Pneumatic layout of dual flying wings of UAV (Unmanned Aerial Vehicle)
A technology of aerodynamic layout and unmanned aerial vehicle, applied in the direction of unmanned aerial vehicle, motor vehicle, wing shape, etc., can solve the problems of poor handling performance and poor stability, and achieve good longitudinal stability and lateral stability. Good, good heading stability effect
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[0025] The following will be combined with Figure 1-10 The present invention is described in further detail with embodiment.
[0026] An embodiment of the aerodynamic layout of the double-flying wing of an unmanned aerial vehicle is characterized in that it includes: the aerodynamic layout of the wing-body fusion body flying wing, the layout where the turbofan engine is installed above the rear section of the wing-body fusion body flying wing, and the installation of a full-motion horizontal tail The aerodynamic layout on both sides of the turbofan engine outer wall nacelle (5), wherein the fuselage (1), wings (2), winglets (3) and direction ailerons (4) together form the high lift The wing-body fusion body flying wing of drag ratio, the flat tail (6) and the flat tail winglet (7) together form the described full-motion horizontal tail that provides positive lift when leveling off, and the wing-body fusion body flying wing and the full-motion flat tail together form the The ...
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