FIELD: transport.
SUBSTANCE: proposed drone aircraft features canard configuration and comprises wing, fuselage, front horizontal tail unit, power plant with pusher propeller arranged at fuselage tail, and control system. Wing represents sweptback configuration, while screw propeller is provided with circular casing. The latter, mage elongated, extends backward from screw propeller and incorporates exhaust turning nozzle furnished with vertical and horizontal drives to turn said nozzle about horizontal and vertical axes. Front horizontal tail is pivoted to axle directed along tail swing and perpendicular to aircraft plane of symmetry, and is self-set to preset angle of attack. Control system is connected with vertical and horizontal drives of turning nozzle.
EFFECT: better aerodynamics characteristics and reduced weight.
4 cl, 2 dwg
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