Disclosed is a landing gear system (100) for an aircraft, the landing gear system comprising: a landing gear (130) that is movable between an extended position and a retracted position, the landing gear comprising an extendible strut (136); a position sensor (140) configured to detect a position of a part of the extendible strut and output a signal indicative of the position; and a landing gear controller (150) that is communicably connected to the position sensor and is configured, in use, to: receive the signal from the position sensor; and, on the basis of the signal, determine that the strut has extended and the landing gear is in contact with the ground and automatically cause performance of at least a portion of a procedure to move the landing gear from the extended position to the retracted position


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    Title :

    LANDING GEAR RETRACTION


    Additional title:

    EINFAHREN DES FAHRWERKS
    RÉTRACTION DE TRAIN D'ATTERRISSAGE


    Contributors:
    KERR SEAN (author) / MARLES DAVID (author)

    Publication date :

    2020-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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