Research on liquid sloshing performance in vane type tank under microgravity

7th International Conference on Pumps and Fans

机械制造;工业技术

Hu, Q.^1 ; Li, Y.^1 ; Liu, J.T.^1 ; Liang, J.Q.^1

Beijing Institute of Control Engineering, Haidian District, Beijing, China^1

关键词: Gas liquid flows;    Liquid surface;    Microgravity environments;    Microgravity experiments;    Orbital maneuvers;    Propellant management devices;    Type structures;    Volume of fluid method;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/129/1/012016/pdf
DOI  :  10.1088/1757-899X/129/1/012016

学科分类：工业工程学

来源: IOP

【 摘 要 】

Propellant management device (PMD) in vane type tank mainly comprises of vane type structure parts, whose performance of restraining liquid sloshing should satisfy spacecraft requirements of high stabilization and fast orbital maneuver. Aiming at liquid sloshing performance in vane type tank under microgravity environment, gas-liquid flow model based on the volume of fluid (VOF) method was put forward, and via numerical simulation liquid sloshing performances of vane type PMD with anti-sloshing baffles and without anti-sloshing baffles in microgravity were analyzed and compared. Simulation results reveal that liquid sloshing performance of vane type PMD with anti-sloshing baffles is markedly superior vane type PMD without anti-sloshing baffles and the baffles make liquid surface become stable fast. Then by comparing between results of microgravity experiments and results of numerical simulations, they are very similar. According to present research, vane type PMD with antisloshing baffles has better effects on restraining liquid sloshing and is able to restrain observably propellant sloshing in tanks in order to satisfy spacecraft requirements of high stabilization and fast orbital maneuver.