This work is concerned with the surface treatment lion nitriding) of fretti
ng fatigue and fatigue resistance of 34CrNiMo6. Tests are made on a servo-h
ydraulic machine under tension for both treated and non-treated specimens.
The test parameters involve the applied displacements delta +/- 80-+/-170 m
um; fretting pressure sigma (n) = 1000-1400 MPa; fatigue stress amplitude s
igma (a) = 380-680 MPa and stress ratio R = -1. The ion nitriding process i
mproves both fatigue and fretting fatigue lives. Subsurface crack initiatio
n from internal discontinuities was found for ion-nitrided specimens. (C) 2
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