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    航天用电路板散热特性及优化设计

    Thermal Characteristics and Optimization Design of Circuit Board for Aerospace Application

    • 摘要: 文中建立某卫星用电路板传热模型,对其在初步热设计下工作时的温度场进行研究,并针对印制电路板上大功率过热元器件的散热问题开展优化设计。借助ANSYS软件模拟该电路板工作时的温度场。依据热阻理论,采用被动热控优化设计方案,通过焊接导热铜条直接连接箱体来实现导热,降低元器件温度。分析优化前后大功率器件的温度变化,发现设置导热铜条能有效降低元器件温度。研究结果表明:在卫星用电路板设计中,通过ANSYS模拟结合热阻理论进行被动热控优化,采用导热铜条连接箱体的方式,在解决大功率过热元器件的散热问题方面具有显著效果,为卫星电路板的热设计提供了有效参考。后续可进一步研究不同工况及元器件布局下该方法的适用性与优化空间。

       

      Abstract: To establish a heat transfer model for a certain satellite circuit board, the temperature field during preliminary thermal design is studied, and the optimization design for heat dissipation problem of high-power overheated components on the printed circuit board is carried out. ANSYS software is used to simulate the temperature field of the circuit board during operation. Based on the theory of thermal resistance, a passive thermal control optimization design scheme is adopted, which uses welded thermal conductive copper bars to directly connect the box to achieve thermal conductivity and reduce component temperature. By analyzing the temperature changes of high-power devices before and after optimization, it is found that setting up thermal conductive copper bars can effectively reduce the temperature of the components. The research result shows that in the design of satellite circuit boards, passive thermal control optimization is carried out through ANSYS simulation combined with thermal resistance theory. The method of connecting the box with thermal conductive copper bar has significant effects on solving the heat dissipation problem of high-power overheated components, providing effective reference for the thermal design of satellite circuit boards. Further research can be conducted on the applicability and optimization space of this method under different working conditions and component layouts.

       

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