期刊文献+

一种高性能柔性导热带设计 被引量:7

Design of High-performance Flexible Thermal Strap
下载PDF
导出
摘要 为了实现大功率活动焦面组件与散热器的高效热耦合及焦面组件与散热器的结构解耦,设计一种由主体段柔性带和刚性端子组成的高性能柔性导热带。主体段柔性导热带通过创新的回型双向传热路径方法完成高导热性及低刚度设计。刚性端子采用轻量化设计,使其具有轻质量及高效接触传热性能。柔性导热带能实现轻质量、高导热性、低刚度和良好的隔振效果。对柔性导热带的导热、隔振和刚度等性能进行测试,并将其应用到卫星的焦面电箱组件。结果表明:柔性导热带的质量较小(300 g),导热性能为0.53 W/℃,刚度小于15 N/m,可满足活动焦面组件散热设计的高导热、低刚度等性能要求。 In order to achieve high-efficiency thermal coupling of the high-power active focal plane components and structural decoupling of the focal plane components,a kind of high-performance flexible thermal strap is designed,which is composed of a main section flexible thermal strap and rigid terminals.The main section flexible thermal strap is designed with high thermal conductivity and low stiffness through the innovative two-way heat transfer path method.The rigid terminals adopt lightweight design,which makes it have light mass and efficient contact heat transfer.The flexible thermal strap can achieve light mass,high thermal conductivity performance,low stiffness and good vibration isolation effect.The thermal conductivity,vibration and stiffness of the flexible thermal strap are tested,and the flexible thermal strap is also applied in the focal plane component of satellite electricity box.The results show that the flexible thermal strap has a light mass of 300g,thermal conductivity performance of 0.53W/℃,and stiffness of less than 15N/m which can basically meet the requirements of high thermal conductivity and low stiffness of active focal plane component.
作者 姜峰 孔林 柏添 李强 JIANG Feng;KONG Lin;BAI Tian;LI Qiang(Chang Guang Satellite Technology Co.,Ltd.,Changchun 130000,China)
出处 《航天器工程》 CSCD 北大核心 2019年第5期89-95,共7页 Spacecraft Engineering
关键词 柔性导热带 活动焦面组件 主体段柔性导热带 刚性端子 导热性能 flexible thermal strap active focal plane component main section flexible thermal strap rigid terminal thermal conductivity performance
  • 相关文献

参考文献3

二级参考文献28

  • 1刘佳,李运泽,张加迅,王佩广,王浚.基于智能Agent的航天器MEMS自主热控系统研究[J].航天器环境工程,2009,26(6):574-579. 被引量:6
  • 2李运泽,魏传锋,袁领双,王浚.应用PTC电加热器的卫星局部温度控制系统仿真[J].系统仿真学报,2005,17(6):1494-1496. 被引量:10
  • 3Tomiyoshi Haryana. Present technology for reduction of vibration in cyocooler [ C ]. Prof. of 28th International Comic Ray Conference,2003.
  • 4Montesano M J. High performance flexible thermal strap [ C]. Proc. of AIAA, 2001.
  • 5Ruth McElroy. Thermal design and analysis for the cryo- genic MIDAS experiment[R]. NASA Report,1998.
  • 6闫涛,洪国同.一种应用于低温系统的冷量传输带[c].北京:第八届全国低温工程大会,2007.
  • 7Rao Singers S. Mechanical vibration [ M ]. US, NJ : Pear- son Prentice Hall,2004.
  • 8周良兴.基于MEMS的微介电液滴冲击冷却系统建模及其实施技术研究[D]浙江大学,浙江大学2008.
  • 9K. Shimazaki,A. Ohnishi,Y. Nagasaka.Development of Spectral Selective Multilayer Film for a Variable Emittance Device and Its Radiation Properties Measurements[J]. International Journal of Thermophysics . 2003 (3)
  • 10Eric S,Kurt L,Mike P,et al.Wax-actuated heat switchfor Mars surface applications. . 2002

共引文献47

同被引文献59

引证文献7

二级引证文献6

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