| Citation: | Chen Lihua, Huang Kewen, Mi Jingchuan, et al. Finite element study on effect of fretting wear on crack initiation of dovetail[J]. Journal of Aerospace Power, 2026, 41(9):20250151 doi: 10.13224/j.cnki.jasp.20250151 |
The influence of fretting wear on crack initiation of dovetail joint structure was studied. The ball/plane finite element model was established, and the method of the fretting wear simulation and Smith-Watson-Topper (SWT) parameter calculation was given and verified by comparing with existing literature. A two-dimensional finite element analysis model of dovetail structure was established, and SWT parameter values of contact surface were calculated. It was found that fretting wear made stress distribution uniform and the SWT parameter values decline, so the risk of crack initiation was reduced. Because the wear on the upper edge was much greater than that on the lower edge, the location of SWT maximum value transferred from the upper edge of initial stage (no wear) to the lower edge, then, fretting wear made crack initiate on the lower edge. Considering fretting wear, the influences of friction coefficient, base angle and centrifugal force on SWT parameters of dovetail were discussed, and the fretting behavior between contact surfaces of dovetail structure was studied. The results showed that with the decrease of friction coefficient, the surface contact state changed from partial slip to complete slip, and the increase of surface wear resulted in the decline of SWT parameter. When the dovetail angle was 45°, the SWT parameters value was the smallest and the structure was the most reliable. With the enlargement of centrifugal force, the contact surface deformation and stress increased, so the SWT parameter could gradually augment.
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