Thermal disconnect assembly with flight control permanent magnet generator for integrated drive generator

Patent metadata

Field	Value
Publication number	US-9574618-B2
Application number	US-201414548665-A
Country	US
Kind code	B2
Filing date	Nov 20, 2014
Priority date	Nov 20, 2014
Publication date	Feb 21, 2017
Grant date	Feb 21, 2017

Abstract

A thermal disconnect assembly for an integrated drive generator includes an input shaft, an output shaft, a eutectic solder, and a disconnect clutch. The input shaft is driven by an external mechanical source. The output shaft is coupled to the input shaft through a disconnect clutch in a coupled state, is driven by the input shaft and rotates with the input shaft in the coupled state. The eutectic solder is configured to hold the output shaft in the coupled state and melt upon reaching a threshold temperature. The disconnect clutch is configured to urge the output shaft toward a decoupled state upon melting of the eutectic solder such that the output shaft does not rotate with the input shaft in the decoupled state.

First claim

The invention claimed is:

1. A thermal disconnect assembly for an integrated drive generator, the thermal disconnect assembly comprising:
an input shaft driven by an external mechanical source;
an output shaft coupled to the input shaft through a disconnect clutch in a coupled state, wherein the output shaft is driven by the input shaft and rotates with the input shaft in the coupled state;
a eutectic solder configured to hold the output shaft in the coupled state, wherein the eutectic solder is configured to melt upon reaching a threshold temperature; and
a flight control permanent magnet generator operably coupled to rotate with the output shaft, wherein the flight control generator is located annularly about the input shaft and is coupled to the input shaft through a disconnect bearing, and wherein the disconnect bearing comprises:
an inner race coupled to the input shaft and configured to rotate with the input shaft;
an outer race coupled to the flight control permanent magnet generator and configured to rotate with the flight control permanent magnet generator, wherein the outer race is coupled to the inner race through ball bearings; and
wherein the outer race and the inner race rotate together in the coupled state, and wherein the inner race rotates relative to the outer race in the decoupled state; and

wherein the disconnect clutch is configured to urge the output shaft toward a decoupled state upon melting of the eutectic solder, and wherein the output shaft does not rotate with the input shaft in the decoupled state.

2. The thermal disconnect assembly of claim 1 , wherein the input shaft and the output shaft are oriented about a common centerline, and wherein the output shaft is configured to move axially along the centerline upon melting of the eutectic solder.

3. The thermal disconnect assembly of claim 1 , wherein the flight control permanent magnet generator is operably coupled to rotate with the output shaft through an output gear.

4. The thermal disconnect assembly of claim 3 , wherein the output gear is coupled to the output shaft through a spline.

5. The thermal disconnect assembly of claim 1 , further comprising a spring that biases the output shaft to the decoupled state upon melting of the eutectic solder.

6. The thermal disconnect assembly of claim 5 , further comprising a solder collector, wherein the spring biases the output shaft into the solder collector in the decoupled state to collect the eutectic solder.

7. A method of disconnecting an input shaft from an output shaft of an integrated drive generator, the method comprising:
holding, using a eutectic solder, the input shaft and the output shaft in a coupled state;
driving, by a mechanical power source, the input shaft, wherein the input shaft rotates about a first axis;
driving, by the input shaft, the output shaft in the coupled state;
driving, by the output shaft, a permanent magnet generator oriented annularly about the input shaft, wherein the permanent magnet generator is coupled to the input shaft through a disconnect bearing;
rotating an outer race of the disconnect bearing together with an inner race of the disconnect bearing;
melting the eutectic solder upon a temperature of the eutectic solder reaching a threshold value;
moving, using a disconnect clutch, the output shaft axially away from the input shaft to a decoupled state upon melting of the eutectic solder; and
rotating the inner race of the disconnect bearing relative to the outer race of the disconnect bearing in the decoupled state.

8. The method of claim 7 , further comprising:
biasing, using a spring, the output shaft axially away from the input shaft to hold the output shaft in the decoupled state.

9. The method of claim 7 , further comprising:
collecting, using a solder collector, the melted eutectic solder, wherein the output shaft moves axially toward the solder collector to force the melted eutectic solder into the solder collector.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Lemmers Jr Glenn C

Classifications

• F16D9/02 Primary

  by thermal means, e.g. melting member · CPC title

• F16D2023/123

  Clutch actuation by cams, ramps or ball-screw mechanisms · CPC title