Method for linking the shaft of a tachometer and an aircraft wheel
10690692 ยท 2020-06-23
Assignee
Inventors
- Eric Evenor (Velizy Villacoublay, FR)
- Nathanael Richard (Velizy Villacoublay, FR)
- Alain Roy (Velizy Villacoublay, FR)
Cpc classification
B64C25/34
PERFORMING OPERATIONS; TRANSPORTING
International classification
F16D1/108
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64C25/36
PERFORMING OPERATIONS; TRANSPORTING
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.
Claims
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.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will be better understood in light of the following description of an implementation of the invention, referring to the figures of the attached drawings in which:
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION OF THE INVENTION
(6) The invention applies to a landing gear of which a hub 1 can be seen which receives a wheel 2 of which the rim provided with its rolling bearings 3 can be seen here. Inside the hub 1, a cartridge 4 is inserted comprising a motor 5 driving a fan 6, and, at the rear of the motor 5, a tachometer 7 whose shaft 8 can be seen passing through the motor 5 and the fan 6 to emerge outside the hub 1. The shaft 8 has a splined end 9 which is engaged in a bush 10 secured to a wheel protection cap 11 which is secured thereto. Thus, the rotation of the wheel drives the rotation of the shaft 8, which leads the tachometer 7 to generate a signal representative of the speed of the rotation of the wheel.
(7) Referring to
(8)
(9) It will be noted that the input of the housing 14 is of flared form, allowing a slight swivelling of the end 9 of the shaft 8 in the housing 14, which contributes to reducing the stresses on the shaft 8 and thus reducing the production of noise interfering with the signal from the tachometer. Also to allow this slight swivelling, the length of the splines of the housing 14 have been reduced to the strict minimum to accept a slight angle between the axis of the shaft 8 and the central axis of the housing 14. These arrangements make it possible to absorb a flexing of the hub on landing and in taxiing, due to the forces that the ground applies to the wheel borne by the hub.
(10) The invention is not limited to what has just been described that encompasses any variant falling within the scope defined by the claims.
(11) In particular, although here the housing forms part of a bush 10 added to the wheel cap, it will more generally be possible to equip the wheel with a housing with a bearing member coming to bear on the end of the shaft against the action of an elastic member for taking up any play between the end of the shaft and the housing.