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).
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
ELEKTRISCHE ANTRIEBSEINHEIT EINES FLUGZEUGS MIT EINEM KÜHLSYSTEM MIT MINDESTENS EINEM FRONTLUFTEINLASS UND FLUGZEUG MIT MINDESTENS EINER SOLCHEN ELEKTRISCHEN ANTRIEBSEINHEIT
UNITÉ DE PROPULSION ÉLECTRIQUE D'UN AÉRONEF COMPORTANT UN SYSTÈME DE REFROIDISSEMENT COMPRENANT AU MOINS UNE ENTRÉE D'AIR AVANT ET AÉRONEF COMPRENANT AU MOINS UNE TELLE UNITÉ DE PROPULSION ÉLECTRIQUE
2025-03-05
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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