The invention relates to a brake for an aircraft wheel comprising firstly calipers with an outer jaw (103) receiving a stationary brake pad (108) and an inner jaw that is movable under drive from the braking actuator (105) and that receives a movable brake pad (107), and secondly a disk (109) that extends between the brake pads and that includes means (110) for constraining it to move in rotation with the wheel; at least one of the brake pads includes a protrusion (120) projecting from a rear face of the pad to be received in a matching receptacle (123) of the associated jaw and serving both to position the pad on the jaw and to transmit braking forces from the stationary pad to the associated jaw.


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    Titel :

    FREIN POUR ROUE D'AERONEF, EN PARTICULIER POUR UN HELICOPTERE.


    Beteiligte:
    DELAYRE XAVIER (Autor:in) / HARDY JEREMY (Autor:in)

    Erscheinungsdatum :

    23.09.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge



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