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System Integration of a Thermal Storage Device for High-Power-Density Systems

机译:用于高功率密度系统的热存储装置的系统集成

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High power levels and high power densities associated with directed energy weapon systems, electronic warfare systems, and high thrust-to-weight aircraft propulsion systems require the development of effective and efficient thermal management solutions. As the objective for many high-power electronic systems is integration onto mobile platforms, strict requirements are also placed on the size, weight, and power draw of the corresponding thermal management system. High peak waste heat loads cannot be efficiently rejected to ambient air in a package integrated onto a mobile platform, leading to the need to store large amounts of energy in a compact, lightweight package. Thermal storage devices must not only be able to store energy rapidly at high power levels but they must also reject energy efficiently, allowing the thermal storage device to recharge for multiple uses. This paper will discuss the design of an advanced phase-change thermal storage device and present the effects of the storage device on system performance. Results of theoretical and experimental performance evaluations will also be presented. For this study, a model was developed and experimentally validated for determining heat rejection based on phase change material temperature and fluid temperature. For comparison, the heat rejection and thermal storage capabilities of a system using a 50%/50% by volume mixture of propylene glycol and water was established. The comparison shows how integrating the phase-change thermal storage device into a single-phase loop impacts the size, weight, and power draw of a system on a mobile platform. The thermal storage systems discussed in this paper are applicable to many different thermal management architectures, are easily adapted to meet the requirements of a wide range of high-power systems, and have potential to significantly reduce thermal management size, weight, and power requirements.
机译:与定向能量武器系统,电子战系统和高推力 - 重量飞机推进系统相关的高功率水平和高功率密度需要开发有效和高效的热管理解决方案。由于许多高功率电子系统的目标是在移动平台上集成,因此也放置了相应的热管理系统的尺寸,重量和功率绘制的严格要求。在集成在移动平台上的封装中,不能有效地拒绝高峰浪费热载荷,这导致需要将大量能量存储在紧凑,轻质的包装中。热存储设备不仅必须能够在高功率水平迅速存储能量,但它们还必须有效地拒绝能量,允许热存储设备为多种用途进行充电。本文将讨论高级相变热存储设备的设计,并呈现存储设备对系统性能的影响。还将提出理论和实验性能评估的结果。对于本研究,开发和实验验证了一种基于相变材料温度和流体温度来确定热抑制的模型。为了比较,建立了使用50%/ 50%的丙二醇和水的体积混合物的系统的热排出和热储存能力。比较示出了将相变热存储装置集成到单相环路中的集成如何影响移动平台上系统的大小,重量和功率绘制。本文讨论的热存储系统适用于许多不同的热管理架构,易于适应满足各种大功率系统的要求,并具有显着降低热管理尺寸,重量和功率要求的潜力。

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