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METHOD FOR PREDICTING FATIGUE LIFE OF GEOMETRICALLY DISCONTINUOUS STRUCTURE

机译:预测几何不连续结构的疲劳寿命的方法

摘要

A method for predicting the fatigue life of a geometrically discontinuous structure, comprising the steps of: establishing a geometrically continuous first finite element model, defining a crystal plasticity constitutive equation, thereby obtaining a stress-strain relationship of a material under a given cyclic loading condition (S1); carrying out a uniaxial tensile test and a uniaxial fatigue test to obtain a tensile curve and a hysteresis loop (S2); obtaining the tensile curve and hysteresis loop by means of test parameter fitting, and acquiring material parameters and a critical value of fatigue plastic slip required by the crystal plasticity constitutive equation (S3); establishing a second finite element model of the geometrically discontinuous structure, and acquiring a stress-strain relationship of each cycle and a single-cycle fatigue plastic slip value (S4); and calculating the crack initiation life of a notched specimen (S5). The method for predicting the fatigue life of the geometrically discontinuous structure may better achieve the fatigue analysis of the geometrically discontinuous structure at different temperatures, and may also accurately predict the location of crack initiation. The method has the advantages of intuitiveness, strong applicability and high accuracy.
机译:一种方法,用于预测几何不连续结构的疲劳寿命,包括步骤:建立几何连续的第一有限元模型,限定晶体塑性本构方程,从而在给定的循环负载条件下获得材料的应力 - 应变关系(S1);进行单轴拉伸试验和单轴疲劳试验,得到拉伸曲线和滞后回路(S2);通过测试参数配件获得拉伸曲线和滞后回路,并获取材料参数和晶体塑性本构方程所需的疲劳塑料滑动的临界值(S3);建立几何不连续结构的第二有限元模型,获取每个循环的应力 - 应变关系和单循环疲劳塑性滑动值(S4);并计算缺口样本的裂纹起始寿命(S5)。用于预测几何不连续结构的疲劳寿命的方法可以更好地实现不同温度下几何不连续结构的疲劳分析,并且还可以精确地预测裂纹引发的位置。该方法具有直观,适用性和高精度的优点。

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