Temperature-Controllable Oscillating Heat Pipe

被引:19
作者
Iwata, Naoko [1 ]
Ogawa, Hiroyuki [1 ]
Miyazaki, Yoshiro [2 ]
机构
[1] Japan Aerosp Explorat Agcy, Thermal Syst Grp, Inst Space & Astronaut Sci, Kanagawa 2525210, Japan
[2] Fukui Univ Technol, Dept Elect Elect & Comp Engn, Fukui 9108505, Japan
关键词
PART; PERFORMANCE;
D O I
10.2514/1.51128
中图分类号
O414.1 [热力学];
学科分类号
摘要
Experiments are conducted to investigate whether an oscillating heat pipe with a liquid reservoir can serve as a thermal control device in space. The oscillating heat pipe consists of a stainless steel capillary tube (inner and outer diameters of 0.8 mm and 1 mm, respectively), which meanders between a heating section and a cooling section 15 times in each direction (30 times in total). A 50 mL reservoir is connected to the oscillating heat pipe via another capillary tube. The 1,1,1,2-tetrafluoroethane (HFC-134a) is used as the working fluid. The heat input to the heating section is increased from 0 and 70 W, in 10 W increments. When the oscillating heat pipe is set horizontally, the temperature of the heating section remains at about the reservoir temperature of 40 degrees C for three orientations of the reservoir with respect to gravity: vertical, horizontal, and vertically inverted. In the top-heating mode, the temperature of the heating section also remains at about the reservoir temperature. The oscillating heat pipe with a liquid reservoir is confirmed to operate as a variable conductance heat pipe, and its operating temperature can be controlled to almost be the liquid reservoir temperature for each investigated orientation of the reservoir. The oscillating heat pipe with a liquid reservoir is confirmed not to lose its temperature control function in gravity; thus, the operating temperature can be controlled by regulating the liquid reservoir temperature, not only on the ground but also in space.
引用
收藏
页码:386 / 392
页数:7
相关论文
共 20 条
[1]  
Akachi H, 1990, Patent No. [4,921,041, 4921041]
[2]  
Akachi H., 1996, PROC 5 INT HEAT PIPE, P208
[3]  
Akachi H, 1993, Patent No. [5. 219. 020, 5219020]
[4]  
BSIBSI M, 2006, 36 INT C ENV SYST NO
[5]   Closed loop pulsating heat pipes - Part A: parametric experimental investigations [J].
Charoensawan, P ;
Khandekar, S ;
Groll, M ;
Terdtoon, P .
APPLIED THERMAL ENGINEERING, 2003, 23 (16) :2009-2020
[6]   Performance Characteristics of a Concentric Annular Heat Pipe: Part I-Experimental Prediction and Analysis of the Capillary Limit [J].
Faghri, A. ;
Thomas, S. .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 1989, 111 (1-4) :844-850
[7]   Effects of gravity on the performance of pulsating heat pipes [J].
Gu, JJ ;
Kawaji, M ;
Futamata, R .
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2004, 18 (03) :370-378
[8]  
Hosoda M, 1999, JSME INT J B-FLUID T, V42, P737
[9]   Thermal operational characteristics of a small-loop heat pipe [J].
Kaya, T ;
Ku, JT .
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2003, 17 (04) :464-470
[10]   Closed loop pulsating heat pipes - Part B: visualization and semi-empirical modeling [J].
Khandekar, S ;
Charoensawan, P ;
Groll, M ;
Terdtoon, P .
APPLIED THERMAL ENGINEERING, 2003, 23 (16) :2021-2033