Engine accessory disconnect system

Patent metadata

Field	Value
Publication number	US-10393196-B2
Application number	US-201715619527-A
Country	US
Kind code	B2
Filing date	Jun 11, 2017
Priority date	Jun 11, 2017
Publication date	Aug 27, 2019
Grant date	Aug 27, 2019

Abstract

An example system for disconnecting a driven member from a driving member is described. The system includes a vibration detection device configured to output vibration signals indicative of vibration levels of the driven member. The system also includes a controller including at least one processor. The controller is arranged to (i) determine that a vibration signal output by the vibration detection device satisfies a threshold condition and (ii) based at least on the determination that the vibration signal satisfies the threshold condition, trigger a mechanical disconnection of the driven member from the driving member by a mechanical disconnect device.

First claim

What is claimed is:

1. A system for disconnecting a driven member from a driving member, the system comprising:
a vibration detection device configured to output vibration signals indicative of vibration levels of the driven member; and
a controller comprising at least one processor, the controller arranged to (i) receive an indication of a rotation speed of the driven member, (ii) determine a disconnect threshold based on the rotation speed, (iii) determine that a vibration signal output by the vibration detection device satisfies a threshold condition, and (iv) based at least on the determination that the vibration signal satisfies the threshold condition, trigger a mechanical disconnection of the driven member from the driving member by a mechanical disconnect device,
wherein determining that the vibration signal output by the vibration detection device satisfies the threshold condition comprises determining that a magnitude of the vibration signal exceeds the disconnect threshold.

2. The system of claim 1 , further comprising the mechanical disconnect device.

3. The system of claim 2 , further comprising a relay, wherein triggering the mechanical disconnection comprises activating the relay to trigger the mechanical disconnection.

4. The system of claim 2 , wherein the mechanical disconnect device comprises a cutter configured to sever a drive shaft of the driven member.

5. The system of claim 2 , wherein the mechanical disconnect device comprises a clutch configured to disengage the driven member from the driving member.

6. The system of claim 1 , wherein the vibration detection device comprises an accelerometer.

7. The system of claim 1 :
wherein the driving member comprises an engine, and
wherein the driven member comprises an engine accessory.

8. The system of claim 7 , wherein the engine comprises an aircraft engine.

9. The system of claim 7 , wherein the engine accessory comprises an engine accessory selected from the group consisting of: a generator, a fuel pump, an oil pump, a hydraulic pump, and a compressor.

10. The system of claim 7 , wherein the vibration detection device is located on the engine accessory or is located on an accessory gearbox that drives the engine accessory.

11. A method for disconnecting a driven member from a driving member, the method comprising:
receiving, by a controller, an indication of a rotation speed of the driven member;
determining, by the controller, a disconnect threshold based on the rotation speed;
receiving, by the controller from a vibration detection device, a vibration signal that is indicative of a vibration level of the driven member;
determining, by the controller, that the received vibration signal satisfies a threshold condition, wherein determining that the received vibration signal satisfies the threshold condition comprises determining that a magnitude of the received vibration signal exceeds the disconnect threshold; and
based at least on the determination that the received vibration signal satisfies the threshold condition, triggering, by the controller, a mechanical disconnection of the driven member from the driving member by a mechanical disconnect device.

12. The method of claim 11 , wherein determining that the magnitude of the received vibration signal exceeds the disconnect threshold corresponding to the rotation speed comprises determining that for at least a predetermined time period the magnitude of the received vibration signal exceeds the disconnect threshold corresponding to the rotation speed.

13. The method of claim 11 , further comprising enhancing the received vibration signal using signal processing before determining that the received vibration signal satisfies the threshold condition, wherein enhancing the received vibration signal distinguishes vibrations due to the driven member from vibrations due to other sources of vibration.

14. The method of claim 11 , wherein triggering the mechanical disconnection comprises activating a relay that controls the mechanical disconnect device.

15. A system comprising:
a vibration detection device configured to output vibration signals while a driving member drives a driven member; and
a controller comprising at least one processor, the controller arranged to (i) determine that a vibration signal output by the vibration detection device satisfies a maintenance threshold condition (ii) based at least on the determination that the vibration signal satisfies the maintenance threshold condition, trigger generation of a maintenance notification,
wherein determining that the vibration signal satisfies the maintenance threshold condition comprises determining that a magnitude of the vibration signal exceeds a maintenance threshold but does not exceed a disconnect threshold.

16. The system of claim 15 :
wherein the driving member comprises an engine, and
wherein the driven member comprises an engine accessory.

17. The system of claim 16 , wherein the vibration detection device is located on the engine accessory or is located on an accessory gearbox that drives the engine accessory.

18. The system of claim 16 , wherein the engine comprises an aircraft engine.

Assignees

• Boeing Co

Inventors

• Smith Paul R
• Garcia Victoria L
• Farstad Jerry E
• Dunkelberg Kenneth B
• Kanning Ernest H
• Peterson Kyle A
• Will Joel R
• Malett Michel G

Classifications

• F16D2500/50293

  Reduction of vibrations · CPC title

• F16D48/06

  Control by electric or electronic means, e.g. of fluid pressure · CPC title

• G07C5/006

  Indicating maintenance · CPC title

• F01D21/045

  special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title

• F05D2270/334

  Vibration measurements · CPC title