DEVICE FOR TWIN EJECTION

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...

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Bibliographische Detailangaben
Hauptverfasser:	SAVINOV AL'BERT PAVLOVICH, GIPICH AL'BERT FEDOROVICH, SEVERIN GAJ IL'ICH, SOBOLEV PETR PETROVICH, RAFEENKOV VLADIMIR MIKHAJLOVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	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