IP Library › Granted Patent US 6,988,304
Granted Patent B2
US 6,988,304 · App. 10/130,394 · Granted Jan 24, 2006

Method of containing a phase change material in a porous carbon material and articles produced thereby

Assignee: Aircraft Braking Systems Corporation
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Quick Facts
Patent No.
US 6,988,304
App. No.
10/130,394
Granted
Jan 24, 2006
Kind
B2
Abstract

A process for fabricating a carbon composite structure that is lightweight, structurally sound, and characterized by high heat capacity. A carbon structure is devised with cavities therein receiving a phase change medium. The phase change medium demonstrates both high energy absorption capacity and high thermal conductivity and is formed from a carbon fiber to establish a high porosity medium having a large volume fraction. The surface energy of the carbon fibers is enhanced in various ways as by deposition of a carbide former, a metallurgical coating or a precursor liquid or by electroplating or etching the surfaces of the carbon fibers. The enhanced surface energy allows for the retention of phase change material.

Claims (20)

1. A process for fabricating a carbon composite structure that is lightweight, structurally sound, and characterized by high heat capacity, comprising:

forming a carbon structure with at least one cavity therein;

placing a phase change medium within said cavity, said phase change medium demonstrating high energy absorption capacity, high thermal conductivity, and high void volume for phase change material retention; and

closing said phase change medium within said cavity to allow vapor diffusion and liquid containment.

2. The process according to claim 1 , wherein said phase change medium is formed from a carbon fiber to establish a high porosity medium having a large volume fraction available for containment of phase change material.

3. The process according to claim 1 , wherein said phase change medium is formed from a carbon foam to establish a high porosity medium having a large volume fraction available for containment of phase change material.

4. The process according to claim 1 , wherein said phase change medium is an isotropic high porosity medium.

5. The process according to claim 1 , wherein said phase change medium is an anisotropic high porosity medium.

6. The process according to claim 1 , further including the step of altering a surface energy of said carbon fibers of said phase change medium to enhance retention of phase change material.

7. The process according to claim 6 , wherein said surface energy is enhanced by deposition of at least one of a carbide and ceramic formed by thermal decomposition of a precursor gas containing at least one of silicon, tantalum, titanium, molybdenum and nickel.

8. The process according to claim 6 wherein said surface energy is enhanced by deposition of one of a metallurgical and ceramic coating by decomposition of a precursor gas containing at least one of silicon, tantalum, titanium and molybdenum.

9. The process according to claim 6 , wherein said surface energy is enhanced by electroless deposition of a precursor liquid containing at least one of silicon, tantalum, titanium, molybdenum and nickel.

10. The process according to claim 6 , wherein said surface energy is enhanced by electroplating with a plating solution consisting of at least one of silicon, tantalum, titanium, chromium, molybdenum and nickel.

11. The process according to claim 6 , wherein said surface energy is enhanced by etching said carbon fibers with at least one of gaseous water, carbon monoxide, carbon dioxide, oxygen, nitric acid and peracitic acid.

12. The process according to claim 6 , wherein a phase change material retained by said high porosity medium is at least one of a lithium salt and a metal having a characteristic melting point.

13. The process according to claim 12 , wherein said metal is a low melting metal and comprises one of copper and aluminum.

14. The process according to claim 6 , wherein said phase change medium is formed from one of vapor grown carbon fibers and carbon foam.

15. The process according to claim 6 , wherein said surface energy is enhanced by a coating deposited thereon having a thickness of 1–1000 nanometers.

16. The process according to claim 15 , wherein said surface energy is enhanced by a coating deposited thereon having a coating volume fraction of between 0.001 and 0.1.

17. The process according to claim 15 , wherein said surface energy is enhanced by alteration at temperatures between 400° C. and 1200 C.

Assignments (3)
RELEASE AND REASSIGNMENT OF PATENTS Recorded Aug 9, 2007
From: AIRCRAFT BRAKING SYSTEM CORPORATION
To: LEHMAN COMMERCIAL PAPER INC.
Reel/Frame 019668/0314 →
SECURITY AGREEMENT Recorded Feb 1, 2005
From: AIRCRAFT BRAKING SYSTEMS CORPORATION
To: LEHMAN COMMERCIAL PAPER INC., AS ADMINISTRATIVE AGENT
Reel/Frame 015621/0978 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 24, 2003
From: MOSELEY, DOUGLAS; FATE, DOUGLAS; LAKE, MAX; TANG, CHI; BURTON, DAVID; HAGER, JOSEPH
To: AIRCRAFT BRAKING SYSTEMS CORPORATION; APPLIED SCIENCES, INC.
Reel/Frame 014310/0273 →
Continuity (1)
Related Publication 20030145447A1 · Aug 7, 2003