The Finite Element Analysis of HLCF Life Prediction for PM FGH95 Based on Damage Mechanics
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The Finite Element Analysis of HLCF Life Prediction for PM FGH95 Based on Damage Mechanics
Vol. 18, Issue 1, (2003)
作者机构:
1. 北京航空航天大学动力系,北京,100083
2. 中国运载火箭技术研究院航天发射技术研究所,北京,100076
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Published:2003
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LIU Xiang-xin, ZHANG Xue-ren, YAN Xiao-jun, et al. The Finite Element Analysis of HLCF Life Prediction for PM FGH95 Based on Damage Mechanics[J]. 2003, 18(1).
DOI:
LIU Xiang-xin, ZHANG Xue-ren, YAN Xiao-jun, et al. The Finite Element Analysis of HLCF Life Prediction for PM FGH95 Based on Damage Mechanics[J]. 2003, 18(1).DOI:
The Finite Element Analysis of HLCF Life Prediction for PM FGH95 Based on 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.