Systems, methods, and apparatus for supported shafts

Patent metadata

Field	Value
Publication number	US-10294982-B2
Application number	US-201615370956-A
Country	US
Kind code	B2
Filing date	Dec 6, 2016
Priority date	Mar 28, 2014
Publication date	May 21, 2019
Grant date	May 21, 2019

Abstract

Systems, methods, and apparatus are disclosed for transferring a rotational force. Apparatus include a shaft member that has a first end configured to receive a rotational force from a first mechanical component, and configured to receive a torsional load in response to receiving the rotational force. The shaft member also includes a second end configured to provide the rotational force to a second mechanical component. Apparatus also include a support member that includes a plurality of lobes coupled to the shaft member and configured to transmit the torsional load of the shaft member, where the plurality of lobes is coupled to each other along a central coupling and extend radially from the central coupling, where the plurality of lobes has a spiral geometry along a length of the support member such that an orientation of the plurality of lobes rotates along the length of the support member.

First claim

What is claimed is:

1. An apparatus for transferring a rotational force, the apparatus comprising:
a shaft member comprising:
a first end of the shaft member configured to receive the rotational force from a first mechanical component, wherein the shaft member is configured to receive a torsional load in response to receiving the rotational force at the first end,
a second end of the shaft member configured to provide the rotational force to a second mechanical component,
an outer surface, and
an inner surface, wherein the inner surface defines an internal volume of the shaft member; and

a support member included in the internal volume of the shaft member, the support member comprising a plurality of lobes coupled to the shaft member and configured to transmit the torsional load of the shaft member, wherein the plurality of lobes are coupled to each other along a central coupling and extend radially from the central coupling, wherein the central coupling is formed by a bond between the plurality of lobes, wherein the plurality of lobes has a spiral geometry along a length of the support member such that an orientation of the plurality of lobes rotates along the length of the support member.

2. The apparatus of claim 1 , wherein the plurality of lobes comprises three lobes.

3. The apparatus of claim 2 , wherein the three lobes are symmetric lobes.

4. The apparatus of claim 1 , wherein a direction of the spiral geometry is in the direction of the torsional load generated in response to the rotational force.

5. The apparatus of claim 1 , wherein the length of the support member is substantially equal to a length of the shaft member.

6. The apparatus of claim 1 , wherein the plurality of lobes is mechanically coupled to the inner surface, and wherein each lobe of the plurality of lobes extends radially from the central coupling.

7. The apparatus of claim 1 , wherein the first end is coupled to a first cap, and wherein the second end is coupled to a second cap.

8. The apparatus of claim 7 , wherein the first cap and the second cap are configured to seal the internal volume of the shaft member.

9. The apparatus of claim 7 , wherein the first cap comprises a first flange and a second flange, and wherein the second cap comprises a third flange and a fourth flange.

10. The apparatus of claim 1 , wherein the support member includes at least one of titanium, a composite material, and a polymer.

11. The apparatus of claim 1 , wherein the support member is coupled to the shaft member by a bonding process selected from a group consisting of: a welding process, a brazing process, and a soldering process.

12. A system for transferring a rotational force, the system comprising:
a first cap configured to receive the rotational force from a first mechanical component;
a shaft member coupled to the first cap, the shaft member comprising:
a first end configured to receive the rotational force from the first cap mechanically coupled with the first mechanical component, wherein the shaft member is configured to receive a torsional load in response to receiving the rotational force at the first end,
a second end opposite to the first end,
an outer surface, and
an inner surface, wherein the inner surface defines an internal volume of the shaft member;

a support member included in the internal volume of the shaft member, the support member comprising a plurality of lobes coupled to the shaft member and configured to transmit the torsional load of the shaft member, wherein the plurality of lobes are coupled to each other along a central coupling and extend radially from the central coupling, wherein the central coupling is formed by a bond between the plurality of lobes, wherein the plurality of lobes has a spiral geometry along a length of the support member such that an orientation of the plurality of lobes rotates along the length of the support member; and
a second cap coupled to the second end of the shaft member, wherein the second cap is configured to provide the rotational force to a second mechanical component.

13. The system of claim 12 , wherein the plurality of lobes comprises three symmetric lobes.

14. The system of claim 12 , wherein a direction of the spiral geometry is in a direction of the torsional load generated in response to the rotational force.

15. The system of claim 12 , wherein the plurality of lobes is mechanically coupled to the inner surface, and wherein each lobe of the plurality of lobes extends radially from the central coupling.

16. The system of claim 12 , wherein the first cap and the second cap are configured to seal the internal volume of the shaft member.

17. The system of claim 12 , wherein the first cap comprises a first flange and a second flange, and wherein the second cap comprises a third flange and a fourth flange.

18. A method of using an internally supported shaft capable of transferring a rotational force, the method comprising:
receiving, from a first mechanical component, the rotational force at a first end of a shaft member, wherein the shaft member has an outer surface and an inner surface, and wherein the inner surface defines an internal volume of the shaft member;
receiving a torsional load at the shaft member in response to receiving the rotational force;
transmitting, using support provided by a support member included in the internal volume of the shaft member, the torsional load received at the shaft member, wherein the support member comprises a plurality of lobes coupled to the shaft member and configured to transmit the torsional load of the shaft member, wherein the plurality of lobes are coupled to each other along a central coupling and extend radially from the central coupling, wherein the central coupling is formed by a bond between the plurality of lobes, and wherein the plurality of lobes has a spiral geometry along a length of the support member such that an orientation of the plurality of lobes rotates along the length of the support member;
transferring the rotational force to a second end of the shaft member; and
providing the rotational force to a second mechanical component.

19. The method of claim 18 , wherein the first end is coupled to a first cap, and wherein the second end is coupled to a second cap.

Assignees

• Boeing Co

Inventors

• Gabrys Jonathan W
• Trivedi Dinesh J

Classifications

• B29L2031/75

  Shafts · CPC title

• Y10T29/49881

  of separate helix [e.g., screw thread] · CPC title

• F16C2226/30

  Material joints · CPC title

• F16C3/023

  made of several parts, e.g. by welding · CPC title

• B33Y80/00 Primary

  Products made by additive manufacturing · CPC title