Constant velocity joint with spring rate control mechanism

Patent metadata

Field	Value
Publication number	US-9878783-B2
Application number	US-201414258187-A
Country	US
Kind code	B2
Filing date	Apr 22, 2014
Priority date	Nov 9, 2012
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

According to one embodiment, a constant velocity (CV) joint includes a first yoke, a second yoke, and three bearings. The first yoke is configured to be rotatably coupled to an input device about a first axis and configured to receive the input device through a first opening. The second yoke is rotatably coupled to the first yoke about a second axis and rotatably coupled to an output device about a third axis. The first bearing is disposed about the first axis adjacent to the first yoke, the second bearing is disposed about the second axis adjacent to the first yoke or the second yoke, and the third bearing disposed about the third axis adjacent to the second yoke. The first and third bearings torsionally constrain movement the first yoke and the second yoke so as to achieve a substantially CV characteristic between the input device and the output device.

First claim

What is claimed is:

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 hub;
a rotor blade coupled to the hub; and
a constant velocity (CV) joint coupled between the drive shaft and the hub, the CV joint comprising:
a first yoke rotatably coupled to the drive shaft about a first axis and configured to receive the drive shaft through a first opening;
a first bearing disposed about the first axis adjacent to the first yoke;
a second yoke rotatably coupled to the first yoke about a second axis and rotatably coupled to the hub about a third axis;
a second bearing disposed about the second axis adjacent to the first yoke or the second yoke; and
a third bearing disposed about the third axis adjacent to the second yoke, wherein the first and third bearings torsionally constrain movement of the first yoke and the second yoke so as to achieve a substantially CV characteristic between the drive shaft and the hub,
wherein, when the hub is tilted at a first angle relative to the drive shaft, the first and third bearings are adapted to position the first and second yokes such that the second axis is tilted at a second angle relative to the drive shaft which is smaller in magnitude than the first angle.

2. The rotorcraft of claim 1 , wherein at least one of the first bearing, the second bearing, or the third bearing comprise an elastomeric material.

3. The rotorcraft of claim 1 , wherein the second yoke is disposed at least partially about the first yoke.

4. The rotorcraft of claim 3 , wherein the second yoke is disposed completely about the first yoke.

5. The rotorcraft of claim 1 , wherein the hub is disposed about the drive shaft.

6. The rotorcraft of claim 1 , wherein the first axis is substantially normal to an axis of rotation of the drive shaft.

7. The rotorcraft of claim 1 , wherein the third axis is substantially normal to an axis of rotation of the hub.

8. The rotorcraft of claim 1 , wherein the first and third bearings are adapted to position the first and second yokes such that the second axis substantially resides on a bisector of the first angle.

9. The rotorcraft of claim 8 , wherein the second bearing is positioned to travel along an arc representing a range of bisection angles.

10. The rotorcraft of claim 1 , wherein the second bearing is disposed about the second axis adjacent to the first yoke and the second yoke.

11. The rotorcraft of claim 1 , wherein the first and third bearings are operable to torsionally constrain movement of the first yoke and the second yoke when the first and third axes are substantially collinear.

12. The rotorcraft of claim 11 , wherein the first and third bearings are operable to position the first and second yokes such that the second axis substantially resides on a bisector of the first angle when the first and third axes are substantially collinear.

13. A method of achieving a substantially constant velocity (CV) characteristic between an input device and an output device, comprising:
receiving the input device through a first opening in a first yoke, the first yoke rotatably coupled to the input device about a first axis and rotatably coupled directly to a second yoke about a second axis, the second yoke rotatably coupled to the output device about a third axis; and
constraining rotation of the first yoke about the first axis and rotation of the second yoke about the third axis so as to achieve a substantially CV characteristic between the input device and the output device.

14. The method claim 13 , wherein constraining rotation of the first yoke and the second yoke comprises constraining an orientation of the second axis.

15. A constant velocity (CV) joint comprising:
a first yoke configured to be rotatably coupled to an input device about a first axis and configured to receive the input device through a first opening;
a first bearing disposed about the first axis adjacent to the first yoke;
a second yoke rotatably coupled to the first yoke about a second axis and rotatably coupled to an output device about a third axis;
a second bearing disposed about the second axis adjacent to the first yoke or the second yoke; and
a third bearing disposed about the third axis adjacent to the second yoke, wherein the first and third bearings torsionally constrain movement of the first yoke and the second yoke so as to achieve a substantially CV characteristic between the input device and the output device,
wherein, when the output device is tilted at a first angle relative to the input device, the first and third bearings are adapted to position the first and second yokes such that the second axis is tilted at a second angle relative to the input device which is smaller in magnitude than the first angle.

16. The CV joint of claim 15 , wherein the second yoke is disposed at least partially about the first yoke.

17. The CV joint of claim 16 , wherein the second yoke is disposed completely about the first yoke.

18. The CV joint of claim 15 , wherein the first and third bearings are adapted to position the first and second yokes such that the second axis substantially resides on a bisector of the first angle.

19. The CV joint of claim 18 , wherein the second bearing is positioned to travel along an arc representing a range of bisection angles.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Sutton Drew
• Stamps Frank B
• Foskey Christopher

Classifications

• B64C27/32

  Rotors · CPC title

• B64C27/41 Primary

  with flapping hinge or universal joint, common to the blades · CPC title

• F16D3/30

  in which the coupling is specially adapted to constant velocity-ratio · CPC title

• F16D3/28

  in which the interconnecting pivots include elastic members · CPC title

• F16D3/33

  with ball or roller bearings · CPC title