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Application filed by Михаил Евменович БабкинfiledCriticalМихаил Евменович Бабкин
Priority to UAA200705468ApriorityCriticalpatent/UA85130C2/en
Publication of UA85130C2publicationCriticalpatent/UA85130C2/en
Is disclosed an aircraft for cargo and cargo-and-passenger transportation of increased load capacity, and also for average load capacity. A horizontal tail is installed above the flight deck, and a vertical tail is made at an angle of 45° from two planes, in which nose and tail sections turn synchronously to one and the same side. The horizontal and vertical tails create additional lift of wing. In this caseof the wing of aircraft can have larger value, since on the wing cannot be a stall, because on the horizontal tail a stall will emerge earlier because its angle of attack is bigger than in the wings. A fuselage is made from two symmetrical parts. In the middle part the large-dimension loads are placed, for which in the fuselage tail section a hatch is made, which is closed by one fold (ramp). Forward fuselage is intended for positioning the people. Main landing gear is three-leg, which provides required passability.