Wheel drive system, in particular for an aircraft

• US 10,442,528 B2
• Filed: 06/30/2015
• Issued: 10/15/2019
• Est. Priority Date: 06/30/2014
• Status: Expired due to Fees

• Current Assignee: Compagnie Generale DES Etablissements Michelin SCA
• Original Assignee: Compagnie Generale DES Etablissements Michelin SCA
• Inventors: Essinger, Olivier, Marro, Patrick, Blanc, Claude
• Primary Examiner(s): Green, Richard R.
• Assistant Examiner(s): Shur, Steven J
• Application Number:
  US15/318,137
• Publication Number:
  US 20170129594A1
• Time in Patent Office: 1,568 Days
• CPC Class Codes: B64C 25/34 wheeled type, e.g. multi-wheeled bogies
• CPC Class Codes: B64C 25/40 the elements being rotated before touch-down
• CPC Class Codes: B64C 25/405 Powered wheels, e.g. for taxing
• CPC Class Codes: B64C 25/58 Arrangements or adaptations of shock-absorbers or springs shimmy-dampers B64C25/50
• CPC Class Codes: B64C 25/64 using rubber or like elements
• CPC Class Codes: Y02T 50/80 Energy efficient operational measures, e.g. ground operations or mission management

Abstract

A wheel drive system for ground movement of an aircraft includes a motor system and a clutch system. The motor system, which is borne by an unsuspended part of a landing gear strut of the aircraft, includes an electric motor and a reduction gearing system. The clutch system, which connects an output shaft of the electric motor to a wheel of the aircraft via the reduction gearing system, includes a dog-clutch and a translational movement system. The dog-clutch includes a drive part, which is secured to the motor system, and a receiving part, which secures to a tire of the wheel. The translational movement system moves the drive part along an axis of an axle crossbeam of the landing gear strut into an engaged position, in which the drive part collaborates with the receiving part, and a disengaged position, in which the drive part is separated from the receiving part.

Claims

1. A wheel drive system for ground movement of an aircraft, the wheel drive system comprising:

a motor system supported by an unsuspended part of a landing gear strut of the aircraft, the motor system including;

(a) an electric motor, and (b) a reduction gearing system; and

a clutch system, which connects an output shaft of the electric motor to a wheel of the aircraft via the reduction gearing system, the clutch system including;

(a) a dog-clutch including (i) a drive part, which is secured to the motor system, and (ii) a receiving part, which is secured to a tire of the wheel, and (b) a translational movement system, which translationally moves the drive part along an axis of an axle crossbeam of the landing gear strut into (i) an engaged position, in which the drive part collaborates with the receiving part, and (ii) a disengaged position, in which the drive part is separated from the receiving part,

wherein the receiving part includes a plurality of shock-absorbing pads overmolded directly on a lateral sidewall of the tire and extending axially from the lateral sidewall towards the drive part, the plurality of shock-absorbing pads being circumferentially spaced apart so as to leave a square-edged slot between each adjacent pair of the shock-absorbing pads.

2. The wheel drive system according to claim 1, wherein the shock-absorbing pads are made of a rubbery material.

3. The wheel drive system according to claim 2, wherein the shock-absorbing pads are made from a material that differs from a material used to form the tire.

4. The wheel drive system according to claim 1, wherein the drive part includes:

an annulus fixed to the motor system, and

a plurality of coupling fingers fixed uniformly around a circumference of the annulus such that, in the engaged position, the coupling fingers engage respectively with the square-edged slots.

5. The wheel drive system according to claim 1, wherein the translational movement system includes a connector secured to the reduction gear system of the motor system, the connector being slidingly mounted on two guide pins secured to the axle crossbeam of the unsuspended part of the landing gear strut.

6. The wheel drive system according to claim 5, wherein the translational movement system further includes:

an electric actuator fixed to the unsuspended part of the landing gear strut, and

an actuator rod slidingly connected to the electric actuator, with one end of the actuator rod being fixed to the connector, the translation movement of the actuator rod being translated into a translation movement of the connector along the guide pins.

7. The wheel drive system according to claim 1, wherein the clutch system includes a blocker, which blocks the translational movement system to cause the drive part to be kept in the disengaged position.

8. The wheel drive system according to claim 7, wherein the translational movement system includes a connector secured to the reduction gear system of the motor system, the connector being slidingly mounted on two guide pins secured to the axle crossbeam of the unsuspended part of the landing gear strut, and

wherein the blocker includes an actuating cylinder secured to the connector, the actuating cylinder including an electromagnetically actuatable piston comprising (a) a first end connected to a body of the actuating cylinder by a compression spring and (b) a second end that engages in a corresponding housing on one of the guide pins when in the disengaged position.

9. The wheel drive system according to claim 1, wherein the reduction gearing system includes:

a drive pinion connected to the output shaft of the electric motor, and

a planetary reduction gearset rotationally driven by the drive pinion and arranged to drive a reduction gearset output bevel annulus gear via a reduction gearset output bevel pinion.

10. The wheel drive system according to claim 9, wherein the drive part of the dog-clutch is fixed to the reduction gearset output bevel annulus gear.

11. The wheel drive system according to claim 9, wherein the planetary reduction gearset includes at least two reduction stages.

12. The wheel drive system according to claim 1, wherein the wheel drive system is incorporated in the aircraft.

13. An aircraft comprising:

(a) a wheel;

(b) a landing gear strut; and

(c) a wheel drive system for ground movement of the aircraft, the wheel drive system including;

(1) a motor system supported by an unsuspended part of the landing gear strut, the motor system including;

(a) an electric motor, and (b) a reduction gearing system, and (2) a clutch system, which connects an output shaft of the electric motor to the wheel via the reduction gearing system, the clutch system including;

(a) a dog-clutch including (i) a drive part, which is secured to the motor system, and (ii) a receiving part, which secures is secured to a tire of the wheel, and (b) a translational movement system, which translationally moves the drive part along an axis of an axle crossbeam of the landing gear strut into (i) an engaged position, in which the drive part collaborates with the receiving part, and (ii) a disengaged position, in which the drive part is separated from the receiving part,

wherein the receiving part includes a plurality of shock-absorbing pads overmolded directly on a lateral sidewall of the tire and extending axially towards from the lateral sidewall towards the drive part, the plurality of shock-absorbing pads being circumferentially spaced apart so as to leave a square-edged slot between each adjacent pair of the shock-absorbing pads.

14. The aircraft according to claim 13, further comprising a landing gear system that includes the landing gear strut and a pair of wheels, the pair of wheels including the wheel and a second wheel,

wherein (1) the wheel and the second wheel share the wheel drive system or (2) the second wheel is separately equipped with its own wheel drive system.