An aeronautical propulsion system (200), comprises a propeller (202) mounted to a propeller shaft (204) defining a propeller axis (214); an electric motor (208) comprising a motor output shaft defining a motor axis (216); wherein the motor output shaft and propeller shaft are connected by a linkage such that, in use, driving the motor output shaft for rotation drives rotation of the propeller via the propeller shaft and linkage; and a motor power unit configured to receive power from a power source and provide a motor drive signal to the motor; wherein the motor power unit is spaced along the motor axis from the motor.
AERONAUTICAL PROPULSION SYSTEM
AERONAUTISCHES ANTRIEBSSYSTEM
SYSTÈME DE PROPULSION AÉRONAUTIQUE
25.06.2025
Patent
Elektronische Ressource
Englisch
NTRS | 1975
NTIS | 1975