Coaxial contra-rotating motors for differential landing gear steering

1. A landing gear for an aircraft comprising:

a pair of spaced wheels, and a drive and steering arrangement operable to drive each of the wheels in either rotational direction;

said drive and steering arrangement including a pair of permanent magnet rotors, with each of said permanent magnet rotors connected to rotate with one of said wheels;

a single stator positioned to drive both of said rotors;

said single stator being radially intermediate an outer one of said two rotors and an inner one of said two rotors;

said inner one of said two rotors has a shaft with a pair of spaced bearings, and said shaft being supported within said stator by said pair of spaced bearings;

said outer one of said rotors being mounted on said shaft of said inner one of said rotors;

said outer one of said rotors being connected to rotate with one of said wheels, and said shaft of said inner one of said rotors supported on bearings within said outer one of said rotors; and;

said rotor associated with one of said wheels is driven in a first rotational direction and a rotor associated with the other of said wheels is driven in an opposed direction to cause an airplane receiving the landing gear to turn;

both of said wheels are driven by their respective rotors in a forward direction to cause the aircraft to move forwardly;

both of said rotors are driven in a rearward direction to cause a braking effect on an aircraft receiving said landing gear; and

said landing gear has an actuator for moving said pair of spaced wheels between a stowed and extended position when mounted on an aircraft.