FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to unmanned aerial vehicles. Quadcopter comprises four engines with propellers, four beams by one end fixed on quadcopter frame, onboard equipment located on quadcopter frame in the form of speed controller, accumulator battery, flight controller, receiver, transmitter and camera. Quadcopter additionally contains four engines with propellers. On the second free ends of each beam, Z-shaped equal-flange profiles without bends are rigidly fixed. Two engines with propellers are installed on free ends of each Z-shaped profile. First four propellers located diametrically can rotate clockwise, and the second four propellers located diametrically – counterclockwise.
EFFECT: increased reliability of quadcopter circular motion.
1 cl, 1 dwg
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