Method for linking the shaft of a tachometer and an aircraft wheel

Patent metadata

Field	Value
Publication number	US-10690692-B2
Application number	US-201715728912-A
Country	US
Kind code	B2
Filing date	Oct 10, 2017
Priority date	Oct 13, 2016
Publication date	Jun 23, 2020
Grant date	Jun 23, 2020

Abstract

The invention relates to a method for linking an end ( 9 ) of a shaft ( 8 ) of a tachometer ( 7 ) positioned in a landing gear hub ( 1 ) and a wheel ( 2 ) mounted to rotate on said hub, the method comprising the step of equipping the wheel with a housing ( 14 ) suitable for receiving the end of the shaft of a tachometer and driving the shaft in rotation with the wheel, the housing comprising a bearing member ( 17 ) protruding inside the housing to be pushed back by the end of the shaft against an elastic member ( 18 ) to take up any play between the end of the shaft and the housing. The invention also relates to a bush ensuring application.

First claim

The invention claimed is:

1. A method for linking an end of a shaft of a tachometer positioned in a landing gear hub and a wheel mounted to rotate on said hub, the method comprising;
a step of equipping the wheel with a bush comprising a hollow body defining a housing suitable for receiving the end of the shaft of the tachometer and driving the shaft in rotation with the wheel, the housing comprising a receptacle in which a sleeve is mounted to rotate and the sleeve having a bearing member protruding inside the housing to be pushed back by the end of the shaft of the tachometer when the end of the tachometer shaft is engaged in the housing against a return force exerted by an elastic member to take up any play between the end of the shaft of the tachometer and the housing.

2. The method according to claim 1 ,
wherein the housing comprises a splined input followed by a receptacle for a sleeve mounted to revolve in the receptacle,
wherein the bearing member is snug inside the sleeve, and
wherein the elastic member comprises a torsion spring acting on the sleeve to return it to a position in which the snug extends between two splines when the end of the shaft of the tachometer is not engaged in the housing.

3. The method according to claim 1 , in which the bush comprises a flange for fixing the bush to a cap secured to the wheel.

4. A bush for an aircraft wheel cap to receive and drive an end of a tachometer shaft housed in a landing gear hub bearing the wheel, the bush comprising:
a hollow body defining a housing in which the end of the tachometer shaft is received, the housing having an input of section matching that of the end of the tachometer shaft followed by a cylindrical receptacle which receives a sleeve which comes into continuity with the input of the housing to receive the end of the tachometer shaft and which is mounted to rotate in the cylindrical receptacle, the sleeve having a bearing member protruding towards an interior of the sleeve which extends so as to be pushed back by the end of the tachometer shaft when the end of the tachometer shaft is engaged in the housing against a return force exerted by an elastic member.

Assignees

• Safran Landing Systems

Inventors

• Evenor Eric
• Richard Nathanael
• Roy Alain

Classifications

• B64C25/36 Primary

  Arrangements or adaptations of wheels, tyres or axles in general · CPC title

• G01P1/04 Primary

  Special adaptations of driving means · CPC title

• B64C25/34

  wheeled type, e.g. multi-wheeled bogies · CPC title