FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation. The balancing aircraft includes two body parts that mirror each other, that is, they have the same structural shape and the same weight. The central parts of the body have an angle diverging to the sides, about 60 degrees. The extreme parts of the body have an angle directed downwards, about 30 degrees relative to the central parts of the body and have the ability to rise. There is a cockpit for pilots, cargo-passenger and fuel compartments. Support(e) engine(s) reactive type made(s) with the ability to deflect the thrust vector and change its position relative to the protruding structural element, made with the ability to move to the sides, back and forth. There are cruising-shunting engines made of a fan or jet type with the ability to control the deviation of the thrust vector, shunting engines, as well as a landing gear.
EFFECT: invention is aimed at increasing the carrying capacity and ensuring economical consumption of aviation fuel.
1 cl, 6 dwg
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