期刊文献+

热负荷分布对双蒸发器环路热管传热性能的影响

Influence of thermal load distribution on heat transfer characteristics of dual-evaporator loop heat pipe
下载PDF
导出
摘要 针对各自带液体补偿器的双蒸发器环路热管,采用模块化建模方式,数值模拟了不同热负荷分布下蒸发器毛细芯内的温度分布,确定了最优负荷分布模式以及系统传热极限。结果表明:施加于双蒸发器上的热负荷将同时影响双芯的温度变化,最优的热负荷分布模式为等热量分布。在一定的热沉温度下,并联双蒸发器环路热管的传热性能要明显优于单蒸发器环路热管,并以此求得该模型的传热极限为130 W,远大于同尺寸单蒸发器环路热管的传热极限37 W。 The impacts of thermal load distribution on steady-state heat transfer performance of dual-evaporator loop heat pipe were investigated,including the temperature characteristics of capillary wick in dual-evaporator,optimum thermal load distribution mode,and system heat transfer limit,using the modularized simulation method.The results show that the thermal loads applied on two evaporators influence the temperature distribution in each wick. The optimum thermal load distribution is even heat load mode.Given the heat sink temperature,the heat transfer capacity of dual-evaporator loop heat pipe is demonstrably superior to that of the same size single-evaporator loop heat pipe.Based on this simulation,the heat transfer limit of dual-evaporator loop heat pipe is 130 W,which is much higher than 37 W of single-evaporator loop heat pipe.
作者 曲燕 官枭
出处 《化学工程》 CAS CSCD 北大核心 2014年第8期35-40,共6页 Chemical Engineering(China)
基金 国家自然科学基金青年基金资助项目(51206189) 中国石油大学(华东)自主创新科研计划项目(27R1204024A)
关键词 双蒸发器环路热管 热负荷分布 传热性能 毛细芯 温度分布 dual evaporator loop heat pipe thermal load distribution heat transfer characteristics capillary wick temperature distribution
  • 相关文献

参考文献11

  • 1BUGBY D,WRENN K,WOLF D,et al.Multi-evaporator hybrid loop heat pipe for small spacecraft thermal management[C]∥Aerospace Conference.Big Sky,MT:IEEE,2005:810-823.Doi:10.1109/AERO.2005.1559373.
  • 2GONCHAROV K A,GOLOVIN O A,KOLESNIKOV V.Multi-evaporator loop heat pipe[C]∥Space technology and applications international forum.America:American Institute of Physics,2000:779-784.
  • 3KU J,OTTENSTEIN L,DOUGLAS D,et al.Multievaporator miniature loop heat pipe for small spacecraft thermal control-Part1:New technologies and validation approach[C]∥48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition,Orlando,Florida:Curran Associates,Inc,2010.
  • 4KU J,OTTENSTEIN L,DOUGLAS D,et al.Multievaporator miniature loop heat pipe for small spacecraft thermal control-Part2:Validation results[C]∥48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition,Orlando,Florida:Curran Associates,Inc,2010.
  • 5KIM C J,YOO B O,PARK Y J.Experimental study of two-phase close loop thermosyphon with dual evaporator in parallel arrangement[J].Journal of Mechanical Science and Technology,2005,19(1):189-198.
  • 6VAN HELDEN P G M,DEN OUDEN M,DOS SANTOS N.Novel loop heat pipes development for ground and space applications[C]∥Proceedings of the COBEM:18th International Congress of Mechanical Engineering.Ouro Preto,MG:ABCM,2005.
  • 7NAGANO H,KU J.Capillary limit of a miniature loop heat pipe with multiple evaporators and multiple Condensers[C]∥9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference,San Francisco,California,2006.
  • 8QU Y,CHENG L,LUAN T.Manufacture and performance simulation of a visible miniature loop heat pipe[C]∥2007First International Conference on Integration and Commercialization of Micro and Nanosystems.America:American Society of Mechanical Engineers,2007:777-783.
  • 9DEMIDOV A S,YATSENKO E S.Investigation of heat and mass transfer in the evaporation zone of a heat pipe operating by the‘inverted meniscus’principle[J].Int J Heat Mass Transfer,1994,37(14):2155-2163.
  • 10FIGUS C,LE BRAY Y,BORIES S,et al.Heat and mass transfer with phase change in a porous structure partially heated:continum model and pore network simulations[J].Int J Heat Mass Transfer,1999,42(14):2557-2569.

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部