Claims
- 1. A method of cooling a heat source, comprising:
- (a) transferring thermal energy with heat transfer means from the heat source, which is at a suitable temperature, to an endothermic fuel decomposition catalyst, wherein the catalyst comprises a metal selected from the group consisting of platinum, rhenium, rhodium, iridium, ruthenium, palladium, and mixtures thereof or a zeolite, thereby heating the catalyst to a temperature between about 1000.degree. F. and about 1500.degree. F. to catalytically crack at least a portion of a stream of a normal paraffinic hydrocarbon fuel stream; and
- (b) contacting the heated endothermic fuel decomposition catalyst with the fuel stream at a liquid hourly space velocity of at least about 10 hr.sup.-1, thereby causing the fuel stream to catalytically crack into a reaction product stream with a conversion of greater than about 60% to produce a total heat sink of at least about 2000 Btu/lb of fuel, wherein
- the reaction product stream comprises hydrogen and unsaturated hydrocarbons; thereby cooling the heat source to a temperature less than its original temperature.
- 2. The method of claim 1 further comprising combusting the reaction product stream in a combustor.
- 3. The method of claim 1 wherein the zeolite is a faujasite, chabazite, mordenite, or silicalite.
- 4. The method of claim 1 wherein the normal paraffinic hydrocarbon fuel is selected from the group consisting of C.sub.2 to C.sub.20 normal paraffins and blends thereof.
- 5. The method of claim 1 wherein the endothermic fuel stream is contacted with the heated endothermic fuel decomposition catalyst at a liquid hourly space velocity of about 20 hr.sup.-1 to about 1000 hr.sup.-1.
- 6. The method of claim 1 wherein the heat source is located on an aircraft.
- 7. A method of cooling high speed vehicle engine and airframe components, comprising:
- (a) transferring thermal energy with heat transfer means from the high speed vehicle engine and airframe components, which are at a suitable temperature, to an endothermic fuel decomposition catalyst that comprises a mixture of copper oxides and zinc oxides, thereby heating the catalyst to a temperature between about 500.degree. F. and about 1200.degree. F. to dissociate at least a portion of a methanol fuel stream; and
- (b) contacting the heated endothermic decomposition catalyst with the fuel stream at a liquid hourly space velocity of at least about 10 hr.sup.-1, thereby causing the fuel stream to dissociate into a reaction product stream comprising hydrogen and carbon monoxide;
- thereby cooling the high speed vehicle engine and airframe components to a temperature less than their original temperature.
- 8. The method of claim 7 further comprising combusting the reaction product stream in a combustor.
- 9. The method of claim 7 wherein the methanol fuel stream is contacted with the heated endothermic fuel decomposition catalyst at a liquid hourly space velocity of about 20 hr.sup.-1 to about 1000 hr.sup.-1.
- 10. A method of cooling high speed vehicle engine and airframe components, comprising:
- (a) transferring thermal energy with heat transfer means from the high speed vehicle engine and airframe components, which are at a suitable temperature, to a zeolite hydrocarbon cracking catalyst with heat transfer means, thereby heating the catalyst to a temperature of about 1000.degree. F. to about 1500.degree. F.; and
- (b) contacting the heated zeolite hydrocarbon cracking catalyst with a normal paraffinic hydrocarbon fuel stream at a liquid hourly space velocity of at least about 10 hr.sup.-1, thereby causing the fuel stream to catalytically crack into a reaction product stream with a conversion of greater than about 60% to produce a total heat sink of at least about 2000 Btu/lb of fuel, wherein the reaction product stream comprises hydrogen and unsaturated hydrocarbons;
- thereby cooling the high speed vehicle engine and airframe components to a temperature less than their original temperature.
- 11. The method of claim 10 further comprising combusting the reaction product stream in a combustor.
- 12. The method of claim 10 wherein the normal paraffinic hydrocarbon fuel is selected from the group consisting of C.sub.2 to C.sub.20 normal paraffins and blends thereof.
DESCRIPTION
This invention was made with Government support under contract number F33615-87-C-2744 awarded by the Department of the Air Force. The Government has certain rights in this invention.
US Referenced Citations (10)
Non-Patent Literature Citations (2)
Entry |
Chem Abst 63: 396B-Ritchie et al. 1965. |
Chem Abst 75: 14252 Faith et al. 1971. |