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微重力下冷凝及传热研究进展

郭帅 秦业超 王鑫 许波 陈振乾

郭帅, 秦业超, 王鑫, 许波, 陈振乾. 微重力下冷凝及传热研究进展[J]. 空间科学学报. doi: 10.11728/cjss2026.02.2025-0028
引用本文: 郭帅, 秦业超, 王鑫, 许波, 陈振乾. 微重力下冷凝及传热研究进展[J]. 空间科学学报. doi: 10.11728/cjss2026.02.2025-0028
GUO Shuai, QIN Yechao, WANG Xin, XU Bo, CHEN Zhenqian. Review of Progress in Condensation and Heat Transfer Research in Microgravity (in Chinese). Chinese Journal of Space Science, 2026, 46(2): 1-14 doi: 10.11728/cjss2026.02.2025-0028
Citation: GUO Shuai, QIN Yechao, WANG Xin, XU Bo, CHEN Zhenqian. Review of Progress in Condensation and Heat Transfer Research in Microgravity (in Chinese). Chinese Journal of Space Science, 2026, 46(2): 1-14 doi: 10.11728/cjss2026.02.2025-0028

微重力下冷凝及传热研究进展

doi: 10.11728/cjss2026.02.2025-0028 cstr: 32142.14.cjss.2025-0028
基金项目: 国家自然科学基金项目(52306075, 52376049), 中国博士后科学基金项目(2023M740591), 江苏省基础研究计划自然科学基金项目(BK20230849)和载人空间站工程空间科学和应用项目(冷凝过程强化和液膜非稳定性研究)共同资助
详细信息
    作者简介:
    • 郭帅 男, 现为东南大学能源与环境学院博士研究生, 主要研究方向为常/微重力环境下液滴动力学及冷凝传热研究. E-mail: Shuai_Guo@seu.edu.cn
    • 陈振乾 男, 现为东南大学能源与环境学院教授, 博士生导师, 主要研究方向为常/微重力环境下流体传热及强化技术、系统热控技术. E-mail: zqchen@seu.edu.cn
  • 中图分类号: TK124

Review of Progress in Condensation and Heat Transfer Research in Microgravity

  • 摘要: 综述微重力下膜/滴状冷凝的研究进展, 揭示两相流传热机理及重力影响规律. 对于管内冷凝, 可采用重力无关准则数(Bond数与Froude数等)判断重力是否影响传热, 通过增加蒸汽质量流速和减小管径减弱重力影响, 分析微重力冷凝下传热关联式以指导工程设计. 对于滴状冷凝, 在微重力环境下可通过提高蒸汽流速、使用功能性表面结合气流吹扫去除冷凝液滴, 实现持续滴状冷凝. 当前微重力冷凝实验研究的发展因缺少长期连续微重力环境而受到限制, 需借助中国空间站和国际空间站开展长时间冷凝传热实验, 以弥补可重复实验数据的不足, 探索重力作用机制, 为空间两相换热系统提供理论支撑.

     

  • 图  1  水平管道内冷凝两相流流型分布[8]

    Figure  1.  Flow pattern distribution of two-phase condensation flow in horizontal pipe

    图  2  不同重力条件下管内流型变化[9]

    Figure  2.  Change of flow pattern in pipe under different gravity conditions

    图  3  不同重力水平下的可视化流型[12]

    Figure  3.  Flow pattern visualizations under different gravity levels

    图  4  不同重力情况下圆管内的气液界面[14]

    Figure  4.  Liquid-vapor interfaces inside round tubes under different gravitational accelerations

    图  5  气液两相流动中的主导作用力分区[20]

    Figure  5.  Partition diagram of dominant forces in gas-liquid two-phase flow

    图  6  ENCOM-2项目翅片膜状冷凝实验装置[33]

    Figure  6.  ENCOM-2 Project fin film condensation experiment setup

    表  1  微重力条件下管内冷凝模拟的主要内容及结论

    Table  1.   Main contents and conclusions of the simulation of condensation in tubes under microgravity condition

