Small UAV aerodynamic layout for vertical rope-type recovery
A small unmanned aerial vehicle, aerodynamic layout technology, applied in the direction of wing adjustment, automatic control, control start method, etc., can solve the problems of occupying aircraft loading space, reducing aircraft payload capacity, difficulties, etc.
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[0013] The technical scheme of the present invention will be described in further detail below in conjunction with accompanying drawing and embodiment:
[0014] See attached figure 1 As shown, the aerodynamic layout of the small unmanned aerial vehicle for vertical rope recovery on the moving base includes fuselage 1, wing 2, engine 3 and tail. Wing 2 is the upper wing with an installation angle of 3° , engine 3 is installed on the afterbody of fuselage 1, it is characterized in that: the aspect ratio of wing 2 is 9, adopts the sweep type, and the sweep angle is 23 °, and the lower surface of wing 2 middle part is provided with for installing empennage Horizontal strut 4, horizontal empennage 5 and vertical tail 6 of upside-down installation are installed at the rear end of horizontal strut 4, and vertical tail 6 is inwardly inclined 15 °.
[0015] According to the results of numerical calculation and analysis, the aerodynamic layout of the vertical rope recovery unmanned aer...
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