FIELD: security means.
SUBSTANCE: group of inventions relates to emergency means of leaving the aircraft. Method of paratrooper landing is to use a gunpowder engine and a sensor, which turns a gunpowder engine on with electric command, depending on the current height, vertical rate of decline and the pre-measured mass of the pilot in the equipment. Gunpowder engine is made with the shortest possible operating time and the optimal direction of action of thrust. Information about the weight of the paratrooper in the equipment is transmitted from the strain gauge in the process of steady reduction to the sensor, which turns a gunpowder engine on with electrical command. System for reducing the vertical landing speed of the paratrooper contains a gunpowder engine mounted under the seat cover of the ejection seat, a sensor that measures the current altitude, the vertical speed of descent and receives information about the mass of the pilot in the equipment. Gunpowder engine is attached to a towing strand connected to a parachute harness and a quick-release coupling to a parachute with a reduced surface area of the dome.
EFFECT: group of inventions is aimed at expansion of technical facilities array.
2 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
PROCEDURE FOR DECREASING PILOT LANDING VERTICAL SPEED AFTER EJECTION AND SYSTEM TO THIS END | 2013 |
|
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AIRCRAFT CATAPULT SYSTEM | 2013 |
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RU2540133C1 |
METHOD OF PILOT (PASSENGER) CATAPULTING FROM AIRCRAFT | 2013 |
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RU2538481C1 |
METHOD AND SYSTEM FOR EJECTION AT HIGH RECTIFIED AIR SPEEDS | 2022 |
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RU2788230C1 |
METHOD AND SYSTEM FOR INFORMING THE CREW ABOUT THE SAFETY OF CATAPULTING | 2021 |
|
RU2774269C1 |
METHOD OF GENERATION OF EJECTION SEAT PARACHUTE DEPLOYMENT COMMAND | 2004 |
|
RU2280592C1 |
Authors
Dates
2018-11-07—Published
2017-05-17—Filed