VERTICAL TAKEOFF AND LANDING AIRCRAFT IMPLEMENTED ACCORDING TO CANARD CONFIGURATION Russian patent published in 2017 - IPC B64C29/00 B64C39/12 

FIELD: aviation.

SUBSTANCE: invention relates to the structure of vertical takeoff and landing aircraft (VTOL). The VTOL is designed according to canard configuration, it is equipped with an additional height tail fin, consisting of a bow and a tail part with the lower and upper surfaces fixed with the possibility of rotation on the spinning axis. The width of the height tail fin is equal to the width of the fuselage. The outlet of each lifting and cruise fan is equipped with side air flow restrictors of the fan. Rotary profiles of the grids are made in the form of assembly flexible blades, and the outlet section of the outlet is made of a complex shape with upper and lower horizontal flexible edges. The exhaust nozzles of the engines are adjacent to the upper surface of the additional height tail fin, longitudinal ridges are installed along the edges of the fuselage lower surface.

EFFECT: possibility of obtaining additional lift on takeoff, landing and transitional flight modes.

6 cl, 4 dwg