The increasing demands on aircraft electronic equipment dissipation systems requires heat-pipes more suitable for the aircraft environment to cool electronic parts effectively and to maintain proper operating temperatures for electronic equipment.Dual compensation chamber loop heat pipe is shown to be the most suitable for airborne electronic equipment after analysis of four main types of heat-pipes and taking both the acceleration and changes in incline of aircrafts into consideration.Likewise, flat heat-pipe with rectangular micro-grooves is another type of heat-pipe with potential.
ZHAO Guo-chang, LU Tian-dong, SONG Li-ping, CAO Lei
. Analysis on the application of heat-pipe in cooling airborne electronic equipment[J]. Journal of Shenyang Aerospace University, 2013
, 30(5)
: 1
-4
.
DOI: 10.3969/j.issn.2095-1248.2013.05.001
[1]赵晓军, 余莉.热管的电子设备冷却技术[J].世界科技研究与发展, 2007, 29(6):19-23.
[2]张娅妮, 陈菲儿, 田沣.机载电子设备冷却散热技术的发展[J].航空计算技术, 2012, 42(4):113-114.
[3]张孟瑞.歼击机机载电子设备用热管散热时重力与惯性力影响其性能的探讨[J].航空电子技术, 1984(2):1-2, 6.
[4]曲燕, 栾涛, 程林.放置倾角对轴向槽道热管传热特性影响的实验研究[J].宇航学报, 2006, 27(3):493-497.
[5]明章鹏, 董素君, 王浚.机载热管的可行性研究和优化设计[J].航空动力学报, 2011, 26(4):848-849.
[6]张春林, 潘仁良, 张孟瑞.平板热管承受重力和惯性力时的性能[J].航空电子技术, 1992(2):31-38.
[7]王晨, 刘中良, 张广孟, 等.倾斜角度对平板热管性能影响的实验研究[J].工程热物理学报, 2012, 33(8):1400-1402.
[8]郭舜, 米珉, 曹剑锋, 等.环路热管的应用[C].第五届空间热物理会议论文集, 北京:航天器工程, 2000.
[9]凤健婷, 林贵平, 柏立战.双储液器环路热管稳态运行特性的实验研究[J].航空学报, 2010, 31(8):1558-1564.
[10]张红星, 苗建印, 邵兴国.双储液器环路热管的设计与实验研究[J].中国空间科学技术, 2009(5):8-14, 41.
[11] Donald Gluck, Charlotte Gerhart, Scott Stanley.Characterization of a high capacity, dual compensation chamber loop heat pipe[C].Space Technology and Application International Forum-1999, American Institute of Physics, Albuquerque, 1999:943- 948.
[12]李燕, 贾力.脉动热管传热性能实验研究[J].中国电机工程学报, 2009, 29(11):75-80.
[13]杨洪海, Khandekar Sameer, Groll Manfred.脉动热管技术的研究现状及前沿热点[J].东华大学学报(自然科学版), 2006, 32(3):134-138.
[14]林梓荣, 汪双凤, 吴小辉.脉动热管技术研究进展[J].化工进展, 2008, 27(10):1526-1528.
