An aircraft propulsion system comprising a propeller, a plurality of electric motors, a transmission system configured to couple the electric motors to the propeller, and a propeller pitch adjustment system positioned at the rear of the transmission system. At least one of the electric motors is positioned in front of the transmission system. A connection structure is interposed between the propeller and the transmission system, the connection structure and the output shaft of the transmission system connected to the propeller being configured so that no electric motor positioned in front of the transmission system interferes with the propeller. Also an aircraft with such a system.
ENSEMBLE DE PROPULSION ÉLECTRIQUE COMPORTANT AU MOINS UN MOTEUR ÉLECTRIQUE POSITIONNÉ À L'AVANT D'UN SYSTÈME DE TRANSMISSION, AÉRONEF COMPORTANT AU MOINS UN TEL ENSEMBLE DE PROPULSION
ELECTRIC PROPULSION ASSEMBLY COMPRISING AT LEAST ONE ELECTRIC MOTOR POSITIONED IN FRONT OF A TRANSMISSION SYSTEM, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY
ELEKTRISCHE ANTRIEBSANORDNUNG MIT MINDESTENS EINEM ELEKTROMOTOR, DER AN DER FRONT EINES ÜBERTRAGUNGSSYSTEMS POSITIONIERT IST, LUFTFAHRZEUG, DAS MINDESTENS EINE SOLCHE ANTRIEBSANORDNUNG UMFASST
2025-03-19
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2024
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