FIELD: unmanned aerial vehicles (UAVs).
SUBSTANCE: helicopter-type unmanned aerial vehicle comprises a fuselage, coaxial rotors. The fuselage comprises several cylindrical modules, including two electric motors equipped with counter-rotating folding propeller blades, a receiver module, a battery module, a swashplate module that changes the plane of rotation of the lower motor propeller blades to change the direction of flight, and a flight control module. All the modules are installed along their central axis on a hollow rod, inside which communication and power wires connect them to each other.
EFFECT: expanded functionality of the UAV due to the possibility of launching it in several ways, depending on the conditions of use.
1 cl, 6 dwg
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