Drive system with integrated torque sensing device

Patent metadata

Field	Value
Publication number	US-12037101-B2
Application number	US-202217714534-A
Country	US
Kind code	B2
Filing date	Apr 6, 2022
Priority date	Apr 7, 2021
Publication date	Jul 16, 2024
Grant date	Jul 16, 2024

Abstract

A drive system for driving a movable flow body having a drive unit, a shaft, a torque sensing device, a no-back friction unit, and an axial bearing. The drive unit is coupled with the shaft to rotate the shaft, the torque sensing device is coupled with at least one of the drive unit and the shaft to detect a torque transferred from the drive unit into the shaft, the no-back friction unit is arranged between the axial bearing and an axial support means of the shaft, such that an axial load of the shaft is supported by the axial bearing, and the no-back friction unit is configured to substantially not counteract a rotation of the shaft in a first direction of rotation of the shaft and to apply a friction-induced additional torque to the shaft in an opposite second direction of rotation.

First claim

The invention claimed is:

1. A drive system for driving a movable flow body of an aircraft, comprising:
a drive unit,
a shaft having an axial support means,
a torque sensing device,
a no-back friction unit, and
an axial bearing,
wherein the drive unit is coupled with the shaft to rotate the shaft,
wherein the torque sensing device is coupled with at least one of the drive unit and the shaft to detect a torque transferred from the drive unit into the shaft,
wherein the no-back friction unit is disposed along a longitudinal axis of the drive system, entirely between the axial bearing and the axial support means of the shaft, such that an axial load of the shaft is supported by the axial bearing,
wherein the no-back friction unit is configured to not counteract a rotation of the shaft in a first direction of rotation of the shaft and to apply a friction-induced additional torque to the shaft in an opposite second direction of rotation,
wherein the no-back friction unit comprises a one-way clutch and a friction disc device having a first friction disc and a second friction disc in friction contact,
wherein the one-way clutch and the friction disc device are designed to mutually rotate the first friction disc and the second friction disc with the one-way clutch in the first direction of rotation of the shaft, and to provide a relative rotation between the first friction disc and the second friction disc in the second direction of rotation.

2. The drive system according to claim 1 , wherein the axial support means is a shoulder radially extending from the shaft.

3. The drive system according to claim 1 , wherein the one-way clutch comprises an inner clutch ring and an outer clutch ring, wherein the inner clutch ring is arranged between the friction disc device and the axial bearing.

4. The drive system according to claim 3 , wherein the outer clutch ring is couplable with a fixed structural part to be immovable.

5. The drive system according to claim 3 , wherein the first friction disc is coupled with the inner clutch ring.

6. The drive system according to claim 1 , wherein the torque sensing device is arranged adjacent to the no-back friction unit.

7. The drive system according to claim 1 , further comprising a load cell integrated into the shaft.

8. The drive system according to claim 1 , further comprising
a ball screw spindle coupled with a ball screw nut on the shaft.

9. The drive system according to claim 1 , further comprising a control unit couplable with the torque sensing device,
wherein the control unit is designed to receive torque representing signals from the torque sensing device, and
wherein the control unit is designed to determine a deviation between a measured torque and an expected torque and to generate a maintenance signal if the deviation exceeds a predetermined threshold.

10. A high lift system, comprising
at least one movable flow body and
at least one drive system according to claim 1 ,
wherein the at least one movable flow body is configured to be coupled with the respective one of the at least one drive system, such that the respective one of the at least one drive system is operable to extend and retract the at least one movable flow body.

11. The high lift system according to claim 10 , wherein the at least one movable flow body comprises at least one of a trailing edge flap and a slat.

12. The high lift system according to claim 10 , the at least one movable flow body is a plurality of movable flow bodies in a symmetrical arrangement, and the at least one drive system is a plurality of drive systems, wherein the plurality of the flow bodies are driven by a respective of the at least one drive system each, wherein the torque sensing devices of the drive systems are configured to couple with a skew and loss detection computer of an aircraft.

13. A wing for an aircraft, comprising at least one high lift system according to claim 10 .

14. An aircraft, comprising a wing according to claim 13 .

15. A wing for an aircraft, comprising a movable flow body coupled with a drive system according to claim 1 .

16. An aircraft, comprising a high lift system according to claim 10 .

Assignees

• Airbus Operations Gmbh

Inventors

• Haserodt Jan
• Winkelmann Christoph
• Fleddermann Andreas

Classifications

• F16D47/02

  of which at least one is a coupling · CPC title

• F16D41/02

  disengaged by contact of a part of or on the freewheel or freewheel clutch with a stationarily-mounted member · CPC title

• B64D2045/001

  for indicating symmetry of flaps deflection · CPC title

• B64C9/14

  forming slots · CPC title

• F16H2025/2075

  Coaxial drive motors · CPC title