The device has a gear rim (104) mounted to rotate on an undercarriage axle (105) and constrained in rotation with a torsion tube (106). Braking actuators (110) i.e. electromechanical actuators, are carried by the rim for selectively pressing a stack of disks (116) together. A drive member (130) carries a secondary winding (120) of a single-phase transformer with a primary winding (121) arranged facing the rim while being stationary in rotation, where the secondary winding is electrically coupled to the actuators and the primary winding is coupled to a non-direct current (DC) voltage source.


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    Title :

    Dispositif de freinage/entraînement d'une roue d'aéronef


    Additional title:

    Device for braking/powering an aircraft wheel.
    Vorrichtung zum Bremsen/Antrieb eines Rads eines Luftfahrzeugs


    Contributors:

    Publication date :

    2016-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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