The invention discloses a fault isolation system and a fault isolation method, relates to the related technical field of aircraft power device control and control systems, and is used for solving the problem that jamming of a driving part can generate adverse effects on control of a thrust part. The fault isolation system provided by the invention comprises a control unit; the information acquisition unit is coupled to the control unit and is used for acquiring working information of an accelerator table; the isolation actuating unit is coupled to the control unit and is connected with the driving piece; wherein the control unit judges whether the driving piece is jammed or not according to the working information; and when the driving piece is blocked, the control unit controls the isolation actuating unit to drive the driving piece to be far away from the thrust piece.

    本申请公开了故障隔离系统及故障隔离方法,涉及飞机动力装置控制与操纵系统相关技术领域,用于解决驱动件卡阻会对推力件的操纵产生不利影响的问题。本申请提供的故障隔离系统包括控制单元;信息获取单元耦合至所述控制单元,用于获取油门台的工作信息;隔离作动单元耦合至所述控制单元,并与驱动件连接;其中:所述控制单元根据所述工作信息,判断所述驱动件是否发生卡阻;当所述驱动件发生卡阻时,所述控制单元控制所述隔离作动单元带动所述驱动件远离所述推力件。


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    Title :

    Fault isolation system and fault isolation method


    Additional title:

    故障隔离系统及故障隔离方法


    Contributors:
    ZHANG XU (author) / YE DONGXIN (author) / KE JIE (author) / LYU ZHAN (author) / HE BIHAI (author)

    Publication date :

    2024-05-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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