PARATROOP DEVICE Russian patent published in 2017 - IPC B64C39/02 B64D19/00 B64D1/14 

FIELD: aviation.

SUBSTANCE: paratroop device includes an inflatable shell filled with a gas containing a compartment socket for a paratrooper, a shock-absorbing device in the form of springs and simultaniously charged metal plates. The shell at the bottom part is connected to the compressor, the side walls of which at the bottom part transform into a large nozzle connected with springs to the support ring. The device is provided with a power source, a control unit and a source of a high voltage. The compressor as a thrust producer is provided with metallic plates connected to the high voltage source. The upper basement of the compressor comprises intake and outlet valves, channels for connecting of inner shell to the atmosphere through the nozzle, and shoulder is formed along the edge of the basement forming a compartment stow the shell. The basement is connected through the spring to the paratrooper compartment. The lower basement of the compressor is movable and is connected to the support ring with columns. The wheel on a spherical support with a drive is formed in the lower part of the nozzle. The paratroop device is designed so that the centre of gravity is at its bottom part.

EFFECT: higher reliability and controllability.

3 cl, 4 dwg