FIELD: aviation.
SUBSTANCE: proposed aircraft has fuselage on which wing consisting of two halves is secured; turbo-jet engine is secured inside it. Mounted in aircraft wing is flat gas guide device whose interior is divided into two separate bow-shaped channels by means of partitions. Inlet ends of channels are located closer to aircraft fuselage axis and are connected with turbine part of engine and outlet ends of channels are located far away form aircraft axis along wing; they are communicated with atmosphere. Additional engine is secured in fuselage. Turbine part of each engine mounted on fuselage port side is connected with inlet ends of channels located in starboard half of wing; turbine part of each engine mounted on fuselage starboard side is connected with inlet ends of channels located in port half of wing. Channels of port and starboard halves of wing intersect inside fuselage and run at different levels relative to wing plane.
EFFECT: enhanced efficiency of aircraft.
4 cl, 4 dwg
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