基于临界面法的多轴低周疲劳损伤参量
Multiaxial Damage Parameter Based on Critical Plane Approach for Low Cycle Fatigue
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摘要: 为了更简便地预测多轴低周疲劳寿命,通过分析裂纹扩展特点和最大剪应变面上的最大剪应变和相应的法向应变变化特点,提出以最大剪应变平面作为损伤临界平面,将最大剪应变和相应的法向应变作为基本的多轴疲劳损伤参数,建立了基于临界面法的多轴低周疲劳损伤参量.对GH4169合金和45#钢的寿命预测结果表明,该损伤模型误差基本在2个因子之内.Abstract: To predict life of multiaxial low cycle fatigue more conveniently,a multiaxial low cycle fatigue damage parameter is proposed based on the crack extension characteristics and changes of the maximum shear strain and the corresponding normal strain on the maximum shear stain plane and the maximum shear strain plane is considered as the critical plane.The maximum shear strain and corresponding normal strain are selected as the basic damage parameters for low fatigue.The life prediction is proceeded by using the model with GH4169 alloy and 45 steel.The results showed that the error between life prediction and experimental results is basically within 2 factors.