加注流量对叶片式贮箱中气液分布的影响

doi:10.3969/j.issn.1674-1579.2013.06.004

Abstract

Abstract: In the microgravity environment, the position of the ullage bubble is uncertain. It’s hard to vent and control the center of mass for the receiver tank on mission of on-orbit refilling. The test tank of NASA FARE II is taken as reference. According to the theory of surface tension tank, calculation model is established. Under the conditions of different refill flow rates, the gas-liquid distribution in the vane-type surface-tension tank is studied with the method of numerical simulation. The hydrazine is chosen as working liquid. Using the CFD（computational fluid dynamics） software Fluent, the process of vane-type tank on-orbit refilling is simulated. Simulation results show that the greater the inflow rate is, the higher the gas-liquid interface protrudes. When the inflow rate exceeds the critical value, liquid is vented. The results can provide reference for the control of refill flow rate.

CLC Number:

SI Ping-Jun, WANG Hua, CUI Cun-Yan, WANG Yan, LI Wei, SUN Jian. Effect of Refill Flow Rate on Gas-Liquid Distribution in Vane-Type Tank[J]., 2013, 39(6): 17-22.

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http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2013/V39/I6/17

References

［1］David J C, Timothy A M. Vented tank resupply experiment: flight test results［J］. Journal of Spacecraft and Rockets, 2006, 43(5): 1124-1130 ［2］李永, 潘海林, 魏延明. 第二代表面张力贮箱的研究与应用进展［J］. 字航学报, 2007, 28(2): 503-507 Li Y, Pan H L, Wei Y M. The evolvement of the study and application on the second generation surface tension tank［J］. Journal of Astronautics, 2007, 28(2): 503-507 ［3］Bicknell B A, Czysz P M. Low-g venting tests to support on-orbit fluid resupply systems［C］.The 26th AIAA/ASME/SAE/ASEE Joint Propulsion Conference，Orlando, FL, July 16-18, 1990 ［4］Dominick S M, Tegart J R, Driscoll S L, et al. Fluid acquisition and resupply experiments on space shuttle flights STS-53 and STS-57［R］. Alabama, USA: Marshall Space Flight Center, 2011 ［5］Dipprey N F, Rotenberger S J. Orbital express propellant resupply servicing［C］. The 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, July 20-23, 2003 ［6］李永, 潘海林, 魏延明, 等. 板式贮箱内部流动的定常和非定常数值模拟［J］. 宇航学报, 2007, 28(3): 623-627 Li Y, Pan H L, Wei Y M, et al. The steady and unsteady numerical simulations of the flow in vane type surface tension tank［J］. Journal of Astronautics, 2007, 28(3): 623-627 ［7］胡齐, 陈健, 李永. 微重力板式贮箱推进剂重定位的数值仿真［J］. 空间控制技术与应用, 2009, 35(6): 54-57 Hu Q, Chen J, Li Y. Numerical simulation for reorientation of propellant in a vane tank under microgravity［J］. Aerospace Control and Application, 2009, 35(6): 54-57 ［8］胡齐, 李永, 耿永兵, 等. 一种板式推进剂管理装置(PMD)性能的数值仿真［J］. 空间控制技术与应用, 2010, 36(3): 55-58 Hu Q, Li Y, Geng Y B, et al. Numerical simulation for capability of a vane PMD to manage propellant［J］. Aerospace Control and Application, 2010, 36(3): 55-58 ［9］李永, 胡齐, 潘海林, 等. 推进剂在轨加注流体传输过程的数值模拟和地面试验研究［J］. 空间控制技术与应用, 2011, 37(4): 54-57 Li Y, Hu Q, Pan H L, et al. Numerical simulation and ground test research on orbital refueling process［J］. Aerospace Control and Application, 2011, 37(4): 54-57 ［10］魏月兴, 陈小前, 黄奕勇. 内角流动及其在卫星贮箱设计中的应用［J］. 中国科学, 2011, 41(9): 1218-1224 Wei Y X, Chen X Q, Huang Y Y. Interior corner flow theory and its application to the satellite propellant management device design［J］. Science China, 2011, 41(9): 1218-1224 ［11］李京浩, 陈小前, 黄奕勇, 等. 微重力环境下的不对称内角流动研究［J］. 中国科学, 2012, 42(8): 957-962 Li J H, Chen X Q, Huang Y Y, et al. Study on asymmetric interior corner flow in microgravity condition［J］. Science China, 2012, 42(8): 957-962 ［12］李京浩, 陈小前, 黄奕勇. 基于内角流动的板式表面张力贮箱内推进剂流动过程研究［J］. 国防科技大学学报, 2012, 34(4): 18-21 Li J H, Chen X Q, Huang Y Y. A study of propellant flow in the vanetype surface tension tank based on interior corner flow［J］. Journal of National University of Defense Technology, 2012, 34(4): 18-21 ［13］张天平. 表面张力贮箱推进剂管理装置设计进展［J］. 中国空间科学技术, 2000(5): 36-42 Zhang T P. The progress in design of propellant management devices for surface tension tanks［J］. Chinese Space Science and Technology, 2000(5): 36-42 ［14］薛国宇, 陈志坚, 王德忠. 低温表面张力贮箱研究［J］. 火箭推进, 2006, 31(3): 26-29 Xue G Y, Chen Z J, Wang D Z. Study on cryogenic surface tension propellant tank［J］. Journal of Rocket Propulsion, 2006, 31(3): 26-29 ［15］胡文瑞, 徐硕昌. 微重力流体力学［M］. 北京: 科学出版社，1999: 55-56 ［16］李治. 卫星用表面张力贮箱设计研究［D］. 长沙: 国防科技大学, 2002 Li Z. Design and research of the surface tension tank for satellite［D］.Changsha: National University of Defense Technology, 2002 ［17］刘桢, 李红, 褚桂敏, 等. 液体流过金属编织网的流阻损失［J］. 强度与环境, 2010, 37(2): 4248 Liu Z, Li H, Chu G M, et al. Pressure drop of fluid flowing through woven screens［J］. Structure & Environment Engineering, 2010, 37(2): 42-48 ［18］Cady E C. Study of thermodynamic vent and screen baffle integration for orbital storage and transfer of liquid hydrogen［R］. Huntington Beach, California: NASA Lewis Research Center, August 1973 ［19］McQuillen J B, Chao D F, Hall N R, et al. CFD simulations of flow in capillary flow liquid acquisition device channel［J］. World Academy of Science, Engineering and Technology, 2012, 68: 759-765

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Effect of Refill Flow Rate on Gas-Liquid Distribution in Vane-Type Tank

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