Laser hardening technologies are widely used to modify the surface of steel
s. Generally, the contact fatigue life of laser hardened steels are still e
valuated by the conventional rolling, contact fatigue tests. However, it is
found that some cracks in fatigue testing may initiate from the boundary b
etween the hardened layer and the substrate. In this paper, the appropriate
ness of the conventional rolling contact fatigue testing method in the lase
r hardened steel test is evaluated. Experiments were done on a standard lin
e contact fatigue tester with contact loads of 1800-2600 Mpa and a rotation
al frequency of 2000 ipm. The location of crack initiation is examined by S
EM. It is found that the contact fatigue life of laser hardened steels is i
nfluenced by the depth of the hardened layer. Experimental results are comp
ared with theoretical calculation. The meaning of these results is discusse
d.