Abstract
TA15 (Ti–6Al–2Zr–1Mo–1V) titanium alloy is an important new aeronautical material. The research on the Ni60–TiC–Mo laser cladded composite coating on TA15 alloy is novelty, which provided the essential experimental and theoretical basis to promote the applications of the laser cladding technique in reinforcing and repairing the aerospace parts. The proper selection of the cladding process parameters allowed us to get the composite coating with a metallurgical combination to TA15 substrate. SEM and TEM test results indicated that a number of the interdendritic lamellar eutectics and the amorphous phases were produced in the composite coating. Compared with the TA15 substrate, an improvement of the wear resistance was observed for this composite coating.
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