Constant velocity drive for tilt rotor assembly

Patent metadata

Field	Value
Publication number	US-9452830-B2
Application number	US-201414153482-A
Country	US
Kind code	B2
Filing date	Jan 13, 2014
Priority date	Jan 13, 2014
Publication date	Sep 27, 2016
Grant date	Sep 27, 2016

Abstract

A constant velocity drive includes a drive ring and a driven ring positioned around the drive ring. Drive links extend from the drive ring to the driven ring to transfer torque applied at the drive ring to the driven ring. Elastomeric bearings are positioned at the driven ring to transfer torque from a drive link of the plurality of drive links to the driven ring. Each elastomeric bearing includes both spherical bearing elements and planar bearing elements to allow for tilt of an axis of rotation of the driven ring with respect to an axis of rotation of the drive ring while ensuring a constant rotational velocity of the driven ring with respect to the rotational velocity of the drive ring.

First claim

What is claimed is:

1. A constant velocity drive comprising;
a drive ring having a drive ring axis of rotation;
a driven ring disposed around the drive ring and which is driven by the drive ring to rotate about a driven ring axis of rotation;
a plurality of drive links extending from the drive ring to the driven ring to transfer torque applied at the drive ring to the driven ring, each of the drive links comprising an extended portion with an outer surface; and
a plurality of elastomeric bearings, each elastomeric bearing disposed in contact with and between the driven ring and the outer surface of the extended portion of one of the plurality of drive links to transfer torque from one of the plurality of drive links to the driven ring, each elastomeric bearing including both spherical bearing elements and planar bearing elements to allow for tilt of the driven ring axis of rotation with respect to the drive ring axis of rotation while ensuring a constant rotational velocity of the driven ring with respect to the rotational velocity of the drive ring wherein a center to center distance between the spherical bearing elements of the elastomeric bearings varies as the driven ring and drive ring rotate about their respective axes of rotation.

2. The constant velocity drive of claim 1 , further comprising a gimbal bearing connected to the driven ring and which reacts the tilt of the driven ring relative to the drive ring.

3. The constant velocity drive of claim 1 , wherein each elastomeric bearing includes an intermediate race separating the spherical bearing elements from the planar bearing elements.

4. The constant velocity drive of claim 3 , wherein each elastomeric bearing includes an inner bearing race interfacing with the respective drive link of the plurality of drive links, the spherical bearing elements disposed between the inner bearing race and the intermediate race.

5. The constant velocity drive of claim 3 , wherein each elastomeric bearing includes an outer bearing race interfacing with the driven ring, the planar bearing elements disposed between the outer bearing race and the intermediate race.

6. A rotor assembly comprising:
a rotor hub;
a plurality of rotor blades extending radially outwardly from the rotor hub;
a constant velocity drive operably connecting the rotor hub to a rotor shaft including;
a drive ring having a drive ring axis of rotation and which is operably connectible to the rotor shaft;
a plurality of drive links extending from the drive ring toward the rotor hub to transfer torque applied at the drive ring to the rotor hub, each of the drive links comprising an extended portion with an outer surface; and
a plurality of elastomeric bearings, each elastomeric bearing operably connected to the rotor hub and in surrounding contact with the outer surface of the extended portion of one of the plurality of drive linksto transfer torque from one of the plurality of drive links to the rotor hub, each elastomeric bearing including both spherical bearing elements and planar bearing elements to allow for tilt of an axis of rotation of the rotor hub with respect to the drive ring axis of rotation while ensuring a constant rotational velocity of the rotor hub with respect to the rotational velocity of the drive ring, wherein as the rotor hub is tilted, a center distance between the spherical bearing elements of the elastomeric bearings varies as the rotor hub and rotor shaft rotate about their respective axes of rotation.

7. The rotor assembly of claim 6 , further comprising a driven ring secured to the rotor hub and interposed between the rotor hub and the drive ring and driven by the drive ring to rotate about a driven ring axis of rotation, the plurality of elastomeric bearings disposed at the driven ring.

8. The rotor assembly of claim 7 , further comprising a gimbal bearing connected to the driven ring and which reacts the tilt of the driven ring relative to the drive ring.

9. The rotor assembly of claim 6 , wherein each elastomeric bearing includes an intermediate race separating the spherical bearing elements from the planar bearing elements.

10. The rotor assembly of claim 9 , wherein each elastomeric bearing includes an inner bearing race interfacing with the respective drive link of the plurality of drive links, the spherical bearing elements disposed between the inner bearing race and the intermediate race.

11. The rotor assembly of claim 9 , wherein each elastomeric bearing includes an outer bearing race, the planar bearing elements disposed between the outer bearing race and the intermediate race.

12. A rotorcraft comprising:
an airframe;
a drive system disposed at the airframe, the drive system including a drive shaft rotating about a shaft axis; and
a rotor assembly operably connected to the drive system including:
a rotor hub;
a plurality of rotor blades extending radially outwardly from the rotor hub;
a constant velocity drive operably connecting the rotor hub to the rotor shaft including;
a drive ring operably connected to the rotor shaft and having a drive ring axis of rotation;
a plurality of drive links extending from the drive ring toward the rotor hub to transfer torque applied at the drive ring to the rotor hub, each of the drive links comprising an extended portion with an outer surface; and
a plurality of elastomeric bearings, each elastomeric bearing operably connected to the rotor hub and in surrounding contact with the outer surface of the extended portion of one of the plurality of drive links to transfer torque from one of the plurality of drive links to the rotor hub, each elastomeric bearing including both spherical bearing elements and planar bearing elements to allow for tilt of an axis of rotation of the rotor hub with respect to the drive ring axis of rotation while ensuring a constant rotational velocity of the rotor hub with respect to the rotational velocity of the drive ring, wherein as the rotor hub is tilted, a center distance between the spherical bearing elements of the elastomeric bearings varies as the rotor hub and rotor shaft rotate about their respective axes of rotation.

13. The rotorcraft of claim 12 , further comprising a driven ring secured to the rotor hub and interposed between the rotor hub and the drive ring and driven by the drive ring to rotate about a driven ring axis of rotation, the plurality of elastomeric bearings disposed at the driven ring.

14. The rotorcraft of claim 12 , further comprising a gimbal bearing connected to the driven ring and which reacts the tilt of the driven ring relative to the drive ring.

15. The rotorcraft of claim 12 , wherein each elastomeric bearing includes an outer bearing race, the planar bearing elements disposed between the outer bearing race and the intermediate race.

16. The rotorcraft of claim 12 , wherein each elastomeric bearing includes an intermediate race separating the spherical bearing elements from the planar bearing elements.

17. The rotorcraft of claim 16 , wherein each elastomeric bearing includes an inner bearing race interfacing with the respective drive link of the plurality of drive links, the spherical bearing elements disposed between the inner bearing race and the intermediate race.

Assignees

• Sikorsky Aircraft Corp

Inventors

• D'Anna Frank P
• Darrow Jr David A

Classifications

• B64C27/41

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

• F16D3/70

  comprising elastic elements arranged in holes in one coupling part and surrounding pins on the other coupling part · CPC title

• B64C27/35 Primary

  having elastomeric joints · CPC title

• F16D3/50

  with the coupling parts connected by one or more intermediate members (F16D3/16 takes precedence) · CPC title

• B64C27/14 Primary

  Direct drive between power plant and rotor hub · CPC title