摘要
目的针对航天器内微重力、变压力的工作环境,进行质子交换膜水电解制氧装置环境适应性设计。方法利用两相流仿真技术辅助进行电解芯体等部件微重力适应性设计,建立适应微重力、变压力环境的系统流程。研制了环境适应性评测装置,模拟考核设计的合理性。结果设计的电解制氧装置能够适应微重力、变压力工作环境,在轨连续运行96.88 h,累计产氧2097.8 SL,产氧速率0.74 kg/d。结论电解制氧装置环境适应性设计方案基本满足航天环境需求,地面评测方法可行。
Objective To carry out adaptability design of oxygen generation assembly by electrolysis（ OGA） for microgravity and variable pressure environment condition in spacecraft. Methods Microgravity adaptability design of electrolysis cell stack was accomplished by simulation method on two-phase flow and an OGA system flow suitable for microgravity and variable pressure environment was designed. Testing device for evaluating the design rationality was developed. Results The OGA worked stably in TG-1 space module. It produced2097. 8 SL oxygen during 96. 88 h,and the yield reached 0. 74 kg / d. Conclusions Design scheme of the OGA meets the requirements of space environment,and the ground-based evaluation methods are feasible.
出处
《航天医学与医学工程》
CAS
CSCD
北大核心
2015年第5期358-362,共5页
Space Medicine & Medical Engineering
基金
中国载人航天工程基金资助
关键词
电解制氧装置
环境适应性
设计与试验
航天器
oxygen generation assembly by electrolysis
environmental adaptability
design and test
space-craft
