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The Effects of Machining-induced Surface Topography on Fatigue Performance of Titanium Alloy Ti-6Al-4V

机译:机加工表面形貌对钛合金Ti-6Al-4V疲劳性能的影响

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摘要

Machining-induced surface integrity has an important effect on reliability and service life of the components used in the aerospace industry where titanium alloy Ti-6Al-4V is widely applied. Characterization of machining-induced surface integrity and reveal its effect on fatigue life are conducive to structural fatigue life optimization design. In the present study, surface topography was characterized in peripheral milling of titanium alloy Ti-6Al-4V. And then, low cycle fatigue performances of machined specimens were studied on the basis of the tension-tension tests. Finally, the regular pattern of influence on fatigue performances by cutting process parameters was discussed. Conclus ions were drawn that three-dimensional surface roughness parameters showed almost the same trend as two-dimensional ones under different cutting conditions, while fatigue life models based on surface stress concentration factor that calculated using three-dimensional surface roughness parameters are more accurate than that using two-dimensional ones. Through sensitivity analysis, it can be found that feed rate was the key factor to affect the fatigue life, followed by cutting speed and depth of cut, respectively.
机译:机加工引起的表面完整性对于广泛应用钛合金Ti-6Al-4V的航空航天业中使用的组件的可靠性和使用寿命具有重要影响。表征加工引起的表面完整性并揭示其对疲劳寿命的影响有利于结构疲劳寿命的优化设计。在本研究中,在钛合金Ti-6Al-4V的外围铣削中表征了表面形貌。然后,在拉伸试验的基础上研究了机加工样品的低周疲劳性能。最后,讨论了切削参数对疲劳性能的影响规律。得出的结论是,在不同切削条件下,三维表面粗糙度参数与二维参数几乎呈现出相同的趋势,而基于三维表面粗糙度参数计算的基于表面应力集中因子的疲劳寿命模型比二维模型更准确。使用二维的。通过敏感性分析,可以发现进给速度是影响疲劳寿命的关键因素,其次是切削速度和切削深度。

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