The present invention relates to an unmanned aerial vehicle. The present invention forms a fuselage connected with a joined wing as an inflatable fuselage having a cylindrical envelope filled with an inert gas to simplify the fuselage; and enables the fuselage to be super-lightweight, improving impact resistance of the fuselage and improving short-range landing performance and long-term hang performance. A propulsion engine is installed in a nose cone of the inflatable fuselage, and a vertical wing having a rudder is provided to a rear end part of the inflatable fuselage.
UNMANNED AERIAL VEHICLE HAVING JOINED WINGS AND INFLATABLE FUSELAGE
2015-09-02
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge |
UNMANNED AERIAL VEHICLE HAVING JOINED WINGS AND DELTA WINGS
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