Author/Authors :
C. Feng، نويسنده , , Tahir I. Khan، نويسنده ,
Abstract :
The aerospace alloy, Ti–6Al–4V is a difficult
material to machine, and, in general, shows poor wear
resistance due to the soft, ductile properties of the alloy. In
this study, the Ti–6Al–4V alloy has been heat treated to a
temperature above and below the b-transus temperature
and then quenched using a medium of oil, water or liquid
nitrogen to change the surface wear behaviour of the alloy.
The results showed that no significant change in microstructure
and surface properties was achieved when the
alloy was heated to 750 C and then quenched in liquid
nitrogen. However, when the alloy was heated to 1,000 C
(above the b-transus), the hardness of the titanium alloy
significantly increased from 400 VHN to about 800 VHN,
but the wear resistance of the alloy did not improve. In fact,
the wear resistance of the alloy decreased as the surface
hardness increased, and this change in wear behaviour was
attributed to a change in the mechanism of wear from
plastic deformation to brittle-fracture of the surface.