FIELD: aviation technology.
SUBSTANCE: invention relates to aviation technology, in particular to unmanned aerial vehicles (UAVs) of an aerodynamic type with a special payload. A high-speed UAV contains a fuselage with a radio-transparent rotary fairing in the nose, a wing including a center section connected to the fuselage in the central part, a folding wing with an oblique leading edge 45°, detachable parts and mechanization means that include a leading edge flap formed by two separate sections placed on the front, nose, wing part, slit flaps formed by two separate sections, and the aileron, which are placed on the rear of the wing. The UAV has a V-shaped tail with all-movable planes and an angle between the all-movable planes of 90° and is equipped with an aircraft turbojet two-circuit engine, which is located in the tail of the fuselage, and an air intake located above the fuselage.
EFFECT: increase in aerodynamic stability, aerodynamic control and maneuverability of the UAV.
4 cl, 4 dwg
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Authors
Dates
2023-01-13—Published
2021-12-16—Filed