Sliding wear of composite DLC coatings deposited on two types of alumi
nium substrates, 2618 alloy and 6063 aluminium extrusion, with differe
nt surface finishes have been investigated. A transition load was usua
lly observed, above which the whole coating layer was completely scrap
ed off the wear surface within a short sliding time/distance. The tran
sition load for coatings on polished substrate surfaces was significan
tly lower than that on the rougher machined substrate surfaces. Wear m
echanisms varied with substrate surface finish and load. Close to the
transition load, the dominant mechanism for failure of coatings on pol
ished substrates was fragmentation and spallation in a large scale wit
h the nature of fatigue. However, for coatings on relatively rough sub
strate surfaces, the coating was first fractured/fragmented and then t
he comminuted coating fragments and wear debris particles were mechani
cally mixed into the substrate to develop a mechanically alloyed wear-
protective layer on the wear surface. The higher transition loads for
coatings on the rougher substrate surface compared with those on the p
olished substrate surface mainly resulted from the development of such
mechanically alloyed layers on the wear surface. A physical model des
cribing wear processes during the sliding wear of hard coatings deposi
ted on a soft substrate with a rough initial surface finish has been d
eveloped which can explain the observed experimental results. (C) 1997
Elsevier Science S.A.