FIELD: aviation.
SUBSTANCE: invention relates to the aviation equipment. Multipurpose super-heavy transport technological platform of aircraft shortened takeoff and landing is made in aerodynamic scheme "integral longitudinal triplane" represents a free-carrying monoplane and comprises fuselage, basic wing of variable sweep, trapezoidal arms, swept front horizontal empennage, front vertical empennage of trapezoidal shape in plan view, power plant with engines arranged in rear part of fuselage, three-support chassis. Bearing fuselage is integrated with wing in length and shape and includes nose part of cylindrical shape, conjugations connected with trapezoidal central part, and rear part. In the longitudinal section from the cylindrical part to the stern cut the rear part is made as profiled equidistant to the wing profile. Engines of power plant are packaged in tail part of fuselage in horizontal row along span above its top surface or in arrangement with location inside tail part of aircraft with air intake integrated with airframe, with control device of thrust vector and reversing thrust. Basic wing of aircraft consists of developed influx in central part, having trapezoid shape in plane.
EFFECT: invention is aimed at higher safety.
6 cl, 12 dwg
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Authors
Dates
2020-02-12—Published
2019-02-04—Filed