Inboard bearing assemblies with anti-rotation features

Patent metadata

Field	Value
Publication number	US-10514060-B2
Application number	US-201715698796-A
Country	US
Kind code	B2
Filing date	Sep 8, 2017
Priority date	Jul 13, 2017
Publication date	Dec 24, 2019
Grant date	Dec 24, 2019

Abstract

A bearing assembly for coupling a proprotor blade to a yoke in a proprotor system. The bearing assembly is positionable within an inboard pocket of a blade arm of the yoke. The proprotor system is operable for use on a tiltrotor aircraft having helicopter and airplane flight modes. The bearing assembly includes a centrifugal force bearing and a shear bearing having an inboard beam coupled therebetween. The centrifugal force bearing has a mating surface, a lateral movement constraint feature and at least one radially extending anti-rotation feature. The inboard beam has a mating surface in a contact relationship with the mating surface of the centrifugal force bearing, a lateral movement constraint feature operably associated with the lateral movement constraint feature of the centrifugal force bearing and at least one radially extending anti-rotation feature that corresponds with the at least one radially extending anti-rotation feature of the centrifugal force bearing.

First claim

What is claimed is:

1. A bearing assembly for coupling a proprotor blade to a yoke in a proprotor system, the bearing assembly positionable in an inboard pocket of a blade arm of the yoke, the proprotor system for a tiltrotor aircraft having a helicopter flight mode and an airplane flight mode, the bearing assembly comprising:
a centrifugal force bearing coupleable to the yoke, the centrifugal force bearing having a mating surface, a lateral movement constraint feature and at least one radially extending anti-rotation feature;
a shear bearing coupleable to the yoke; and
an inboard beam coupled between the centrifugal force bearing and the shear bearing, the inboard beam having a mating surface in a contact relationship with the mating surface of the centrifugal force bearing, a lateral movement constraint feature operably associated with the lateral movement constraint feature of the centrifugal force bearing and at least one radially extending anti-rotation feature that corresponds with the at least one radially extending anti-rotation feature of the centrifugal force bearing.

2. The bearing assembly as recited in claim 1 wherein the centrifugal force bearing is positionable outboard of the shear bearing in the inboard pocket of the blade arm of the yoke.

3. The bearing assembly as recited in claim 1 wherein the mating surfaces of the centrifugal force bearing and the inboard beam further comprise generally planar mating surfaces.

4. The bearing assembly as recited in claim 1 wherein the mating surfaces of the centrifugal force bearing and the inboard beam further comprise generally conical mating surfaces.

5. The bearing assembly as recited in claim 1 wherein the mating surfaces of the centrifugal force bearing and the inboard beam further comprise generally planar mating surface sections and generally conical mating surface sections.

6. The bearing assembly as recited in claim 1 wherein at least a portion of the mating surfaces of the centrifugal force bearing and the inboard beam have a spaced apart relationship.

7. The bearing assembly as recited in claim 1 wherein the lateral movement constraint feature and the at least one radially extending anti-rotation feature of the centrifugal force bearing are integral to one another.

8. The bearing assembly as recited in claim 1 wherein the lateral movement constraint feature and the at least one radially extending anti-rotation feature of the centrifugal force bearing are independent of one another.

9. The bearing assembly as recited in claim 1 wherein the radially extending anti-rotation features of the centrifugal force bearing and the inboard beam further comprise radially extending non-cylindrical features.

10. The bearing assembly as recited in claim 1 wherein the radially extending anti-rotation features of the centrifugal force bearing and the inboard beam further comprise radially extending multisided geometric prism features.

11. The bearing assembly as recited in claim 1 wherein the radially extending anti-rotation features of the centrifugal force bearing and the inboard beam further comprise radially extending four-sided geometric prism features.

12. The bearing assembly as recited in claim 1 wherein the radially extending anti-rotation features of the centrifugal force bearing and the inboard beam further comprise a plurality of radially extending sockets and wherein the bearing assembly further comprises a plurality of pins that extend into corresponding sockets of the centrifugal force bearing and the inboard beam.

