Composite tube assemblies and methods

Patent metadata

Field	Value
Publication number	US-9726325-B2
Application number	US-201414267720-A
Country	US
Kind code	B2
Filing date	May 1, 2014
Priority date	May 1, 2014
Publication date	Aug 8, 2017
Grant date	Aug 8, 2017

Abstract

Composite tubes comprising a compression sleeve coupled to an inner surface of a composite tube, a carbon extrusion member disposed within the composite tube, and an end fitting comprising a locking feature, wherein the end fitting is coupled to an inner surface of the compression sleeve and the locking feature is configured to engage the carbon extrusion member are disclosed. Methods comprising coupling a compression sleeve to an inner surface of a distal end of a composite tube, placing a carbon extrusion member inside the compression sleeve and the composite tube, and disposing an end fitting on the distal end of the composite tube, wherein the end fitting comprises a locking feature configured to interact with the carbon extrusion member are also disclosed.

First claim

What is claimed is:

1. A composite tube assembly comprising:
a compression sleeve coupled to an inner surface of a composite tube;
a carbon extrusion member disposed within the composite tube; and
an end fitting comprising a locking feature extending from the end fitting, wherein the end fitting is coupled to an inner surface of the compression sleeve and the locking feature is configured to engage the carbon extrusion member.

2. The composite tube assembly of claim 1 , wherein the end fitting is threaded.

3. The composite tube assembly of claim 1 , wherein an outer surface of the compression sleeve is configured to interface with the inner surface of the composite tube.

4. The composite tube assembly of claim 1 , wherein the composite tube comprises low angle carbon fibers.

5. The composite tube assembly of claim 1 , wherein the composite tube comprises high angle carbon fibers at a distal end of the composite tube.

6. The composite tube assembly of claim 1 , wherein the locking feature is configured to radially expand the carbon extrusion member.

7. The composite tube assembly of claim 1 , wherein the end fitting and the compression sleeve comprise a metal.

8. The composite tube assembly of claim 1 , wherein at least a portion of the carbon extrusion member is disposed within the compression sleeve.

9. The composite tube assembly of claim 1 , wherein the composite tube is bonded with the compression sleeve.

10. The composite tube assembly of claim 9 , wherein the composite tube is co-cured to the compression sleeve.

11. The composite tube assembly of claim 1 , wherein the composite tube comprises a polymer-matrix composite.

12. The composite tube assembly of claim 11 , wherein the composite tube comprises carbon fiber.

13. A method of manufacture comprising:
coupling a compression sleeve to an inner surface of a distal end of a composite tube;
placing a carbon extrusion member inside the compression sleeve and the composite tube; and
disposing an end fitting on the distal end of the composite tube, wherein the end fitting comprises a locking feature configured to interact with the carbon extrusion member.

14. The method according to claim 13 , wherein the disposing the end fitting comprises screwing the end fitting into the compression sleeve.

15. The method according to claim 13 , wherein the coupling comprises co-curing.

16. The method according to claim 13 , wherein the coupling comprises coupling the compression sleeve to the inner surface of the distal end of the composite tube with an adhesive.

Assignees

• Goodrich Corp

Inventors

• Ganis Rony Giovanni
• Giddings Peter F

Classifications

• B32B37/18

  involving the assembly of discrete sheets or panels only · CPC title

• F16C7/026 Primary

  made of fibre reinforced resin · CPC title

• B32B2605/18

  Aircraft · CPC title

• F16S3/04 Primary

  designed for being joined to similar members in various relative positions · CPC title

• B32B37/142

  Laminating of sheets, panels or inserts, e.g. stiffeners, by wrapping in at least one outer layer, or inserting into a preformed pocket · CPC title