An aircraft propulsion system comprises a vertical lift propulsor (22) mounted within a wing (13) of the aircraft (10). The vertical propulsor (22) comprises an electric motor (30) comprising a rotor (28) mounted to a plurality of propulsor blades (24), the motor (30) further comprising a stator (32). The rotor (28) is provided radially outwardly of the stator.
Aircraft propulsion system
2018-10-17
Patent
Elektronische Ressource
Englisch