Internal spoke gimbal joint

Patent metadata

Field	Value
Publication number	US-11112040-B2
Application number	US-201816052468-A
Country	US
Kind code	B2
Filing date	Aug 1, 2018
Priority date	Aug 1, 2018
Publication date	Sep 7, 2021
Grant date	Sep 7, 2021

Abstract

A gimbal apparatus is disclosed, including a tubular envelope with a variable length between first and second rim structures. A rigid ring structure inside the tubular envelope is connected to diametrically opposite first and second portions of the first rim structure, and is connected to diametrically opposite first and second portions of the second rim structure. A spoke bisects the ring structure.

First claim

What is claimed is:

1. A gimbal apparatus, comprising:
a tubular envelope having a variable length between first and second rim structures,
a rigid ring structure inside the tubular envelope, the ring structure being connected to diametrically opposite first and second portions of the first rim structure, and connected to diametrically opposite first and second portions of the second rim structure, and
a first spoke bisecting the ring structure,

wherein the ring structure is a cylindrical shell having a height parallel a central axis, the height varying around a circumference of the ring structure such that the height is greatest proximate each end of the first spoke.

2. The gimbal apparatus of claim 1 , further comprising:
a second spoke bisecting the ring structure orthogonal to the first spoke.

3. The gimbal apparatus of claim 2 , wherein the first spoke spans the first and second portions of the first rim structure, and the second spoke spans the first and second portions of the second rim structure.

4. The gimbal apparatus of claim 2 , wherein the tubular envelope defines a fluid flow path, wherein each of the spokes has a cross-section including an elongate axis parallel to the direction of fluid flow.

5. The gimbal apparatus of claim 2 , wherein each spoke diminishes in dimension radially outward from the center of the ring structure.

6. The gimbal apparatus of claim 1 , wherein a first axis spanning the first and second portions of the first rim structure is orthogonal to a second axis spanning the first and second portions of the second rim structure.

7. The gimbal apparatus of claim 6 , wherein the first spoke is collinear with the first axis.

8. The gimbal apparatus of claim 6 , wherein the second rim structure can be pivotally rotated around the first axis relative to the first rim structure causing the tubular envelope to define an adjustable nonlinear fluid flow path.

9. The gimbal apparatus of claim 1 , wherein the tubular envelope includes bellows.

10. The gimbal apparatus of claim 1 , wherein the rigid ring structure is inside the first and second rim structures.

11. A gimbal joint, comprising:
a flexible envelope portion having a first end and a second end and configured to direct a flow of fluid,
a first rim fixed to the first end of the envelope portion,
a second rim fixed to the second end of the envelope portion, and
a gimbal structure including a ring and a spoke, the spoke bisecting the ring,

wherein the ring is rotatably coupled to the first rim by first and second opposing fasteners and the ring is rotatably coupled to the second rim by third and fourth opposing fasteners,
wherein the ring is a cylindrical shell having a height parallel a central axis, the height varying around a circumference of the ring such that the height is greatest proximate each end of the spoke.

12. The gimbal joint of claim 11 , wherein the spoke is a first spoke and the gimbal structure includes a second spoke, the first and second spokes being orthogonal.

13. The gimbal joint of claim 12 , wherein the first spoke, the second spoke, and the ring are a single piece.

14. The gimbal joint of claim 11 , wherein the spoke has a height parallel a central axis of the ring, a radial length, and a thickness, the thickness of the spoke being less than half the height of the spoke.

15. The gimbal joint of claim 14 , wherein the height of the spoke tapers from the central axis of the ring to each end of the spoke.

16. The gimbal joint of claim 11 , wherein the first rim is rotatable about a first axis defined by the first and second fasteners, and the second rim is rotatable about a second axis defined by the third and fourth fasteners, the first and second axes being orthogonal.

17. The gimbal joint of claim 11 , wherein each of the first, second, third, and fourth fasteners is a bolt threadedly engaged with the gimbal structure, a head of the bolt being disposed between the envelope portion and the first or second rim.

18. A feedline for an engine, comprising:
a conduit having a joint, the joint including a tubular envelope having a variable length between first and second rim structures,
a rigid ring structure inside the tubular envelope, the ring structure being connected to the first and second rim structures, and including a plurality of spokes,
wherein the ring structure and spokes form a single unitary structure,
wherein the ring structure includes a cylindrical shell having a height parallel a central axis, the height varying around a circumference of the ring structure.

19. The feedline of claim 18 , wherein the rigid ring structure consists of a solid piece of metal.

20. The feedline of claim 18 , wherein each spoke has a height parallel a central axis of the ring structure, a radial length, and a thickness, the thickness of each spoke being less than half the height of the respective spoke.

Assignees

• Boeing Co

Inventors

• Sparks Michael Stephen
• Sparks Verbon Blake

Classifications

• F16L27/06 Primary

  with special sealing means between the engaging surfaces · CPC title

• F16L27/0857

  with hinge and bellows sealing · CPC title

• F02K9/44 Primary

  Feeding propellants · CPC title

• F16L27/02

  Universal joints, i.e. with mechanical connection allowing angular movement or adjustment of the axes of the parts in any direction · CPC title

• F16L27/111

  the bellows being reinforced · CPC title