The invention belongs to the technical field of aircraft engine health management system design, and particularly relates to an aircraft engine health management system, which comprises an engine data acquisition unit, an engine controller, an engine data processing unit, an engine data processing unit and an engine data processing unit, the engine data collector is used for collecting corresponding engine parameters, and can only unidirectionally receive data sent by the engine controller; and the engine health monitoring unit is mounted on an aircraft, connected to an aircraft system and connected with the engine data collector so as to be capable of receiving and storing the corresponding engine parameters, generating an engine state monitoring report based on the corresponding engine parameters, storing the engine state monitoring report and sending the engine state monitoring report to the aircraft system.

    本申请属于飞机上发动机健康管理系统设计技术领域,具体涉及一种飞机上发动机健康管理系统,包括:发动机数据采集器,安装在发动机上,与安装在发动机上的发动机专用传感器连接,以及与发动机控制器连接,以能够采集相应的发动机参数,其中,所述发动机数据采集器仅能够单向接收发动机控制器发送的数据;发动机健康监测单元,安装在飞机上,接入飞机系统,与所述发动机数据采集器连接,以能够接收、存储相应的发动机参数,基于相应的发动机参数生成发动机状态监测报告,并将该发动机状态监测报告存储以及发送给飞机系统。


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    Title :

    Aircraft engine health management system


    Additional title:

    一种飞机上发动机健康管理系统


    Contributors:
    YANG XU (author) / WU XIN (author) / ZHANG RUI (author) / LI JUN (author)

    Publication date :

    2022-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / G06K Erkennen von Daten , RECOGNITION OF DATA





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