IP Library › Granted Patent US 9,764,832
Granted Patent B2
US 9,764,832 · App. 14/510,813 · Granted Sep 19, 2017

Anti-drive mechanism for rise and fall rotating control systems

Inventors: Jason L. Hoyle (Mansfield, TX); Frank B. Stamps (Colleyville, TX)
Assignee: Bell Helicopter Textron Inc.
B64C27/605B64C27/32
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Quick Facts
Patent No.
US 9,764,832
App. No.
14/510,813
Granted
Sep 19, 2017
Kind
B2
Abstract

A rotor blade system includes a hub assembly pivotally attached to a rotor blade, a mast attached to the hub assembly, and a swashplate engaged with the mast, the swashplate includes a non-rotating ring and a rotating ring. The method to raise the swashplate includes using an anti-drive link system pivotally engaged with a transmission top case and pivotally engaged with the non-rotating ring.

Claims (52)

1. A rotor blade system, comprising:

a hub assembly pivotally attached to a rotor blade;

a mast attached to the hub assembly;

a swashplate engaged with the mast, the swashplate having:

a non-rotating ring; and

a rotating ring;

an anti-drive link system comprising:

a first and second link configured to extend relative to each other and form a gap therebetween;

wherein the anti-drive link system is pivotally engaged with a transmission top case and pivotally engaged with the non-rotating ring;

wherein the anti-drive system pivotally engages with a single drive point extending from the non-rotating ring;

wherein the mast extends thorough the gap; and

wherein the anti-drive link system is configured to raise and lower the swashplate along the mast.

2. The system of claim 1 , further comprising:

a drive system configured to drive the anti-drive link system, which in turn raises and lowers the swashplate along the mast.

3. The system of claim 2 , wherein the drive system is a hydraulic system.

4. The system of claim 1 , further comprising:

a cross link configured to engage with the first and second link.

5. The system of claim 1 , further comprising:

a third link pivotally engaged with the first and second links;

wherein the third link is pivotally attached to the non-rotating ring.

6. The system of claim 5 , wherein the third link is pivotally engaged with a drive point extending from the non-rotating ring.

7. The system of claim 5 , further comprising:

a shaft fixedly attached to the third link and configured to pivotally engage with the first and second links.

8. The system of claim 1 , wherein the anti-drive link system is configured to raise and lower the swashplate the entire collective stroke along the mast.

9. A rotor blade system, comprising:

a hub assembly pivotally attached to a rotor blade;

a mast attached to the hub assembly;

a swashplate engaged with the mast, the swashplate having:

a non-rotating ring; and

a rotating ring;

an anti-drive link system pivotally engaged with a transmission top case and pivotally engaged with the non-rotating ring, the anti-drive link system, having:

a first and second link configured to extend relative to each other and form a gap therebetween;

wherein the anti-drive system pivotally engages with a single drive point extending from the non-rotating ring;

wherein the mast extends thorough the gap; and

wherein the anti-drive link system is configured to raise and lower the swashplate along the mast.

10. The system of claim 9 , further comprising:

a drive system configured to drive the anti-drive link system, which in turn raises and lowers the swashplate along the mast.

11. The system of claim 10 , wherein the drive system is a hydraulic system.

12. The system of claim 9 , further comprising:

a cross link configured to engage with the first and second link.

13. The system of claim 9 , further comprising:

a third link pivotally engaged with the first and second links;

wherein the third link is pivotally attached to the non-rotating ring.

14. The system of claim 13 , wherein the third link is pivotally engaged with a drive point extending from the non-rotating ring.

15. The system of claim 13 , further comprising:

a shaft fixedly attached to the third link and configured to pivotally engage with the first and second links.

16. A method to raise and lower a swashplate along a mast, comprising:

providing the anti-drive link system of claim 9 ;

positioning the mast within the gap formed by the first and second links;

raising and lowering the swashplate along the mast via the anti-drive link system.

17. The method of claim 16 , further comprising:

raising and lowering the swashplate with a drive system via the anti-drive link system.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 14, 2014
From: HOYLE, JASON L.; STAMPS, FRANK B.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 033945/0637 →
Continuity (1)
Related Publication 20160101851A1 · Apr 14, 2016