IP Library › Granted Patent US 10,494,090
Granted Patent B2
US 10,494,090 · App. 15/699,677 · Granted Dec 3, 2019

Rotor hub with structural reinforcements

Inventors: Jason C. Owens (Lewisville, TX); Frank B. Stamps (Colleyville, TX); Andrew Paul Haldeman (Fort Worth, TX); Robert P. Wardlaw (Keller, TX); John R. McCullough (Weatherford, TX); Gary Miller (North Richland Hills, TX); Andrew Ryan Maresh (Hurst, TX); Drew A. Sutton (Georgetown, KY)
Assignee: BELL HELICOPTER TEXTRON INC.
B64C27/35B64C27/48B64C27/51F16C27/00F16C2326/43
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Quick Facts
Patent No.
US 10,494,090
App. No.
15/699,677
Granted
Dec 3, 2019
Kind
B2
Abstract

In one embodiment, a rotor hub comprises a hub plate, a yoke for attaching a plurality of rotor blades, a plurality of yoke support bearings, and a plurality of cushioned damper bearings for attaching a plurality of dampers.

Claims (36)

1. A rotor hub, comprising:

a hub plate;

a yoke configured for attaching a plurality of rotor blades;

a plurality of yoke support bearings; and

a plurality of cushioned damper bearings configured for attaching a plurality of dampers, wherein each of the cushioned damper bearings further comprises a bearing support plate positioned between a damper attachment bearing and a cushion.

2. The rotor hub of claim 1 , wherein the hub plate comprises a plurality of brackets, wherein the plurality of brackets is configured to fasten the plurality of yoke support bearings between the hub plate and the yoke.

3. The rotor hub of claim 1 , wherein each yoke support bearing of the plurality of yoke support bearings comprises an elastomeric bearing.

4. The rotor hub of claim 3 , wherein the elastomeric bearing comprises a spring.

5. The rotor hub of claim 4 , wherein the spring comprises a compression spring.

6. The rotor hub of claim 1 , wherein the damper attachment bearing comprises a shear bearing.

7. The rotor hub of claim 1 , wherein the cushion comprises an elastomeric cushion.

8. The rotor hub of claim 1 , wherein the bearing support plate extends near an edge of the yoke.

9. A rotorcraft, comprising:

a rotor mast;

a plurality of rotor blades;

and

a rotor hub, comprising:

a hub plate;

a yoke coupled to the plurality of rotor blades;

a plurality of yoke support bearings; and

a plurality of cushioned damper bearings coupled to the plurality of dampers, wherein each of the cushioned damper bearings further comprises a bearing support plate positioned between a damper attachment bearing and a cushion.

10. The rotorcraft of claim 9 , wherein the hub plate comprises a plurality of brackets, wherein the plurality of brackets is configured to fasten the plurality of yoke support bearings between the hub plate and the yoke.

11. The rotorcraft of claim 9 , wherein each yoke support bearing of the plurality of yoke support bearings comprises an elastomeric bearing.

12. The rotorcraft of claim 11 , wherein the elastomeric bearing comprises a shear spring.

13. A rotor hub, comprising:

a hub plate;

a yoke configured for attaching a plurality of rotor blades;

a plurality of yoke support bearings, wherein each of the yoke support bearings comprises a shear spring; and

a plurality of cushioned damper bearings configured for attaching a plurality of dampers.

14. The rotor hub of claim 13 , wherein the hub plate comprises a plurality of brackets, wherein the plurality of brackets is configured to fasten the plurality of yoke support bearings between the hub plate and the yoke.

15. The rotor hub of claim 13 , wherein each cushioned damper bearing of the plurality of cushioned damper bearings comprises:

a damper attachment bearing; and a cushion.

16. The rotor hub of claim 15 , wherein the damper attachment bearing comprises a shear bearing.

17. The rotor hub of claim 15 , wherein the cushion comprises an elastomeric cushion.

18. The rotor hub of claim 15 , wherein each cushioned damper bearing of the plurality of cushioned damper bearings further comprises a bearing support plate positioned between the damper attachment bearing and the cushion.

19. The rotor hub of claim 18 , wherein the bearing support plate extends near an edge of the yoke.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 6, 2017
From: OWENS, JASON C.; STAMPS, FRANK B.; HALDEMAN, ANDREW PAUL; WARDLAW, ROBERT P.; MCCULLOUGH, JOHN R.; MILLER, GARY; MARESH, ANDREW RYAN; SUTTON, DREW A.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 043808/0820 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 8, 2017
From: OWENS, JASON C.; STAMPS, FRANK B.; HALDEMAN, ANDREW PAUL; WARDLAW, ROBERT P.; MCCULLOUGH, JOHN R.; MILLER, GARY; MARESH, ANDREW RYAN; SUTTON, DREW A.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 043538/0321 →
Continuity (1)
Related Publication 20190077502A1 · Mar 14, 2019
Cited By (1)
US 12,459,638