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Sorption cooling: a valid extension to passive cooling

机译:吸附冷却:被动冷却的有效扩展

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Passive cooling has shown to be a very dependable cryogenic cooling method for space missions. Several missions employ passive radiators to cool down their delicate sensor systems for many years, without consuming power, without exporting vibrations or producing electromagnetic interference. So for a number of applications, passive cooling is a good choice. At lower temperatures, the passive coolers run into limitations that prohibit accommodation on a spacecraft. The approach to this issue has been to find a technology able to supplement passive cooling for lower temperatures, which maintains as much as possible of the advantages of passive coolers. Sorption cooling employs a closed cycle Joule-Thomson expansion process to achieve the cooling effect. Sorption cells perform the compression phase in this cycle. At a low temperature and pressure, these cells adsorb the working fluid. At a higher temperature they desorb the fluid and thus produce a high-pressure flow to the restriction in the cold stage. The sorption process selected for this application is of the physical type, which is completely reversible. It does not suffer from degradation as is the case with chemical sorption of e.g. hydrogen in metal hydrides. Sorption coolers include no moving parts except for some check valves, they export neither mechanical vibrations nor electromagnetic interference, and are potentially very dependable due to their simplicity. The required cooling temperature determines the type of working fluid to be applied. Sorption coolers can be used in conjunction with passive cooling for heat rejection at different levels. This paper starts with a brief discussion on applications of passive coolers in different types of orbits and the limitations on passive cooling at low cooling temperatures. Next, the working principle of sorption cooling is summarized. The DARWIN mission is chosen as an example application of sorption and passive cooling and special attention is paid to the reduction of the radiator area needed by the sorption cooler. By examining the performance of alternative working fluids suitable for different cooling temperatures, the application field of this type of sorption cooling is currently expanded.
机译:对于太空飞行,被动冷却已被证明是一种非常可靠的低温冷却方法。许多任务使用无源辐射器冷却其精密的传感器系统多年,而无需消耗功率,不产生振动或产生电磁干扰。因此,对于许多应用而言,被动冷却是一个不错的选择。在较低的温度下,被动冷却器会遇到限制,无法容纳航天器。解决此问题的方法是找到一种能够补充较低温度的被动冷却的技术,该技术尽可能保留了被动冷却器的优点。吸附冷却采用闭环焦耳-汤姆森膨胀工艺来达到冷却效果。吸附细胞在此循环中执行压缩阶段。这些细胞在低温和低压下吸收工作流体。在较高的温度下,它们会解吸流体,因此会在冷段产生高压流到节流阀。为此应用选择的吸附过程是物理类型的,这是完全可逆的。它不会像化学吸附例如B2那样遭受降解。金属氢化物中的氢。吸附式冷却器除某些止回阀外不包括活动部件,它们既不输出机械振动也不产生电磁干扰,并且由于其简单性而可能非常可靠。所需的冷却温度决定了要施加的工作流体的类型。吸附式冷却器可以与被动式冷却一起使用,以实现不同级别的散热。本文首先简要讨论了被动式冷却器在不同类型轨道上的应用以及低冷却温度下被动式冷却的局限性。接下来,总结了吸附冷却的工作原理。选择DARWIN任务作为吸附和被动冷却的示例应用,并特别注意减小吸附冷却器所需的散热器面积。通过检查适用于不同冷却温度的替代工作流体的性能,目前正在扩大这种吸附冷却的应用领域。

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