Methods and systems for operating a hybrid electric aircraft propulsion system mounted to an aircraft. The method comprises driving a first rotating propulsor from a first electric motor operatively connected to a generator, driving a second rotating propulsor from a second electric motor operatively connected to the generator, and driving a third rotating propulsor from a thermal engine, the thermal engine operatively connected to the generator and configured to drive the generator.


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    Titel :

    HYBRID ELECTRIC PROPULSION SYSTEM AND METHOD OF OPERATION


    Weitere Titelangaben:

    SYSTEME DE PROPULSION HYBRIDE ELECTRIQUE ET SA METHODE DE FONCTIONNEMENT


    Beteiligte:
    LATULIPE ERIC (Autor:in) / FREER RICHARD (Autor:in)

    Erscheinungsdatum :

    2020-03-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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