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| Effect of Laser Shock Peening on Fretting Wear Behavior of TB6 Titanium Alloy |
| ZHANG Hao1 , SUN Zhiqiang2 , CAO Ziwen3 , LI Zhiqiang3 , ZHOU Wenlong1 , FU Xuesong1 |
| (1. Dalian University of Technology, Dalian 116024, China; 2. Beijing Aerospace Petrochemical Technology & Equipment Engineering Co., Ltd., Beijing 100176, China; 3. Science and Technology on Power Beam Processes Laboratory, AVIC Manufacturing Technology Institute, Beijing 100024, China) |
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Abstract The fretting wear behavior of TB6 titanium alloy before and after laser shock peening (LSP) was studied. The influence of displacement amplitude on friction coefficient and wear mechanism was analyzed. The surface integrity, friction morphology and wear volume of the original sample and the sample after LSP treatment were analyzed by X–ray diffraction, microhardness, laser confocal microscopy and scanning electron microscopy. The results show that after LSP treatment, the surface roughness (Ra) of TB6 increases from 0.203μm to 0.321μm. The surface microhardness increases from 322HV to 400HV. The residual compressive stress layer is introduced into the surface layer, and the maximum residual stress reaches –650MPa. In the fretting friction process, when the displacement amplitude is small (≤50μm), the adhesion appears on the friction surface of the sample, and the adhesion degree and friction coefficient increase after LSP. When the displacement amplitude is larger (≥75μm), pits appear on the friction surface of the sample. After LSP, the slope of the pits decreases, the friction coefficient and wear volume decrease, and the fatigue wear and abrasive wear are alleviated, which is helpful to improve the wear resistance of the material.
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2021, 
