西锐整机降落伞系统设计研究  

Study on the Design of Cirrus Airframe Parachute System

作　　者：韩寒 朱铮 Han Han;Zhu Zheng(AVIC Aerospace Life-support Industries,Ltd.,Hubei Xiangyang,441003)

机构地区：[1]航空工业航宇救生装备有限公司,湖北襄阳441003

出　　处：《中国个体防护装备》2021年第1期14-20,共7页China Personal Protective Equipment

摘　　要：随着通航产业的蓬勃发展,轻型飞机已成为通用航空市场中非常具有发展潜力的机型,保障飞行安全对于轻型飞机的长远发展而言至关重要。弹道式整机降落伞救生系统作为飞行安全的最后一道防线,可大大提升驾驶员和乘客的旅程安全性。本文以西锐公司飞机配备的整机降落伞系统为研究对象,详细介绍了CAPS系统的设计验证、结构、工作程序、适用情况、使用条件和着陆考虑因素等方面,以期使相关专业设计人员对CAPS系统有一个较全面的认识,更好地把握整机降落伞系统的研究和发展方向。With the rapid development of general aviation industry,light aircraft has a great potential of development in general aviation market.Flight safety is very important for the long-term development of light aircraft.As the last line of defense for flight safety,the whole-plane ballistic parachute recovery system can greatly improve the safety of pilots and passengers.In this paper,the Cirrus Airframe Parachute System(CAPS)equipped for Cirrus aircraft is described in detail,including the design verification,structure,deployment procedures,deployment scenarios,general deployment information and landing considerations of CAPS.Thus,the professional designers will have a comprehensive understanding of CAPS,and forecast the development direction of the whole-plane parachute recovery system.

关 键 词：轻型飞机 飞行安全 西锐整机降落伞 

分 类 号：V244.216[航空宇航科学与技术—飞行器设计]