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多轴载荷下缺口件的疲劳寿命估算方法
引用本文:吴志荣, 胡绪腾, 宋迎东. 多轴载荷下缺口件的疲劳寿命估算方法[J]. 工程力学, 2014, 31(10): 216-221. DOI: 10.6052/j.issn.1000-4750.2013.04.0360
作者姓名:吴志荣  胡绪腾  宋迎东
作者单位:1.南京航空航天大学能源与动力学院,南京 210016;;2.南京航空航天大学机械结构力学及控制国家重点实验室,南京 210016
基金项目:国防基础科研项目(B2520110003)
摘    要:
提出了一种多轴载荷下缺口件的疲劳寿命估算方法。该方法基于临界平面理论,计算出缺口件各部位的多轴疲劳损伤参数,以损伤参数最大的部位为缺口件的多轴疲劳危险点。根据临界距离思想,提出了热点法和线法的临界距离的计算方法,采用热点法和线法考虑缺口件疲劳危险点附近损伤梯度的影响,以临界距离修正的损伤参数计算多轴载荷下缺口件的疲劳寿命。采用SAE1045钢缺口件的多轴疲劳试验对该文提出的寿命估算方法进行评估和验证,结果表明:该文所建立的寿命预测方法具有较好的预测能力,预测结果大部分分布在试验结果的3倍分散带之内。

关 键 词:寿命预测  多轴疲劳  缺口疲劳  疲劳危险点  临界距离
收稿时间:2013-04-22
修稿时间:2013-06-07

ESTIMATION METHOD FOR FATIGUE LIFE OF NOTCHED SPECIMEN UNDER MULTI-AXIAL LOADING
WU Zhi-rong, HU Xu-teng, SONG Ying-dong. ESTIMATION METHOD FOR FATIGUE LIFE OF NOTCHED SPECIMEN UNDER MULTI-AXIAL LOADING[J]. Engineering Mechanics, 2014, 31(10): 216-221. DOI: 10.6052/j.issn.1000-4750.2013.04.0360
Authors:WU Zhi-rong  HU Xu-teng  SONG Ying-dong
Affiliation:1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;;2.State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:
An estimation method for the fatigue life of notched specimen under multi-axial loading is proposed. The multi-axial fatigue damage parameter in every part of notched specimen is calculated based on a critical plane criteria. The location of notched specimen with the maximum damage parameter is taken as a multi-axial fatigue dangerous point. The critical distance calculation methods of a hot point method and a line method are proposed based on a critical distance thought. The hot method and line method are taken to consider the effects of a damage gradient nearby the fatigue damage point of notched specimen. The modified damage parameter based on a critical distance is taken to calculate the multi-axial fatigue life of notched specimen. The method of estimation fatigue life is evaluated by the multi-axial fatigue tests of SAE1045 steel notched specimen. The result shows that the estimation method for fatigue life has good predictive ability. The prediction results are almost within a factor of three scatter bands of test results.
Keywords:life prediction  multi-axial fatigue  notch fatigue  fatigue dangerous point  critical distance
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