Roller pinions for driving an aircraft wheel in rotation

Patent metadata

Field	Value
Publication number	US-10738871-B2
Application number	US-201815939121-A
Country	US
Kind code	B2
Filing date	Mar 28, 2018
Priority date	Mar 29, 2017
Publication date	Aug 11, 2020
Grant date	Aug 11, 2020

Abstract

A roller pinion for rotating about a central axis generally includes a core having an axial bore at its center for mounting on a drive shaft and recesses extending the length of the core. The recesses define faces with a plurality of regularly distributed sectors extending between them. The roller pinion also includes a cage associated with a plurality of rollers. The cage extends around the outer peripheral surface of the core, and presents, facing the outer peripheral surface of the core, a concentric spherical inner surface that faces the recesses of the core. Protuberances are provided that extend into the recesses. The protuberances have faces positioned parallel to and facing the faces of the recesses. Metal strips arranged in bundles with elastomer material interposed between the strips are inserted in a space between the respective faces of one recess in the core and one protuberance of the cage.

First claim

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:

1. A roller pinion for rotating about a central axis, comprising:
a core having an axial bore at a center of the core for mounting the core on a drive shaft, the core having an outer peripheral surface that is spherical, and recesses extending over the entire length of the core, the recesses defining faces parallel to the central axis, with a plurality of regularly distributed sectors extending between the recesses;
a cage supporting a plurality of rollers, the cage configured to extend around the outer peripheral surface of the core, forming a concentric spherical inner surface, wherein the cage includes protuberances extending into the recesses, the protuberances having faces positioned parallel to and facing the faces of the recesses; and
a plurality of metal strips arranged in bundles with elastomer material interposed between the strips, each bundle being inserted in a space extending between the respective faces of one recess in the core and one protuberance of the cage.

2. The roller pinion of claim 1 , wherein the rollers are carried by an annular support that is fitted onto an outer peripheral surface of the cage.

3. The roller pinion of claim 1 , wherein the peripheral outer surface of the core and the concentric spherical inner surface of the cage define a free space filled with elastomer material.

4. The roller pinion of claim 1 , wherein the peripheral outer surface of the core and the concentric spherical inner surface of the cage extend facing each other with operating clearance suitable for providing a ball-joint connection between the core and the cage.

5. The roller pinion of claim 4 , wherein the cage is split into two half-cages that are assembled together on a plane normal to the central axis.

6. The roller pinion of claim 1 , wherein balls are interposed between the core and the cage.

7. The roller pinion of claim 6 , wherein the balls extend firstly in cavities formed in the cage, and secondly in ball races formed in the core.

Assignees

• Safran Landing Systems

Inventors

• Vaslin Jean-Philippe
• Mallet Laurent
• IVALDI Frédéric
• Giraud Frédérik
• Daffos Mathieu

Classifications

• F16D3/221

  the rolling members being located in sockets in one of the coupling parts · CPC title

• F16D3/64

  comprising elastic elements arranged between substantially-radial walls of both coupling parts · CPC title

• Y02T50/80

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

• B64C25/405 Primary

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

• F16H1/006

  the driving and driven axes being designed to assume variable positions relative to one another during operation · CPC title