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Figure 20 shows the micromorphology of the fretting damage contact region of Ti6Al4V FF specimens with different modifications. As can be seen from Figure 20a, during the initiation progress (I stage), cracks propagated in a bank angle with a specimen surface. As the crack length increased, the crack propagation direction tended to be normal to the extra alternating fatigue stress (that is, in a direction normal to the specimen surface). The test results indicate that the value of the bank angle and the depth of the crack are related to the material properties, fretting slipping status, contact stress, friction force, surface modification state, extra alternating stress status and so on [6,8,14]. As can be seen from Figure 20b, the FF crack of the ZrN specimen propagated normally to the specimen surface (or extra alternating fatigue force). No crack propagation existed in the first stage in the bank direction as titanium alloy. This occurs because it is difficult to form slip plastic deformation with effects of multi-axis stress in the fretting contact region, and fatigue cracks initiate and propagate depending on the effect of primary stress in the ZrN layer with high hardness and low ductility. It can also be seen from Figure 20b that secondary brittle fatigue cracks exist in the fretting contact region of the ZrN specimen. Its direction is the same as the normal direction of the extra alternating force. As can be seen from Figure 20c, although microcracks exist parallel to the ZrN+SP specimen surface, these cracks do not all develop to propagate in the depth direction of the FF specimen. Thus, fractures do not lie in the fretting contact region but in the edge corner with a higher stress concentration existing outside the fretting contact region. The failure mechanism of the ZrN+SP specimen is a plain fatigue fracture. 2b1af7f3a8