FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed drone has fuselage, wing, V-like tail unit and engine with tractor propeller. Fuselage 1 consists of nose part 9 and conical tail part 10 attached to central part 8. Wing 2 comprises centre section 5 connected with outer wings 6 with ailerons 7. Tail unit 3 incorporates cradle 12 connecting cantilever 11 and connected with tail part 10. Centre section 5 has buildup 13 and payload fasteners. Outer wings 6 are arranged at transverse angle and feature geometrical warp with reduction of pitch angle at end cross-sections. Ailerons 7 are connected with top surface of outer wing 6 by flexible skin 16.
EFFECT: higher aerodynamics.
7 cl, 12 dwg
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