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Machining for an increased fatigue life for a Ti-6A1-4V ELI component

机译:加工Ti-6A1-4V ELI组分增加的疲劳寿命

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Fatigue life is an important design criterion for many structural parts.The surface integrity induced by a typical machining operation may have a marked effect on fatigue life.Literature evidence suggests that the compressive surface residual stress state may change appreciably from the state obtained at the recommended conventional cutting speeds when intermediate cutting speeds are utilized.Titanium alloys typically show an increased compressive residual stress state at intermediate speeds before eventually tending towards tensile stresses at elevated cutting speeds.This paper investigates the effect of an optimised cutting strategy to control the residual stress state of a machined Ti-6A1-4V ELI(extra low interstitial)component to thereby control the fatigue life.An experimental program is conducted whereby stepped shafts are machined at various cutting speeds before being subjected to a full cyclic in-plane bending moment fatigue test.Cutting speed is varied between the typically recommended speed of 40 m/min to an intermediate speed of 110 m/min.Residual stresses are measured by XRD and compared to the fatigue life achieved.Other surface integrity descriptors including surface roughness,sub surface microstructure and selected surface damage effects are presented and discussed in relation to the fatigue performance.In essence the paper reports that fatigue life can be improved by machining at the optimum cutting speeds.These optimum intermediate speeds do however introduce other less desirable effects such as an increase in surface damage including the presence of weldments and ploughing grooves that may have a negative effect on the reliability of the improvements obtained.
机译:疲劳寿命是许多结构部件的重要设计标准。由典型的加工操作引起的表面完整性可能对疲劳寿命具有显着的影响.Liritorign证据表明,压缩表面残余应力状态可能会从推荐的状态下获得的状态变得明显变化当使用中间切割速度时,常规切割速度。硝酸钛合金通常在高温切削速度下朝向拉伸应力倾斜之前在中间速度下显示增加的压缩残余应力状态。本文研究了优化的切削策略控制残余应力状态的效果由此加工的Ti-6A1-4V ELI(超低间隙)组分,从而控制疲劳寿命。在进行阶梯式轴的情况下进行实验程序,然后在各种切割速度下进行加工,然后进行全循环面内弯曲力矩疲劳试验。典型速度在典型r之间变化40 m / min的eMommenceed速度为110米/分钟的中间速度。通过XRD测量抗敏感应力,并与达到的疲劳寿命相比。提供包括表面粗糙度,子表面微观结构和所选表面损伤效果的其他表面完整性描述符和选择关于疲劳性能的讨论。本文本文通过以最佳的切削速度加工可以通过加工改善疲劳寿命。然而,可以通过加工改善疲劳寿命,但是引入了其他不太理想的效果,例如包括焊件的存在的表面损坏的增加和犁槽可以对所获得的改进的可靠性产生负面影响。

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