Granted Patent B2

US 12,359,697 · App. 18/511,258 · Granted Jul 15, 2025

Inventors: Karl Potier (Aix en Provence, FR); Raphael Medina (Pierrefitte sur Seine, FR)

Assignee: GOODRICH ACTUATION SYSTEMS SAS

F16D7/027B64C13/50

Abstract

Claims (39)

1. A device for selectively transmitting torque between an input shaft and an output shaft, comprising:

a first plurality of friction disks configured to rotate with the input shaft;

a second plurality of friction disks configured to rotate with the output shaft and interdigitated with the first plurality of friction disks;

a plurality of roller disks wherein each of the plurality of roller disks includes a first disk-to-roller interface with one of the first plurality of friction disks and a second disk-to-roller interface with one of the second plurality of friction disks;

a first resilient member configured to provide a force (FSPR) through the first and second plurality of friction disks and roller disks; and

a solenoid configured to overcome the force (FSPR) from the resilient member when energised;

wherein the device is configured to be selectively placed in one of a first mode and a second mode, wherein the solenoid is energised in one of the first mode and the second mode and not energised in the other of the first mode and the second mode,

wherein:

in the first mode, a first axial load path through the device configured to transmit torque below a first transmittable torque threshold is provided through each of the first and second disk-to-roller interfaces; and

in the second mode, a second axial load path through the device configured to transmit torque below a second transmittable torque threshold is provided through disk-to-disk interfaces between the disks of the first plurality of friction disks and corresponding disks of the second plurality of friction disks and through each of the first and second disk-to-roller interfaces,

wherein the second transmittable torque threshold is greater than the first transmittable torque threshold.

2. The device of claim 1 , wherein the solenoid is energised in the first mode and not energised in the second mode.

3. The device of claim 1 , wherein the first axial load path comprises a pair of load paths acting in parallel.

4. The device of claim 1 , further comprising:

a set of first splined connections between each of the first plurality of friction disks and the input shaft; and

a second set of splined connections between each of the plurality of second friction disks and the output shaft.

5. The device of claim 1 , wherein the first plurality of friction disks are carbon friction disks.

6. The device of claim 1 , wherein the second plurality of friction disks are steel friction disks.

7. The device of claim 1 , wherein the first resilient member comprises a Belleville spring.

8. The device of claim 1 , wherein each of the plurality of roller disks comprises needle thrust bearings.

9. An assembly comprising:

an input shaft;

an output shaft; and

a device according to claim 1 , wherein the device is configured to selectively transmit torque from the input shaft to the output shaft.

10. The assembly of claim 9 , wherein part of the input shaft is disposed concentrically within part of the output shaft.

11. An aircraft wing comprising:

a flight control surface; and

an assembly of claim 10 , wherein the output shaft is configured to actuate the flight control surface.

12. An aircraft comprising:

the aircraft wing of claim 11 .

13. A method of selectively transmitting torque from an input shaft to an output shaft using the device claim 1 , the method comprising:

rotating an input shaft to provide a torque above a first transmittable torque threshold and below a second transmittable torque threshold;

in a first mode:

energising the solenoid to create a first axial load path through which torque may be transmitted through the device, wherein the first axial load path through which torque may be transmitted passes through only the disk-to-roller interfaces; and

allowing rollers in the roller disks to roll so as to substantially not transmit the torque from the input shaft to the output shaft; and

in a second mode:

not energising the solenoid to create a second axial load path through the device, wherein the second axial load path through which torque may be transmitted passes through disk-to-roller interfaces and disk-to-disk interfaces; and

the disk-to-disk and disk-to-roller interfaces cumulatively transmit the torque from the input shaft to the output shaft.

14. A method of controlling a flight control surface on an aircraft wing including the method of claim 13 , wherein transmitting torque from the input shaft to the output shaft deploys or retracts the flight control surface.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (12)