An example embodiment includes a landing pad having a housing and a power terminal configured to draw electric power from a power source. The landing pad further includes an electrically conductive landing terminal dorsal to the housing and configured such that, during a landing state of an aerial vehicle, the landing terminal makes contact with a plurality of electric contacts disposed ventrally to a fuselage of the aerial vehicle. The landing terminal is configured to transfer electric power drawn by the power terminal to the aerial vehicle via the electric contacts during the landing state of the aerial vehicle.


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    Titel :

    Systems for Charging Aerial Vehicles


    Beteiligte:
    RENOLD NICK (Autor:in) / NUBBE MATTHEW (Autor:in) / SCHMALZRIED JIM (Autor:in) / BLAKE JESSE (Autor:in) / VELEZ SCOTT (Autor:in) / SANDERS DUSTIN (Autor:in) / BENSON STEPHEN (Autor:in) / TWYFORD EVAN (Autor:in)

    Erscheinungsdatum :

    24.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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