Thermal Design and Thermal Analysis of Space Observation Equipment

徐. X. Zhen
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Abstract

On the research of observation equipment,the method of heat conduction was chosen aiming at high-power electronic components based on the working environment and structure characteristics.The thermal design was finished on the research of heat conduction theory for the high-power electronic components.After the finite element model was built,the relations between the thickness and contact area of heat sink and the steady temperature of high-power electronic components were analyzed,and the design of heat sink was optimized.The experimental results showed that the equipment worked well in range of-30~50 ℃ environment,and the steady temperature was less than 85 ℃.Therefore,the equipment of thermal design can satisfy the temperature requirements in the space environment.
空间观测设备热设计与热分析
在观测设备的研究中,根据大功率电子器件的工作环境和结构特点,选择了热传导方法。在研究了热传导理论的基础上,完成了大功率电子元件的热设计。在建立有限元模型后,分析了大功率电子元件散热片厚度、接触面积与稳定温度的关系,并对散热片的设计进行了优化。实验结果表明,该装置在-30~50℃范围内工作良好,稳定温度小于85℃。因此,热设计的设备能够满足空间环境下的温度要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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