FUEL CONDITIONING SYSTEM

The present invention relates to a conditioning system (100) for an aircraft. In particular, the present invention belongs to a conditioning system having a new architecture including a power unit (1) and a heat recovery circuit (8). The present invention also relates to an aircraft comprising said...

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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 ; fre ; ger
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:	The present invention relates to a conditioning system (100) for an aircraft. In particular, the present invention belongs to a conditioning system having a new architecture including a power unit (1) and a heat recovery circuit (8). The present invention also relates to an aircraft comprising said conditioning system and to a method for conditioning fuel by means of the conditioning system of the invention.