载人飞行舱内压力服技术研究与实现  被引量:3

Research and Realization of Technigue of Intra-vehicular Pressure Garment.

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作  者:李潭秋[1] 陈景山[1] 边晋梅 

机构地区:[1]航天医学工程研究所,北京100094

出  处:《航天医学与医学工程》2003年第z1期508-513,共6页Space Medicine & Medical Engineering

基  金:中国载人航天工程基金资助

摘  要:目的研究用于载人飞行舱内压力服的实现技术 ,研制舱内压力服系统。方法通过分析提出研制方案 ,针对载人航天器应急救生的技术性能要求 ,研究压力服的结构实现技术、压力控制技术、操作活动性能的保证技术、通风供氧技术、视觉保证和防雾技术的实现方法 ,通过研制和试验验证保证航天服的技术性能。结果在设计和工艺上实现了载人航天飞行所需压力防护和工效保障要求的舱内压力服系统 ,并通过了性能和接口匹配试验以及严酷的环境试验验证。结论所研制的舱内压力服完全能够满足天地往返运输系统的压力应急工况使用要求。Objective To study the technology of intra-vehicular pressure protection for manned space craft pressure emergency and to develop the pressure garment.Method According to the requirements of manned spacecraft emergency,the research scheme was proposed.Then the realization method of the following techniques were studied:structure of the pressure suit,pressure control,ergonomics,ventilation and oxygen supply,vision support and anti-fog.The performance of the space suit was verified by research and environment experiment. Result An intra-vehicular pressure garment system was realized.It could fulfil the requirements of pressure protection and ergonomics and has passed overall performance test,interface test,and environment test. Conclusion The intra-vehiclar pressure garment developed by us can meet the requirements of space transportation system during pressure emergency.

关 键 词:载人航天 生命保障系统 航天服 压力服 

分 类 号:R852.81[医药卫生—航空、航天与航海医学]

 

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