taptap下载安装安卓学报 ›› 2024, Vol. 42 ›› Issue (5): 1-8.

• 民机安全性与适航 •    下一篇

基于多应力加速退化的机载电子部件可靠性试验方法

王 鹏 1a,2
,田润操 1b
,杜洪光 1b
,丛 玮 1c
,张 帆 1a,2
,于 光 3
,杨吕珊 4
  

  1. 1.taptap下载安装安卓 a. 科技创新研究院;b. 安全科学与工程学院;c.电子信息与自动化学院,天津 300300;2. 民航航空器适航
    审定技术重点实验室,天津 300300;3. 中国南方航空股份有限公司工程技术分公司新疆分部,乌鲁木齐 830000;
    4.中国东方航空技术有限公司武汉分公司生产技术部,武汉 430000
  • 收稿日期:2024-03-15 修回日期:2024-07-24 出版日期:2024-12-21 发布日期:2024-12-21
  • 作者简介:王鹏(1982— ),男,新疆霍城人,研究员,博士,研究方向为民机系统安全性、机械软硬件适航技术
  • 基金资助:
    国家重点研发计划项目(2021YFB160061)

Reliability test method of airborne electronic components based on multi-stress accelerated degradation

WANG Peng1a,2#br# , TIAN Runcao1b#br# , DU Hongguang1b#br# , CONG Wei#br# 1c#br# , ZHANG Fan1a,2#br# ,#br# YU Guang3#br# , YANG Lyushan4#br#   

  1. 1a. Research Institute of Science and Technology Innovation; 1b. College of Safety Science and Engineering; 1c. College of Electronic
    Information and Automation, CAUC, Tianjin 300300, China; 2. Key Laboratory of Airworthiness Certification Technology for Civil
    Aviation Aircraft, Tianjin 300300, China; 3. Xinjiang Branch of Engineering and Technology Affiliate of China Southern Airlines
    Co., Ltd., Urumqi 830000, China; 4. Production and Technology Department of Wuhan Branch of China Eastern Airlines
    Technology Co., Ltd., Wuhan 430000, China
  • Received:2024-03-15 Revised:2024-07-24 Online:2024-12-21 Published:2024-12-21

摘要: 可靠性试验是获取基础安全性数据的重要来源之一。 考虑机载设备的实际工作环境,多种应力共同作用导
致产品失效且存在复杂的相互作用,本文提出一种基于多应力广义耦合加速退化的可靠性试验方法,可以直
接获取用于适航符合性验证的基础安全性数据。 首先,建立考虑多应力广义耦合的非线性 Wiener 加速退化
模型,结合相关性分析确定应力耦合形式;其次,提出基于多应力加速退化模型的最大似然估计与参数优化
方法,解决多参数估计难题;最后,以某机载 LED 芯片为对象开展三应力加速退化试验,实现寿命评估。结果
表明,相比于传统多应力加速模型,本文所提方法更贴近实际工况,误差控制在 1%以内,寿命评估精度较高,
可以有效解决基础数据缺失和不准确的现实适航问题。

关键词: 适航审定, 民机系统安全性评估, 基础安全性数据, 加速试验技术, 多应力耦合

Abstract: The reliability test is one of the important sources to obtain the basic safety data. Considering the actual working
environment of airborne equipment, where multiple stress act together to cause product failure and there are complex interaction, a reliability test method based on accelerated degradation of multi-stress generalized coupling is
proposed in this paper, which can directly obtain the basic safety data for airworthiness compliance verification.
Firstly, a nonlinear Wiener accelerated degradation model considering multi-stress generalized coupling is established, and the form of stress coupling is determined by combining correlation analysis. Secondly, maximum likelihood estimation and parameter optimization method based on the multi-stress accelerated degradation model is
proposed to solve the problem of multi-parameter estimation. Finally a three-stress accelerated degradation test is
carried out with an airborne LED chip as the object to realize the life assessment. The results show that, compared
with the traditional multi-stress accelerated model, the proposed method is closer to the actual working condition,
and the error is controlled within 1%, and the accuracy of life assessment is high, which can effectively solve the real airworthiness problem of missing and inaccurate of basic data.

Key words: airworthiness certification, civil aircraft system safety assessment, basic safety data, accelerated test technique;
multi-stress coupling

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