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基于T-S 模糊FTA 与仿真的舱盖机构故障诊断方法
引用本文:陈鹏飞,吴锋,何培垒,文晓武.基于T-S 模糊FTA 与仿真的舱盖机构故障诊断方法[J].航空发动机,2018,44(1):97-102.
作者姓名:陈鹏飞  吴锋  何培垒  文晓武
作者单位:中国航发四川燃气涡轮研究院航空发动机高空模拟技术重点实验室,四川绵阳621024
摘    要:针对高空舱舱盖机构系统故障源与故障程度难以判定以及故障特征值难以提取的问题,提出了基于T-S模糊故障树分析与仿真相结合的故障诊断方法。将T-S模型引入到舱盖机构不同步的典型故障分析中,用模糊可能性描述部件的故障概率;用T-S门来描述事件间的联系;用模糊数描述部件的故障程度,结合模型仿真模拟故障分析,获取部件发生故障时对顶事件的贡献或重要度,计算出顶事件发生故障的模糊可能性及其诊断决策。为高空舱舱盖机构的故障诊断和维修保养提供参考。

关 键 词:高空舱  模糊故障树  故障重现  综合决策  航空发动机

Fault Diagnosis Method of Chamber Cover Mechanism Based on T-S Fuzzy FTA and Simulation
Authors:CHEN Peng-fei  WU Feng  HE Pei-lei  WEN Xiao-wu
Institution:Key Laboratory of Technology on Aero-engine Altitude Simulation, Sichuan Gas Turbine Establishment of AECC, Mianyang Sichuan 621024, China
Abstract:According to the problem of difficult to determin fault source and foult degree and difficult to obtain fault characteristic value of high-altitude simulation test chamber cover mechanism system, a fault diagnosis method of chamber cover mechanism system based on T-S fuzzy fault tree analysis and fault simulation was proposed. T-S model was presented to typical fault analysis unsynchronized for chamber cover mechanism, which fault probabilities were described as fuzzy possibilities, events'' relationships were described by T-S gates, and fault degrees were described as fuzzy numbers. The fault were simulated in the failure mode, which the fault contribution to top event were achieved, as well as fuzzy fault possibilities of top event and comprehensive decision were achieved. It provides reference for the troubleshooting and maintenance of high-altitude simulation test chamber cover mechanism
Keywords:high-altitude simulation test chamber  Fuzzy Fault Tree  failure to reproduce  comprehensive decision  aeroengine
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