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RESEARCH PAPERS: Gas Turbines: Combustion and Fuels

Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion

[+] Author and Article Information
D. R. Sobel, L. J. Spadaccini

United Technologies Research Center, East Hartford, CT 06108

J. Eng. Gas Turbines Power 119(2), 344-351 (Apr 01, 1997) (8 pages) doi:10.1115/1.2815581 History: Received February 15, 1995; Online November 19, 2007

Abstract

Storable hydrocarbon fuels that undergo endothermic reaction provide an attractive heat sink for future high-speed aircraft. An investigation was conducted to explore the endothermic potential of practical fuels, with inexpensive and readily available catalysts, under operating conditions simulative of high-speed flight applications. High heat sink capacities and desirable reaction products have been demonstrated for n -heptane and Norpar 12 fuels using zeolite catalysts in coated-tube reactor configurations. The effects of fuel composition and operating condition on extent of fuel conversion, product composition, and the corresponding endotherm have been examined. The results obtained in this study provide a basis for catalytic-reactor/heat-exchanger design and analysis.

Copyright © 1997 by The American Society of Mechanical Engineers
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