Centrifugal force bearing with piezo clutch

Patent metadata

Field	Value
Publication number	US-11618557-B2
Application number	US-202017004919-A
Country	US
Kind code	B2
Filing date	Aug 27, 2020
Priority date	Aug 27, 2020
Publication date	Apr 4, 2023
Grant date	Apr 4, 2023

Abstract

An elastomeric bearing assembly has a centrifugal force bearing axially captured relative to a sliding interface. The sliding interface has one or more low friction regions and one or more high friction regions. One or more piezo actuators are configured to force one or more corresponding high friction regions against the centrifugal force bearing when actuated. The sliding interface may have a circular shape, wherein the one or more low friction regions and the one or more high friction regions are alternating concentric segments of the sliding interface. The one or more high friction regions are recessed on the sliding interface relative to the one or more low friction regions.

First claim

What is claimed is:

1. An elastomeric bearing assembly, comprising:
a centrifugal force bearing axially captured relative to a sliding interface pad, the sliding interface pad having one or more low friction regions and one or more high friction regions; and
one or more piezo actuators configured to force one or more of the high friction regions against the centrifugal force bearing when actuated, wherein the high friction regions are configured to restrict rotation of the centrifugal force bearing when the one or more piezo actuators are actuated.

2. The elastomeric bearing assembly of claim 1 , wherein the sliding interface pad has a circular shape, and wherein the one or more low friction regions and the one or more high friction regions are alternating concentric segments of the sliding interface pad.

3. The elastomeric bearing assembly of claim 1 , wherein the one or more high friction regions are recessed on the sliding interface pad relative to the one or more low friction regions.

4. The elastomeric bearing assembly of claim 1 , wherein the sliding interface pad comprises a polytetrafluoroethylene coating in the one or more low friction regions.

5. The elastomeric bearing assembly of claim 1 , further comprising:
a spindle axially received through at least a portion of the centrifugal force bearing.

6. An elastomeric bearing assembly, comprising:
a centrifugal force bearing axially captured relative to a sliding interface, the centrifugal force bearing having a first end with a hollow region defined by an inner wall of the first end;
one or more piezo actuators disposed within the hollow region;
one or more high friction elements disposed within the hollow region, each of the high friction elements positioned between one of the piezo actuators and the inner wall; and
wherein the one or more piezo actuators are configured to force the one or more corresponding high friction elements against the inner wall when actuated.

7. The elastomeric bearing assembly of claim 6 , wherein the sliding interface has a circular shape, and wherein the sliding interface is in contact with the first end of the centrifugal force bearing.

8. The elastomeric bearing assembly of claim 6 , wherein the sliding interface comprises a polytetrafluoroethylene coating in contact with the first end of the centrifugal force bearing.

9. The elastomeric bearing assembly of claim 6 , wherein the high friction elements are configured to restrict rotation of the centrifugal force bearing when the one or more piezo actuators are actuated.

10. The elastomeric bearing assembly of claim 6 , further comprising:
a spindle axially received through at least a portion of the centrifugal force bearing.

11. A rotor assembly for a tiltrotor aircraft, comprising:
a rotor hub;
a spindle attached to the rotor hub and configured to attach a rotor blade to the rotor hub;
an elastomeric bearing assembly mounted axially on the spindle, the elastomeric bearing assembly comprising:
a centrifugal force bearing having a first end;
a sliding interface pad having one or more low friction regions in contact with the first end of the centrifugal force bearing;
one or more high friction elements; and
one or more piezo actuators configured to force one or more of the high friction elements against the centrifugal force bearing when actuated, and wherein the high friction elements are configured to restrict rotation of the centrifugal force bearing when the one or more piezo actuators are actuated.

12. The rotor assembly of claim 11 , wherein the sliding interface pad has a circular shape, and wherein the one or more low friction regions and the one or more high friction elements are alternating concentric segments of the sliding interface pad.

13. The rotor assembly of claim 11 , wherein the one or more high friction regions are recessed on the sliding interface pad relative to the one or more low friction regions.

14. The rotor assembly of claim 11 , wherein the sliding interface pad comprises a polytetrafluoroethylene coating in the one or more low friction regions.

15. The rotor assembly of claim 11 , wherein the sliding interface pad comprises a polytetrafluoroethylene coating in contact with the first end of the centrifugal force bearing.

16. The rotor assembly of claim 11 , further comprising:
a hollow region in the first end, the hollow region defined by an inner wall of the first end, wherein the one or more piezo actuators are disposed within the hollow region;
wherein the one or more high friction elements are disposed within the hollow region, each of the high friction elements positioned between one of the piezo actuators and the inner wall; and
wherein the one or more piezo actuators are configured to force the one or more of the high friction elements against the inner wall when actuated.

17. The rotor assembly of claim 11 , further comprising:
a flight control computer coupled to the one or more piezo actuators, the flight control computer configured to activate the one or more piezo actuators by applying an electrical signal to the one or more piezo actuators.

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Baskin Bryan Kenneth

Classifications

• B64C13/50

  using electrical energy · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• B64C27/35 Primary

  having elastomeric joints · CPC title

• F16C27/02

  Sliding-contact bearings · CPC title

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title