北京航空航天大学学报 ›› 2021, Vol. 47 ›› Issue (4): 690-697.doi: 10.13700/j.bh.1001-5965.2020.0024

• 论文 • 上一篇    下一篇

飞机舱门泄压阀机构磨损可靠性与灵敏度分析

周长聪, 赵浩东, 常琦, 吉梦瑶, 李琛   

  1. 西北工业大学 工程力学系, 西安 710129
  • 收稿日期:2020-01-16 发布日期:2021-04-30
  • 通讯作者: 周长聪 E-mail:changcongzhou@nwpu.edu.cn
  • 作者简介:周长聪,男,博士,副教授,博士生导师。主要研究方向:多体动力学仿真、机械可靠性分析与设计;赵浩东,男,硕士研究生。主要研究方向:多体动力学仿真、机械可靠性分析与设计。
  • 基金资助:
    国家自然科学基金(51975476);陕西省自然科学基础研究计划(2020JM-135);西北工业大学硕士研究生创意创新种子基金(CX2020115)

Reliability and sensitivity analysis of relief valve mechanism of aircraft door considering wear

ZHOU Changcong, ZHAO Haodong, CHANG Qi, JI Mengyao, LI Chen   

  1. Department of Engineering Mechanics, Northwestern Polytechnical University, Xi'an 710129, China
  • Received:2020-01-16 Published:2021-04-30
  • Supported by:
    National Natural Science Foundation of China (51975476); Natural Science Basic Research Program of Shaanxi (2020JM-135); Seed Foundation of Innovation and Creation for Graduate Students in Northwestern Polytechnical University (CX2020115)

摘要: 泄压阀机构是飞机舱门的重要组成部分,对维持飞机正常安全运行起到重要作用。在ADAMS软件中建立了飞机舱门泄压阀机构多体动力学仿真模型,研究销轴发生以磨损为主要形式的性能退化时,对泄压阀机构定位精度的影响。建立了泄压阀机构定位精度的功能函数,引入主动学习Kriging代理模型,挑选符合学习准则的点提高代理模型精度。采用Monte Carlo方法计算了不同磨损次数下泄压阀机构的失效概率与3种全局灵敏度指标的变化规律,并给出了不同阈值情况下失效概率和基于失效概率的全局灵敏度指标的变化规律。结果表明:在不同磨损次数下,对于磨损量较大的销轴,其全局灵敏度指标值也较大,并且各项指标随磨损次数的变化规律存在差异。

关键词: 飞机舱门, Kriging模型, 可靠性, 全局灵敏度, 运动精度

Abstract: As an important part of the aircraft door, the relief valve mechanism plays an important role in maintaining the normal and safe operation of the aircraft. In this paper, the multi-body dynamical model of the relief valve mechanism is built in ADAMS to study the effect of pin wear on positioning accuracy. The performance function of the positioning accuracy of the mechanism is established. The active Kriging model is introduced to find samples points which can obviously improve the fitting accuracy according to learning criteria. The Monte Carlo method is used to estimate failure probability and three sensitivity indices at different wear times, and the change rules of failure probability and failure probability based global sensitivity indices under different thresholds have been studied. The results show that under different wear times, the global sensitivity indices of a pin with a larger wear amount are also larger, and there are differences in the changes of various indices with the wear times.

Key words: aircraft door, Kriging model, reliability, global sensitivity, motion accuracy

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