FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to systems for aircraft crew emergency rescue by ejection. Proposed system comprises pneumatic drive composed of power supply, pressure regulator, parachute feed mechanism, and pilot shooting mechanism. Pneumatic drive parachute feed mechanism fixed and moving air cylinders comprises thrust for air cylinders and seals to thrust against at the end of stroke and ensure tight and permanent joint between said components.
EFFECT: higher reliability, lower weight and decreased sizes.
2 cl, 2 dwg
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Authors
Dates
2013-04-27—Published
2011-10-26—Filed