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多轴疲劳寿命预测及验证
引用本文:王雷,王德俊.多轴疲劳寿命预测及验证[J].东北大学学报(自然科学版),2002,23(2):174-177.
作者姓名:王雷  王德俊
作者单位:东北大学机械工程与自动化学院;东北大学机械工程与自动化学院辽宁沈阳110004;辽宁沈阳110004
基金项目:国家自然科学基金资助项目 (5 9775 0 3 0 ) ·
摘    要:以薄壁管试件为研究对象,分析了拉扭联合加载作用下的多轴疲劳应变变化特性·根据多轴疲劳临界平面法原理,以临界平面上最大剪应变幅、正应变幅以及表征材料总体损伤水平的非比例度为参数建立多轴疲劳损伤参量,结合MansonCoffin方程建立了多轴疲劳寿命预测模型·该模型考虑了材料总体损伤程度·模型中表征材料总体损伤的非比例度是加载参数的函数,与多轴疲劳应变变化特性密切相关·试验验证,预测寿命误差因子小于15·

关 键 词:拉扭联合加载  多轴疲劳  临界平面  最大剪应变幅  非比例度  材料损伤  寿命预测
文章编号:1005-3026(2002)02-0174-04
修稿时间:2001年6月8日

Fatigue Life Prediction Under Multiaxial Loading
WANG Lei,WANG De jun.Fatigue Life Prediction Under Multiaxial Loading[J].Journal of Northeastern University(Natural Science),2002,23(2):174-177.
Authors:WANG Lei  WANG De jun
Abstract:The strain varying characteristics of multiaxial fatigue were analyzed under the condition of combined tensional and torsional loading for thin walled tubuar specimens. Based on the principle of multiaxial critical plane approach, a multiaxial fatigue damage parameter was established, which takes account for the effect of not only the maximum shear strain amplitude and normal strain amplitude on the critical plane but also the parameter of non proportionality. The non proportionality can indicate the whole damage level of materials and is the function of loading parameters which is closely contact with the strain varying characteristics of multiaxial fatigue. The experiments under the tension-torsion proportional and non proportional loading were conducted to verify the multiaxial fatigue life model. The life prediction has a good correlation with the experimental results.
Keywords:combined tensional and forsional loading  multiaxial fatigue  critical plane  maximum shear strain amplitude  non  proportionality  material damage  life prediction
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