Force Controlled Low Cycle Fatigue (LCF) Life Evaluation Methodology Based on Unstabilized Material Properties

I. Men'
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Abstract

Low Cycle Fatigue (LCF) is a prominent failure mechanism in many design components; therefore, an evaluation of cycles to failure in this regime is of high importance. Most international standards recommend a closed loop strain-controlled mode specimen testing in this regime. However, the ꜪN data obtained from this test is not suitable for life evaluation of parts enduring force-controlled history during actual service without correction for control mode. Many existing procedures, which accounts for cyclic strain stabilization during force-controlled loading may significantly complicate the finite elements analysis (FEA) at solving or post processing stages and are often an inherent source of uncertainty. A heuristic, cost effective and sufficiently accurate approach for LCF life estimation is advocated. The method involves only two force loading FEA simulations, one of the actual parts and the other of the test specimen, using initial unstabilized stress strain curve, followed by a limited number of force-controlled specimens testing. Actual part and specimen life correlation performed using first loading unstabilized equivalent plastic strain value Ꜫp1 under locality and similitude assumptions. Unstabilized strain vs. number of cycles to failure curve Ꜫp1N is constructed and discussion regarding specimen geometry considerations for providing sufficient accuracy is included. Method validation and crack propagation study are provided.
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基于不稳定材料性能的力控低周疲劳寿命评价方法
低周疲劳(LCF)是许多设计构件的主要失效机制;因此,在这种情况下,对循环到失效的评估是非常重要的。大多数国际标准建议在这种情况下采用闭环应变控制模式试样试验。但是,在没有对控制方式进行校正的情况下,从该试验中获得的ꜪN数据不适用于实际使用中承受力控历史的部件的寿命评估。在力控制加载过程中,考虑循环应变稳定的许多现有程序可能会使有限元分析(FEA)在求解或后处理阶段变得非常复杂,并且通常是不确定性的固有来源。提出了一种启发式的、具有成本效益的、足够精确的LCF寿命估计方法。该方法采用初始非稳定应力应变曲线,对实际零件和试件进行两次力加载有限元模拟,然后进行有限数量的力控制试件试验。在局部和相似假设下,使用首次加载非稳定等效塑性应变值Ꜫp1进行实际零件和试样寿命相关性。构建了不稳定应变与循环次数到失效曲线Ꜫp1N,并讨论了提供足够精度的试样几何考虑因素。提供了方法验证和裂纹扩展研究。
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