An assembly for a propulsion system (20) of an aircraft (1000) includes a gearbox module (32), at least one accessory load assembly (24), a propulsor (34), and an electric motor (38). The gearbox module (32) includes a gear assembly (88) and an output shaft (90). The gear assembly (88) is connected to the output shaft (90). The at least one accessory load assembly (24) includes at least one accessory load (124) coupled to the output shaft (90). The propulsor (34) is coupled to the output shaft (90). The electric motor (38) includes a rotor (42). The rotor (42) is coupled to the gear assembly (88) to drive rotation of the output shaft (90) about a rotational axis (104). The rotation of the output shaft (90) drives rotation of the propulsor (34) and the at least one accessory load (124) for each accessory load assembly (24) of the at least one accessory load assembly (24).
ELECTRIC MOTOR PROPULSION SYSTEM FOR AN AIRCRAFT
ELEKTROMOTORANTRIEBSSYSTEM FÜR EIN FLUGZEUG
SYSTÈME DE PROPULSION À MOTEUR ÉLECTRIQUE POUR AÉRONEF
2024-12-11
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |