中国民航大学学报2024,Vol.42Issue(5) :1-8.

基于多应力加速退化的机载电子部件可靠性试验方法

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

王鹏 田润操 杜洪光 丛玮 张帆 于光 杨吕珊
中国民航大学学报2024,Vol.42Issue(5) :1-8.

基于多应力加速退化的机载电子部件可靠性试验方法

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

王鹏 1田润操 2杜洪光 2丛玮 3张帆 1于光 4杨吕珊5
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作者信息

  • 1. 中国民航大学科技创新研究院,天津 300300;民航航空器适航审定技术重点实验室,天津 300300
  • 2. 中国民航大学安全科学与工程学院,天津 300300
  • 3. 中国民航大学电子信息与自动化学院,天津 300300
  • 4. 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
  • 5. 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
  • 折叠

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.

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 com-plex 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 estab-lished,and the form of stress coupling is determined by combining correlation analysis.Secondly,maximum likeli-hood 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 re-al airworthiness problem of missing and inaccurate of basic data.

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

Key words

airworthiness certification/civil aircraft system safety assessment/basic safety data/accelerated test technique/multi-stress coupling

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出版年

2024
中国民航大学学报
中国民航大学

中国民航大学学报

影响因子:0.363
ISSN:1674-5590
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