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

机译:带缺口的Ti-6Al-4V钛棒的单轴和多轴疲劳裂纹萌生寿命:基于平均应变能密度方法的合成

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摘要

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 of the titanium alloy, 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 alloweds 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.
机译:分析了由钛合金Ti-6Al-4V制成的周向缺口试样的疲劳行为。为了研究缺口对钛合金疲劳强度的影响,已经对以两个不同的根半径(即0.1和4 mm)为特征的试样进行了纯弯曲,纯扭转和多轴弯曲-扭转疲劳测试。通过使用直流电势降(DCPD)技术,可以准确地监测裂纹成核和随后的扩展。基于从电位下降技术获得的结果,对应于相对电位下降增加V/V0等于1%定义了裂纹萌生寿命,并将其用作破坏准则。这样做,有望减小在裂纹扩展阶段运行的外部机制(例如,滑动接触,摩擦和断裂表面之间的啮合)的影响。通过使用在半径为R0且环绕着缺口尖端的结构体积上平均的局部应变能密度(SED),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可以使我们适当地关联Ti-6Al-4V缺口试样的裂纹萌生寿命,尽管试验中涉及不同的缺口几何形状和载荷条件。

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