| 摘要 |
A device for rescue of aircraft comprises a brake parachute, a multi-canopy system of cargo parachutes connected by cable to the aircraft, a centering device to maintain the aircraft fuselage in a horizontal position, a device forming a braking effort made in the form of a pulley with an adjustable reverse drive, an additional mechanism to change the angle of inclination of the axis of aircraft fuselage to the horizontal line, and in case of emergency - within the range from 0° to 90°, in this case the seats of aircraft have gyroscopic mechanisms for maintaining a constant angle of inclination of the lower part of seats to the horizontal, &bgr;→ 0, in the pockets of the fuselage (and wings) of an aircraft are located at least four systems of air bags connected by pipes and valves to a source of high pressure of gas (air), such as high pressure cylinders, and it also comprises the main and backup systems of automatic control of emergency descent and manual control system of descent. Said multi-canopy system of cargo parachutes connected by cable to the aircraft, centering device, device that creates a braking effort, which is made in the form of a pulley with an adjustable reverse drive and additional mechanism to change the inclination of the axis of aircraft fuselage α are located in a additional unpressurized streamlined body of fuselage, which is attached to the main pressurized fuselage along the contour of the joint. |
