主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
零件疲劳平均失效率计算方法研究
作者:
作者单位:

1.航空工业第一飞机设计研究院总体气动设计研究所;2.西北工业大学航空学院;3.西安交通大学航天航空学院

作者简介:

通讯作者:

中图分类号:

V215.7

基金项目:

国家自然科学基金(No. 11672238),陕西省自然科学基础研究计划(No. 2021JQ-005, 2020JZ-06),


Research on calculation method of fatigue average failure rate
Author:
Affiliation:

1.Institute of General Aerodynamic Design,AVIC The First Aircraft Institute School of Aeronautics,Northwestern Polytechnical University School of Aeronautics,Northwestern Polytechnical University School of Aerospace Engineering,Xi’An Jiaotong University;2.School of Aeronautics, Northwestern Polytechnical University

Fund Project:

The National Natural Science Foundation of China; National Natural Science Foundation of China(No. 11672238),Natural Science Basic Research Program of Shaanxi(No. 2021JQ-005, 2020JZ-06),

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    摘要:

    失效率、平均失效率、平均剩余寿命决定了结构的寿命分布和可靠度,在机械产品的可靠性研究中具有非常重要的作用。基于可靠性度量的基本指标,推导寿命分布为两参数威布尔分布时疲劳可靠性系数与可靠度的关系,提出基于疲劳可靠性系数计算结构失效率和平均失效率的方法,并给出相应的计算过程,形成不同寿命度量指标下较为简便的计算方法。利用已有的整体搭接壁板结构疲劳寿命试验数据,采用本文所提方法与传统积分方法对整体搭接壁板结构进行疲劳平均失效率计算和误差分析。结果表明:所推导的计算公式形式简单,便于计算,且具有高度准确性,对机械结构的FMECA 以及维修决策的制定具有指导意义。

    Abstract:

    Failure rate and average failure rate play a very important role in the reliability research of mechanical products. They and average residual life determine the life distribution and reliability of structures. Based on the basic index of reliability measurement, the rela-tionship between fatigue reliability coefficient and reliability was deduced when the life distribution is two parameter Weibull distri-bution. A method for calculating the structural failure rate and average failure rate was proposed based on fatigue reliability coeffi-cient, and the corresponding calculation process was derived. Based on the existing fatigue life test data of integral lap panel structure, the proposed method and the traditional integral method are used to calculate the average failure rate and error analysis of integral lap panel structure. The results show that the formula is simple, easy to calculate, and has the characteristics of high accuracy and relia-bility. It is of great significance for FMECA and maintenance decision-making of mechanical structure.

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引用本文

火建卫,张亚丹,谢伟,冯威.零件疲劳平均失效率计算方法研究[J].航空工程进展,2023,14(3):178-186,198

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  • 收稿日期:2022-06-06
  • 最后修改日期:2022-11-13
  • 录用日期:2022-11-18
  • 在线发布日期: 2023-04-19
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