液冷服散热原理模型及其分析  

A Heat Transfer Model for Liquid Cooling Garment (LCG) and Its Analysis.

作　　者：张万欣[1] 陈景山[1] 李潭秋[1] 

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》2000年第5期350-354,共5页Space Medicine & Medical Engineering

摘　　要：目的建立舱外航天液冷服散热的原理模型 ,提出其在工程设计中应遵循的基本原则。并以该原理模型为基础找到液冷服设计参数与散热量和散热效率的模化关系。方法根据工程实际 ,对舱外航天液冷服散热过程进行分析。结果液冷服各参数 (管长、管径、流率和进口液温 )对散热量和散热效率的影响是相互制约 ,相互作用的。因此各参数的合理取值是设计液冷服的关键。结论该分析和研究对今后舱外航天液冷服的设计研制具有一定的指导意义。Objective To establish the heat transfer model for liquid cooling gannent(LCG) and,basing on this model,to find the relations between the design parameters and heat removing,as well as that between the design parameters and heat transfer efficiency. Method Heat transfer process of the LCG was analyzed according to engineering facts.Result The relations between the design parameters and heat removing,and also that between the design parameters and heat transfer efficiency were interelative and the optimal values of the parameters were essential to the design of LCG. Conclusion The results might be useful in the design of LCG in extra vehicular activity(EVA) space suit.

关 键 词：液冷服 散热效率 设计参数 数学模型 航空航天 

分 类 号：R852.81[医药卫生—航空、航天与航海医学]