从零故障数据确定设备故障率的实用贝叶斯方法

M. V. Bremerman
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引用次数: 4

摘要

本文提出了几种实用的方法,可以用来补充经典的可靠性预测技术,通常用于计算电子系统故障率。这些方法采用贝叶斯数据分析技术,利用可用的现场可靠性数据和加速寿命试验(ALT)结果。方法包括Clopper-Pearson方法,该方法在文献中已被证明是贝叶斯方法的一个特例。在可靠性方面解决了Clopper-Pearson低单侧置信边界方程,并允许在没有可靠的先验信息可用且现场零故障发生时推导故障率点估计。当较低水平的测试数据,如加速寿命测试结果(先验信息)可用时,可以使用gamma-指数共轭模型,使用GAMMAINV Excel函数从结果的后验分布中得出故障率。给出了一个在航天工业背景下的应用示例,其中使用从多个空间有效载荷收集的实际加速寿命试验结果和零故障在轨数据推导了动力混合装置的故障率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Practical Bayesian methods for determining device failure rates from zero-failure data
This paper presents several practical methods that can be used to supplement classical reliability prediction techniques typically used to calculate electronic system failure rates. These methodologies employ Bayesian data analysis techniques utilizing available field reliability data and accelerated life test (ALT) results. Methodologies include the Clopper-Pearson method which has been shown in the literature to be a special case of the Bayesian method. The Clopper-Pearson lower one-sided confidence bound equation is solved in terms of reliability and allows for the derivation of a failure rate point estimate when no credible prior information is available and zero failures have occurred in the field. When lower level test data such as accelerated life test results (informative prior) are available, a gamma-exponential conjugate model can be used to derive the failure rate from the resulting posterior distribution over a range of credibility intervals using the GAMMAINV Excel function. An example of application in the context of the space industry is presented where the failure rate for a power hybrid device was derived using real accelerated life test results and zero-failure on-orbit data collected from multiple space payloads.
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