IP Library › Granted Patent US 9,151,162
Granted Patent B2
US 9,151,162 · App. 13/672,309 · Granted Oct 6, 2015

Preventing rotation of a fixed ring of a swashplate

Inventors: George M. Thompson (Irving, TX); Frank B. Stamps (Colleyville, TX); Glenn A. Shimek (Kennedale, TX)
Assignee: Bell Helicopter Textron Inc.
F01D5/02B64C27/605
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,151,162
App. No.
13/672,309
Granted
Oct 6, 2015
Kind
B2
Abstract

According to one embodiment, a rotor system includes an anti-rotation sleeve featuring an outer recess portion and a tilt sleeve positioned about the anti-rotation sleeve and having an opening therethrough. A first swashplate ring is positioned about the tilt sleeve and features an inner recess portion. An anti-rotation mechanism is disposed through the opening and at least partially in the outer recess portion and the inner recess portion. The anti-rotation mechanism is operable to prevent the first swashplate ring from rotating about the anti-rotation sleeve. A second swashplate ring is positioned about the first swashplate ring and rotatable about the anti-rotation sleeve.

Claims (49)

1. A rotorcraft, comprising:

a body;

a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source;

a gearbox surrounding a portion of the drive shaft;

a hub;

a rotor blade coupled to the hub;

an anti-rotation sleeve coupled to the gearbox and featuring an outer recess portion;

a tilt sleeve positioned about the anti-rotation sleeve and having an opening therethrough, wherein the tilt sleeve is configured to slide in a strictly axial direction relative to the anti-rotation sleeve;

a first swashplate ring positioned about the tilt sleeve and featuring an inner recess portion;

an anti-rotation mechanism disposed through the opening and at least partially in the outer recess portion and the inner recess portion, the anti-rotation mechanism operable to prevent the first swashplate ring from rotating about the anti-rotation sleeve, the anti-rotation mechanism comprising:

a pin disposed through the opening and at least partially in the outer recess portion and the inner recess portion;

a key disposed at least partially in the outer recess portion and the opening and configured to receive the pin; and

a nut at least partially disposed in the outer recess portion and coupling the pin to the key; and

a second swashplate ring positioned about the first swashplate ring and rotatable about the anti-rotation sleeve with rotation of the plurality of rotor blades.

2. The rotorcraft of claim 1 , wherein:

the tilt sleeve comprises a curved surface; and

the first swashplate ring is pivotable along the curved surface.

3. The rotorcraft of claim 1 , wherein the key abuts the first swashplate ring.

4. The rotorcraft of claim 1 , wherein the outer recess portion is an elongated slot.

5. The rotorcraft of claim 1 , wherein the key abuts a surface of the anti-rotation sleeve that at least partially defines the outer recess portion.

6. The rotorcraft of claim 1 , wherein the anti-rotation sleeve is coupled to the gearbox such that the anti-rotation sleeve does not move relative to the gearbox.

7. A rotor system, comprising:

an anti-rotation sleeve featuring an outer recess portion;

a tilt sleeve positioned about the anti-rotation sleeve and having an opening therethrough, wherein the tilt sleeve is configured to slide in a strictly axial direction relative to the anti-rotation sleeve;

a first swashplate ring positioned about the tilt sleeve and featuring an inner recess portion;

an anti-rotation mechanism disposed through the opening and at least partially in the outer recess portion and the inner recess portion, the anti-rotation mechanism operable to prevent the first swashplate ring from rotating about the anti-rotation sleeve, the anti-rotation mechanism comprising:

a pin disposed through the opening and at least partially in the outer recess portion and the inner recess portion;

a key disposed at least partially in the outer recess portion and the opening and configured to receive the pin; and

a nut at least partially disposed in the outer recess portion and coupling the pin to the key; and

a second swashplate ring positioned about the first swashplate ring and rotatable about the anti-rotation sleeve.

8. The rotor system of claim 7 , further comprising a gearbox, wherein the anti-rotation sleeve is coupled to the gearbox.

9. The rotor system of claim 7 , wherein:

the tilt sleeve comprises a curved surface; and

the first swashplate ring is pivotable along the curved surface.

10. The rotor system of claim 7 , wherein the key abuts the first swashplate ring.

11. The rotor system of claim 7 , wherein the outer recess portion is an elongated slot.

12. The rotor system of claim 7 , wherein the key abuts a surface of the anti-rotation sleeve that at least partially defines the outer recess portion.

13. The rotor system of claim 7 , wherein the tilt sleeve is coupled to a gearbox such that the anti-rotation sleeve does not move relative to the gearbox.

14. A method of preventing rotation a fixed ring of a swashplate, comprising:

maintaining a tilt sleeve positioned about an anti-rotation sleeve, the anti-rotation sleeve featuring an outer recess portion, the tilt sleeve having an opening therethrough, the tilt sleeve being configured to slide in a strictly axial direction relative to the anti-rotation sleeve;

maintaining a first swashplate ring positioned about the tilt sleeve, the first swashplate ring featuring an inner recess portion;

providing an anti-rotation mechanism disposed through the opening and at least partially in the outer recess portion and the inner recess portion, the anti-rotation mechanism operable to prevent the first swashplate ring from rotating about the anti-rotation sleeve, the anti-rotation mechanism comprising:

a pin disposed through the opening and at least partially in the outer recess portion and the inner recess portion;

a key disposed at least partially in the outer recess portion and the opening and configured to receive the pin; and

a nut at least partially disposed in the outer recess portion and coupling the pin to the key;

maintaining a second swashplate ring rotatable about the first swashplate ring; and

preventing the first swashplate ring from rotating about the anti-rotation sleeve by maintaining an anti-rotation mechanism disposed through the opening and at least partially in the outer recess portion and the inner recess portion.

15. The method of claim 14 , further comprising rotating the second swashplate ring about the first swashplate ring.

16. The method of claim 14 , wherein the tilt sleeve comprises a curved surface, the method further comprising pivoting the first swashplate ring along the curved surface.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 8, 2012
From: THOMPSON, GEORGE M.; STAMPS, FRANK B.; SHIMEK, GLENN A.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 029266/0370 →
Continuity (1)
Related Publication 20140124615A1 · May 8, 2014