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.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT WITH MULTI-POWER SOURCE ELECTRIC PROPULSION SYSTEM


    Contributors:
    HUH JAESUNG (author)

    Publication date :

    2025-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft electric power propulsion system

    PENG XINGLIN / XIAO FEI / DONG WENCHAO | European Patent Office | 2024

    Free access

    Electric propulsion system for aircraft, aircraft comprising such electric propulsion system

    VALLIERE J E RU ME | European Patent Office | 2024

    Free access

    Electric aircraft propulsion system

    RABBI SHEIKH FAZLE / PILGRIM RICK RALPH / GENGE KYLE REUBEN et al. | European Patent Office | 2023

    Free access

    ELECTRIC AIRCRAFT PROPULSION SYSTEM

    WOOD NORMAN / IQBAL KAMRAN | European Patent Office | 2022

    Free access

    ELECTRIC AIRCRAFT PROPULSION SYSTEM

    RABBI SHEIKH FAZLE / PILGRIM RICK RALPH / GENGE KYLE REUBEN et al. | European Patent Office | 2021

    Free access