Methods and systems for operating a hybrid electric aircraft propulsion system. The method comprises providing alternating current (AC) electric power to a first electric motor to drive a first rotating propulsor, providing the first electric motor with AC electric power from at least one motor inverter operatively coupled to a direct current (DC) power source, detecting a failure in a path to the first electric motor, and selectively rearranging a first switching arrangement between the generator, the at least one motor inverter, and the first electric motor.


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    Titel :

    OPERATION OF A HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM


    Weitere Titelangaben:

    FONCTIONNEMENT D`UN SYSTEME DE PROPULSION D`AERONEF HYBRIDE ELECTRIQUE


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

    Erscheinungsdatum :

    06.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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