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某直升机主减速器传动系统的寿命与可靠性计算方法
引用本文:薛向珍,李育锡,王三民.某直升机主减速器传动系统的寿命与可靠性计算方法[J].航空动力学报,2011,26(3):635-641.
作者姓名:薛向珍  李育锡  王三民
作者单位:西北工业大学,机电学院,西安,710072
基金项目:国家高技术研究发展计划
摘    要:通过对直升机典型任务剖面原始载荷数据谱进行统计处理,经三维有限元分析将所编系统载荷谱转化为齿轮应力谱;结合Goodman公式及材料P-S-N曲线(给定存活率下的疲劳寿命曲线)算出该系统各齿轮在各级载荷下的疲劳寿命,利用统计软件Minitab对寿命数据进行分析,得出齿轮的接触疲劳寿命服从两参数威布尔分布,根据威布尔分布的...

关 键 词:直升机传动系统  载荷谱  疲劳寿命  可靠性  威布尔分布
收稿时间:2010/2/28 0:00:00
修稿时间:2010/6/29 0:00:00

Method of lifetime and reliability of some helicopter's main reducer
XUE Xiang-zhen,LI Yu-xi and WANG San-min.Method of lifetime and reliability of some helicopter''s main reducer[J].Journal of Aerospace Power,2011,26(3):635-641.
Authors:XUE Xiang-zhen  LI Yu-xi and WANG San-min
Institution:School of Mechanical Engineering, Northwestern Polytechnical University,Xi'an 710072,China;School of Mechanical Engineering, Northwestern Polytechnical University,Xi'an 710072,China;School of Mechanical Engineering, Northwestern Polytechnical University,Xi'an 710072,China
Abstract:The reliability of the main reducer drive system was acquired by dealing with the original load date of a typical mission profile of the helicopter,the load spectrum was changed into the stress spectrum of all gears using three-dimensional finite element analysis;the fatigue life of all gears at each load stage was calculated with Goodman formula and materials P-S-N curves,the life date was analyzed using Minitab.It's concluded that the contact fatigue life of gears is subject to Weibull distribution with two parameters,thus working out the reliability of each transmission part according to the reliability function of Weibull distribution and based on series-to-parallel reliability model of the system.Then,this thesis can provide a method for determining life and reliability of complex drive systems.
Keywords:rotorcraft drive system  load spectrum  fatigue life  reliability
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