FIELD: aeronautical engineering. SUBSTANCE: mechanism is mounted on load-bearing framework 1 of ejection seat and in seat 2 provided with through longitudinal slot 3; mechanism has oxygen equipment unit 5 with cut-in device 6, starter 7 made in form of cylinder 8 with spring-loaded rod 9 and carrier 10 secured on rod 9 and mounted in slot 3 of seat 2, cut-in drive of unit 5 made in form of rope linkage 12 whose one end is connected with rod 9 of starter 7; other end of rope linkage is provided with cotter pin 13 locking cut-in device 6. Articulated on side member of load-bearing framework 1 is spring-loaded bell crank 14 connected with leg strap by means of starting link 17. EFFECT: enhanced reliability. 2 cl, 3 dwg
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Authors
Dates
1995-08-20—Published
1990-01-29—Filed