首页 | 本学科首页   官方微博 | 高级检索  
     检索      

用塑性滞后能原理估算随机载荷下的疲劳寿命
引用本文:吴富民,田丁栓.用塑性滞后能原理估算随机载荷下的疲劳寿命[J].航空学报,1994,15(3):264-268.
作者姓名:吴富民  田丁栓
作者单位:西北工业大学强度研究所
基金项目:国家自然科学基金,航空科学基金
摘    要: 材料的疲劳损伤包括静力损伤和循环损伤,静力损伤为第一次静力加载引起的塑性应变能与静力韧性之比;循环损伤由循环塑性滞后能与疲劳韧性之比来计算,计算中计及了材料循环硬化(或软化)引起的屈服应力增大(或减小)的影响。为了简化计算,假设在循环加载时应力一应变曲线均按迟滞回线规律变化;不同应力变程下材料疲劳韧性可由对称循环的应力控制疲劳试验确定。本文提出了一种比较合理又便于工程应用的、用塑性滞后能原理估算随机载荷下疲劳寿命的新方法,初步的试验验证是令人满意的。

关 键 词:塑性变形  静力特性  疲劳试验  疲劳寿命  随机载荷  

FATIGUE LIFE ESTIMATE UNDER RANDOM LOADING BASED ON PLASTIC HYSTERESIS ENERGY PRINCIPLE
Wu Fumin.FATIGUE LIFE ESTIMATE UNDER RANDOM LOADING BASED ON PLASTIC HYSTERESIS ENERGY PRINCIPLE[J].Acta Aeronautica et Astronautica Sinica,1994,15(3):264-268.
Authors:Wu Fumin
Institution:1. Strength Research Institute,Northwestern Polytechnical University,Xi'an,710072;2. Box 73 of Xi'an,Xi'an,710089
Abstract:There are static and cyclic damages in materials.The static damage is the ratio of plas- tic strain energy due to first applied static load to static toughness of material,and the cyclic damage can be obtained by calculating the ratio of cyclic plastic hysteresis energy to fatigue toughness of material.In calculating the cyclic damage,we have been concerned with influences of yield stress increment(or decrement)caused by cycle-dependent hardening(or softening)of material.In order to simplify the calculating,we assume that the stress-strain curves at cyclic loading all follow hysteresis loops and fatigue toughness of material under different stress ranges can be detennined by cyclic symmetry stress control fatigue tests.In this paper,we have advanced anew fatigue life estimating method under random loading.The new method is reasonable and convenient in engineering application. It is satisfactory in the preliminary experimental verification.
Keywords:plastic deformation  static characteristics  fatigue tests  fatigue life  random loads
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号