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2 551 049

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(51)

IPC

B64D25/10(2006-01-01)

(21) (22)

Application

2013149325/11, 2013-11-07

(24)

Start date

2013-11-07

(22)

Actual filing date

2013-11-07

(45)

Published

2015-05-20

(72)

Inventor

Pozdnjakov Sergej SergeevichRafeenkov Vladimir MikhajlovichShmukler Boris Jur'EvichZernov Valerij RafailovichKiselev Jurij AndreevichKovba Vjacheslav ViktorovichSharun Vladislav Fedorovich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Predprijatie Imeni Akademika G.I. Severina"

METHOD OF AIRCRAFT CREW RESCUE AND SYSTEM TO THIS END Russian patent published in 2015 - IPC B64D25/10

Abstract RU 2551049 C1

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering, particularly, to catapult seat deceleration system. Ejection system comprises pneumatic drive composed by moving pneumatic cylinder-accumulator. Pneumatic cylinder comprises restrictor and safety valve. Method of ejection consists in sequential operation of, first, restrictor, then, safety valve to ensure compressed air design magnitude.

EFFECT: decreased weight and overall dimensions.

4 cl, 3 dwg

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RU 2 551 049 C1

Authors

Pozdnjakov Sergej Sergeevich

Rafeenkov Vladimir Mikhajlovich

Shmukler Boris Jur'Evich

Zernov Valerij Rafailovich

Kiselev Jurij Andreevich

Kovba Vjacheslav Viktorovich

Sharun Vladislav Fedorovich

Dates

2015-05-20—Published

2013-11-07—Filed