Provided is an aircraft with a multi-power source electric propulsion system. The aircraft includes a fuselage, a power turbine accommodated in the fuselage and having a power shaft, a generator accommodated in the fuselage and connected to one end of the power shaft, a forward propeller for a forward flight and connected to another end of the power shaft, and a lift propeller for vertical take-off and landing (VTOL) and configured to receive power from the generator.
AIRCRAFT WITH MULTI-POWER SOURCE ELECTRIC PROPULSION SYSTEM
2025-05-29
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Electric propulsion system for aircraft, aircraft comprising such electric propulsion system
European Patent Office | 2024
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