Aircraft engine generator disconnect device with latch

Patent metadata

Field	Value
Publication number	US-11859557-B2
Application number	US-201917282606-A
Country	US
Kind code	B2
Filing date	Oct 2, 2019
Priority date	Oct 5, 2018
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

A generator drive disconnect device comprising a drive transfer means ( 100 ) having a connected configuration, and a disconnected configuration. The disconnect device further comprises a disconnect mechanism, configured to move the drive transfer means from the connected configuration to the disconnected configuration, and a latch mechanism configured to the hold the drive transfer means in the disconnected configuration. The latch mechanism includes a latch member, which is moveable between a retracted position and an extended position, and a biasing mechanism. The biasing mechanism is configured to generate a biasing force to bias the latch member towards the extended position and to apply a reaction force to the latch member to resist movement of the latch member towards the retracted position, the reaction force having a magnitude which increases as a function of the distance of the latch member from the retracted position.

First claim

The invention claimed is:

1. A generator drive disconnect device of a generator arranged to be driven by an aircraft engine, the disconnect device comprising:
a drive transfer means for transferring drive from an input shaft of the generator to a rotor of the generator, the drive transfer means having a connected configuration and a disconnected configuration;
a disconnect mechanism configured to move the drive transfer means from the connected configuration to the disconnected configuration; and
a latch mechanism configured to hold the drive transfer means in the disconnected configuration, the latch mechanism comprising:
a support structure;
a latch member, moveable between an extended position in which the latch mechanism restricts movement of the drive transfer means from the disconnected configuration to the connected configuration, and a retracted position in which the latch mechanism does not restrict movement of the drive transfer means from the disconnected configuration to the connected configuration; and
a biasing mechanism configured to generate a biasing force to bias the latch member towards the extended position and to apply a reaction force to the latch member to resist movement of the latch member towards the retracted position, the reaction force having a magnitude which increases as the distance of the latch member from the retracted position increases.

2. The generator drive disconnect device of claim 1 , further comprising a cam-follower mechanism comprising a cam surface and a follower by which the biasing force and the reaction force are applied to the latch member.

3. The generator drive disconnect device of claim 2 , wherein the latch member comprises the cam-surface and the biasing mechanism comprises the follower.

4. The generator drive disconnect device of claim 3 , wherein the biasing mechanism comprises a biasing means configured to apply the biasing force to the follower in a biasing direction.

5. The generator drive disconnect device of claim 4 , wherein the cam surface is shaped such that, when the latch member is in the retracted position, the follower is in contact with a first portion of the cam surface which is at a first angle to the biasing direction, and, when the latch member is in the extended position, the follower is in contact with a second portion of the cam surface which is at a second angle to the biasing direction, the second angle being less than the first angle.

6. The generator drive disconnect device of claim 3 , wherein the latch member comprises a latch slot which defines the cam surface and within which the follower is received such that relative movement between the latch member and the follower is constrained along the latch slot.

7. The generator drive disconnect device of claim 3 , wherein the support structure comprises a bearing surface along which the follower is configured to slide, the bearing surface being opposed to the cam surface.

8. The generator drive disconnect device of claim 7 , wherein the support structure comprises a support slot which defines the bearing surface and within which the follower is received such that the follower is constrained to move along the support slot.

9. The generator drive disconnect device of claim 7 , wherein the biasing mechanism comprises a biasing means for generating the biasing force in a biasing direction, and wherein the bearing surface is linear and is substantially parallel to the biasing direction.

10. The generator drive disconnect device of claim 2 , wherein the cam surface is curved such that the magnitude of the reaction force increases exponentially as the latch member moves towards the extended position.

11. The generator drive disconnect device of claim 1 , wherein the latch member is rotatably mounted to the support structure about a pivot for rotation between the retracted position and the extended position.

12. The generator drive disconnect device of claim 11 , wherein the pivot is positioned such that, when the latch member is in the extended position, movement of the drive transfer means towards the connected configuration biases the latch member toward the extended position.

13. The generator drive disconnect device of claim 11 , further comprising a cam-follower mechanism comprising a cam surface and a follower by which the biasing force and the reaction force are applied to the latch member, the cam follower mechanism being configured such that a position of contact between the cam surface and the follower moves away from the pivot as the latch member moves towards the extended position.

14. The generator drive disconnect device of claim 1 , wherein the disconnect mechanism comprises an actuator arranged to move the drive transfer means from the connected configuration to the disconnected configuration, and wherein the latch member comprises a latch surface which is biased against an outer surface of the actuator by the biasing mechanism to prevent movement of the actuator when the latch member is in the extended position.

15. The generator drive disconnect device of claim 14 , wherein the outer surface of the actuator comprises a recess in which at least part of the latch surface is received when the drive transfer means is in the disconnected configuration.

16. The generator drive disconnect device of claim 14 , wherein the latch surface is tapered relative to the outer surface of the actuator such that the latch surface is in contact with the outer surface of the actuator towards a radially outer end of the latch surface.

17. The generator drive disconnect device of claim 1 , wherein the support structure comprises an access port through which a latch disengage tool is insertable to return the latch member to the retracted position from the extended position.

18. An aircraft engine assembly comprising the generator drive disconnect device in accordance with claim 1 .

19. An aircraft comprising the aircraft engine assembly in accordance with claim 18 .

Assignees

• Safran Electrical & Power

Inventors

• Nixon John

Classifications

• F02C7/32 Primary

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F16D11/04 Primary

  with clutching members movable only axially · CPC title

• F16D11/14

  with clutching members movable only axially (F16D11/02, F16D11/08 take precedence) · CPC title

• F16D2011/002

  using an external and axially slidable sleeve for coupling the teeth of both coupling components together · CPC title