The invention belongs to the field of aircraft landing system design and relates to an aircraft cabin door separation mechanism. The aircraft cabin door separation mechanism adopts a multi-connecting-rod rotating throwing and pushing impact unlocking separation principle and comprises an aircraft body structure, an undercarriage cabin door, a short connecting rod, a long connecting rod, an actuating cylinder, a free hinge, a rotating unlocking hinge and an undercarriage cabin door lock.

    本发明属于飞行器着陆系统设计领域,涉及飞行器舱门分离机构。所述的飞行器舱门分离机构,采用多连杆旋抛+推冲解锁分离原理,包括飞行器机体结构、起落架舱门、短连杆、长连杆、作动筒、自由铰链、旋转解锁铰链和起落架舱门锁。


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    Title :

    Aircraft undercarriage cabin door separation mechanism


    Additional title:

    一种飞行器起落架舱门分离机构


    Contributors:
    LIAO MAOXIONG (author) / LIANG ZAN (author) / YUAN YUAN (author) / MA YUANHONG (author) / CHEN LIANG (author) / SONG GUOLIAN (author)

    Publication date :

    2025-03-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / E05B LOCKS , Schlösser



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