IP Library Granted Patent US 9,074,638
Granted Patent B2
US 9,074,638 · App. 13/828,509 · Granted Jul 7, 2015

Multilink constant velocity joint

Inventors: Christopher Foskey (Keller, TX); Frank B. Stamps (Colleyville, TX); Richard Rauber (Euless, TX)
Assignee: Bell Helicopter Textron Inc.
F16D3/60Y10T29/49643B64C27/37B64C2027/125
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Quick Facts
Patent No.
US 9,074,638
App. No.
13/828,509
Granted
Jul 7, 2015
Kind
B2
Abstract

An apparatus comprising a rotor hub system comprising a floating plate, a plurality of drive link trunnions each comprising a pivoting arm and positioned radially about the floating plate, wherein each drive link trunnion is coupled to the floating plate via the pivoting arm, and a housing disposed about the floating plate, coupled to each of the drive link trunnions, and configured to couple to a mast. Included is an apparatus comprising a floating plate, a plurality of drive link trunnions each comprising a pivoting arm and positioned radially about the floating plate, wherein each drive link trunnion is coupled to the floating plate via the pivoting arm, and wherein the drive link trunnions are configured to move the floating plate in response to a force applied to the drive link trunnions, and a housing disposed about the floating plate and coupled to each of the drive link trunnions.

Claims (30)

1. An apparatus comprising:

a rotor hub system comprising:

a floating plate;

a plurality of drive link trunnions each comprising a pivoting arm and a trunnion body and positioned radially about the floating plate, wherein each drive link trunnion is coupled to the floating plate via a respective pivoting arm, and each drive link trunnion is rotatably coupled to a housing disposed about the floating plate via a respective trunnion shaft disposed within the drive link trunnion, each drive link trunnion configured to rotate about the respective trunnion shaft to move the floating plate; and

wherein the housing is configured to couple to a mast.

2. The apparatus of claim 1 , further comprising:

a plurality of drive links each coupled to one of the trunnion bodies of the drive link trunnions; and

a yoke coupled to each of the drive links.

3. The apparatus of claim 2 , wherein the floating plate comprises a mast bore.

4. The apparatus of claim 3 , wherein the floating plate is configured to not contact the mast when being moved by the drive link trunnions.

5. The apparatus of claim 2 , wherein the rotor hub system comprises three drive link trunnions and three drive links.

6. The apparatus of claim 1 , further comprising a fuselage and an engine mechanically coupled to the mast.

7. An apparatus comprising:

a floating plate; and

a plurality of drive link trunnions each comprising a pivoting arm and a trunnion body and positioned radially about the floating plate, wherein each drive link trunnion is coupled to the floating plate via a respective pivoting arm, and each drive link trunnion is rotatably coupled to a housing disposed about the floating plate via a respective trunnion shaft disposed within the drive link trunnion;

wherein the drive link trunnions are configured to rotate about the respective trunnion shafts and move the floating plate in response to a force applied to the drive link trunnions.

8. The apparatus of claim 7 , wherein the housing is configured to engage a mast, and wherein the floating plate is configured to translate relative to the mast.

9. The apparatus of claim 8 , wherein the force comprises a plurality of lateral forces, and wherein the floating plate movement is dependent on a sum of lateral forces.

10. The apparatus of claim 9 , wherein a rotational force error is compensated by transferring the lateral forces onto the floating plate.

11. The apparatus of claim 10 , wherein the floating plate moves along a circular path.

12. The apparatus of claim 8 , wherein the floating plate is configured to not contact the mast when being moved by the drive link trunnions.

13. The apparatus of claim 12 , further comprising:

a plurality of drive links each coupled to one of the trunnion bodies of the drive link trunnions; and

a yoke coupled to each of the drive links.

14. The apparatus of claim 8 , further comprising a fuselage and an engine mechanically coupled to the mast.

15. A method comprising:

providing a rotor hub system comprising a multilink constant velocity joint (MCVJ) comprising:

a floating plate; and

a plurality of drive link trunnions each comprising a pivoting arm and a trunnion body and positioned radially about the floating plate, wherein each drive link trunnion is coupled to the floating plate via a respective pivoting arm, and each drive link trunnion is rotatably coupled to a housing disposed about the floating plate via a respective trunnion shaft disposed within the drive link trunnion; and

wherein the drive link trunnions are configured to rotate about the respective trunnion shafts and move the floating plate in response to a force applied to the drive link trunnions.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 18, 2022
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 058681/0257 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 15, 2013
From: FOSKEY, CHRISTOPHER; STAMPS, FRANK B.; RAUBER, RICHARD
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 030009/0317 →
Continuity (1)
Related Publication 20140274427A1 · Sep 18, 2014