UNMANNED AERIAL VEHICLE HAVING MAIN WINGS WITH ENHANCED AERODYNAMIC PERFORMANCE

摘要

Provided is an unmanned aerial vehicle having main wings enhanced to reduce the resistance of an unmanned aerial vehicle through the shape change thereof according to flying conditions, to increase lift, and to improve aerodynamic performance. The unmanned aerial vehicle having main wings enhanced to improve aerodynamic performance comprises: a fuselage; a wing body which is formed on the side surface of the fuselage to be extended from the fuselage to the outside; a moving wing which is connected to the end of the wing body to change an angle to the wing body by moving against the wing body; and a moving wing drive unit which is installed in the wing body to be connected to the moving wing to change the angle to the wing body by moving the moving wing.