控制与系统

微小通道表面射流冲击冷却系统实验研究

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  • 上海卫星工程研究所, 上海 200240

收稿日期: 2015-08-31

  修回日期: 2015-10-13

  网络出版日期: 2016-03-30

基金资助

国家"863"高技术研究发展计划基金(No.2014AA8073034);上海市科委启明星课题基金(No.14QB1404200)资助

Experimental Study of Micro-jet Impingement Cooling Loop System with Micro/Mini-channels

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  • Shanghai Institute of Satellite Engineering, Shanghai 200240, China

Received date: 2015-08-31

  Revised date: 2015-10-13

  Online published: 2016-03-30

摘要

根据电子器件的高热流密度散热需求,设计了阵列式射流与微小通道热沉相结合的闭环回路冷却系统,并进行流动及换热性能测试.通过实验探索了系统运行工况参数如流量、背压、工质除气和入口过冷度对冷却性能的影响;比较了不同结构尺寸参数(射流孔形状、射流孔直径d、射流高度H)下热沉换热及流动性能的差异.实验数据与现有文献中经验关系式的预测结果相符.

本文引用格式

朱丽瑶, 董丽宁, 王江, 徐涛, 曹建光 . 微小通道表面射流冲击冷却系统实验研究[J]. 应用科学学报, 2016 , 34(2) : 227 -236 . DOI: 10.3969/j.issn.0255-8297.2016.02.012

Abstract

A liquid cooling loop system with micro-jet arrays and micro/mini-channels was designed for high-heat-flux cooling applications. Flow boiling experiments under different operation conditions were conducted to study flow and heat transfer performance of the heat sink. The effects of micro-jet geometry such as shape, diameter and height of jet hole are analyzed. Good agreement between the experimental data and the predictions has been found.

参考文献

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