FIELD: unmanned aerial vehicles.
SUBSTANCE: proposed unmanned aerial vehicle comprises fuselage, power plant, power supply of which provides at least electric accumulators and/or photoelectric elements, first wing, characterized by span and area of upper surface, wherein upper surface of first wing is covered with photoelectric elements, and second wing, swing and surface area of which are essentially same as those of first wing. Second wing is displaced along fuselage and height relative to first wing, and upper surface of second wing is also covered with photoelectric elements. At that, fuselage cross-section has shape of isosceles trapezoid, smaller base of which is formed by fuselage upper surface, from which fuselage side surfaces pass, note here that fuselage top surface and lateral surfaces are covered by photoelectric elements.
EFFECT: proposed is an unmanned aerial vehicle with two wings to which photoelectric elements are attached.
9 cl, 10 dwg
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Authors
Dates
2020-07-02—Published
2017-01-12—Filed