Mechanical clutch device and method for operating a mechanical clutch device

Patent metadata

Field	Value
Publication number	US-10753409-B2
Application number	US-201816052249-A
Country	US
Kind code	B2
Filing date	Aug 1, 2018
Priority date	Aug 18, 2017
Publication date	Aug 25, 2020
Grant date	Aug 25, 2020

Abstract

A mechanical clutch device for coupling two connecting parts in a gas turbo engine, in particular a geared aircraft turbofan engine, with means to automatically trigger a position change of one of the connecting parts relative to the respective other connecting parts and/or relative to an engine part from the first position into a second position in dependence of a torque effective on the connecting parts and/or the engine part, in particular through the transmission via a shaft, in particular a non-nominal torque, more in particular a reversal in the direction of the torque. It also relates to a method for operating a mechanical clutch device.

First claim

The invention claimed is:

1. A mechanical clutch device for coupling two connecting parts in a gas turbo engine, comprising:
a position change device for automatically triggering a position change, in at least one of the two connecting parts relative to at least one chosen from the respective other of the two connecting parts and an engine part, from a first position into a second position in dependence of a torque effective on at least one chosen from the two connecting parts and the engine part,
wherein the engine part is positioned in the first position fixedly relative to the two connecting parts and in the second position at least one of the two connecting parts is movable relative to the engine part,
wherein, in the first position, the engine part and at least one of the two connecting parts are in a pressure plate arrangement with one another such that axial pressure therebetween provides a locking arrangement, and
a clamping preloading device to apply a predetermined preload force to the mechanical clutch device;
wherein at least one of the two connecting parts is coupled to at least one chosen from an input shaft and an output shaft of a gearbox.

2. The mechanical clutch device according to claim 1 , wherein the position change device comprises at least one chosen from a helical spline connection between the two connecting parts, an automatic clutch device and a hydraulic device for changing the position from the first position to the second position.

3. The mechanical clutch device according to claim 2 , and further comprising at least one chosen from:
wherein torque transmission characteristics of the helical spline connection are asymmetric relative to the torque applied to the helical spline connection, and
the automatic clutch device is suitable for balancing axial loads.

4. The mechanical clutch device according to claim 1 , wherein in the first position, the two connecting parts are mechanically engaged with at least one chosen from each other and the engine part, so that torque is transmittable between the connecting parts, and in the second position, the two connecting parts are mechanically disengaged at least one chosen from each other and the engine part, enabling a torque-free relative movement between the two connecting parts and the engine part.

5. The mechanical clutch device according to claim 1 , and further comprising at least one chosen from:
wherein at least one of the two connecting parts is coupled to a ring gear mount of the gearbox,
wherein at least one of the two connecting parts is rigidly connected to the ring gear mount of the gearbox,
wherein at least one of the two connecting parts is one piece with the ring gear mount of the gearbox, and
wherein at least one of the two connecting parts is coupled with a static structure of the gas turbo engine.

6. The mechanical clutch device according to claim 1 , wherein the two connecting parts comprise contact interfaces to the engine part, the contact interfaces being parallel to each other.

7. The mechanical clutch device according to claim 1 , wherein the engine part comprises a ring structure which is positioned in the first position of the mechanical clutch device between the two connecting parts, and wherein the two connecting parts also comprise ring structures.

8. The mechanical clutch device according to claim 1 , and further comprising an axial retention device.

9. The mechanical clutch device according to claim 1 , wherein a connection between the at least one of the two connecting parts and the engine part comprises a high friction coating on at least one surface of an interface of the connection.

10. The mechanical clutch device according to claim 8 , wherein at least one chosen from a connection between the clamping preloading device and the engine part and a connection between the axial retention device and the at least one of the two connecting parts comprises a low friction coating on at least one surface.

11. The mechanical clutch device according to claim 1 , and further comprising at least one chosen from:
the mechanical clutch device being coupled to a propulsive fan of a geared aircraft turbofan engine, the propulsive fan suitable for driving an electrical generator in windmilling operation conditions; and
the propulsive fan suitable for being driven by an external power source when decoupled through the mechanical clutch device from a primary power source for the propulsive fan.

12. The mechanical clutch device according to claim 1 , wherein:
the gas turbo engine is a geared aircraft turbofan engine,
the position change device for automatically triggering the position change from the first position into the second position in dependence of the torque is carried out through a transmission via a shaft, wherein the torque is a non-nominal torque and there is a reversal in a direction of the torque,
wherein the engine part is friction locked with the connecting parts, and
wherein the clamping preloading device presses at least one of the two connecting parts against the engine part with a preload force.

13. The mechanical clutch device according to claim 1 , wherein the gearbox is a planetary gearbox.

14. The mechanical clutch device according to claim 1 , wherein the two connecting parts comprise contact interfaces to the engine part, the contact interfaces being angled to each other.

15. A method for operating a mechanical clutch device coupling two connecting parts in a gas turbo engine, comprising:
automatically triggering a position change of the mechanical clutch device from a first position into a second position of at least one of two connecting parts relative to at least one chosen from the respective other of the two connecting parts and an engine part in dependence of a torque effective on at least one chosen from the two connecting parts and the engine part,
wherein the engine part is positioned in the first position fixedly relative to the two connecting parts and in the second position at least one of the two connecting parts is movable relative to the engine part,
wherein, in the first position, the engine part and at least one of the two connecting parts are in a pressure plate arrangement with one another such that axial pressure therebetween provides a locking arrangement, and
applying a predetermined preload force to the mechanical clutch device;
providing that at least one of the two connecting parts is coupled to at least one chosen from an input shaft and an output shaft of a gearbox.

16. The method according to claim 15 , wherein:
the gas turbo engine is a geared aircraft turbofan engine,
the automatically triggering the position change of the mechanical clutch device from the first position into the second position in dependence of the torque is carried out through a transmission via a shaft, wherein the torque is a non-nominal torque and there is a reversal in a direction of the torque,
wherein the engine part is friction locked with the connecting parts, and
wherein the clamping preloading device presses at least one of the two connecting parts against the engine part with a preload force.

17. A mechanical clutch device for coupling two connecting parts in a gas turbo engine, comprising:
a position change device for automatically triggering a position change, in at least one of the two connecting parts relative to at least one chosen from the respective other of the two connecting parts and an engine part, from a first position into a second position in dependence of a torque effective on at least one chosen from the two conne

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Wuestenberg Hannes

Classifications

• F01D21/14

  responsive to other specific conditions · CPC title

• F16D43/215 Primary

  with flat friction surfaces, e.g. discs · CPC title

• F02K3/06

  with front fan · CPC title

• F16D41/22

  with clutching ring or disc axially shifted as a result of lost motion between actuating members (F16D41/02, F16D41/24 take precedence) · CPC title

• F05D2260/4023

  through a friction clutch · CPC title