Drive system with harmonic drive for self-propelled aircraft wheel

Patent metadata

Field	Value
Publication number	US-9233752-B2
Application number	US-201213561066-A
Country	US
Kind code	B2
Filing date	Jul 29, 2012
Priority date	Jul 29, 2011
Publication date	Jan 12, 2016
Grant date	Jan 12, 2016

Abstract

A drive system with harmonic drive designed to meet the high power and torque requirements required to drive an aircraft independently on the ground is provided. The drive system includes an electric motor driven by a harmonic drive assembly that may be configured to be integral with the motor. This drive system with harmonic drive can be effectively installed in an existing aircraft nose wheel or main wheel without changes to other components.

First claim

The invention claimed is:

1. A compact drive system for installation completely within an aircraft nose or main landing gear wheel to drive the aircraft on the ground independently of the aircraft's engines or tow vehicles, comprising:
a. an electric motor assembly comprising at least a stationary stator element and a rotatable rotor element adapted to produce torque required to drive one or more aircraft landing gear wheels and drive an aircraft independently on the ground; and
b. a harmonic drive assembly mounted integrally with the electric motor to drive said electric motor, comprising at least a wave generator element, a toothed flex spline element, and a toothed circular spline element rotatably and concentrically mounted for rotation on a shaft comprising an input shaft coaxial with an output shaft and adapted to produce a desired gear reduction ratio during operation of said electric motor assembly and said harmonic drive assembly to drive said aircraft, wherein the electric motor assembly and the harmonic drive assembly are integrally configured and sized to fit completely and operationally within space defined by interior structures of an aircraft nose or main landing gear wheel, wherein said stator element comprises said toothed circular spline element; and
said toothed flex spline element has an elliptical configuration during rotation, and wherein selected ones of a plurality of teeth on said toothed flex spline element mesh with corresponding teeth on said circular spline element at opposed points 180 degrees apart along a major axis of the elliptical toothed flex spline element.

2. The compact drive system of claim 1 , wherein said rotor element is located internally of said stator element, said wave generator element is positioned within said toothed flex spline element, and said toothed circular spline element is positioned outwardly of said flex spline element so that teeth on said flex spline element and teeth on said circular spline element mesh during rotation.

3. The compact drive system of claim 1 , wherein said flex spline element has a cup-shaped configuration with an open end, said wave generator element is positioned within said open end, and said toothed circular spline element is positioned outwardly of said wave generator element with said toothed flex spline element disposed therebetween.

4. The compact drive system of claim 1 , wherein said harmonic drive assembly comprises said wave generator element mounted to input rotation to said harmonic drive assembly, said toothed flex spline formed with a plurality of teeth on an outer circumferential surface and positioned to mesh with a plurality of corresponding teeth on an inner circumferential surface of said toothed circular spline element, and a number of the plurality of teeth on said toothed flex spline element is less than a number of the plurality of teeth on said toothed circular spline element so that rotation of said wave generator element causes said toothed flex spline element to rotate more slowly than said wave generator element and in an opposite direction from the direction of rotation of said wave generator element.

5. The compact drive system of claim 1 , wherein an inner circumferential surface of said toothed circular spline element and an outer circumferential surface of said toothed flex spline element each comprise a plurality of teeth spaced and configured to mesh when said toothed circular spline element and said toothed flex spline element rotate about said shaft, wherein said toothed flex spline element has fewer teeth than said toothed circular spline element.

6. The compact drive system of claim 1 , wherein said rotor element is mounted eccentrically with respect to said stator element and said toothed flex spline element or concentrically with respect to said stator element and said toothed flex spline element.

7. The compact drive system of claim 1 , wherein said toothed flex spline element is made entirely from a flexible non-magnetic material or from a flexible non-magnetic material supporting teeth made from a rigid material.

8. The compact drive system of claim 2 , wherein said rotor element, said wave generator element, said toothed flex spline element, and said toothed circular spline element are concentrically rotatably mounted between the input shaft and the output shaft.

9. The compact drive system of claim 8 , wherein an inner circumferential surface of said stator element and an outer circumferential surface of said toothed flex spline element each include comprise a plurality of teeth spaced and configured to mesh when said rotor element and said toothed flex spline element rotate about said shaft, wherein said toothed flex spline element has fewer teeth than said stator element.

10. The compact drive system of claim 8 , wherein said rotor element is mounted eccentrically with respect to said stator element and said toothed flex spline element.

11. The compact drive system of claim 9 , wherein a number of teeth on said toothed flex spline element is at least two less than a number of teeth on said toothed circular spline element.

12. The compact drive system of claim 4 , wherein said electric motor assembly comprises an electric motor selected from the group comprising induction type motors, high phase order motors, permanent magnet motors, switched reluctance motors, and toroidally wound motors.

13. The compact drive system of claim 5 , wherein said toothed flex spline element has an elliptical configuration during rotation about the shaft, and wherein selected ones of the plurality of teeth of said toothed flex spline element mesh with corresponding teeth of said toothed circular spline element at opposed points 180 degrees apart along a major axis of the elliptical toothed flex spline element.

14. The compact drive system of claim 5 , wherein a number of teeth on said toothed flex spline element is at least two less than a number of teeth on said toothed circular spline element.

15. The compact drive system of claim 5 , wherein a difference in numbers or sizes of teeth between said toothed flex spline element and said toothed circular spline element is selected to produce a desired gear reduction ratio for the drive system.

16. A drive system designed to be installed completely within one or more aircraft landing gear wheels to drive the aircraft independently on the ground, comprising:
a. a motor assembly adapted to provide power to drive an aircraft wheel to move an aircraft on the ground comprising a rotor located internally of a stator; and
b. a harmonic drive assembly adapted to drive the motor assembly positioned integrally with the motor assembly in one or more aircraft landing gear wheels, comprising a wave generator positioned within a toothed flex spline and
a toothed circular spline positioned outwardly of said toothed flex spline, wherein said wave generator, said toothed flex spline, and said toothed circular spline are concentrically mounted for rotation on a shaft comprising a coaxial input and output,
said toothed flex spline has an elliptical configuration during rotation about the shaft, and
teeth of said toothed flex spline mesh with corresponding teeth of said toothed circular spline at opposed points 180 degrees apart along a major axis of the elliptical toothed flex spline, and
wherein said motor assembly and said harmonic drive assembly are configured and sized to fit completely within an interior space defined in the aircraft wheel.

Assignees

• Walitzki Hans
• Edelson Jonathan
• Cox Rodney T
• Cox Isaiah W
• Borealis Tech Ltd

Inventors

• Walitzki Hans
• Edelson Jonathan
• Cox Rodney T
• Cox Isaiah W

Classifications

• B64C25/405 Primary

  Powered wheels, e.g. for taxing · CPC title

• Y02T50/823

  Cross-Sectional Technologies · mapped topic

• Y02T50/80

  Energy efficient operational measures, e.g. ground operations or mission management · CPC title