In some embodiments, an apparatus includes a fuselage of an unmanned aircraft that includes a first section removably coupled to a second section, and a third section removably coupled to the second section such that the second section is disposed between the first section and the third section in a vertical direction. The first section includes a first rotor and a second rotor disposed at a non-zero spaced distance in the vertical direction from each other. The first rotor and the second rotor share a common and aligned rotational axis defined along a longitudinal centerline of the fuselage defined in the vertical direction. The second section is configured to contain a selected payload, and the third section includes a control system. A plurality of legs are coupled to the third section and serve as landing gear for the unmanned aircraft.


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    Title :

    RAPID AERIAL DEPLOYED DRONE


    Contributors:

    Publication date :

    2019-06-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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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