FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the designs of unmanned aerial vehicles. The unmanned tiltrotor includes a battery, a control system with a homing module for the target, a body made according to a normal "airplane" aerodynamic scheme with a rectangular wing. On the leading edge of the wing, a rotary shaft is mounted on support bearings with two electric motors rigidly fixed on it with impellers with the opposite direction of rotation. The rotation of the motors at an angle of 90 degrees is carried out by a rotary shaft through a worm gear drive with an additional control motor. On the lower surface of the wing are installed suspension devices for missile and bomb weapons and means of destruction of drones. A plug-in device for disconnecting an electrical cable with power supply from an external power source is installed in the bow of the hull.
EFFECT: it is possible to carry out a vertical take-off without using the charge of its own battery and to be at a height limited by the length of an electric cable with power supply from an external power source.
5 cl, 6 dwg
