Micro Evaporators

C. Rops, F. V. Graaf, J. Velthuis
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引用次数: 2

Abstract

The use of micro evaporation for cooling electronic components on small satellites is very promising because of its great potential on heat transferring capacity and its low mass flow. Due to the size reduction, the energy density increases in a lot of applications in space industry. On top of this, the thermal specifications on micro devices are often more tight than in macroscopic applications. Therefore, a proper design is essential for devices to be capable of dealing with associated high heat fluxes. Using evaporation high heat fluxes can be obtained. However, a good understanding of the heat transfer and evaporation on micro scales is necessary since some physical phenomena become more (or less) important. The PhD research performed at TNO TPD (in collaboration with the Delft university of technology) leads to insight on the behaviour of two phase liquid- gas flow in micro channels. The knowledge on both the heat transfer and the two phase flow patterns can be used to formulate relationships which can be used to design micro fluidic systems. Since gravity plays a minor role on micro scales these engineering tools will be appropriate for designing space systems as well.
微型蒸发器
利用微蒸发技术对小型卫星上的电子元件进行冷却,具有传热潜力大、质量流小等优点,具有广阔的应用前景。由于尺寸减小,在航天工业的许多应用中,能量密度增加。最重要的是,微设备的热规格通常比宏观应用更严格。因此,适当的设计对于能够处理相关的高热通量的设备是必不可少的。采用蒸发法可获得较高的热流密度。然而,由于一些物理现象变得更重要(或更不重要),在微观尺度上对传热和蒸发有一个很好的理解是必要的。在TNO TPD(与代尔夫特理工大学合作)进行的博士研究导致了对微通道中两相液气流动行为的深入了解。关于传热和两相流型的知识可以用来建立可用于设计微流体系统的关系。由于重力在微观尺度上的作用很小,这些工程工具也将适用于空间系统的设计。
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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