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首页> 外文期刊>Journal of Failure Analysis and Prevention >Surface Integrity and Fatigue Behavior for High-Speed Milling Ti-10V-2Fe-3Al Titanium Alloy
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Surface Integrity and Fatigue Behavior for High-Speed Milling Ti-10V-2Fe-3Al Titanium Alloy

机译:高速铣削Ti-10V-2Fe-3Al钛合金的表面完整性和疲劳行为

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摘要

Influence of cutting parameters on surface integrity when milling Ti-10V-2Fe-3Al is investigated based on high-speed cutting experiments. Surface integrity measurements, fatigue fractography analysis, and fatigue life tests are conducted to reveal the effect of surface integrity on crack initiation and fatigue life. The results show that under given experiment conditions, surface roughness decreases linearly when increasing cutting speed or decreasing feed per tooth. The latter has a greater impact on surface roughness than the former. Compressive stress can be detected on all machined surfaces. With the increase of feed per tooth or cutting speed, respectively, residual stress presents a linear increase. Cutting parameters have no significant impact on micro-hardness. When the surface roughness ranges from 0.5 to 1.0 μm, the effect of surface residual stress on fatigue life is more than that of surface roughness. When the surface residual compressive stress increases, the fatigue life improves significantly. Compared with 60 m/min, when cutting speed is 100 or 140 m/min, the surface roughness decreases, the surface residual compressive stress increases, and the fatigue life improves by 124 and 59%, respectively. Under a tensile load, fatigue crack on machined surface of Ti-10V-2Fe-3Al titanium alloy originates at the cross-edge of the specimen surface. With the increase of surface roughness, the area ratio of fatigue crack propagation zone, and fatigue fracture zone decreases.
机译:基于高速切削实验,研究了切削参数对铣削Ti-10V-2Fe-3Al时表面完整性的影响。进行了表面完整性测量,疲劳断裂分析和疲劳寿命测试,以揭示表面完整性对裂纹萌生和疲劳寿命的影响。结果表明,在给定的实验条件下,当提高切削速度或降低每齿进给量时,表面粗糙度线性降低。后者对表面粗糙度的影响比前者大。可以在所有机加工表面上检测到压应力。随着每齿进给量的增加或切削速度的增加,残余应力呈线性增加。切削参数对显微硬度没有显着影响。当表面粗糙度在0.5至1.0μm的范围内时,表面残余应力对疲劳寿命的影响大于表面粗糙度。当表面残余压应力增加时,疲劳寿命显着提高。与60 m / min相比,当切削速度为100或140 m / min时,表面粗糙度降低,表面残余压应力增加,疲劳寿命分别提高124%和59%。在拉伸载荷下,Ti-10V-2Fe-3Al钛合金机加工表面的疲劳裂纹起源于试样表面的交叉边缘。随着表面粗糙度的增加,疲劳裂纹扩展区和疲劳断裂区的面积比减小。

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