A landing gear actuation system is disclosed herein. The landing gear actuation system includes an attachment point integral to a movable member, a flexible pull member having a first end coupled to the attachment point, and a motor configured to move the flexible pull member, wherein the movement of the flexible pull member moves the attachment point and the movable member.


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    Title :

    LANDING GEAR ACTUATION SYSTEM


    Additional title:

    SYSTEME D'ACTIONNEMENT DE TRAIN D'ATTERRISSAGE


    Contributors:
    KLODE HARALD (author) / MADEY KYLE M (author) / COX GERARD (author)

    Publication date :

    2023-10-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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