DEVICE FOR TWIN EJECTION Russian patent published in 2006 - IPC B64D25/10 

Abstract RU 2286288 C1

FIELD: aeronautical engineering; ejection systems.

SUBSTANCE: twin ejection is carried out by means of ejection system including three pyro-mechanisms mounted on one of ejection seats; one pyro-mechanism actuates pyro-cylinder of other seat through gas duct feeding pulse to its ejection drive. Two other pyro-mechanisms actuate at time delay pyro-cylinder feeding pulse to ejection drive of first ejection seat.

EFFECT: simplification of system; enhanced reliability and self-containment due to use of pyro-system.

1 dwg

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RU 2 286 288 C1

Authors

Severin Gaj Il'Ich

Rafeenkov Vladimir Mikhajlovich

Sobolev Petr Petrovich

Savinov Al'Bert Pavlovich

Gipich Al'Bert Fedorovich

Dates

2006-10-27Published

2005-03-03Filed