Elektromotorantriebssystem für ein Flugzeug

Details

Veröffentlichungs-Nr.

EP4474289

Aktenzeichen

EP24181124

Anmeldetag

10. Juni 2024

Veröffentlichung

11. Dezember 2024

Rechtsraum

EP

IPC

B64D35/021

Abstract

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).

Anmelder

Firma

PRATT & WHITNEY CANADA CORP.

Land

🇨🇦 Kanada

Fachgebiete