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A fatigue life prediction method from magnetic pole material to simulation part

机译:磁极材料与仿真部件的疲劳寿命预测方法

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摘要

Due to the higher reliability needs of the large moving component motor-generator rotor, the assessment of the service life has drawn more and more attention. After finite element analysis of the rotor, the simulation part which can represent the magnetic pole with the most dangerous position of the rotor was designed to investigate the S-N curves. Compared with the conventional specimen, considering the main influencing factors of fatigue life for simulation part, the comprehensive factor was proposed to establish the fatigue life relationship between magnetic pole material and simulation part. It was found that the calculation method of fatigue notch factor based on the notch sensitivity factor is relatively simple and practical, and there is no significant effect of surface roughness on high and low cycle fatigues for low roughness (R-a is about 1 mu m), and the dimension factor changes linearly with the scale factor. Based on those results, a fatigue life prediction method was proposed and validated, and the predicted results were in good agreement with the experimental data. This study will provide a reasonable reference to determine the fatigue life prediction of large moving components.
机译:由于大型移动元件电动发电机转子的可靠性需求越高,服务寿命的评估越来越受到关注。在转子的有限元分析之后,设计具有转子最危险位置的磁极的模拟部分以研究S-N曲线。与传统标本相比,考虑到模拟部分疲劳寿命的主要影响因素,提出了综合因素来建立磁极材料与仿真部件之间的疲劳寿命关系。结果发现,基于凹口敏感性因子的疲劳缺口因子的计算方法是相对简单实用的,并且表面粗糙度对低粗糙度(Ra约1μm)的表面粗糙度没有显着影响,尺寸因子与比例因子线性变化。基于这些结果,提出和验证了疲劳寿命预测方法,预测结果与实验数据吻合良好。该研究将提供合理的参考,以确定大型移动部件的疲劳寿命预测。

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