Crack initiation life in notched Ti-6Al-4V titanium bars under uniaxial and multiaxial fatigue: synthesis based on the averaged strain energy density approach

G. Meneghetti, A. Campagnolo, F. Berto, Keisuke Tanaka
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引用次数: 5

Abstract

The fatigue behaviour of circumferentially notched specimens made of titanium alloy, Ti-6Al-4V, has been analysed. To investigate the notch effect on the fatigue strength, pure bending, pure torsion and multiaxial bending-torsion fatigue tests have been carried out on specimens characterized by two different root radii, namely 0.1 and 4 mm. Crack nucleation and subsequent propagation have been accurately monitored by using the direct current potential drop (DCPD) technique. Based on the results obtained from the potential drop technique, the crack initiation life has been defined in correspondence of a relative potential drop increase ?V/?V0 equal to 1%, and it has been used as failure criterion. Doing so, the effect of extrinsic mechanisms operating during crack propagation phase, such as sliding contact, friction and meshing between fracture surfaces, is expected to be reduced. The experimental fatigue test results have been re-analysed by using the local strain energy density (SED) averaged over a structural volume having radius R0 and surrounding the notch tip. Finally, the use of the local strain energy density parameter allowed us to properly correlate the crack initiation life of Ti-6Al-4V notched specimens, despite the different notch geometries and loading conditions involved in the tests.
缺口Ti-6Al-4V钛棒在单轴和多轴疲劳下的裂纹起裂寿命:基于平均应变能密度法的综合
对Ti-6Al-4V钛合金周向缺口试样的疲劳性能进行了分析。为了研究缺口对疲劳强度的影响,对0.1和4mm两种不同根半径的试件进行了纯弯曲、纯扭转和多轴弯曲-扭转疲劳试验。利用直流电位降(DCPD)技术对裂纹的形核和扩展过程进行了精确的监测。基于势滴技术的结果,定义了裂纹起裂寿命,对应于相对势滴增加V/?V0 = 1%,作为失效判据。这样,在裂纹扩展阶段运行的外部机制的影响,如破裂面之间的滑动接触、摩擦和啮合,有望减少。通过对缺口尖端周围半径为R0的结构体的局部应变能密度(SED)进行平均,对实验疲劳测试结果进行了重新分析。最后,使用局部应变能密度参数使我们能够正确地关联Ti-6Al-4V缺口试样的裂纹起裂寿命,尽管试验中涉及不同的缺口几何形状和加载条件。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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