FIELD: transportation.;SUBSTANCE: invention relates to hybrid vehicles, in particular, to the construction of aircraft based on automobiles. Feature of an aircraft construction is the absence of an open rotor and its small dimensions, which allows it to fit into the dimensions of a car. Rotor and an impeller located under the rotor form an annular gap, an air flow that passed through the gap with the n-transformers is intercepted, located behind the annular gap and the n-flexible ducts, all the air ducts are combined into four groups of dense matrices. Three of them are spatially distributed along the aircraft base, creating three points of support for aircraft during take-off and landing, ensuring its spatial stability. Rotor blades are installed at an angle of 8-10° to the disk plane with a cycle between them. Aircraft is equipped with an impeller with two blades and a reducer connected to the impeller, ensuring its rotation opposite to the rotor, channeling air mass through the air ducts, and deflecting it at the capture of the aircraft.;EFFECT: higher reliability of an aircraft and a new product are provided.;1 cl, 12 dwg
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