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锯齿翅片微小通道中R134a的冷凝传热实验研究

李杰 张大林 詹宏波 张朋磊 朱光亚

李杰, 张大林, 詹宏波, 等. 锯齿翅片微小通道中R134a的冷凝传热实验研究[J]. 航空动力学报, 2026, 41(2):20230669 doi: 10.13224/j.cnki.jasp.20230669
引用本文: 李杰, 张大林, 詹宏波, 等. 锯齿翅片微小通道中R134a的冷凝传热实验研究[J]. 航空动力学报, 2026, 41(2):20230669 doi: 10.13224/j.cnki.jasp.20230669
LI Jie, ZHANG Dalin, ZHAN Hongbo, et al. Experimental study on flow condensation heat transfer of R134a in serrated mini channel[J]. Journal of Aerospace Power, 2026, 41(2):20230669 doi: 10.13224/j.cnki.jasp.20230669
Citation: LI Jie, ZHANG Dalin, ZHAN Hongbo, et al. Experimental study on flow condensation heat transfer of R134a in serrated mini channel[J]. Journal of Aerospace Power, 2026, 41(2):20230669 doi: 10.13224/j.cnki.jasp.20230669

锯齿翅片微小通道中R134a的冷凝传热实验研究

doi: 10.13224/j.cnki.jasp.20230669
基金项目: 国家自然科学基金(52176157,52106247); 教育部“春晖计划”合作科研项目(202201007); 江苏高校优势学科建设工程
详细信息
    作者简介:

    李杰(1992-),男,博士,主要从事飞行器环境控制和两相流传热传质研究。E-mail:jl1901031@nuaa.edu.cn

    通讯作者:

    张大林(1970-),男,教授,博士,主要从事飞行器环境控制、飞机结冰防冰、两相流传热传质研究。E-mail:zhangdalin@nuaa.edu.cn

  • 中图分类号: V245.3

Experimental study on flow condensation heat transfer of R134a in serrated mini channel

  • 摘要:

    采用空气射流冲击通道壁面的冷却方式,研究了制冷剂R134a在3种规格锯齿翅片微小通道内的冷凝传热特性,通道当量直径分别为1.13、1.18 mm和1.44 mm。工况范围为:干度0~1,质量流率:56~430 kg/(m2·s), 饱和温度:50~70 ℃,热流密度:8.4~44.2 kW/m2。实验获得了通道内局部冷凝传热系数,分析了锯齿翅片几何结构、干度、质量流率、饱和温度以及热流密度对冷凝传热的影响。结果表明:干度和质量流率的增加导致流体湍流度上升、冷凝液膜厚度减小,冷凝传热增强。饱和温度提高伴随着制冷剂液相导热系数、液汽密度比和黏度比降低,增加液膜热阻的同时减小了汽液界面的剪切力,减弱了冷凝传热。提高热流密度可引起传热系数的提高,但随着干度降低,液膜厚度增加,热流密度的作用逐渐减小并趋于消失。对于翅片高度相同的锯齿通道,减小翅片截距可以增大冷凝传热系数。对比截距相同的锯齿通道,翅片高度变化对冷凝传热系数的影响不明显。基于实验数据,提出了适用于不同锯齿翅片微小通道的冷凝传热系数的计算关联式。

     

  • 图 1  实验系统示意图

    Figure 1.  Schematic diagram of the experiment system

    图 2  标定实验系统实物图

    Figure 2.  Real picture of the calibration experimental system

    图 3  射流装置传热系数的标定实验结果

    Figure 3.  Calibration experimental results of heat transfer coefficient of jet device

    图 4  实验件照片(单位:mm)

    Figure 4.  Photograph of experimental section (unit:mm)

    图 5  热平衡分析

    Figure 5.  Analysis of energy balance

    图 6  质量流率对冷凝传热系数的影响

    Figure 6.  Effect of mass flux on condensation heat transfer coefficient

    图 7  饱和温度对冷凝传热系数的影响

    Figure 7.  Effect of saturation temperature on condensation heat transfer coefficient

    图 8  热流密度对冷凝传热系数的影响

    Figure 8.  Effect of heat flux on condensation heat transfer coefficient

    图 9  不同锯齿通道的冷凝传热系数比较

    Figure 9.  Comparison of condensation heat transfer coefficients of different serrated channel

    图 10  新经验公式预测值与实验数据的比较

    Figure 10.  Comparison of experimental data and new correlation predicted value

    表  1  锯齿翅片几何尺寸

    Table  1.   Structure size of serrated fins mm

    编号 h s L t d
    JC1614 1.6 1.4 3 0.15 1.44
    JC1610 1.6 1.0 3 0.15 1.18
    JC1014 1.0 1.4 3 0.15 1.13
    下载: 导出CSV

    表  2  流动冷凝实验工况范围

    Table  2.   Range of working conditions for flow condensation experiment

    序号 G/(kg/(m2·s)) tsat/℃ qk/(kW/m2
    JC1614 56~270 50, 60, 70 9.7~28.6
    JC1610 110~323 50, 60, 70 8.4~28.9
    JC1014 213~430 50, 60, 70 12.1~44.2
    下载: 导出CSV

    表  3  参数的不确定度

    Table  3.   Uncertainties of parameters in present study

    参数 不确定度
    温度/℃ ±0.2
    绝对压力/kPa ±4.8
    质量流量(空气)/(kg/h) ±2.5
    质量流量(制冷剂)/(kg/h) ±0.125
    冷凝热流密度/% ±1.93~2.88
    冷凝传热系数/% ±3.18~10.94
    干度/% ±2.06~2.99
    下载: 导出CSV
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  • 收稿日期:  2023-10-20
  • 网络出版日期:  2025-11-07

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