FUEL CONDITIONING SYSTEM

A conditioning system for an aircraft including a fuel conduit which receives a liquid fuel, an evaporator and a heater which heat the liquid fuel to convert the fuel to a gas fuel supplied to an engine on the aircraft, the evaporator transfers heat from a hot working fluid to the liquid fuel and th...

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Bibliographische Detailangaben
Hauptverfasser:	CASADO MONTERO, Carlos, CASTAÑO DE LA MOTA, David, GÓMEZ FERNÁNDEZ, Agustín, ZAMARRO MARTÍN, María Cruz, CALDERÓN GÓMEZ, Pablo Manuel
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A conditioning system for an aircraft including a fuel conduit which receives a liquid fuel, an evaporator and a heater which heat the liquid fuel to convert the fuel to a gas fuel supplied to an engine on the aircraft, the evaporator transfers heat from a hot working fluid to the liquid fuel and the heater converts energy into heat applied to the liquid fuel, and a heat recovery circuit which circulates the working fluid through the evaporator and a heat exchanger in a hot exhaust gas stream generated by the engine.