| 摘要 |
FIELD: aeronautical engineering. SUBSTANCE: flying vehicle includes round case with flat lower surface, control cabin, wing, air intake ducts, supercharger. power plant and hinged movable dampers. Hollow vertical frame is provided for bounding central circular cavity of case. Flying vehicle has gas-turbine engine with three-stage compressor which is mounted on vertical axle of circular opening of frame; its upper portion is coupled by control cabin with egg-shaped outer surface. Biconvex wing is coupled with vertical frame. Body of this wing is provided with air intake ducts which are connected with zone where compressor of gas-turbine engine is installed. Gas-turbine engine compressor is provided with three-stage blades. EFFECT: simplified construction; ease in servicing; reduced drag in horizontal flight. 3 cl, 10 dwg
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