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A new methodology for predicting crack initiation life for rolling contact fatigue based on dislocation and crack propagation

机译:基于位错和裂纹扩展的滚动接触疲劳裂纹萌生寿命预测新方法

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摘要

A new methodology for predicting crack initiation life is presented and validated experimentally. The methodology considers that the total fatigue life is the summation of crack initiation life and crack propagation life, since fatigue failures are due to crack initiation and crack propagation. It has been established that the crack propagation life can be estimated based on a modified Paris' law when the size of crack is larger than a certain value. However, there has been no verified method for estimating the crack initiation life with good accuracy. The proposed methodology for predicting the crack initiation life is based on a dislocation model, and the constants for the model are determined by the crack initiation lives obtained by a new approach. This new approach determines the crack initiation life by subtracting the predicted crack propagation life from the experimentally obtained total fatigue life. The developed crack initiation life model is combined with a crack propagation life model for the prediction of fatigue life. It is noted that the standard deviation in the ratios of experimental life to predicted life by the developed fatigue life model is only 14% of that by the International Standard.
机译:提出了一种预测裂纹萌生寿命的新方法,并进行了实验验证。该方法认为总疲劳寿命是裂纹萌生寿命和裂纹扩展寿命的总和,因为疲劳失效是由于裂纹萌生和裂纹扩展引起的。已经确定,当裂纹的尺寸大于一定值时,可以根据修改后的巴黎定律估算裂纹的扩展寿命。但是,还没有用于以良好的精度来估计裂纹萌生寿命的经验证的方法。所提出的预测裂纹萌生寿命的方法是基于位错模型,并且该模型的常数由通过新方法获得的裂纹萌生寿命来确定。这种新方法通过从实验获得的总疲劳寿命中减去预测的裂纹扩展寿命来确定裂纹的起始寿命。将开发的裂纹萌生寿命模型与裂纹扩展寿命模型相结合,以预测疲劳寿命。值得注意的是,通过开发的疲劳寿命模型得出的实验寿命与预测寿命之比的标准偏差仅为国际标准的14%。

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