Unmanned aerial vehicle

Abstract

The subject of the application is an unmanned aerial vehicle, a multi-rotor drone designed for flights with a large payload at a high average speed, for a long time, in windy weather. The unmanned aerial vehicle, a drone, is equipped with a fuselage (1), to which beams (4) are attached by means of scissor mechanisms (3) enabling folding, at the ends of which are mounted carrier motors (5) with horizontal propellers (6) and legs (16), wherein the legs (16) are equipped with a mechanism enabling folding (15), furthermore, a battery (14) is attached to the fuselage (1), and an electrical system distributing electrical power and a control system with an antenna (12) are mounted inside the fuselage (1), characterized in that at least one end of the fuselage (1) is equipped with a front engine (8) with a front propeller (9).