Multimode clutch assemblies having engagement status sensors

Patent metadata

Field	Value
Publication number	US-11708155-B2
Application number	US-202117516093-A
Country	US
Kind code	B2
Filing date	Nov 1, 2021
Priority date	Feb 5, 2019
Publication date	Jul 25, 2023
Grant date	Jul 25, 2023

Abstract

A multimode clutch assembly is positioned in a powertrain of a rotorcraft. The clutch assembly includes a freewheeling unit having a driving mode in which torque applied to the input race is transferred to the output race and an overrunning mode in which torque applied to the output race is not transferred to the input race. A bypass assembly has an engaged position that couples the input and output races of the freewheeling unit. An actuator assembly shifts the bypass assembly between engaged and disengaged positions. An engagement status sensor is configured to determine the engagement status of the bypass assembly. In the disengaged position, the overrunning mode of the freewheeling unit is enabled such that the clutch assembly is configured for unidirectional torque transfer. In the engaged position, the overrunning mode of the freewheeling unit is disabled such that the clutch assembly is configured for bidirectional torque transfer.

First claim

What is claimed is:

1. A multimode clutch assembly for a rotorcraft, the clutch assembly comprising:
a freewheeling unit having an input race and an output race, the freewheeling unit having a driving mode in which torque applied to the input race is transferred to the output race and an overrunning mode in which torque applied to the output race is not transferred to the input race;
a bypass assembly having an engaged position in which the bypass assembly couples the input and output races of the freewheeling unit and a disengaged position in which the bypass assembly does not couple the input and output races of the freewheeling unit;
an actuator assembly having an engagement configuration supplying an engagement force to shift the bypass assembly from the disengaged position to the engaged position and a disengagement configuration supplying a disengagement force to shift the bypass assembly from the engaged position to the disengaged position, the actuator assembly including a liner, a piston and a bearing sled, the piston slidably disposed relative to the liner, the bearing sled coupled between the piston and the bypass assembly; and
an inductive proximity sensor operably associated with the actuator assembly, the inductive proximity sensor configured to monitor the position of the bearing sled relative thereto to determine an engagement status of the bypass assembly;
wherein, in the disengaged position of the bypass assembly, the overrunning mode of the freewheeling unit is enabled such that the clutch assembly is configured for unidirectional torque transfer from the input race to the output race; and
wherein, in the engaged position of the bypass assembly, the overrunning mode of the freewheeling unit is disabled such that the clutch assembly is configured for bidirectional torque transfer between the input and output races.

2. The clutch assembly as recited in claim 1 wherein the engagement force is configured to shift the bypass assembly from the disengaged position to the engaged position when the disengagement force is not provided.

3. The clutch assembly as recited in claim 1 wherein the actuator assembly further comprises a mechanical biasing element configured to provide the engagement force.

4. The clutch assembly as recited in claim 1 wherein the actuator assembly further comprises a pressurized lubricating oil configured to provide the engagement force.

5. The clutch assembly as recited in claim 1 wherein the actuator assembly further comprises a pressure switch configured to selectively provide the disengagement force.

6. The clutch assembly as recited in claim 5 wherein the pressure switch further comprises a hydraulic switch.

7. The clutch assembly as recited in claim 5 wherein the pressure switch further comprises a compressed air switch.

8. The clutch assembly as recited in claim 1 wherein the actuator assembly further comprises an electric switch configured to selectively provide the disengagement force.

9. The clutch assembly as recited in claim 1 wherein the actuator assembly is in a default configuration when the disengagement force is not provided.

10. A multimode clutch assembly for a rotorcraft, the clutch assembly comprising:
a freewheeling unit having an input race and an output race, the freewheeling unit having a driving mode in which torque applied to the input race is transferred to the output race and an overrunning mode in which torque applied to the output race is not transferred to the input race;
a bypass assembly having an engaged position in which the bypass assembly couples the input and output races of the freewheeling unit and a disengaged position in which the bypass assembly does not couple the input and output races of the freewheeling unit;
an actuator assembly having an engagement configuration supplying an engagement force to shift the bypass assembly from the disengaged position to the engaged position and a disengagement configuration supplying a disengagement force to shift the bypass assembly from the engaged position to the disengaged position; and
a variable differential transformer operably associated with at least one of the bypass assembly and the actuator assembly, the variable differential transformer configured to determine an engagement status of the bypass assembly;
wherein, in the disengaged position of the bypass assembly, the overrunning mode of the freewheeling unit is enabled such that the clutch assembly is configured for unidirectional torque transfer from the input race to the output race; and
wherein, in the engaged position of the bypass assembly, the overrunning mode of the freewheeling unit is disabled such that the clutch assembly is configured for bidirectional torque transfer between the input and output races.

11. The clutch assembly as recited in claim 10 wherein the variable differential transformer further comprises a linear variable differential transformer.

12. The clutch assembly as recited in claim 10 wherein the variable differential transformer further comprises a rotary variable differential transformer.

13. The clutch assembly as recited in claim 10 wherein the engagement force is configured to shift the bypass assembly from the disengaged position to the engaged position when the disengagement force is not provided.

14. The clutch assembly as recited in claim 10 wherein the actuator assembly further comprises a mechanical biasing element configured to provide the engagement force.

15. The clutch assembly as recited in claim 10 wherein the actuator assembly further comprises a pressurized lubricating oil configured to provide the engagement force.

16. The clutch assembly as recited in claim 10 wherein the actuator assembly further comprises a pressure switch configured to selectively provide the disengagement force.

17. The clutch assembly as recited in claim 16 wherein the pressure switch further comprises a hydraulic switch.

18. The clutch assembly as recited in claim 16 wherein the pressure switch further comprises a compressed air switch.

19. The clutch assembly as recited in claim 10 wherein the actuator assembly further comprises an electric switch configured to selectively provide the disengagement force.

20. The clutch assembly as recited in claim 10 wherein the actuator assembly is in a default configuration when the disengagement force is not provided.

Assignees

• Textron Innovations Inc

Inventors

• Goodwin Douglas Andrew
• Prater David Andrew
• Olson Eric Stephen
• Roberts David Bryan
• Su Chia-Wei
• Trantham Michael David
• Covington Charles Eric

Classifications

• B64D35/08

  characterised by the transmission being driven by a plurality of power plants (for hybrid-electric power plants B64D35/022) · CPC title

• B64D27/33

  Hybrid electric aircraft · CPC title

• B64C27/12 Primary

  Rotor drives · CPC title

• F16D41/04

  combined with a clutch for locking the driving and driven members (F16D41/02, F16D41/24 take precedence) · CPC title

• B64D2027/026

  Operations & Transport · mapped topic