中国民航大学学报 ›› 2013, Vol. 31 ›› Issue (4): 6-9.

• 民用航空 • 上一篇    下一篇

航空发动机点火组件故障诊断系统设计

田立强1,李晓晖2a,刘承宗2a,石旭东2b,王立文2b   

  1. (1.北京航空工程技术研究中心,北京 100076;2.中国民航大学a.航空自动化学院;b.天津市民用航空器适航与维修重点实验室,天津 300300)
  • 收稿日期:2012-11-01 修回日期:2013-04-15 出版日期:2013-08-25 发布日期:2013-10-08
  • 作者简介:田立强(1977—),男,河北唐山人,硕士,工程师,研究方向为航空电子系统研究.
  • 基金资助:

    国家自然科学基金项目(U1233201);天津市科技支撑计划重点项目(11ZCKFGX04000);中央高校基本科研业务费专项(ZXH2012B002,
    31220BP05)

Design of fault diagnosis system for aircraft engine ignition component

TIAN Li-qiang1,LI Xiao-hui2a,LIU Cheng-zong2a,SHI Xu-dong2b,WANG Li-wen2b   

  1. (1.Beijing Aeronautical Technology Research Center,Beijing 100076,China;2a. College of Aeronautical Automation 2b. Tianjin Key Laboratory for Civil Aircraft Airworthiness and Maintenance,CAUC,Tianjin 300300,China)
  • Received:2012-11-01 Revised:2013-04-15 Online:2013-08-25 Published:2013-10-08

摘要:

航空发动机点火组件是发动机的核心部分,该组件设计的合理性及其工作的可靠性直接关系到发动机的工作状况,进行航空发动机点火组件故障诊断研究,对保障飞机点火组件的正常运行、提高飞机的安全性和持续适航性具有十分重要的意义。以航空发动机点火组件为研究对象,以航空发动机点火组件不同类型故障下产生的二次电压波形为基础,建立相应的故障特征库,设计基于图形匹配的航空发动机点火组件故障诊断系统。该系统能够采集点火电压波形及相应特征参数,将待检测波形与故障特征库中典型波形进行对比,得出相应故障类型。

关键词: 航空发动机, 点火组件, 故障特征库, 故障诊断

Abstract:

Aircraft engine ignition component is the core of the engine. Whether the engine can run safely and efficiently depends on the rationality and reliability of ignition component. For ensuring the normal running of ignition component and improving the safety as well as the continuing airworthiness of the aircraft,it is highly meaningful to do the research of the faults diagnosis of aircraft engine ignition component. Focusing on the aircraft engine ignition component fault diagnosis,the fault feature library is built,basing on the secondary voltage waveform generated from aircraft engine ignition component failures. With the library and shape matching approach,the fault diagnosis system can collect ignition voltage waveform and the corresponding characteristic parameters,then the detected waveform can be compared with the fault feature library, in which way the fault type can be determined.

Key words: aircraft engine, ignition system, fault feature library, fault diagnosis

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