共查询到18条相似文献,搜索用时 109 毫秒
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本文建立了小型平板CPL蒸发器毛细多孔芯内汽液两相流动与传热的模型以及金属外壁和工质区的导热模型,并进行耦合求解.分析了金属侧壁效应对蒸发器性能的影响,提出小型平板CPL存在着侧壁效应传热极限.数值结果表明,工质蒸发发生在多孔芯加热表面附近,蒸发器采用单一金属外壁时由于侧壁效应导致系统传热极限低,而上壁采用导热系数大,侧壁及下壁采用导热系数小的新型结构能够明显的提高系统的传热能力,同时使加热表面的温度维持在较低的水平. 相似文献
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分析了小型平板CPL蒸发器毛细多孔芯上下表面温差对启动的影响,建立了蒸发器满液启动的数学模型.结果表明,对不同的金属外壁,多孔芯上下表面平均温差存在一个最大值,铜壁时,温差较小,侧壁效应明显;采用不锈钢壁及上壁铜、侧壁下壁不锈钢时,温差大,侧壁效应小;采用不锈钢外壁时蒸发器加热面的温度过高.上壁采用导热系数大、侧壁下壁为导热系数小的金属对小型平板CPL蒸发器的正常启动以及降低加热表面温度非常有利. 相似文献
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基于质量守恒、能量守恒方程,耦合环路热管各关键节点处压力、温度及传热传质关系,通过计算冷凝器中汽液界面位置,将环路热管内压力损失分为蒸汽侧压损和液相侧压损,并构建了从局部到整体的稳态运行数学物理模型,重点分析了冷凝界面位置和蒸发器热泄漏对环路热管稳态运行的影响规律。发现,低热流密度下,冷凝界面越靠近蒸汽出口越有利于提高环路热管的传热性能,但随着热流密度增加,冷凝位置对环路热管稳态性能的影响程度越来越小;抑制热泄漏或增加流入补偿室内的冷量,均可增大毛细芯两侧温度梯度,降低运行温度,进而提高环路热管的传热性能。 相似文献
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圆偏振荧光光谱(Circularly Polarized Luminescence,CPL)是一种手性化合物表征与分析的光谱手段,然而,直接CPL检测只适用于具有特征发色团的手性化合物,这极大限制了CPL的应用范围。本文报道了一种利用非手性荧光探针分子间接检测分子手性的CPL方法。以手性氨基醇的检测为例,研究发现:非手性铕化合物Eu(fod)3探针分子可与手性氨基醇相互作用,并使得Eu(fod)3产生诱导CPL(Induced circularly polarized luminescence,ICPL)信号,该ICPL信号不仅具有较高的不对称因子glum,而且其正负性与待测手性氨基醇的手性构型表现出极大的相关性。同时,研究发现ICPL光谱的glum值对不同结构的手性氨基醇表现出不同的变化趋势。以上结果表明以非手性铕化合物Eu(fod)3为探针分子的间接CPL检测方法是手性氨基醇类分子手性构型检测的有效手段。 相似文献
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The design and test results for a capillary pumped loop (CPL) for thermal management of up to 210 W at the source and heat transfer over a distance of 1 m are discussed. The design configuration of the CPL evaporator consists of an internally grooved aluminum evaporator, 31.70-mm outer diameter and 500-mm long, fitted with a porous ultra-high molecular weight polyethylene wick, 8- to 15-μm pore radius, and 38% porous volume. Heat was transferred using a stainless steel tube of 4.5-mm internal diameter for vapor and liquid lines. High-grade acetone (99.99% pure) was used as the heat transfer fluid inside the loop. In the tests, thermal characteristics of the CPL were specifically studied with respect to the temperature control capability using an active thermal device on the reservoir and to the start-up process through pressure priming of the capillary evaporator. The loop was able to start-up successfully at both low and high heat loads, although proper priming of the wick structure before start-up was necessary to attain low evaporator temperatures during steady-state operation. While maintaining constant reservoir temperature through active means, the loop was able to control evaporator temperature within 55 ± 3°C, even with changing input heat from 30 to 210 W. Total thermal resistance from the evaporator surface to the surroundings was 0.19° to 1.15° C/W with the minimum value achieved at the maximum heat load of 210 W. This study is intended to illustrate the thermal potential of the CPL as an effective temperature control device in automotive applications. 相似文献
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CPL技术在空间飞行器上的应用 总被引:16,自引:0,他引:16
本文对CPL技术进行了简要概述,介绍了其工作原理与工作特性,并讨论了CPL技术在空间飞行器上的可能应用方式。其中,对CPL技术应用于空间设备的散热进行了全面阐述,并给予理论分析;此外,对CPL技术应用于空间设备的主动热控制,也作了简要介绍;对CPL技术未来有发展前景的应用方式进行了展望。 相似文献
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Summary Capillary Pumped Loop (CPL) is a thermal management device for advanced spacecrafts. This paper presents the operating principles
of a CPL and the design characteristics of the components. Another purpose of this experiment was to build up a transparent
loop in order to better determine and observe the internal thermofluid dynamics. The results indicated that the CPL could
be in normal operation under various heat modes. Observation also told Non-Condensed Gas (NCG) was moving and collecting to
somewhere between the condenser section.
Paper presented at the I International Conference on Scaling Concepts and Complex Fluids, Copanello, Italy, July 4–8, 1994. 相似文献
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