    研究类型 研究对象 研究工质及条件 主要结论 文献
    VOF模拟 内径1 mm圆形微通道 工质: R134 a
    G= 100, 800 kg·m–2·s–1
     低质量流速时, 产生偏心环流, 管道上部传热效果远优于底部; 高质量流速时, 重力的影响可忽略不计 [13]
    VOF模拟 内径3.78 mm水平光滑圆管 工质: R410 A
    G = 307~720 kg·m–2·s–1
    g = 0~9.81 m·s–2
     低流速时重力显著提高传热系数, 高流速时重力影响减弱; 零重力下质量传递率显著降低, 液膜分布更均匀 [14]
    VOF模拟 内径0.25~4 mm水平
    光滑圆管
    工质: R410 A
    G = 400~1000 kg·m–2·s–1
     传热系数和压降随质量流速增加、管径减小而增大; 小通道底部液膜堆积, 微通道中均匀分布, 重力效应可忽略 [15]
    三维瞬态VOF模型 内径1~2 mm水平圆管 工质: Neon
    G = 20~187 kg·m–2·s–1
    饱和温度: 34.5~37.5 K
    壁温: 29~32 K
     重力对低温工质冷凝影响显著, 零重力下界面波动增强传热; 小直径管抑制重力分层效应, 液膜分布更均匀; 质量流速增加可削弱重力影响 [17,18]
    下载: 导出CSV

    表  2  环状流冷凝传热关联式

    Table  2.   Condensation heat transfer correlations for annular flow

    关联式 适用工质及管道尺寸 文献
    $ \dfrac{{h}_{tp}{D}_{h}}{{k}_{f}}=0.0274{\text{Pr}}_{f}\text{Re}_{f}^{0.6792}{x}^{0.2208}\dfrac{{\phi }_{g}}{{X}_{tt}} $ R134 a多通道Dh = 1.46 mm [26]
    $ \dfrac{{h}_{tp}{D}_{h}}{{k}_{f}}=0.0152(1+0.6\text{Pr}_{f}^{0.8})\dfrac{{\phi }_{g}}{{X}_{tt}}\text{Re}_{f}^{0.77} $ R134 a多通道Dh = 0.80 , 1.11 mm [27]
    $ \dfrac{{h}_{tp}D}{{k}_{f}}=0.0152(-0.33+0.83\text{Pr}_{f}^{0.8})\dfrac{{\phi }_{g}}{{X}_{tt}}\text{Re}_{f}^{0.77} $ R410 A, R410 A/油D = 1.6, 4.18 mm [28]
    $ \dfrac{{h}_{tp}D}{{k}_{f}}=25.084\text{Re}_{f}^{0.258}\text{Pr}_{f}^{-0.495}P_{R}^{-0.288}{\left(\dfrac{x}{1-x}\right)}^{0.266} $ R134 a, R404 AD = 0.31~3.30 mm [29]
    $ \dfrac{{h}_{tp}D}{{k}_{f}}=0.0055\text{Pr}_{f}^{1.37}\dfrac{{\phi }_{g}}{{X}_{tt}}\text{Re}_{f}^{0.7} $ R134 a, R236 fa, R1234 ze(E)多通道Dh = 1.45 mm [30]
    下载: 导出CSV

    表  3  微重力下强化冷凝传热技术对比

    Table  3.   Comparison of enhanced condensation heat transfer techniques under microgravity

    方法类型代表技术传热强化效果重力敏感性工程复杂度适用场合
    表面润湿改性超疏水/超亲水涂层小型航天器热控表面
    多孔结构强化金属泡沫/烧结毛细芯空间站两相流体回路
    微纳沟槽结构V型槽/螺旋沟槽较高高热流密度冷凝器
    电场强化脉冲电场辅助冷凝精密电子设备冷却
    离心力辅助旋转冷凝器航天器可旋转部件热控
    振动/超声波扰动压电致动器高频振动较低小型设备局部强化
    下载: 导出CSV
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  • 收稿日期:  2025-02-25
  • 修回日期:  2025-05-22
  • 网络出版日期:  2025-05-26

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