The invention relates to a landing gear (P) for an aircraft comprising an axle (E) carried by a strut (T), said axle being provided with a rotatably-mounted wheel (RM) and a drive device (1, 1') for rotating the wheel (RM), the drive device comprising a motor (11) mounted at one end of the axle for transmitting a rotational torque to the wheel and a body (20, 20') projecting out of the motor and snugly received in the axle, at least a first harness (22) extending along the body and connecting the motor to a first coupler (21, 21') carried by a free end of the body in order to co-operate with a second coupler (30, 30') of the landing gear so as to supply the motor with power, characterised in that the second coupler is received in an opening (E2) formed in the axle at the junction between the strut and the axle.


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    Titel :

    DISPOSITIF D'ENTRAINEMENT EN ROTATION D'UNE ROUE D'AERONEF


    Weitere Titelangaben:

    DEVICE FOR ROTATING AN AIRCRAFT WHEEL
    VORRICHTUNG ZUM DREHEN EINES FLUGZEUGRADES


    Beteiligte:
    BLANPAIN THIERRY (Autor:in) / BRUN DIDIER (Autor:in) / PIQUEUX OLIVIER (Autor:in) / BASSET STÉPHANE (Autor:in)

    Erscheinungsdatum :

    12.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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