A power control device is provided for an aircraft. The power control device may include at least one first battery, a second battery having a lower power density and higher energy density than the at least one first battery, at least one lift motor connected, via a first electrical path, to the at least one first battery, a cruise motor connected, via a second electrical path, to the second battery, and a power control circuit configured to control the at least one first battery, the second battery, the at least one lift motor, and the cruise motor.


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    Titel :

    APPARATUS FOR CONTROLLING POWER


    Weitere Titelangaben:

    VORRICHTUNG ZUR LEISTUNGSREGELUNG
    APPAREIL DE COMMANDE DE PUISSANCE


    Beteiligte:
    JEON YOON CHEOL (Autor:in) / JANG JIN SOO (Autor:in) / KIM JONG PIL (Autor:in) / CHO HYUN KI (Autor:in)

    Erscheinungsdatum :

    30.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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