System level reliability analyses and predictions in a varying stress environment

D. Johnson, D. Coit, R. Kosaka, K. Megow
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引用次数: 1

Abstract

New flexible methods have been developed to predict reliability and estimate failure time distribution parameters for equipment and systems that are to be exposed to more stressful and diverse usage conditions in the future. Decades ago, the design reference mission for steam catapults and arresting gear on aircraft carriers was quite simple. The design engineers of these systems had a good understanding of the loads and added factors of safety to be cautious. Move ahead to the present, the mixture of aircraft has changed drastically, sortie rate has increased and so has the kinetic energy imparted to these critical systems. This has led to a need to develop a more generalized and flexible reliability predictive tool. This tool can be described as a stress-sensitive Weibull distribution. The entire process is outlined for this innovative technique. It includes the options for several methods of analysis. The base model is a Weibull distribution based solely on failure data without modifications. The first method is also a Weibull distribution, but the Weibull scale parameter is modified by a stress ratio, using end speed and the aircraft weight. The second method uses mean and standard deviation of end speed and aircraft weight to modify the Weibull scale parameter. These scale parameter modifiers are calculated based on an assumed general log-linear model and maximum likelihood estimation tools. The third method decouples any correlation that may exist between aircraft weight and end speed by binning aircraft launches into groups and calculating their proportion of the total. Once evaluated, these methods are able to extrapolate future failures at different levels of stress all across these critical systems.
系统级可靠性分析和预测在不同的压力环境
新的灵活方法已经被开发出来,用于预测设备和系统的可靠性和估计故障时间分布参数,这些参数将在未来暴露在更大的压力和多样化的使用条件下。几十年前,航空母舰上的蒸汽弹射器和拦阻装置的设计参考任务相当简单。这些系统的设计工程师对载荷和附加的安全因素有很好的了解,需要谨慎。向前推进到现在,飞机的组合发生了巨大的变化,出动率增加了,传递给这些关键系统的动能也增加了。这就需要开发一种更通用、更灵活的可靠性预测工具。这个工具可以被描述为应力敏感的威布尔分布。整个过程概述了这一创新技术。它包括几种分析方法的选项。基本模型是不加修改的基于失效数据的威布尔分布。第一种方法也是威布尔分布,但威布尔尺度参数通过应力比进行了修正,使用了末端速度和飞机重量。第二种方法是利用终端速度和飞机重量的均值和标准差来修改威布尔尺度参数。这些尺度参数修正是基于假设的一般对数线性模型和最大似然估计工具计算的。第三种方法是通过将飞机发射分组并计算它们在总数中的比例来解耦飞机重量和最终速度之间可能存在的任何相关性。一旦进行评估,这些方法就能够推断出这些关键系统在不同压力水平下的未来故障。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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