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作 者:赵权[1] 葛红娟[1,2] 张璐[1] 陈舒文[1] 薛建良 ZHAO Quan;GE Hongjuan;ZHANG Lu;CHEN Shuwen;XUE Jianliang(College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China;College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China)
机构地区:[1]南京航空航天大学民航学院,南京211106 [2]南京航空航天大学自动化学院,南京211106
出 处:《北京航空航天大学学报》2018年第6期1246-1252,共7页Journal of Beijing University of Aeronautics and Astronautics
基 金:南京航空航天大学研究生创新基地(实验室)开放基金(kfjj20160701)~~
摘 要:针对航空电子设备有替换Ⅰ型截尾试验无失效的情形,提出了一种改进综合E-Bayesian方法用于可靠性参数的综合估计。该方法利用失效因子和自适应系数,并结合可靠性参数先验值及其经典E-Bayesian评估结果,引入失效数据,同时使用相对概率法构造失效权重模型。以航空电子设备平均寿命为目标,建立了平均寿命的改进综合E-Bayesian估计模型,并以某型变压整流器(TRU)为对象进行应用研究和方法比较分析。结果表明,提出的改进综合E-Bayesian方法具有更好的评估性能,并能够改善可靠性评定中可能出现的"冒进"问题。In this paper,an improved synthetic E-Bayesian method is proposed to estimate the reliability parameters of aviation electronic equipment for the zero-failure situation of type-Ⅰ censoring test with replacement. This method employs the failure factor and self-adaptive coefficient,which are combined with the priori value and classical E-Bayesian estimation result of the reliability parameters,to import the failure data,and then structures the corresponding failure weight model with the method of relative probability. Aimed at the mean life of the aviation electronic equipment,this paper builds the improved synthetic E-Bayesian estimation model and employs a certain type of transformer rectifier unit(TRU) as the object to make application research and method comparison analysis. The results show that the improved synthetic E-Bayesian method has better estimation performance and can ameliorate the "rash"problem that may emerge in reliability assessment.
关 键 词:航空电子设备 可靠性 综合E-Bayesian估计 有替换Ⅰ型截尾试验 无失效数据
分 类 号:V240.2[航空宇航科学与技术—飞行器设计]
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