Drive link for tiltrotor rotor system

Patent metadata

Field	Value
Publication number	US-9657816-B2
Application number	US-201314069425-A
Country	US
Kind code	B2
Filing date	Nov 1, 2013
Priority date	Nov 1, 2013
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

A drive link includes a first bearing housing, a second bearing housing, and a central portion coupled between the first bearing housing and the second bearing housing. The central portion includes a central radial bearing configured such that the central portion twists in response to cocking of the first bearing housing relative to the second bearing housing.

First claim

What is claimed is:

1. A tiltrotor aircraft, comprising:
a body;
a wing member;
a power train coupled to the body and comprising a power source and a drive shaft in mechanical communication with the power source; and
a rotor system coupled to the wing member and in mechanical communication with the drive shaft, at least part of the rotor system being tiltable between a helicopter mode position and an airplane mode position, the rotor system comprising:
a first drive element in mechanical communication with the drive shaft;
a yoke disposed at least partially about the drive shaft;
a second drive element in mechanical communication with the yoke;
a rotor blade coupled to the yoke; and
a drive link coupled between the drive shaft and the yoke, the drive link comprising:
a first bearing housing defining an opening therethrough configured to receive the first drive element;
a first radial bearing disposed between an inner surface of the opening of the first bearing housing and an outer surface of the first drive element;
a second bearing housing defining an opening therethrough configured to receive the second drive element;
a second radial bearing disposed between an inner surface of the opening of the second bearing housing and an outer surface of the second drive element; and
a central portion coupled between the first bearing housing and the second bearing housing, the central portion including a central radial bearing configured such that the central portion twists in response to cocking of the first bearing housing relative to the second bearing housing.

2. The tiltrotor aircraft of claim 1 , wherein:
the first bearing housing, the opening of the first bearing housing, the second bearing housing, the opening of the second bearing housing, and the central portion are coaxial along a drive link axis; and
the central radial bearing defines a bearing axis that is substantially parallel to the drive link axis.

3. The tiltrotor aircraft of claim 2 , wherein the central portion has less torsional stiffness relative to the drive link axis than the first and second radial bearings.

4. The tiltrotor aircraft of claim 1 , the central portion comprising:
a central element in mechanical communication with the first bearing housing;
a central bearing housing in mechanical communication with the second bearing housing, the central bearing housing defining an opening therethrough configured to receive the central element; and
the central radial bearing disposed between an inner surface of the opening of the central bearing housing and an outer surface of the central element.

5. The tiltrotor aircraft of claim 1 , the central radial bearing comprising an elastomeric bearing.

6. The tiltrotor aircraft of claim 1 , the central radial bearing comprising a roller thrust bearing.

7. The tiltrotor aircraft of claim 1 , wherein:
the first radial bearing defines a first bearing axis; and
the central radial bearing defines a central bearing axis that is substantially perpendicular to the first bearing axis.

8. A method of transmitting torque from a drive shaft to a rotor yoke, the method comprising:
providing a drive link;
receiving, at a first bearing housing opening of the drive link, a first drive element in mechanical communication with the drive shaft;
wherein the drive link comprises a first radial bearing disposed between an inner surface of the opening of the first bearing housing and an outer surface of the first drive element;
receiving, at a second housing opening of the drive link, a second drive element in mechanical communication with the rotor yoke;
wherein the drive link comprises a second radial bearing disposed between an inner surface of the opening of the second bearing housing and an outer surface of the second drive element;
wherein the drive link comprises a central portion coupled between the first and second bearing housing, the central portion including a central radial bearing; and
allowing twisting of the central portion about the central radial bearing in response to cocking of the first bearing housing relative to the second bearing housing.

9. The method of claim 8 , the central portion comprising:
a central element in mechanical communication with the first bearing housing;
a central bearing housing in mechanical communication with the second bearing housing, the central bearing housing defining an opening therethrough configured to receive the central element; and
the central radial bearing disposed between an inner surface of the opening of the central bearing housing and an outer surface of the central element.

10. The method of claim 8 , the central radial bearing comprising an elastomeric bearing.

11. The method of claim 8 , the central radial bearing comprising a roller thrust bearing.

12. A drive link, comprising:
a first bearing housing defining an opening therethrough configured to receive a first drive element;
a first radial bearing disposed between an inner surface of the opening of the first bearing housing and an outer surface of the first drive element;
a second bearing housing defining an opening therethrough configured to receive a second drive element;
a second radial bearing disposed between an inner surface of the opening of the second bearing housing and an outer surface of the second drive element; and
a central portion coupled between the first bearing housing and the second bearing housing, the central portion including a central radial bearing configured such that the central portion twists in response to cocking of the first bearing housing relative to the second bearing housing.

13. The drive link of claim 12 , wherein:
the first bearing housing, the opening of the first bearing housing, the second bearing housing, the opening of the second bearing housing, and the central portion are coaxial along a drive link axis; and
the central radial bearing defines a bearing axis that is substantially parallel to the drive link axis.

14. The drive link of claim 13 , wherein the central portion has less torsional stiffness relative to the drive link axis than the first and second radial bearings.

15. The drive link of claim 12 , the central portion comprising:
a central element in mechanical communication with the first bearing housing;
a central bearing housing in mechanical communication with the second bearing housing, the central bearing housing defining an opening therethrough configured to receive the central element; and
the central radial bearing disposed between an inner surface of the opening of the central bearing housing and an outer surface of the central element.

16. The drive link of claim 12 , the central radial bearing comprising an elastomeric bearing.

17. The drive link of claim 12 , the central radial bearing comprising a roller thrust bearing.

18. The drive link of claim 12 , wherein:
the first radial bearing defines a first bearing axis; and
the central radial bearing defines a central bearing axis that is substantially perpendicular to the first bearing axis.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Burnett Michael
• Foskey Christopher
• Mcintyre Joel

Classifications

• F16F1/393

  with spherical or conical sleeves · CPC title

• F16C27/063

  Sliding contact bearings · CPC title

• B64C27/35

  having elastomeric joints · CPC title

• Y10T74/20006

  Resilient connections · CPC title

• F16D3/62

  the links or their attachments being elastic · CPC title