Method for rotationally driving an aircraft wheel

1. A method for rotationally driving an aircraft wheel, the wheel being equipped with a rim comprising two half-rims assembled by bolts ( 5 ), comprising:

controlling a drive member for generating a torque for driving the wheel, and

transferring the drive torque to the wheel via the rim assembly bolts by means of a drive member which comprises a motor ( 10 ) having an output member ( 15 ) forming part of a rotor of the motor ( 10 ) mounted coaxially to the wheel, the output member being connected to the rim assembly bolts ( 5 ) by an interfacing member ( 20 ; 120 ),

wherein the interfacing member ( 20 ) comprises two coaxial rings ( 21 ) connected to one another by crossmembers ( 22 ), each ring comprising sleeves for receiving ends of the rim assembly bolts ( 5 ) and ends of tie rods secured to the output member ( 15 ).

2. A method for rotationally driving an aircraft wheel, the wheel being equipped with a rim comprising two half-rims assembled by bolts ( 5 ), comprising:

controlling a drive member for generating a torque for driving the wheel, and

transferring the drive torque to the wheel via the rim assembly bolts by means of a drive member which comprises a motor ( 10 ) having an output member ( 15 ) forming part of a rotor of the motor ( 10 ) mounted coaxially to the wheel, the output member being connected to the rim assembly bolts ( 5 ) by an interfacing member ( 20 ; 120 ),

wherein the interfacing member ( 120 ) comprises a plurality of stirrups ( 121 ) comprising two arms ( 123 ) connected by a bridge ( 122 ) and terminated by lugs ( 124 ), the bridge of each stirrup being fixed to the one of the output member or rim, the lugs being fixed to the other of the output member or rim.