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.
DISPOSITIF D'ENTRAINEMENT EN ROTATION D'UNE ROUE D'AERONEF
DEVICE FOR ROTATING AN AIRCRAFT WHEEL
VORRICHTUNG ZUM DREHEN EINES FLUGZEUGRADES
2025-02-12
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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