多轴非比例载荷谱条件下高强度螺栓疲劳强度分析
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  • 英文篇名:FATIGUE STRENGTH ANALYSIS OF HIGH-STRENGTH JOINT BOLTS UNDER MULTIAXIAL NONPROPORTIONAL LOADING SPECTRUM
  • 作者:曹罚君
  • 英文作者:CAO FaJun;NFAIC High Precision Transmission Co.,Ltd.;
  • 关键词:多轴疲劳 ; 非比例载荷谱 ; 强度螺栓 ; 风机主齿轮箱
  • 英文关键词:Multi-axial fatigue;;Nonproportional loading spectrum;;High-strength joint bolts;;Main gearbox of wind turbine
  • 中文刊名:JXQD
  • 英文刊名:Journal of Mechanical Strength
  • 机构:湖南南方宇航高精传动有限公司;
  • 出版日期:2019-01-24
  • 出版单位:机械强度
  • 年:2019
  • 期:v.41;No.201
  • 基金:湖南省科技重大专项(2012FJ1002)资助~~
  • 语种:中文;
  • 页:JXQD201901037
  • 页数:6
  • CN:01
  • ISSN:41-1134/TH
  • 分类号:235-240
摘要
以风机主齿轮箱的箱体连接螺栓疲劳强度分析为研究背景,提出一种在多轴非比例载荷谱作用下高强度螺栓连接疲劳强度的分析方法。该方法基于多轴疲劳理论,将外部多轴非比例的风力载荷谱通过连接箱体模型有限元应力计算及雨流计数处理,转化为螺栓各对应载荷方向上的应力雨流谱,然后在螺栓各计算点处进行各载荷方向上的应力合成,按照德国VDI2230标准的计算方法,结合螺栓材料的应力寿命(S-N)曲线,计算得到螺栓各计算点的疲劳损伤率,最后依据线性损伤累计理论,得出连接螺栓的疲劳安全系数。依据本文中的分析方法编制螺栓疲劳强度计算程序,再以某一型号风机齿轮箱的扭力臂与齿圈连接螺栓为例,计算得到该螺栓在风机20年工作寿命内的疲劳安全系数为1. 819。提出的方法为今后计算复杂载荷工况下的螺栓疲劳强度提供了一个新方向。
        A method about fatigue strength analysis of high-strength joint bolts was proposed on the background of gearbox housing joint design of the wind turbine. The method was based on the theory of multi-axial fatigue. And the calculation process of the method described as following: first,the multi-axial non-proportional loads,which loading on the hub blade because of natural wind,were transformed into corresponding stress spectrum after the process of the stress calculation of housing FE model and the stress treated according to the rain-flow counting rules. Second,the Mises stress was synthesized at the calculation nodal location of the bolt cross section from the multi-axial stress spectrum. And third,the fatigue damage of the nodal location was calculated according to the VDI2230 standard under the consideration of the bolt material S-N curve. Finally,the fatigue safety factor of the joint bolts was obtained according to the theory of Palmgren-Miner. Application software was programmed according to the method. With the software,a case of high-strength joint bolt fatigue strength was analyzed,and the fatigue safety factor is1. 819 within the design life of 20 years. The paper proposes a new way to evaluate the fatigue strength of high-strength joint bolts under complex loading condition.
引文
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