| 摘要 |
A device for stabilizing an aircraft comprises an air intake, a distribution and control unit of gas flow, the gas-flow channels and the side nozzle, the system of control and drives, arranged in the nose part of the aircraft and connected in series. The distribution and control unit of gas flow is made in the form of rotating movable and fixed discs, the axe of which is coincided with the longitudinal axis of the aircraft. The fixed discs consists a specified number of holes with the same diameter, which are arranged concentric and evenly, and a movable disc consists only one similar hole. The holes of all disks are arranged on the same radius from the axis of symmetry of discs and the number of nozzle corresponds to the number of holes of fixed disk. |
