in four steps. •Dry friction generated by a projectile impact against a couple of samples in titanium alloy in rest.•Sliding velocities ranging from 40m/s to 64m/s under an apparent normal pressure of 110MPa.•Analyses of the material microstructure: confirmation of a decomposition into sub-layers.•Adhesive wear rate depending on the sliding duration.
ISSN:0043-1648
1873-2577
DOI:10.1016/j.wear.2014.08.001