Teetering rotor hub system

Patent metadata

Field	Value
Publication number	US-10501175-B2
Application number	US-201715401233-A
Country	US
Kind code	B2
Filing date	Jan 9, 2017
Priority date	Jan 9, 2017
Publication date	Dec 10, 2019
Grant date	Dec 10, 2019

Abstract

The present invention includes a rotor hub system, comprising: a teetering rotor hub disposed about a mast, the teetering rotor hub comprising: a first and a second yoke; each connected to a set of rotor blades, wherein the second set of rotor blades and the first set of rotor blades are disposed in a common plane, but the first and the second yoke do not come in contact.

First claim

What is claimed is:

1. A rotor hub system, comprising:
a first teetering rotor hub disposed about a mast, the first teetering rotor hub comprising:
a first yoke that is substantially flat having a bridge shape on a first plane;
a first set of rotor blades connected to the first yoke, the first set of rotor blades comprising a first rotor blade connected at a first end of the first yoke and a second rotor blade connected at a second end of the first yoke opposite the first end;

a second teetering rotor hub separate from the first teetering rotor hub, the second teetering rotor hub comprising:
a second yoke that is substantially flat having an inverse bridge shape on a second plane; and
a second set of rotor blades connected to the second yoke, the second set of rotor blades comprising a third rotor blade connected at a first end of the second yoke and a fourth rotor blade connected at a second end of the second yoke opposite the first end, wherein the first and second sets of rotor blades are in the same plane and the first and second yokes never come in contact.

2. The rotor hub system of claim 1 , wherein the first teetering rotor hub is free from contact with the second teetering rotor hub.

3. The rotor hub system of claim 1 , wherein the first set of rotor blades are rotatably offset from the second set of rotor blades by about ninety degrees with respect to a central longitudinal axis of the mast.

4. The rotor hub system of claim 1 , wherein the first yoke comprises a bridge portion adjacent to and offset from a portion of the second yoke.

5. The rotor hub of claim 4 , wherein the second yoke comprises a second bridge portion adjacent to and offset from the bridge portion of the first yoke.

6. The rotor hub system of claim 1 , further comprising:
a pitch assembly connected to the first set of rotor blades and the second set of rotor blades, the pitch assembly configured to control a pitch of the first set of rotor blades and the second set of rotor blades; and
a drive hub assembly connected to a mast and coupled to the first yoke and the second yoke, the drive hub assembly configured to drive the first yoke and the second yoke in response to rotation of the mast.

7. The rotor hub system of claim 6 , wherein the drive hub assembly comprises a mast coupling and a first, a second, a third and a fourth drive member extending from the mast coupling, wherein the first drive member is coupled to the first yoke proximate the first rotor blade, the second drive member is coupled to the first yoke proximate the second rotor blade, the third drive member is coupled to the second yoke proximate the third rotor blade, and the fourth drive member is coupled to the second yoke proximate the fourth rotor blade.

8. The rotor hub system of claim 7 , wherein each of the drive members comprises:
a drive hub arm attached to the mast coupling and extending outwardly from the mast coupling;
a drive extension coupled to the drive hub arm and a respective yoke; and
a drive bearing coupling the drive hub arm to the drive extension, wherein the drive extension is configured to pivot about the drive bearing.

9. The rotor hub system of claim 8 , wherein each of the drive hub arms is configured to flex in torsion and resist shear forces.

10. The rotor hub system of claim 8 , wherein each of the drive hub arms comprises an I-beam cross section along a length of the respective drive hub arm.

11. The rotor hub system of claim 6 , wherein the drive hub assembly connects to the first yoke and the second yoke at locations radially outward of the pitch assembly with respect to a central longitudinal axis of the mast.

12. The rotor hub system of claim 6 , wherein the drive hub assembly extends from the mast on a first, lower side of the first yoke, and the pitch assembly extends from the mast on a second, upper side of the first yoke opposite the first, lower side.

13. The rotor hub system of claim 6 , wherein the drive hub assembly and the pitch assembly each extend from the mast on a first, lower side of the first yoke.

14. The rotor hub system of claim 6 , wherein the pitch assembly comprises a pitch hub connected to the mast, a plurality of pitch links pivotly coupled to the pitch hub, and a plurality of pitch horns coupled to the pitch links and the first set of rotor blades and the second set of rotor blades.

15. The rotor hub system of claim 14 , wherein the pitch hub connects to a single degree of freedom collective control system.

16. A tail rotor hub system, comprising:
a first yoke that is substantially flat having a bridge shape and forming a first plane and a second yoke that is substantially flat disposed about a rotor mast having an inverse bridge shape and forming a second plane, wherein the first plane and the second plane are parallel and the first and second yokes do not come in contact, wherein a first portion of the first yoke overlaps a second portion of the second yoke, the first portion and the second portion spaced separately from each other, the first yoke configured to teeter about a first teetering axis, and the second yoke configured to teeter about a second teetering axis, wherein the first teetering axis and the second teetering axis are disposed in a common plane;
a first set of rotor blades connected to the first yoke, the first set of rotor blades comprising a first rotor blade connected at a first end of the first yoke and a second rotor blade connected at a second end of the first yoke opposite the first end; and
a second set of rotor blades connected to the second yoke, the second set of rotor blades comprising a third rotor blade connected at a first end of the second yoke and a fourth rotor blade connected at a second end of the second yoke opposite the first end.

17. The tail rotor hub system of claim 16 , wherein the first set of rotor blades and the second set of rotor blades are disposed in the common plane.

18. The tail rotor hub system of claim 16 , wherein the first set of rotor blades are offset from the second set of rotor blades by about ninety degrees.

19. The tail rotor hub system of claim 16 , further comprising:
a drive hub assembly coupled to the rotor mast, the first yoke, and the second yoke, the drive hub assembly configured to drive the first yoke and the second yoke in response to rotation of the rotor mast, the drive hub assembly comprising:
a plurality of drive hub arms attached to the rotor mast and extending outwardly from the rotor mast;
a plurality of drive extensions coupled to the plurality of drive hub arms and the first yoke and the second yoke; and
a plurality of drive bearings coupling the plurality of drive hub arms to the plurality of drive extensions, wherein the plurality of drive extensions are configured to teeter about the plurality of drive bearings.

20. The tail rotor hub system of claim 19 , wherein a first drive extension of the plurality of drive extensions attaches to the first end of the first yoke, a second drive extension of the plurality of drive extensions attaches to the second end of the first yoke, a third drive extension of the plurality of drive extensions attaches to the first end of the second yoke, and a fourth drive extension of the plurality of drive extensions attaches to the second end of the second yoke.

21. The tail rotor hub system of claim 19 , further comprising a pitch assembly connected to the first set of rotor blades and the second set of rotor blades, the pitch assembly configured to control a pitch of th

Assignees

• Bell Helicopter Textron Inc

Inventors

• Sutton Drew Alan
• Stamps Frank Brad

Classifications

• B64C27/43 Primary

  see-saw type, i.e. two-bladed rotor · CPC title

• B64C27/78

  in association with pitch adjustment of blades of anti-torque rotor · CPC title

• B64C27/605

  including swash plate, spider or cam mechanisms · CPC title

• B64C2027/8227

  comprising more than one rotor · CPC title

• B64C27/82

  characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft · CPC title