粉末合金(FGH95)蠕变/疲劳交互作用下寿命预测的损伤力学有限元分析
The Finite Element Analysis of HLCF Life Prediction for PM FGH95 Based on Damage Mechanics
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摘要: 采用基于损伤力学的蠕变—疲劳交互作用下的寿命预测模型,应用损伤等效应力进行三维应力状态下的损伤计算,并考虑了压缩时闭合效应,利用ANSYS的二次开发工具APDL和UPFs开发程序,把基于损伤力学的寿命预测方法与ANSYS的结构分析结合起来,实现了对构件的损伤计算和寿命预测。针对粉末合金材料易含夹杂等初始缺陷的特点,提出了在寿命计算中通过单元初始损伤模拟初始缺陷对寿命影响的处理方法,探讨了考虑初始缺陷条件下的寿命预测,并利用试验对计算结果进行了对比验证。Abstract: In this paper,based on the theory of damage mechanics, using damage equivalent stress to calculate the damage under 3 D stress status and taking the close effect into account,a subroutine to calculate damage and predict fatigue life on ANSYS platform was developed by APDL and UPFs of ANSYS.The initiation and growth of cracks are simulated by damage developing.The effect of damage on material properties has been taken into considerations by two ways,one is the method of stiffness matrix modification,the other is the effective stress method.The comparison between fatigue test and calculation results indicates that this method is right and feasible,and high accuracy can be obtained when there are no initial defects in PM components.Concerning components with initial defects,a method to simplify the initial defects by means of initial damage was put forward,and was used to evaluate the life of a specimen with initial defects.The method developed in this paper can be used to predict the life of PM components accurately as long as its initial damage has been obtained in relation to its initial status exactly.If the distribution probability of initial damage is known,the reliability design and evaluation of PM components can be carried out by this method.
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Key words:
- aerospace propulsion /
- powder metallurgy /
- creep /
- fatigue /
- damage mechanics /
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