FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly, to designs of drones. Universal drone comprises fuselage and wing, made according to "flying wing" (1) aerodynamic design, as well as power plant, installed on support (2) and made in form of engine (3) and propeller (4). Power plant is installed in nose part of wing (1) on support (2) with possibility of blowing both wing top surface (1), and additional controls, fixed on power plant support (2) and made in form of foreplane (5) and canard fin (6). Takeoff and landing supports are made in form of three symmetrically arranged telescopic supports (7, 8 and 9). Support (7) is equipped with rudders (10). Supports (8) and (9) are equipped with controlled rotary hydrofoils (11) and chassis (12). On wing lower surface (1) in its front part additional support (13) is installed, provided with controlled rotary hydrofoils (14) and landing gear (15).
EFFECT: aircraft higher maneuverability by pitch, roll and yawing in wide range of angles of attack.
1 cl, 3 dwg
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