首页> 外文期刊>International Journal of Heat and Mass Transfer >Experimental investigation on thermal characteristics of a capillary pumped loop with different reservoir locations
【24h】

Experimental investigation on thermal characteristics of a capillary pumped loop with different reservoir locations

机译:不同水库位置毛细管泵送环热特性的实验研究

获取原文
获取原文并翻译 | 示例
       

摘要

This paper presents an effect of reservoir location on heat transfer characteristics of a capillary pumped loop (CPL). The designed CPL has a cylindrical evaporator with a diameter of 12 mm and a length of 65 mm. A stainless steel porous medium that has a pore radius of 4.4 nm is used as a wick. Heat transport length is designed as 1000 mm. The experiments were conducted with four types of reservoir location such as (1) Distance from the evaporator, L = 150 mm, (2) L = 250 mm, (3) L = 750 mm, (4) L = 1450 mm. As results, it was found that the CPL of case (1) showed high operating temperature and much smaller heat transfer capability such as 10 W. For cases of (2) - (4), the maximum heat transfer capability reached 140 - 160 W and showed the good controllability of the operating temperatures ranging from 60 to 100°C. The reason for the low heat transfer performance of case (1) and the difference in operational characteristics are discussed. It was found that there is a design limitation of the reservoir location of CPLs. In addition, the operation of the CPL that reservoir was located much far from the evaporator was successfully demonstrated.
机译:本文介绍了储层位置对毛细管泵送环(CPL)的传热特性的影响。设计的CPL具有圆柱形蒸发器,直径为12mm,长度为65mm。使用孔半径为4.4nm的不锈钢多孔介质用作芯。热传输长度设计为1000毫米。用四种类型的储存器位置进行实验,例如(1)距蒸发器的距离,L = 150mm,(2)L = 250mm,(3)L = 750mm,(4)L = 1450mm。结果,发现案例(1)的CPL显示出高的工作温度和更小的传热能力,例如10W。对于(2) - (4)的情况,最大传热能力达到140-160W并且显示了操作温度范围为60至100°C的良好可控性。讨论了案例(1)的低传热性能的原因和操作特征的差异。发现CPLS的储层位置存在设计限制。另外,成功地证明了储液器的CPL的操作从蒸发器远离蒸发器。

著录项

  • 来源
    《International Journal of Heat and Mass Transfer》 |2020年第9期|119964.1-119964.9|共9页
  • 作者单位

    Institute of Space and Astronautical Science Japan Aerospace Exploration Agency 3-1-1 Yoshinodai Chuo Sagamihara 252-5210 Kanagawa Japan;

    Department of Mechanical System Engineering Nagoya University Fun Chikusa Nagoya 464-8603 Japan;

    Institute of Space and Astronautical Science Japan Aerospace Exploration Agency 3-1-1 Yoshinodai Chuo Sagamihara 252-5210 Kanagawa Japan;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Capillary pumped loop; Reservoir location; Thermo-fluid behavior;

    机译:毛细管泵送环;水库位置;热流体行为;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号