The invention discloses an electrically-driven passive strut uplock. The uplock comprises a strut uplock mechanism (1) and an electrically-driven unlocking actuator (2), wherein the electrically-driven unlocking actuator (2) enables an unlocking rocker arm (7) of the strut uplock mechanism (1) to swing according to an unlocking control instruction of an upper computer so as to drive a lock hook (3) of the strut uplock mechanism (1) to rotate; and after the strut uplock mechanism (1) is unlocked in place, the unlocking actuator (2) is electrically driven to return according to a return controlinstruction of an upper computer. A hydraulic related driving device is omitted for unlocking a strut uplock, and the weight and the size of the system are reduced; dual-redundancy design is completedthrough electric driving, unlocking reliability is high, and the maintenance requirement is low.

    本发明公开一种电驱动的被动支柱上位锁,包括支柱上位锁机构(1)和电驱动开锁作动器(2),其中电驱动开锁作动器(2)根据上位机的开锁控制指令,使支柱上位锁机构(1)的开锁摇臂(7)摆动,从而带动支柱上位锁机构(1)的锁钩(3)转动,实现支柱上位锁机构(1)的开锁,在开锁到位后,电驱动开锁作动器(2)根据上位机的回位控制指令使回位。本发明取消了液压相关驱动装置进行支柱上位锁的开锁,减轻了系统的重量和体积;电驱动完成双余度设计,开锁可靠性高、维护需求低。


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    Titel :

    Electrically-driven passive strut uplock


    Weitere Titelangaben:

    一种电驱动的被动支柱上位锁


    Beteiligte:
    CHENG MENGGE (Autor:in) / CHANG NAN (Autor:in) / AN TAO (Autor:in) / LIN HONG (Autor:in) / FAN ZHE (Autor:in) / LI HAOYUAN (Autor:in)

    Erscheinungsdatum :

    30.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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