A hybrid powerplant can include a main power bus; an engine; a generator coupled to the engine, the generator in electrical communication with the main power bus; an energy storage; an electrical switch disposed electrically between the main power bus and the energy storage; and a controller in electrical communication with the electrical switch.


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    Titel :

    HYBRID ELECTRIC DRIVE SYSTEMS FOR UNMANNED AIRCRAFT SYSTEMS


    Beteiligte:
    MURPHY CARLOS (Autor:in) / DOUGLAS JASON (Autor:in) / CULBERTSON SEAN (Autor:in)

    Erscheinungsdatum :

    11.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge





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