A propulsion system includes a system for producing electricity that supplies electricity to at least one electric motor to which is mechanically coupled a propeller situated near a first longitudinal end of a nacelle that houses at least the system for producing electricity and the at least one electric motor. An air circulation channel, which receives a heat exchanger provided to allow the system for producing electricity to be cooled, extends inside the nacelle from a first end of the air circulation channel situated at the first longitudinal end of the nacelle. A part of the air circulation channel that is contiguous with its first end is delimited by an outer surface of cylindrical shape that surrounds the longitudinal axis of the nacelle.
SYSTEME DE PROPULSION ELECTRIQUE D'UN AERONEF
METHOD FOR ELECTRIC PROPULSION OF AN AIRCRAFT
ELEKTRISCHES ANTRIEBSSYSTEM FÜR EIN LUFTFAHRZEUG
25.12.2024
Patent
Elektronische Ressource
Französisch
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