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 two movable rotating discs, which arranged on both sides of fixed disk. The axe of movable rotating discs is coincided with the longitudinal axis of the aircraft. The fixed disc consists a specified number of holes with the same diameter, which are arranged concentric and evenly, and a movable discs consist 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. In the nose part of device is arranged the reservoir of compressed gas with the valve for deflation of gas into the distribution and control unit. |