Integrated electric motor and gear in an aircraft wheel
A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a geared motor assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the geared motor assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
1. A wheel and geared motor assembly configured to fit substantially completely within existing wheel well space in an existing aircraft landing gear, wherein a wheel is supported on an axle by opposed support wall means for supporting said wheel and defining a volume within said wheel well, and a motor assembly means for driving said wheel on the ground and a gear system means for driving said motor assembly means are supported within the defined volume between said opposed support wall means, wherein said wheel and geared motor assembly is configured to fit within said defined volume in a landing gear wheel in an existing aircraft without changing the existing aircraft landing gear tires, axle, or piston.
2. A wheel and geared motor assembly as described in claim 1 , wherein said opposed support wall means comprises an inboard support wall connected to an outboard support wall, and said inboard support wall and said outboard support wall are spaced apart a distance selected to maximize said defined volume.
3. A wheel and geared motor assembly as described in claim 2 , wherein said motor assembly means and said gear system means are supported by said inboard support wall and said outboard support wall, respectively.
4. A wheel and geared motor assembly as described in claim 2 , wherein said motor assembly means comprises a rotor element and a stator element and at least one of said rotor element or said stator element is mounted on said inboard support wall.
5. A wheel and geared motor assembly as described in claim 2 , wherein said wheel is supported on each of said inboard and outboard support walls by a pair of bearing means supportingly contacting said wheel and configured to fit within correspondingly configured notches in each of said support walls.
6. A wheel and geared motor assembly as described in claim 4 , wherein said rotor element is supported by said inboard support wall and said inboard support wall includes torque arm means to provide for a torque reaction.
7. A wheel and geared motor assembly as described in claim 1 , wherein said support wall means comprises an inboard support wall and an outboard support wall spaced apart to define a volume that substantially fills said wheel well and completely encloses said motor assembly means and said gear system means.
8. A wheel and geared motor assembly as described in claim 1 , wherein said motor assembly means comprises an electric motor selected from the group consisting of axial flux motors, toroidally wound motors, electric induction motors, permanent magnet brushless DC motors, and switched reluctance motors.
9. A wheel and geared motor assembly as described in claim 1 , wherein said gear system means includes gear means drivingly connected to said motor assembly means and clutch means operatively disposed between said motor assembly means and said gear system means.
10. A wheel and geared motor assembly as described in claim 9 , wherein said solenoid means actuatable to drive said clutch means to selectively engage said motor assembly means and said gear system means to drive the wheel on the ground and disengage said motor assembly means from said gear system means when the wheel is not on the ground.
11. A wheel and geared motor assembly as described in claim 10 , further including sensor means for measuring the speed of said wheel on the ground.
12. A wheel and geared motor assembly as described in claim 1 , wherein said gear system means includes an arrangement of planetary gears connected to clutch means operatively disposed between said gear system means and said motor assembly means.
13. A wheel and geared motor assembly as described in claim 1 , wherein said wheel includes a pair of spaced flange means for mounting a tire on said wheel.
14. A wheel and geared motor assembly as described in claim 13 , wherein said spaced flange means includes an inboard flange formed integrally with said wheel and an outboard flange demountable from said wheel.
15. A wheel and geared motor assembly as described in claim 1 , wherein said wheel is an aircraft nose wheel.
16. A wheel and geared motor assembly as described in claim 1 , configured to fit within said defined volume in a landing gear wheel in an existing aircraft without changing the existing aircraft landing gear tires, axle, or piston.
17. A wheel and geared motor assembly as described in claim 1 , wherein said motor assembly means and said support wall means are configured to conduct heat generated by driving said wheel away from said motor assembly means.
18. A wheel and geared motor assembly as described in claim 1 , further including cockpit interface means operative to activate said motor assembly means and said gear system means when activation of said motor assembly means and said gear system means is indicated to be safe.