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Comparisons of low cycle fatigue behavior of CP-Ti under stress and strain-controlled modes in transverse direction

机译:CP-Ti在横向应力和应变控制模式下的低周疲劳行为比较

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Low cycle fatigue (LCF) behavior of CP-Ti along transverse direction under symmetrical strain and stress-controlled modes was compared systematically. For the strain-controlled tests, tension-compression asymmetry (TCA) has little effect on LCF behavior due to the negligible compressive mean stress. For the stress-controlled tests, TCA is detrimental to LCF resistance. The microstructure evolution during cycling deformation was characterized by EBSD and TEM to identify different deformation mechanisms. It was found that strain cycling deformation was dominated by dislocation slip and exhibited the transition from planar slip to wavy slip with the increase of strain amplitude. For the stress-controlled tests, tensile twinning together with dislocation slip accommodated the increased ratcheting deformation. The strain-life curve under stress-controlled tests is lower than that at strain-controlled tests due to the heterogeneous plastic deformation caused by ratcheting deformation. In order to obtain a unified fatigue life prediction model for different control modes, a novel effective strain range related model was proposed by introducing the TCA factor into the original Manson-Coffin relation. Furthermore, the application of this effective strain range related model was extended to the condition of asymmetrical stress cycling by correcting fatigue ductility coefficient and exponent.
机译:系统地比较了对称应变和应力控制模式下CP-Ti沿横向的低周疲劳(LCF)行为。对于应变控制测试,由于可压缩的平均应力可忽略,因此拉伸-压缩不对称(TCA)对LCF行为的影响很小。对于应力控制测试,TCA不利于LCF抵抗。用EBSD和TEM表征了循环变形过程中的微观结构演变,以识别不同的变形机理。发现应变循环变形以位错滑移为主,并随着应变幅度的增加而呈现出从平面滑移到波浪滑移的转变。对于应力控制试验,拉伸孪晶与位错滑移共同适应了棘轮变形的增加。由于棘齿形变引起的非均匀塑性变形,应力控制试验的应变寿命曲线低于应变控制试验的寿命。为了获得针对不同控制模式的统一疲劳寿命预测模型,通过将TCA因子引入原始Manson-Coffin关系中,提出了一种新颖的有效应变范围相关模型。此外,通过校正疲劳延性系数和指数,将该有效应变范围相关模型的应用扩展到不对称应力循环的条件。

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