Aircraft with vertikal take-off and landing (VTOL)

摘要

Aircraft with vertical take-off and landing (VTOL) comprises two wings connected to the fuselage comprising at least one wing carrier (2) and a stabilizer located at the rear of the fuselage and further comprising at least six lifting units (3, 4) arranged in pairs symmetrically to the fuselage, wherein at least two pairs are front lifting units (3) located forward of the wing support (2) in vertical tunnels, formed in the wings at the wing roots and suspended on longitudinal beams (8), which are located on the upper and lower contour of the sash profile and fixed to the sash support structure. At least one pair of lifting units will form the rear lifting units (4) located in vertical tunnels formed at the root of the horizontal stabilizer. Each of the front and rear lifting units (3, 4) comprises an electric motor (9) to which a propeller, equipped with propeller blades (10), a controller (5) and a battery pack (6), mounted around the perimeter of the vertical tunnel, are attached. Servo-controlled covers (13) are provided on each wing and stabilizer to close the vertical tunnels during the forward flight.