COOLING FLUID USED AS SECONDARY FUEL SOURCE

An aircraft system includes a thermal load (22), a controller (26), a tank (32) for storing a cooling liquid, and a supply system for moving the cooling liquid outwardly of the tank and through a control valve (34) to the thermal load. A controller is programmed to control the supply system. A condu...

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Bibliographische Detailangaben

Hauptverfasser:	EMERSON, Sean C, CORDATOS, Haralambos
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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