FIELD: aircraft engineering.
SUBSTANCE: present invention relates to aviation. Method of vertical displacement and aircraft hovering in air is that the air flow from propeller engines (3,4) blows the wing. Wing has a swept shape in the plan with a large elongation. Flow is separated and directed over the wing along its consoles (1,2), and then a controlled positive pitch angle is given to the aircraft.
EFFECT: invention increases the maximum speed and improves the transverse stability of the aircraft in flight mode at a cruising speed.
1 cl, 3 dwg
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