Rotor system with torque-splitter assembly

Patent metadata

Field	Value
Publication number	US-9254915-B2
Application number	US-201313975830-A
Country	US
Kind code	B2
Filing date	Aug 26, 2013
Priority date	Aug 26, 2013
Publication date	Feb 9, 2016
Grant date	Feb 9, 2016

Abstract

According to one embodiment, a rotor head includes a yoke, a torque-splitter assembly, and a joint assembly. The torque-splitter assembly includes a spine assembly, a first trunion, and a second trunion. The spline assembly is configured to receive the drive shaft through a first opening. The spline assembly has a first plurality of outer splines oriented in a first direction and a second plurality of outer splines oriented in a second direction different from the first direction. The first trunion is disposed about the first plurality of outer splines. The second trunion is disposed about the second plurality of outer splines.

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 in mechanical communication with the power source;
a rotor blade; and
a rotor head coupling the rotor blade to the power source, the rotor head comprising:
a yoke disposed about the drive shaft and coupled to the rotor blade;
a torque-splitter assembly comprising:
a spline assembly configured to receive the drive shaft through a first opening, the spline assembly having a first plurality of outer splines oriented in a first direction and a second plurality of outer splines oriented in a second direction different from the first direction;
a first trunion disposed about the first plurality of outer splines; and
a second trunion disposed about the second plurality of outer splines; and

a joint assembly coupling the first and second trunions to the yoke.

2. The rotorcraft of claim 1 , wherein the joint assembly is operable to achieve a substantially constant velocity (CV) characteristic between the drive shaft and the yoke.

3. The rotorcraft of claim 1 , wherein the spline assembly is configured to move axially relative to the drive shaft.

4. The rotorcraft of claim 1 , the first trunion configured to move relative to the spline assembly in the first direction.

5. The rotorcraft of claim 1 , wherein the first plurality of outer splines are arranged helically about the spline assembly.

6. The rotorcraft of claim 1 , the spline assembly comprising an outer spline member having a plurality of inner splines arranged axially on an inner portion of the outer spline member and having the first plurality of outer splines arranged on an outer portion of the outer spline member.

7. The rotorcraft of claim 6 , wherein the outer spline member is configured to move axially relative to the drive shaft along the plurality of inner splines.

8. The rotorcraft of claim 6 , the spline assembly further comprising an inner spline member disposed at least partially within the outer spline member, the inner spline member having a plurality of outer splines corresponding to the plurality of inner splines of the outer spline member.

9. The rotorcraft of claim 8 , further comprising a bearing material disposed between the inner spline member and the outer spline member.

10. The rotorcraft of claim 1 , the spline assembly comprising:
a first outer spline member having the first plurality of outer splines; and
a second outer spline member having the second plurality of outer splines.

11. The rotorcraft of claim 10 , wherein the first outer spline member is coupled to the second outer spline member.

12. A torque-splitter assembly, comprising:
a spline assembly configured to receive a drive shaft through a first opening, the spline assembly having a first plurality of outer splines oriented in a first direction and a second plurality of outer splines oriented in a second direction different from the first direction;
a first trunion disposed about the first plurality of outer splines; and
a second trunion disposed about the second plurality of outer splines.

13. The torque-splitter assembly of claim 12 , wherein the spline assembly is configured to move axially relative to the drive shaft.

14. The torque-splitter assembly of claim 12 , the first trunion configured to move relative to the spline assembly in the first direction.

15. The torque-splitter assembly of claim 12 , wherein the first plurality of outer splines are arranged helically about the spline assembly.

16. The torque-splitter assembly of claim 12 , the spline assembly comprising:
a first outer spline member having the first plurality of outer splines; and
a second outer spline member having the second plurality of outer splines.

17. The torque-splitter assembly of claim 12 , the spline assembly comprising an outer spline member having a plurality of inner splines arranged axially on an inner portion of the outer spline member and having the first plurality of outer splines arranged on an outer portion of the outer spline member.

18. The torque-splitter assembly of claim 17 , wherein the outer spline member is configured to move axially relative to the drive shaft along the plurality of inner splines.

19. The torque-splitter assembly of claim 17 , the spline assembly further comprising an inner spline member disposed at least partially within the outer spline member, the inner spline member having a plurality of outer splines corresponding to the plurality of inner splines of the outer spline member.

20. The torque-splitter assembly of claim 19 , further comprising a bearing material disposed between the inner spline member and the outer spline member.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Stamps Frank B

Classifications

• B64C27/41 Primary

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

• F16D3/42

  with ring-shaped intermediate member provided with bearings or inwardly-directed trunnions · CPC title