IP Library Granted Patent US 10,994,512
Granted Patent B2
US 10,994,512 · App. 16/389,619 · Granted May 4, 2021

Hybrid composite tube systems and methods

Inventor: Sandeep Daivajna (Sagar, IN)
Assignee: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
B32B5/26B32B1/08B32B5/02F16L11/08B32B2255/02B32B2260/021B32B2260/046B32B2262/101B32B2307/304B32B2597/00
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Quick Facts
Patent No.
US 10,994,512
App. No.
16/389,619
Granted
May 4, 2021
Kind
B2
Abstract

A hybrid composite tube includes a metallic tube, a first silica fiber layer positioned radially of the metallic tube, a fiber reinforced polymer layer positioned radially of the first silica fiber layer, and a second silica fiber layer positioned radially of the fiber reinforced polymer layer, wherein the first silica fiber layer thermally insulates the fiber reinforced polymer layer and the second silica fiber layer thermally insulates the fiber reinforced polymer layer.

Claims (33)

1. A hybrid composite tube, comprising:

a metallic tube;

a first silica fiber layer positioned radially of the metallic tube;

a fiber reinforced polymer layer positioned radially of the first silica fiber layer; and

a second silica fiber layer positioned radially of the fiber reinforced polymer layer;

wherein the first silica fiber layer thermally insulates the fiber reinforced polymer layer and the second silica fiber layer thermally insulates the fiber reinforced polymer layer.

2. The hybrid composite tube of claim 1 , wherein the metallic tube, the first silica fiber layer, the fiber reinforced polymer layer, and the second silica fiber layer, are concentric and the first silica fiber layer surrounds the metallic tube, the fiber reinforced polymer layer surrounds the first silica fiber layer, and the second silica fiber layer surrounds the fiber reinforced polymer layer.

3. The hybrid composite tube of claim 2 , wherein the first silica fiber layer thermally insulates the fiber reinforced polymer layer from the metallic tube.

4. The hybrid composite tube of claim 3 , wherein at least one of the first silica fiber layer and the second silica fiber layer protects the fiber reinforced polymer layer from thermal combustion.

5. The hybrid composite tube of claim 3 , wherein the first silica fiber layer comprises a silica fabric.

6. The hybrid composite tube of claim 5 , wherein the second silica fiber layer comprises at least one of a plurality of glass fibers coated in a silicone rubber, and a silica fabric; and

the fiber reinforced polymer layer comprises at least one of a glass fiber reinforced epoxy and a carbon fiber reinforced epoxy.

7. The hybrid composite tube of claim 3 , wherein the hybrid composite tube is at least twenty five percent lighter than a fully metallic tube of similar strength.

8. The hybrid composite tube of claim 5 , wherein the fiber reinforced polymer layer comprises a plurality of fibers oriented at an angle with respect to a tube axis.

9. The hybrid composite tube of claim 3 , wherein the second silica fiber layer comprises a wall-thickness which varies along a long a tube axis to vary a thermal insulation property of the second silica fiber layer.

10. A hybrid composite tube, comprising:

a metallic tube;

a first silica fiber layer positioned radially of the metallic tube;

a fiber reinforced polymer layer positioned radially of the first silica fiber layer; and

a second silica fiber layer positioned radially of the fiber reinforced polymer layer.

11. The hybrid composite tube of claim 10 , wherein the first silica fiber layer surrounds the metallic tube, the fiber reinforced polymer layer surrounds the first silica fiber layer, and the second silica fiber layer surrounds the fiber reinforced polymer layer, wherein the metallic tube, the first silica fiber layer, the fiber reinforced polymer layer, and the second silica fiber layer, are concentric.

12. The hybrid composite tube of claim 10 , wherein the hybrid composite tube comprises at least one of a round geometry, an ovular geometry, and a polygonal geometry.

13. The hybrid composite tube of claim 11 , wherein the hybrid composite tube is configured to carry a hot fluid.

14. The hybrid composite tube of claim 11 , wherein the first silica fiber layer comprises a wall-thickness of between 15% and 45% of a total wall-thickness of the hybrid composite tube.

15. The hybrid composite tube of claim 11 , wherein the second silica fiber layer comprises a wall-thickness of between 5% and 30% of a total wall-thickness of the hybrid composite tube.

16. The hybrid composite tube of claim 11 , wherein the fiber reinforced polymer layer comprises a wall-thickness of between 30% and 80% of a total wall-thickness of the hybrid composite tube.

17. The hybrid composite tube of claim 11 , wherein the metallic tube comprises a wall-thickness of between 10% and 50% of a total wall-thickness of the hybrid composite tube.

18. A method for forming a hybrid composite tube, comprising:

disposing a first silica fiber layer about a metallic tube;

disposing a fiber reinforced polymer layer about the first silica fiber layer; and

disposing a second silica fiber layer about the fiber reinforced polymer layer.

19. The method of claim 18 , further comprising co-curing the first silica fiber layer and the fiber reinforced polymer layer.

20. The method of claim 18 , further comprising co-curing the first silica fiber layer, the fiber reinforced polymer layer, and the second silica fiber layer.

Assignments (2)
CHANGE OF NAME Recorded Jul 20, 2021
From: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
To: ROHR, INC.
Reel/Frame 056913/0233 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 19, 2019
From: DAIVAJNA, SANDEEP
To: GOODRICH AEROSPACE SERVICES PRIVATE LIMITED
Reel/Frame 048941/0808 →
Priority Claims (1)
IN 201941009135 · Mar 8, 2019 · national
Continuity (1)
Related Publication 20200282697A1 · Sep 10, 2020