An embodiment flying vehicle includes a fuel cell installed in a fuselage and configured to supply power to the fuselage and an auxiliary thruster installed in the fuselage and configured to provide an auxiliary thrust force by ejecting combustion gas generated by burning a portion of fuel to be supplied to the fuel cell.


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    Titel :

    FLYING VEHICLE HAVING AUXILIARY THRUSTER AND METHOD FOR CONTROLLING AUXILIARY THRUSTER


    Beteiligte:
    HWANG EUGENE (Autor:in)

    Erscheinungsdatum :

    12.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



    FLYING VEHICLE HAVING AUXILIARY THRUSTER AND METHOD FOR CONTROLLING AUXILIARY THRUSTER

    HWANG EU GENE | Europäisches Patentamt | 2025

    Freier Zugriff


    An 8-cm electron bombardment thruster for auxiliary propulsion

    Hudson, W. R. / Banks, B. A. | NTRS | 1973


    An 8-cm electron bombardment thruster for auxiliary propulsion

    Hudson, W. R. / Banks, B. A. | NTRS | 1973