首页|空间液氪气液分离装置流阻特性及数值模拟

空间液氪气液分离装置流阻特性及数值模拟

扫码查看
为满足低温推进剂在空间微重力环境中的气液分离要求,针对液氪低温推进剂在轨管理与传输问题,建立筛网式气液分离装置单通道流动压力损失的理论预测模型,获取 120 K饱和状态液氪在 325×2300荷兰斜纹编织网中流动的泡破点压力.对比分析了不同低温流体、通道宽度、质量流量对过网压降的影响规律,获得了液氪在通道中流动的压降分布,并通过国外液氢过网压降实验数据对模型进行了验证.通过建立液氪单通道流动数值仿真模型,较好地预测了过网压力损失.
Analysis and Numerical Simulation of Liquid Krypton Flow Resistance in Membrane Channel Gas-liquid Acquisition Device
In order to meet the requirements of gas-liquid separation of cryogenic propellant in space environment,for the problem of cryogenic liquid-krypton propellant acquisition and transmission in orbit,a theoretical prediction model is es-tablished to obtain the bubble-point pressure of liquid-krypton in saturated state of 120 K flowing in 325×2300 Dutch twill woven mesh.The influence laws of different cryogenic fluids,channel widths,and mass flow rates on the over-the-network pressure drop are comparatively analyzed.The pressure drop distributions of liquid-krypton flowing in the channel are ob-tained.The pressure drop distribution of liquid-krypton flow in the channel is obtained,and the model is verified by the pres-sure drop test data of liquid hydrogen over the network.The numerical simulation model of liquid krypton single-channel flow is established,which can better predict the pressure loss across the network.

gas-liquid separation technologytankpropellant management devicesliquid krypton

原宇琦、朱建炳、于斌、顾森东

展开 >

兰州空间技术物理研究所 真空技术与物理重点实验室,兰州 730000

气液分离技术 贮箱 推进剂管理装置 液氪

甘肃省科技重大专项2023年陇原青年创新创业人才(个人)项目

22ZD6GA011

2024

真空与低温
中国航天科技集团公司第五研究院510研究所

真空与低温

CSTPCD
影响因子:0.567
ISSN:1006-7086
年,卷(期):2024.30(2)
  • 19