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流道弯曲度对微重力膜式水气分离性能的影响

张文伟,  柯鹏

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文章导航 > 北京航空航天大学学报  > 2016 >  42(8): 1639-1648.
金宇林, 庄达民, 杨钦等 . 民航客机油箱建模与油量传感器姿态误差修正[J]. 北京航空航天大学学报, 2005, 31(02): 218-222.
引用本文: 张文伟, 柯鹏. 流道弯曲度对微重力膜式水气分离性能的影响[J]. 北京航空航天大学学报, 2016, 42(8): 1639-1648. doi: 10.13700/j.bh.1001-5965.2015.0533
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Jin Yulin, Zhuang Daming, Yang Qinet al. Modeling of airliner gasoline tank and modification of attitude error of sensor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(02): 218-222. (in Chinese)
Citation: ZHANG Wenwei, KE Peng. Impact of channel curvature on microgravity membrane gas-liquid separation performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1639-1648. doi: 10.13700/j.bh.1001-5965.2015.0533(in Chinese)
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流道弯曲度对微重力膜式水气分离性能的影响

doi: 10.13700/j.bh.1001-5965.2015.0533
  • 1.

    北京航空航天大学 航空科学与工程学院, 北京 100083

  • 2. 北京航空航天大学 交通科学与工程学院, 北京 100083

基金项目: 国家“973”计划（2012CB20100）
详细信息
    作者简介:

    张文伟,男,博士研究生。主要研究方向:气液两相流。Tel.:010-82316627。E-mail:zhangwenwei.good@163.com;柯鹏,男,博士,副教授,硕士生导师。主要研究方向:人机与环境工程。Tel.:010-82316627。E-mail:p.ke@buaa.edu.cn

    通讯作者:

    柯鹏,Tel.:010-82316627,E-mail:p.ke@buaa.edu.cn

  • 中图分类号: V19;O359.1

Impact of channel curvature on microgravity membrane gas-liquid separation performance

  • 1.

    School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

    摘要
  • 摘要: 开展微重力膜式水气分离性能仿真研究，对水气分离技术设计与优化具有重要意义。针对微重力入口边界气液界面多尺度问题（入口流型问题）提出了基于界面概率近似方法的欧拉双流体模型，采用动量源项法解决几何多尺度问题（分离膜边界问题），为仿真研究提供了有效的入口及渗透边界。研究了典型工作参数下流道弯曲度对膜分离性能的影响，并从流动形态和作用力贡献2个方面分析了影响机理。结果表明：膜分离性能随流道弯曲度增大而降低，影响程度与入口含气率相关；直流道适于选作膜式静态水气分离器主要流道形式。

     

    Abstract: The simulation research on the performance of microgravity membrane gas-liquid separation is of great significance for the design and optimization of gas-liquid separation technology. The Eulerian two-fluid model with an interface probability approximation method is introduced for the computability of multi-scale gas-liquid interface problem at inlet boundary in microgravity (inlet flow pattern problem), and the momentum source method is proposed for multi-scale geometric problem at membrane boundary. The model and the method provide a valid entry and permeable boundary for the simulation study. The influence of channel curvature on the membrane separation performance with typical operating parameters is studied, and the influence mechanism is analyzed in the view of flow morphologies and force contributions. The results show that the membrane separation performance reduces with channel curvature increasing, and the influence is related to inlet gas phase volume fraction; straight channel is suitable for membrane static gas-liquid separator.

     

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出版历程
  • 收稿日期:  2015-08-18
  • 网络出版日期:  2016-08-20

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