王肇喜, 白金, 王海东, 仇原鹰, 李静. 临界平面多轴疲劳寿命估算模型的验证与评估[J]. 失效分析与预防, 2020, 15(6): 343-348. DOI: 10.3969/j.issn.1673-6214.2020.06.001
    引用本文: 王肇喜, 白金, 王海东, 仇原鹰, 李静. 临界平面多轴疲劳寿命估算模型的验证与评估[J]. 失效分析与预防, 2020, 15(6): 343-348. DOI: 10.3969/j.issn.1673-6214.2020.06.001
    WANG Zhao-xi, BAI Jin, WANG Hai-dong, QIU Yuan-ying, LI Jing. Verification and Evaluation of Critical Plane-based Multiaxial Fatigue Life Prediction Models[J]. Failure Analysis and Prevention, 2020, 15(6): 343-348. DOI: 10.3969/j.issn.1673-6214.2020.06.001
    Citation: WANG Zhao-xi, BAI Jin, WANG Hai-dong, QIU Yuan-ying, LI Jing. Verification and Evaluation of Critical Plane-based Multiaxial Fatigue Life Prediction Models[J]. Failure Analysis and Prevention, 2020, 15(6): 343-348. DOI: 10.3969/j.issn.1673-6214.2020.06.001

    临界平面多轴疲劳寿命估算模型的验证与评估

    Verification and Evaluation of Critical Plane-based Multiaxial Fatigue Life Prediction Models

    • 摘要: 利用5种材料对比分析6种常用多轴疲劳寿命临界平面模型的寿命估算结果,结果发现:对于同一对象、不同模型的估算结果相差较大;而对于不同对象、同一模型的估算结果,有时低于试验结果,有时却高于试验结果。不同寿命预测模型估算寿命合理与否,一方面取决于预测模型中的疲劳损伤参量是否有效,另一方面也取决于预测模型的表达形式是否合理。另外,模型的预测结果还与材料的开裂形式有关。Fatemi-Socie模型可以针对剪切型开裂材料给出较为理想的疲劳寿命预测结果。针对验证结果,对各模型的适用性进行评述,指出常用临界平面模型的适用条件尚需进一步研究,模型中损伤参量包含的系数的物理意义及系数与应力-应变状态和材料属性的关系也需进一步研究。

       

      Abstract: The multiaxial fatigue lives predicted by six critical models were compared by using five kinds of materials. It is found that for the same material significantly different results may be obtained by the different models. Furthermore, for different materials the predictions from the same model may be lower or higher than the test results. The validity of life prediction of different models not only depends on the validity of fatigue damage parameters for the prediction models but also the rationality of the expression of the prediction models. Besides, the validity of the models is also related to the cracking mode of the materials. Generally speaking, the Fatemi-Socie model can give reasonable fatigue life predictions for shear-typed cracking materials. Based on the verification results, the applicability of the considered fatigue life prediction models is overviewed. Then it is pointed out that the applicable conditions of conven-tional critical plane models need to be further studied. And the physical meaning of the coefficients in the damage parameters and the relationship among the coefficients, the stress-strain state and the material characteristics need to be further studied as well.

       

    /

    返回文章
    返回