13. The bearing assembly as recited in claim 12 wherein the plurality of radially extending sockets of the centrifugal force bearing and the inboard beam further comprises at least four radially extending sockets and the plurality of pins further comprises at least four pins extending into the corresponding sockets of the centrifugal force bearing and the inboard beam.

14. The bearing assembly as recited in claim 1 wherein the lateral movement constraint features of the centrifugal force bearing and the inboard beam further comprise radially extending non-cylindrical features.

15. The bearing assembly as recited in claim 1 wherein the lateral movement constraint features of the centrifugal force bearing and the inboard beam further comprise radially extending cylindrical features.

16. The bearing assembly as recited in claim 1 wherein the lateral movement constraint features of the centrifugal force bearing and the inboard beam further comprise radially extending multisided geometric prism features.

17. The bearing assembly as recited in claim 1 wherein the lateral movement constraint features of the centrifugal force bearing and the inboard beam further comprise radially extending four-sided geometric prism features.

18. The bearing assembly as recited in claim 1 wherein the lateral movement constraint features of the centrifugal force bearing and the inboard beam further comprise radially extending conical features.

19. A bearing assembly for coupling a proprotor blade to a yoke in a proprotor system, the bearing assembly positionable in an inboard pocket of a blade arm of the yoke, the proprotor system for a tiltrotor aircraft having a helicopter flight mode and an airplane flight mode, the bearing assembly comprising:
a centrifugal force bearing coupleable to the yoke, the centrifugal force bearing having a generally planar mating surface, a generally cylindrical lateral movement constraint feature and a plurality of radially extending anti-rotation sockets;
a shear bearing coupleable to the yoke;
an inboard beam coupled between the centrifugal force bearing and the shear bearing, the inboard beam having a generally planar mating surface in a contact relationship with the generally planar mating surface of the centrifugal force bearing, a generally cylindrical lateral movement constraint feature operably associated with the generally cylindrical lateral movement constraint feature of the centrifugal force bearing and a plurality of radially extending anti-rotation sockets that correspond with the plurality of radially extending anti-rotation sockets of the centrifugal force bearing; and
a plurality of pins that extend into corresponding sockets of the centrifugal force bearing and the inboard beam.

20. A bearing assembly for coupling a proprotor blade to a yoke in a proprotor system, the bearing assembly positionable in an inboard pocket of a blade arm of the yoke, the proprotor system for a tiltrotor aircraft having a helicopter flight mode and an airplane flight mode, the bearing assembly comprising:
a centrifugal force bearing coupleable to the yoke, the centrifugal force bearing having a generally conical mating surface and a plurality of radially extending anti-rotation sockets;
a shear bearing coupleable to the yoke;
an inboard beam coupled between the centrifugal force bearing and the shear bearing, the inboard beam having a generally conical mating surface in a contact relationship with the generally conical mating surface of the centrifugal force bearing and a plurality of radially extending anti-rotation sockets that correspond with the plurality of radially extending anti-rotation sockets of the centrifugal force bearing; and
a plurality of pins that extend into corresponding sockets of the centrifugal force bearing and the inboard beam;
wherein, contact between the generally conical mating surfaces of the centrifugal force bearing and the inboard beam provides a constraint against lateral movement therebetween.

Assignees

• Textron Innovations Inc

Inventors

• Shimek Glenn Alan
• Kizhakkepat Amarjit Olenchery
• Shundo Ken
• Dearman Michael Dean
• Cravener Kyle Thomas
• Burnett Michael Christopher

Classifications

• B64C27/39

  with individually articulated blades, i.e. with flapping or drag hinges · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• B64C27/605

  including swash plate, spider or cam mechanisms · CPC title

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title

• F16C27/063 Primary

  Sliding contact bearings · CPC title