宽带隙功率模块直接与间接冷却的对比分析及基于射流冲击的基板直接冷却的性能提升

Himel Barua, E. Gurpinar, Lingxiao Xue, B. Ozpineci
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引用次数: 0

摘要

随着大功率、大扭矩电机的发展,对大功率密度电子器件的要求越来越高。这种系统的热管理需要高的热量提取。传统的基于风冷的散热器和基于冷板的液体冷却在各种应用中都有自己的优点,但在高功率密度应用中有局限性。目前的研究探索了一种基于射流冲击的直接衬底冷却系统,该系统适用于基于SiC的直接键合Cu衬底,用于各种功率损耗。射流冲击冷却与传统水平/间接冷却(针鳍散热器和遗传算法优化散热器)的数值比较表明,两种水平冷却设计的传热系数面积加权平均值都较高,射流冲击冷却设计的局部传热系数较高。设计迭代是为了解决这个冷却系统的瓶颈。增加喷嘴的数量有助于在直接结合的铜底板上覆盖更多的面积,从而大大降低了芯片的温度。在流量一定的情况下,增加喷嘴数量会降低局部射流速度,从而减少射流冲击抽热。这个问题可以通过减小喷嘴直径来解决,但这样做会导致高压降,而设计约束是2 psi。提出了一种喇叭形喷嘴的设计方案,该方案增大了射流的扩散角,增加了气流覆盖范围,减小了冷却剂回路的压降。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Comparative Analysis of Direct and Indirect Cooling of Wide-Bandgap Power Modules and Performance Enhancement of Jet Impingement-Based Direct Substrate Cooling
With the development of high-power and high-torque machines, requirements for high-power density electronics are increasing. Thermal management of such systems requires high heat extraction. Conventional air cooling based heat sinks and cold plate based liquid cooling have their own benefits for various applications but has limitations for high power density applications. The current study explores a jet impingement based direct substrate cooling system that was implemented for a SiC based direct bonded Cu substrate for various power losses. Numerical comparison between jet impingement cooling and conventional horizontal/indirect cooling (pin fin heat sink and genetic algorithm-optimized heat sink) showed that the area weighted average of the heat transfer coefficient (HTC) is high for both horizontal cooling designs, and the local HTC is higher for jet impingement. Design iterations were undertaken to resolve the bottleneck of this cooling system. Increasing the number of nozzles helped to cover more area at the direct bonded Cu bottom plate, which drops the chip temperature considerably. With a constant flow rate, increasing the number of nozzles would decrease local jet velocity, which reduces the heat extraction by jet impingement. This issue can be addressed by reducing the diameter of nozzle but doing so results in a high pressure drop where the design constraint is 2 psi. A flared nozzle design is proposed, which has a higher spreading angle of the jet that increases the flow coverage and reduces the pressure drop of the coolant loop.
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