Thermal-hydraulic performance of ammonia in manifold microchannel heat sink

被引:11
作者
Tang, Kai [1 ]
Huang, Yanpei [1 ,2 ]
Lin, Guiping [1 ,3 ]
Guo, Yuandong [1 ,3 ]
Huang, Jinyin [2 ]
Lin, Haimiao [2 ]
Zhang, Hongxing [2 ]
Yang, Qi [2 ]
Miao, Jianyin [2 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Lab Fundamental Sci Ergon & Environm Control, Beijing 100191, Peoples R China
[2] China Acad Space Technol, Beijing Inst Spacecraft Syst Engn, Beijing Key Lab Space Thermal Control Technol, Beijing 100094, Peoples R China
[3] Beihang Univ, Ningbo Inst Technol, Aircraft & Prop Lab, Ningbo 315100, Peoples R China
基金
中国国家自然科学基金;
关键词
Manifold microchannel; Thermal resistance; Pressure drop; Flow boiling; Ammonia; JET IMPINGEMENT; SMOOTH; OPTIMIZATION; ARRAY; CO2;
D O I
10.1016/j.applthermaleng.2023.121000
中图分类号
O414.1 [热力学];
学科分类号
摘要
With the increasing miniaturisation of electronic devices, the demand for cooling technologies with high efficiency has increased. Therefore, in this study, a manifold microchannel heat sink was designed and fabricated to enhance the dissipating capability of high-heat-flux hotspots. Owing to its excellent thermophysical properties, ammonia was selected as the working fluid, and its thermal-hydraulic characteristics were evaluated. In addition, the effects of flow rate, heat flux, saturation temperature, and inlet conditions were investigated through experiments. High-subcooled inlet experiments revealed that the thermal resistance decreased and pressure drop increased with increasing flow rate. Moreover, localised subcooled boiling was observed near the heated region. In near-saturated inlet experiments, jet impingement and microchannel cooling were identified as the dominant heat transfer mechanisms over different flow ranges. Notably, the higher heat flux, lower saturation temperature, and two-phase inlet condition reduced the thermal resistance under the operating conditions of the study. The proposed heat sink dissipated the heat flux (up to 1542 W/cm2) from the heat source (1 mm x 6 mm) with a pressure drop of 10.6 kPa, and the corresponding heating surface temperature and thermal resistance were 68.05 celcius and 0.450 K/W, respectively.
引用
收藏
页数:10
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