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SYSTEM FOR AIRCRAFT CREW EMERGENCY RESCUE BY EJECTION

机译:飞机乘员紧急救援系统

摘要

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
机译:技术领域本发明涉及飞机工程,尤其涉及用于通过弹出的飞机机组人员紧急救援的系统。拟议的系统包括气动驱动器,该气动驱动器由电源,压力调节器,降落伞进给机构和先导射击机构组成。气动驱动降落伞进给机构固定和移动的气缸包括用于气缸的推力和在冲程结束时推压的密封件,以确保所述组件之间的牢固永久连接。效果:更高的可靠性,更轻的重量和更小的尺寸。; 2 cl ,2载重吨

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