COMBINED AIRCRAFT WING Russian patent published in 2017 - IPC B64C3/32 B64D33/04 

FIELD: aviation.

SUBSTANCE: wing of the aircraft contains a bearing surface and a turbojet engine. The bearing surface is combined and made of a conventional aerodynamic wing and a carrier plate rigidly connected to it. The engine is rigidly fixed to the carrier plate so that the jet of hot gases emerging from it flows around its upper surface. The profile of the carrier plate repeats the profile of the turbojet engine Laval nozzle. Effective areas of aerodynamic plate and carrier plate are equal. The aircraft contains a fuselage with wings, the lifting force vectors of which and the center of gravity of the entire aircraft lie in the same plane perpendicular to the aircraft symmetry axis. The aircraft center of gravity is located below the points of application of all lifting forces.

EFFECT: increased range, load capacity and safety of their use.

2 cl, 4 dwg