A double-battery-powered aircraft comprises a frame, four rotor wings, a lithium battery, a control chip and four driving motors, wherein the rotor wings, the lithium battery and the control chip are all installed on the frame. The aircraft further comprises a solar battery arranged on the surface of the frame, wherein the solar battery is used for absorbing sunlight, converting the absorbed sunlight into electric energy, and then outputting the electric energy to the driving motors and the lithium battery. The invention further provides a power supply control method of the aircraft.


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    Titel :

    Double-battery-powered aircraft and power supply control method thereof


    Beteiligte:
    WU HAN (Autor:in) / GUO SHUANGTAO (Autor:in) / XU YANG (Autor:in) / LI XU (Autor:in) / LI BAOHUA (Autor:in) / LU ZONGXIANG (Autor:in)

    Erscheinungsdatum :

    25.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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