机载电子设备BGA封装热设计
Thermal Design of BGA Package for Avionics
-
摘要: 由于表贴器件制造公差的影响,器件与冷板间的接触热阻无法有效控制。器件上方直接安装散热冷板的方法不能满足大热耗BGA封装器件的散热要求。介绍一种"活塞"式导热组件,充分考虑了上述因素,有效控制了器件与冷板间热阻。经过理论计算和实验验证,能够满足较大热耗器件在密封机载电子设备内的散热要求。Abstract: Because of the influences of such factors as machining tolerance etc., the contact thermal resistance between chip and cold plate can't be controlled effectively. The method of installing a cold plate on the chip surface can't meet the cooling requirements to high power BGA chip. In this paper, a so called "PISTON" thermal conduction module which fully considers these factors is introduced. By thermal performance calculation and test, it is shown that this structure can meet the chip's cooling requirements to sealed avionics.
-
Keywords:
- contact thermal resistance /
- BGA /
- "PISTON" thermal conduction module /
- avionics
-
-
[1] Randy Banton,Don blanchet utilizing advanced thermal management for the optimization of system compute and bandwidth density,Mercury Computer Systems,Inc,2004.
[2] 田沣.任康.焦超锋.南雁 一种高密度电子模块的热设计 [J].-航空计算技术2004(1) [3] 朱金彪 一种星载表贴芯片的散热结构设计与优化 [J].-现代电子技术2008(22) [4] ,GJB2882-1997.机载电子设备通风冷却系统通用规范,1997. [5] Simons R E,Consultant poughkeepsie,new york.the evolution of IBM high performance cooling technology,.
[6] Gregory S H,David L E,Steven P Y,The thermal management of IBM′s ES/9000 advanced thermal conduction module,1992.
[7] 孟庆中.杨伯原 修正的T-J模型分析高速航空润滑脂7018的拖动特性 [J].-润滑与密封2006(3)
计量
- 文章访问数: 89
- HTML全文浏览量: 0
- PDF下载量: 0