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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    Title :

    APPARATUS FOR CONTROLLING POWER


    Additional title:

    VORRICHTUNG ZUR LEISTUNGSREGELUNG
    APPAREIL DE COMMANDE DE PUISSANCE


    Contributors:
    JEON YOON CHEOL (author) / JANG JIN SOO (author) / KIM JONG PIL (author) / CHO HYUN KI (author)

    Publication date :

    2024-10-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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