Drive system for aircraft landing gear

Patent metadata

Field	Value
Publication number	US-10780978-B2
Application number	US-201515302886-A
Country	US
Kind code	B2
Filing date	Apr 9, 2015
Priority date	Apr 10, 2014
Publication date	Sep 22, 2020
Grant date	Sep 22, 2020

Abstract

A drive system for an aircraft landing gear is described. The drive system includes a drive pinion, a drive shaft arranged to rotate the drive pinion about a drive axis, and a casing which rotatably supports the drive shaft. The drive pinion is rotatably supported on the casing by a self-aligning bearing. The drive pinion is coupled to the drive shaft by a flexible coupling adapted to transfer torque between the drive pinion and the drive shaft and to permit tilting of the drive pinion relative to the drive axis.

First claim

The invention claimed is:

1. A drive system for an aircraft landing gear, the drive system comprising:
a drive pinion;
a drive shaft arranged to rotate the drive pinion about a drive axis; and
a casing which rotatably supports the drive shaft, wherein the drive pinion is rotatably supported on the casing by a self-aligning bearing, and wherein the drive pinion is coupled to the drive shaft by a flexible coupling adapted to transfer torque between the drive pinion and the drive shaft and to permit tilting of the drive pinion relative to the drive axis,
wherein the self-aligning bearing includes a spherical outer raceway,
wherein the self-aligning bearing includes a plurality of rolling elements arranged in one or more paths within the spherical outer raceway,
wherein the flexible coupling comprises a crowned spline joint including external teeth and internal teeth, wherein the external teeth are provided on a component fixed to a hub which supports the drive pinion, and the internal teeth are provided on the drive shaft or on a component attached to the drive shaft; and
wherein an inner surface of the spherical raceway of the self-aligning bearing and the crowned spline of the flexible coupling have substantially concentric spheres.

2. A drive system according to claim 1 , wherein the self-aligning bearing is substantially centrally located across the width of the drive pinion.

3. A drive system according to claim 1 , wherein the flexible coupling provides up to 5 degrees of rotation between the drive pinion and the drive axis.

4. A drive system according to claim 3 , wherein the flexible coupling provides up to 2.5 degrees of rotation between the drive pinion and the drive axis.

5. A drive system according to claim 1 , wherein the self-aligning bearing includes a plurality of rolling elements arranged in one or more raceways.

6. A drive system according to claim 5 , wherein the rolling elements are ball bearings or spherical rollers.

7. A drive system according to claim 5 , wherein the self-aligning bearing includes a spherical outer raceway.

8. A drive system according to claim 1 , wherein the self-aligning bearing includes an inner spherical surface in proximity to an outer spherical surface.

9. A drive system according to claim 1 , wherein the self-aligning bearing substantially prevents translation of the drive pinion along the drive axis.

10. A drive system according to claim 1 , wherein the casing and the drive pinion each include a stop to prevent excessive rotation of the drive pinion with respect to the drive axis.

11. A drive system according to claim 1 , further comprising a reduction gear arrangement, wherein the drive shaft is an output shaft of the reduction gear arrangement and the casing is a housing of the reduction gear arrangement.

12. A drive system according to claim 1 , further comprising a reduction gear arrangement, wherein the drive shaft is coupled to an output shaft of the reduction gear arrangement and the casing is a housing of the reduction gear arrangement.

13. A drive system according to claim 1 , wherein each of the series of rollers is rotatable about a pin, the pins being fixed at least at one end to an annular support member.

14. A drive system according to claim 1 , wherein the driven gear is adapted to be mounted to a hub of the wheel.

15. A drive system according to claim 14 , wherein the driven gear is adapted to be mounted to an outer rim of the hub.

16. A landing gear according to claim 1 , wherein the drive system is mounted on a fitting of the landing gear.

17. A drive system according to claim 1 , wherein the external teeth are integrally formed with the drive pinion.

18. A drive system according to claim 1 , wherein the internal teeth are integrally formed with the drive shaft.

19. A drive system according to claim 1 , wherein the flexible coupling permits some degree of misalignment between the drive shaft and drive pinion.

20. A drive system according to claim 1 , wherein the drive pinion comprises a series of rollers and the driven gear comprises a sprocket.

Assignees

• Airbus Operations Ltd

Inventors

• Didey Arnaud
• Wilson Fraser
• Briancourt Stephen
• Teague Phillip

Classifications

• F16D3/22

  the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16D3/185

  radial teeth connecting concentric inner and outer coupling parts · CPC title

• F16D3/10

  Couplings with means for varying the angular relationship of two coaxial shafts during motion · CPC title

• B64C25/405 Primary

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