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Coal-Based Porous Graphite for Aerospace Heat Exchanger Applications

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA8650-04-C-5033
Agency Tracking Number: F031-0493
Amount: $799,971.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: AF03-118
Solicitation Number: 2003.1
Timeline
Solicitation Year: 2003
Award Year: 2004
Award Start Date (Proposal Award Date): 2004-04-22
Award End Date (Contract End Date): 2009-05-20
Small Business Information
The Millennium Centre, R.R. 1, Box 100B
Triadelphia, WV 26059
United States
DUNS: 101582922
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Dwayne Morgan
 (304) 547-5800
 drm@trl.com
Business Contact
 Brian Joseph
Phone: (304) 547-5800
Email: bej@trl.com
Research Institution
N/A
Abstract

A newly developed "coal-based" porous graphite material has been recently produced. This development is a direct result of Touchstone Research Laboratory's Phase I funding to develop enhanced-strength carbon foam heat-exchanger materials for aerospace applications since low density carbon foams cannot endure high bleed air pressures in aerospace pre-coolers and heat exchangers. The newly developed material indicates compressive strength of ~ 6000 psi in comparison with 200-700 psi for graphite foam. In addition, the porous graphite has 3 times the thermal conductivity (55 W/m·K) of Inconel and significantly lower CTE indicating ~3.5 (1/°C), which should be beneficial in reducing thermal stress and improving durability. Preliminary investigations show there will be no added costs related to the production of coal-based porous graphite since similar production methods are employed in the manufacture of other CFOAMr products lines. This makes coal-based porous graphite extremely affordable relative to any other carbon and graphite currently on the market. Touchstone and its partners propose to fabricate a heat exchanger core from porous graphite for pressure drop, heat flow and durability evaluations, which will ultimately lead to the construction of highly efficient, lightweight, and affordable replacements to current heat exchanger technologies in aerospace.

* Information listed above is at the time of submission. *

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