HIGHLY MANEUVERABLE AIRCRAFT Russian patent published in 2019 - IPC B64C3/28 B64D33/02 

FIELD: aviation.

SUBSTANCE: highly maneuverable airplane represents integral longitudinal biplane, comprising fuselage, wings equipped with root extensions, on which there is a front horizontal empennage, two-keel vertical tail unit, engines with variable thrust vector, having air scavers of engine compartments and heat exchangers air conditioning blowers, and chassis. Fuselage is configured to install suspended cargo container. Wings and front horizontal fins have arc-shaped recess of front edge. Air intakes of engines are located on sides of fuselage. Air intake chamfer sections face each other and are closed by ribs of plates of grids, having rhombic in cross section shape and outside coated with fine mesh grids. Inside the air intakes there are inclined grids, closed on the inlet side by fine mesh grids. Air intakes are configured to release air and / or debris into their lower part, with subsequent discharge through open-top valves.

EFFECT: invention is aimed at improvement of aerodynamic quality.

1 cl, 6 dwg