Investigation on thermal behaviours of a methane charged cryogenic loop heat pipe

被引:25
|
作者
Guo, Yuandong [1 ,2 ,3 ]
Lin, Guiping [1 ]
Zhang, Hongxing [3 ]
Miao, Jianyin [3 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Lab Fundamental Sci Ergon & Environm Control, Beijing 100191, Peoples R China
[2] Beihang Univ, Shenyuan Honors Sch, Beijing 100191, Peoples R China
[3] China Acad Space Technol, Beijing Inst Spacecraft Syst Engn, Beijing Key Lab Space Thermal Control Technol, Beijing 100094, Peoples R China
基金
中国国家自然科学基金; 美国国家科学基金会;
关键词
Methane; Loop heat pipe; Cryogenic; Supercritical startup; Temperature hysteresis; WORKING FLUID INVENTORY; OPERATION; PERFORMANCE; SYSTEMS; DESIGN;
D O I
10.1016/j.energy.2018.05.133
中图分类号
O414.1 [热力学];
学科分类号
摘要
As a highly efficient cryogenic heat transfer device, cryogenic loop heat pipe (CLHP) promises great application potential in the thermal control of future space infrared detection system. In this work, a CLHP using methane as working fluid operating at 100-190 K was developed, and its thermal performance including the supercritical startup, heat transport capacity under different heat sink, power cycling characteristics, temperature hysteresis phenomenon and thermal resistance variation, was experimentally investigated. Experimental results showed that the CLHP could successfully realize the supercritical startup under various auxiliary heat loads applied to secondary evaporator, reach a various heat transfer capacity under different heat sink temperature over a 0.6 m distance, and manifest good response characteristics to the cycle of heat load applied to the primary evaporator. The temperature hysteresis phenomenon was detected and thermal resistance of the CLHP varied with increasing heat load applied to the primary evaporator, but not the same with that in heat load reverse motion. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:516 / 525
页数:10
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