Multi-plate clutch

Patent metadata

Field	Value
Publication number	US-9951825-B2
Application number	US-201414915098-A
Country	US
Kind code	B2
Filing date	Jun 24, 2014
Priority date	Aug 28, 2013
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A multi-plate clutch apparatus is provided and includes a multi-plate clutch disposed to occupy clutch and non-clutch positions at which rotation of an input shaft is and is not transmitted to an output shaft, respectively, a drive element disposed about the multi-plate clutch and configured to generate rotational energy and a linear actuator disposed to convert the rotational energy of the drive element to linear movement by which the multi-plate clutch is controllable to occupy one of the clutch and non-clutch positions.

First claim

The invention claimed is:

1. A multi-plate clutch apparatus, comprising:
an outer housing having an external surface, a gear being defined by the external surface;
an inner housing arranged within the outer housing;
a multi-plate clutch arranged within the inner housing, the multi-plate clutch being disposed to occupy clutch and non-clutch positions at which rotation of an input shaft is and is not transmitted to an output shaft, respectively;
a drive element disposed about the multi-plate clutch and configured to generate rotational energy, the drive element having a gear element meshingly engaged with the gear defined by the external surface of the housing; and
a linear actuator disposed to convert the rotational energy of the drive element to linear movement by which the multi-plate clutch is controllable to occupy one of the clutch and non-clutch positions.

2. The multi-plate clutch apparatus according to claim 1 , wherein the input and output shafts are disposed in an end-to-end parallel alignment.

3. The multi-plate clutch apparatus according to claim 1 , wherein the multi-plate clutch comprises:
a first plate coupled to and rotatable with the input shaft;
a second plate coupled to and rotatable with the output shaft;
a plate assembly interposed between and coupled to the first and second plates; and
a movable plate movable with the linear actuator to cause the plate assembly to provide for engagement or disengagement of the first and second plates.

4. The multi-plate clutch apparatus according to claim 3 , wherein the plate assembly comprises a plurality of interleaved thrust and washer plates.

5. The multi-plate clutch apparatus according to claim 3 , wherein the multi-plate clutch further comprises a roller bearing interposed between the input shaft and the movable plate.

6. The multi-plate clutch apparatus according to claim 1 , wherein the drive element comprises a servo motor.

7. The multi-plate clutch apparatus according to claim 1 , wherein the drive element is configured with a hard-over failure safety.

8. The multi-plate clutch apparatus according to claim 1 , wherein the linear actuator comprises a ball-screw drive element.

9. The multi-plate clutch apparatus according to claim 1 , wherein the linear actuator comprises a spur ring engageable with a spur gear of the drive element.

10. The multi-plate clutch according to claim 1 , wherein the drive element comprises a plurality of drive elements arranged about the housing.

11. An aircraft, comprising: an engine;
a propeller; and
a multi-plate clutch apparatus disposed between the engine and the propeller and comprising:
an outer housing having an external surface, a gear being defined by the external surface;
an inner housing arranged within the outer housing;
a multi-plate clutch arranged within the inner housing, the multi-plate clutch being disposed to occupy clutch and non-clutch positions at which engine-driven rotation of an input shaft is and is not transmitted to an output shaft coupled to the propeller, respectively;
a drive element disposed about the multi-plate clutch and configured to generate rotational energy, the drive element having a gear element meshingly engaged with the gear defined by the external surface of the housing; and
a linear actuator disposed to convert the rotational energy of the drive element to linear movement by which the multi-plate clutch is controllable to occupy one of the clutch and non-clutch positions.

12. The aircraft according to claim 11 , wherein the multi-plate clutch comprises:
a first plate coupled to and rotatable with the input shaft;
a second plate coupled to and rotatable with the output shaft;
a plate assembly interposed between and coupled to the first and second plates; and
a movable plate movable with the linear actuator to cause the plate assembly to provide for engagement or disengagement of the first and second plates.

13. The aircraft according to claim 11 , wherein the drive element comprises a servo motor.

14. The aircraft according to claim 11 , wherein the drive element is configured with a hard-over failure safety.

15. The aircraft according to claim 11 , wherein the linear actuator comprises a ball-screw drive element.

16. The aircraft according to claim 11 , wherein the linear actuator comprises a spur ring engageable with a spur gear of the drive element.

17. The aircraft according to claim 11 , wherein the drive element comprises a plurality of drive elements arranged about the housing.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Darrow David A
• Tully Jr Thomas L

Classifications

• B64C2027/8236

  including pusher propellers · CPC title

• B64C27/82

  characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft · CPC title

• B64D35/00

  Transmitting power from power plants to propellers or rotors; Arrangements of transmissions · CPC title

• B64C27/12

  Rotor drives · CPC title

• B64C27/22

  Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft · CPC title