武装直升机抗坠毁救生技术  

Study of Crash Proof Lifesaving Technology of Armed Helicopter

作　　者：丁春全 李保刚[2] 马登武[2] 

机构地区：[1]海军驻襄樊地区航空军事代表室,湖北襄樊441003 [2]海军航空工程学院兵器科学与技术系,山东烟台264001

出　　处：《海军航空工程学院学报》2005年第5期547-550,共4页Journal of Naval Aeronautical and Astronautical University

摘　　要：通过对直升机抗坠毁救生技术的分析,着重阐述了抗坠毁座椅的工作原理、特性要求,讨论了吸能机构、约束装置、座椅垫的设计思想,分析了人体损伤机理和耐限.得出了武装直升机座椅、起落架和机体下部结构的抗坠毁性能,特别是座椅的抗坠毁性能决定抗坠毁生存率的结论.By analyzing crash proof lifesaving technology of armed helicopter, the paper mainly expounds working process and character of crashworthiness seat, discusses design idea of energy absorbing device, confining device and seat pad, analyzes body＇s damaging mechanism and draws a conclusion that the crash proof performance of seat, landing gear and structure, especially the crash proof performance of seat decides crash proof survival rate of armed helicopter.

关 键 词：武装直升机 抗坠毁座椅 救生系统 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]