| 摘要 |
FIELD: aeronautical engineering. ^ SUBSTANCE: proposed flying vehicle has round case, cabin with control members, circular flow-through chamber located horizontally and provided with rectilinear inlet passage; flying vehicle is also provided with supercharger mounted on supports, main revolving ring with drive located inside circular flow-through chamber and control system with channels, shutters and swivel flaps. Flying vehicle is also provided with circular support and additional revolving ring which are mounted inside circular flow-through chamber under main revolving ring. Additional revolving ring is connected with drive of main revolving ring for rotation in opposite direction. Circular flow-through chamber is provided with partition engageable with inlet and outlet rectilinear passages. Supercharger is mounted inside outlet rectilinear passage. Supercharger supports are made in form of hollow pylons whose cavities are communicated with cavity of rectilinear outlet passage through controllable valves and with channels of control system. Shutters of control system are located at inlet of one of outlet holes. Swivel flaps of control system are located above said hole in flow section of outlet rectilinear passage. Revolving rings are provided with electric drive whose generator is connected with drive of supercharger. ^ EFFECT: enhanced efficiency, stability, safety and maneuverability of flying vehicle. ^ 6 dwg |
