FIELD: aviation.
SUBSTANCE: group of inventions refers to aircraft engineering. Method for creating an aircraft wing lift in which an aircraft wing tip is disposed in the region of an incident flow of an expiring jet of one or more TJEs with a contour degree greater than 2. Incident flow of the escaping jet from the nozzles of one or more TJEs is guided along the upper and lower surfaces of the wing with mechanization elements to change the wing profile. Ratio of the volume of the incident flow of the escaping jet from the nozzles of one or more TJEs along the upper and lower surfaces of the wing with the elements of mechanization for changing the wing profile of the aircraft is from 30 % : 70 % to 10 % : 90 %. Exhaust part of the nozzle of one or more turbojet engines is located at a distance from the wing tip of not less than ΔL=3×Cmax, where Cmax is the maximum thickness of the wing along the axis of the jet engine. Variants of aircraft with jet engines that realize the method are proposed.
EFFECT: group of inventions is directed to increase the lift.
4 cl, 21 dwg
