Emergency escape method for an aircraft crew

PCT No. PCT/RU95/00172 Sec. 371 Date Feb. 13, 1998 Sec. 102(e) Date Feb. 13, 1998 PCT Filed Aug. 15, 1995 PCT Pub. No. WO97/07022 PCT Pub. Date Feb. 27, 1997The invention relates to means for the emergency abandonment of an aircraft and makes it possible to create a super-light and effective system...

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Bibliographische Detailangaben
Hauptverfasser:	SEVERIN, GAI ILIICH
Format:	Patent
Sprache:	eng
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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Zusammenfassung:	PCT No. PCT/RU95/00172 Sec. 371 Date Feb. 13, 1998 Sec. 102(e) Date Feb. 13, 1998 PCT Filed Aug. 15, 1995 PCT Pub. No. WO97/07022 PCT Pub. Date Feb. 27, 1997The invention relates to means for the emergency abandonment of an aircraft and makes it possible to create a super-light and effective system for emergency abandonment which can be used in aircraft with a flight speed of 500-600 km/hour. This is achieved by at first catapulting a parachute pack (7) by means of an ejection mechanism (6) and then catapulting a member of the crew using an ejection mechanism (2). In order to ensure safety in the case of pair catapulting, the direction of catapulting of the parachute pack and the member of the crew is at an angle of 15-20 DEG relative to the plane of symmetry of the aircraft. Furthermore, the parachute pack is used as a means for breaking the transparency of the cockpit.