IP Library Granted Patent US 8,205,315
Granted Patent B2
US 8,205,315 · App. 11/981,569 · Granted Jun 26, 2012

Composite tube assemblies and methods of forming the same

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Quick Facts
Patent No.
US 8,205,315
App. No.
11/981,569
Granted
Jun 26, 2012
Kind
B2
Abstract

A composite tube assembly and a method of making the same are provided. The composite tube assembly includes a composite tube and a fitting penetrating the composite tube. The fitting includes a reduced diameter section surrounded by a reduced diameter tube portion of the tube. A bolstering structure surrounds this reduced diameter tube portion. The method includes inserting the fitting into the composite tube, heating the tube portion surrounding the fitting to soften the same, radially compressing the tube portion onto the fitting reduced diameter section, and providing a bolstering structure surrounding the compressed tube portion.

Claims (20)

1. A method for forming a composite tube assembly comprising:

obtaining a composite tube comprising an end, wherein said composite tube is formed from fibers and a resin;

obtaining a fitting comprising a first end opposite a second end, said fitting comprising a first constant diameter outer surface section extending from the first end and comprising a first outer diameter, wherein said fitting comprises a second constant diameter outer surface section between said first and second ends having a second outer surface diameter greater than the first outer diameter, and a flange extending from the fitting, the flange having an annular surface extending radially from said first constant diameter outer surface section and a peripheral surface extending transversely from the annular surface;

inserting the fitting second end and said second constant diameter outer surface section first into the composite tube through the composite tube end followed by at least a portion of the first constant diameter outer surface section, wherein an end portion of said tube surrounds said second constant diameter outer surface section and at least a portion of said first constant diameter outer surface section;

heating said tube end portion to soften the resin;

radially compressing said tube end portion onto said second constant diameter outer surface section and onto at least a portion of said first constant diameter outer surface section;

surrounding said compressed tube end portion with a bolstering structure extending axially from the annular surface and;

placing a collar over the bolstering structure and engaging the peripheral surface of the flange.

2. The method as recited in claim 1 wherein surrounding said compressed end tube portion with a bolstering structure comprises:

wrapping said compressed tube end portion with a material comprising fibers and resin; and

curing said wrapped material onto said compressed end tube portion to form said bolstering structure.

3. The method as recited in claim 1 wherein the fitting further comprises a tapered outer surface annular section between said two constant diameter outer surface sections, wherein said tapered outer surface section tapers radially inward in a direction toward the first end.

4. The method as recited in claim 3 wherein inserting comprises inserting the fitting second end into the composite tube end until the composite tube end abuts the flange.

5. The method as recited in claim 4 wherein surrounding said compressed end tube portion with a bolstering structure comprises:

wrapping said compressed tube end portion with a material comprising fibers and resin, said material abutting said flange annular surface; and

curing said wrapped material onto said compressed end tube portion to form said bolstering structure.

6. The method as recited in claim 5 wherein placing a collar comprises placing a collar surrounding and engaging said bolstering structure.

7. The method as recited in claim 1 wherein placing a collar comprises placing a collar surrounding and engaging said bolstering structure.

8. The method as recited in claim 1 wherein said fitting second constant diameter outer surface section comprises an outer surface having at least a groove.

9. The method as recited in claim 1 further comprising placing an adhesive between said tube end portion and said fitting second constant diameter outer surface section.

Assignments (3)
SECURITY AGREEMENT Recorded Feb 16, 2011
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; HARTWELL CORPORATION; TYEE AIRCRAFT; WESTERN SKY INDUSTRIES, LLC, A.K.A. TYEE AIRCRAFT; AEROCONTROLEX GROUP, INC.; ADAMS RITE AEROSPACE, INC.; CHAMPION AEROSPACE LLC; MARATHONNORCO AEROSPACE, INC.; BRUCE AEROSPACE INC.; ACME AEROSPACE, INC.
To: CREDIT SUISSE AG, AS ADMINISTRATIVE AND COLLATERAL AGENT
Reel/Frame 025810/0177 →
SECURITY AGREEMENT Recorded Dec 22, 2010
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; AEROCONTROLEX GROUP, INC.; ADAMS RITE AEROSPACE, INC.; MARATHONNORCO AEROSPACE, INC.; HARTWELL CORPORATION; WESTERN SKY INDUSTRIES, LLC, A.K.A. TYEE AIRCRAFT
To: CREDIT SUISSE AG, AS ADMINISTRATIVE AND COLLATERAL AGENT
Reel/Frame 025525/0054 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 7, 2008
From: MULLEN, JAMES M.; VALLEROY, DANIEL M.; MOORE, DANIEL L.
To: TYEE AIRCRAFT
Reel/Frame 020618/0784 →