An aircraft landing gear arrangement may comprise a landing gear bogie (300) having an axle, a torque tube (200) surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body (208) extending between a first end (210) and a second end (220). A flange (212) may be disposed at the first end. A mating surface (222) may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange (312) may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.


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    Title :

    AIRCRAFT BRAKE TORQUE LOAD REACTION THROUGH LANDING GEAR BOGIE STRUCTURE


    Additional title:

    BREMSMOMENTLASTREAKTION EINES FLUGZEUGS DURCH DIE FAHRWERKSDREHGESTELLSTRUKTUR
    RÉACTION DE CHARGE DE COUPLE DE FREINAGE D'AÉRONEF PAR L'INTERMÉDIAIRE D'UNE STRUCTURE DE BOGIE DE TRAIN D'ATTERRISSAGE


    Contributors:

    Publication date :

    2019-03-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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