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低周载荷对高周裂纹裂尖塑性区的影响
引用本文:刘华伟,王荣桥,胡殿印.低周载荷对高周裂纹裂尖塑性区的影响[J].航空动力学报,2016,31(10):2339-2345.
作者姓名:刘华伟  王荣桥  胡殿印
作者单位:1. 北京航空航天大学 能源与动力工程学院, 北京 100191;
基金项目:国家自然科学基金(51305012,51375031);北京市科技专项(Z151100001615066)
摘    要:为探明高低周复合疲劳裂纹扩展中高低周载荷交互作用机理,采用弹塑性有限元模型模拟了含中心裂纹试件在高低周载荷交互作用下裂尖塑性区的变化.结果表明:低周载荷的卸载作用导致高周载荷对应的裂尖反向塑性区明显减小,裂纹闭合水平也因此降低,进而加速裂纹扩展,致使高低周复合疲劳裂纹扩展寿命降低.在此基础上,对比研究了低周载荷应力比、高周载荷应力比、高低周载荷循环比对裂尖反向塑性区的影响.结果表明:随着低周载荷应力比降低、高周载荷应力比增加,循环比的减少,均导致低周载荷的卸载作用增加. 

关 键 词:高周疲劳    低周疲劳    高低周复合疲劳    反向塑性区    疲劳裂纹
收稿时间:2015/1/23 0:00:00

Effect of low cycle fatigue loading on the crack tip plastic zone of high cycle fatigue crack
LIU Hua-wei,WANG Rong-qiao and HU Dian-yin.Effect of low cycle fatigue loading on the crack tip plastic zone of high cycle fatigue crack[J].Journal of Aerospace Power,2016,31(10):2339-2345.
Authors:LIU Hua-wei  WANG Rong-qiao and HU Dian-yin
Institution:1. School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;2. Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;3. Team of Aero-engine Structure Integrity and Reliability, Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China
Abstract:To ascertain the loading interaction mechanism of the crack growth under high and low combined cycle fatigue loading, the elastic-plastic finite element numerical simulation method was used to determine the plastic zone of crack tip of the specimens with center crack under high and low combined cycle fatigue loading. It was proven that the unloading of low cycle fatigue loading contributed to the reduction of reversed plastic zone of crack tip corresponding to high cycle fatigue loading. This resulted in the decrease of crack closure level and the increase of crack growth rate, as well as the reduction of crack growth life under high and low combined cycle fatigue loading. The effects of the stress ratio of low cycle fatigue loading, the stress ratio of high cycle fatigue loading, the high cycle fatigue loading number per low cycle fatigue loading on the reversed plastic zone of crack tip were also investigated in contrast. The unloading of low cycle fatigue loading gradually increased along with the decrease of low cycle fatigue loading stress ratios, the increase of high cycle fatigue loading stress ratios, and the decrease of high cycle fatigue loading numbers per low cycle fatigue loading.
Keywords:high cycle fatigue  low cycle fatigue  high and low combined cycle fatigue  reversed plastic zone  fatigue crack
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