FIELD: aircraft engineering.
SUBSTANCE: invention relates to combined vehicles, particularly, to motor-based aircraft. Claimed aircraft differs from known designs in that it is deprived of exposed rotor and features minor sizes for it to be inscribed in car overall dimensions. Said rotor and disc arranged there under make a circular clearance. Airflow forced through said clearance is intercepted by n-transformers arranged behind said circular clearance. N-flexible air lines are integrated into four sets of dense matrices. Three of the latter are spaced along aircraft base to make aircraft three support points at takeoff-landing for aircraft spatial stability purposes. Rotor blades are arranged at 8-10 degrees to disc plane with clearances and coupled with shell ring on one side and on the other side with the barrel. Projection of blades on disc plane makes a continuous ring. Disc outer edge is shaped to torus. Inlet of every n-transformers equals 1/n part of circular clearance.
EFFECT: possibility of spatial displacement of craft in air.
8 dwg
