The invention relates to a method for preventing misoperation of an accelerator table device under the condition of single engine of a civil aircraft. Specifically, a left engine and a right engine are distinguished in information coding form, and a locking device is additionally arranged, so that the throttle lever of the engine which works normally is locked when the single engine fails, and the throttle lever is prevented from being put away by mistake or the engine which works normally is prevented from being shut down by mistake.

    本发明涉及一种民用飞机发动机在单发情况下防止误操作油门台装置的方法。具体而言,本发明利用左、右发动机区别的信息编码形式,同时通过增加锁定装置,在单发失效时锁定正常工作发动机油门杆,并防止错收油门杆或错关正常工作的发动机。


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    Titel :

    Method for preventing misoperation when aero-engine breaks down


    Weitere Titelangaben:

    在航空发动机发生故障时防止误操作的方法


    Beteiligte:
    WANG JUN (Autor:in) / NIU XIAOYING (Autor:in) / ZHU YAO (Autor:in) / LI FEI (Autor:in) / CHEN TIANTIAN (Autor:in) / WANG YUAN (Autor:in)

    Erscheinungsdatum :

    07.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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