The invention discloses a lock pin linear driving device for an aircraft wing folding system, which comprises a shell, a lock pin is arranged in the shell, one end of the lock pin is connected with a driving mechanism, the driving mechanism is used for driving the lock pin to linearly move, the other end of the lock pin movably extends out of the shell, and a locking mechanism is arranged on the shell. And the locking mechanism is used for locking the limiting position of the lock pin. The lock has the advantages that the locking function is added, double insurance is achieved, and the lower safety is improved.

    本申请公开了一种用于飞机机翼折叠系统的锁销直线驱动装置,包括壳体,壳体内设置有锁销,锁销一端连接有驱动机构,驱动机构用于带动锁销直线移动,锁销另一端活动伸出壳体,壳体上设置有锁定机构,锁定机构用于对锁销极限位置进行锁定,本申请具有增加了锁定功能、双重保险、提高下安全性的优点。


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    Titel :

    Lock pin linear driving device for aircraft wing folding system


    Weitere Titelangaben:

    一种用于飞机机翼折叠系统的锁销直线驱动装置


    Beteiligte:
    XIAO WENYAO (Autor:in) / CHENG JIALIN (Autor:in) / ZHANG SHIQUAN (Autor:in) / ZHANG HAN (Autor:in) / LI YUXIANG (Autor:in) / WU DAXIU (Autor:in) / XU YAN (Autor:in)

    Erscheinungsdatum :

    2022-11-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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