An electrical power system is disclosed for an aircraft having a hybrid-electric propulsion system, which includes a battery assembly for storing energy, an electric motor controller operatively connected to the battery assembly for conditioning and controlling power to an electric motor, and an electric motor receiving power through the motor controller for delivering torque to a shaft of the hybrid-electric propulsion system.


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    Titel :

    ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM


    Beteiligte:
    SMITH ANDREW D (Autor:in) / IVES KYLE (Autor:in) / BAIG ZUBAIR A (Autor:in)

    Erscheinungsdatum :

    03.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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