ELECTRIC PROPULSION UNIT OF AN AIRCRAFT COMPRISING A COOLING SYSTEM INCORPORATING AT LEAST ONE FRONT AIR INLET AND AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION UNIT

The invention relates to an electric propulsion unit of an aircraft comprising a nacelle (22) housing an electric power system (16), an electric motor (18) and a cooling system for the electric power system (16); the nacelle comprising a central fairing (32), a front fairing (34) which extends from...

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Bibliographische Detailangaben
Hauptverfasser:	VERSEUX, Olivier, SOLNTSEV, Alexander, SCHERER, Thomas, CARRETERO BENIGNOS, Jorge, BAMMER, Benedikt, MOLANO REMBIASZ, Jorge, JUANAS FERNANDEZ, Maria Del Sagrario
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 invention relates to an electric propulsion unit of an aircraft comprising a nacelle (22) housing an electric power system (16), an electric motor (18) and a cooling system for the electric power system (16); the nacelle comprising a central fairing (32), a front fairing (34) which extends from the central fairing (32) to a front end (34.1) and a rear fairing (36) which extends from the central fairing (32) to a rear end (36.1).According to the invention, the front fairing (34) comprises a protrude (52) positioned in a lower part of the front fairing (34), said protrude (52) having a front face (54) in a transverse plane, a main air inlet (42) of the cooling system being positioned on the front face (54).