烟气型吸收式制冷机的变工况特性研究

基于分布式冷热电联产系统变工况运行的实际需要,建立了烟气型双效溴化锂吸收式制冷机的变工况模型。制冷机变工况模拟计算时,保持浓溶液流量及换热系数(高压发生器除外)不变,得到了烟气进口温度、烟气流量及冷却水进口温度变化时的制冷机各重要性能参数曲线,发现当烟气流量低于50%时,COP下降较快,冷却水进口温度降低时有利于制冷机运行,但是要注意防止浓溶液结晶。制冷机额定工况模拟计算时,与已有文献进行对比,验证模型的可靠性。     

新型涡流管的制冷特性研究

以新型涡流管为研究主体,通过实验,研究涡流管操作参数对涡流管性能的影响。根据实验数据,分析改变温度压力等操作参数对涡流管能量分离效应的影响。试验结果表明:当提高涡流管进气温度,其冷热两端出气温度升高,但并不影响涡流管的制冷效率;增加涡流管进气压力会提高涡流管制冷效应,并在冷流率为0.2时效果最明显;制冷效率随节流阀开度增加而增加且最终趋于稳定,而制热效率则随节流阀开度增加而减小并最终趋于稳定。     

R1336mzz闪蒸喷雾冷却传热特性的实验研究

闪蒸喷雾冷却是高热流密度电子器件有效的散热技术之一.本研究采用新型工质R1336mzz,建立了一个闭式闪蒸喷雾冷却实验平台,研究了喷雾流量和入口温度等影响因素对其传热特性的影响.实验结果表明,闪蒸喷雾冷却的传热性能随流量的增加先增大后减小,在流量为1.4 L/min时,获得最佳的传热性能,临界热流密度最高可达349 W...     

三流道喷嘴涡流管能量分离特性的研究

涡流管是一种可以产生冷热分离效应的结构简单的装置,尽管其在结构和操作上非常简单,但管内发生的能量交换过程却极其复杂。以压缩空气作为涡流管的工作介质,对涡流管能量分离特性进行了实验研究,获得了涡流管制热效应、制冷效应与进气压力以及冷流率之间的关系。研究结果表明:在冷流率 μ_c<85％时,喷嘴进口压力愈高,三流道喷嘴涡流管的制冷效应愈好,制热效应也愈好;冷流率愈高,三流道喷嘴涡流管的制冷效应愈差,但三流道喷嘴涡流管的制热效应愈好。     

HEAT TRANSFER AND PRESSURE DROP MEASUREMENTS FOR IN-TUBE CONDENSATION OF CFC-113 USING MICROFIN TUBES AND WIRE INSERTS

Accurate, repeatable heat transfer and pressure-drop measurements have been made for condensation of CFC-113 with downflow inside enhanced microfin tubes and tubes containing twisted-wire inserts. In the latter case measurements have also been made for CFC-113/air mixtures. The heat transfer rate was calculated from the coolant flow rate and temperature rise, the latter measured using a 10-junction thermopile with careful attention paid to adequate coolant mixing and isothermal immersion of the thermopile leads. The surface temperature was found from thermocouples embedded in the tube wall. One plain tube, nine microfin tubes (with different fin heights, helix angles, and number of fins), and four twisted-wire inserts (with different wire densities) were tested. Enhancement ratios (i.e., vapor-side heat transfer coefficient for the enhanced tube divided by that for a smooth tube at the same vapor-side temperature difference and vapor inlet velocity) between 1.6 and 5.6 for the microfin tubes and between 1.2 and 1.6 for the twisted-wire inserts were found, with values depending on vapor-side temperature difference, vapor inlet velocity, and air inlet mole fraction in the case of CFC-113/air mixtures. The microfin tubes showed moderate pressure-drop penalties of around 50% compared to the plain tube, while the twisted-wire inserts showed increasing pressure-drop penalty with increasing wire density.     

高温超导电缆用波纹管内液氮流动特性的数值研究

随着超导技术的发展,高温超导电缆在电力输运中逐渐得到重视并进行了广泛的研究。由于波纹管具有良好的柔韧性和收缩性,在高温超导电缆中作为杜瓦放置电缆,冷却超导体用的液氮需流经波纹管。在系统设计中,需要对液氮在波纹管中的流动特性加以了解。为了研究液氮在波纹管内的流动特性,对其进行了数值计算及理论分析。分析表明:压力损失随入口速度的增大而增大;在波纹内形成了涡旋流;在所考察的雷诺数范围内,雷诺数对摩擦系数的影响不大,而波纹尺寸对摩擦系数具有主要的影响。摩擦系数随s/t的增大而减小。。     

Flow condensing heat transfer of R410A,R22, and R32 inside a micro-fin tube

An experimental study of condensation heat transfer characteristics of flow inside horizontal micro-fin tubes is carried out using R410A, R22, and R32 as the test fluids. This study especially focuses on the influence of heat transfer area upon the condensation heat transfer coefficients. The test sections were made of double tubes using the counter-flow type; the refrigerants condensation inside the test tube enabled heat to exchange with cooling water that flows from the annular side. The saturation temperature and pressure of the refrigerants were measured at the inlet and outlet of the test sections to defined state of refrigerants, and the surface temperatures of the tube were measured. A differential pressure transducer directly measured the pressure drops in the test section. The heat transfer coefficients and pressure drops were calculated using the experimental data. The condensation heat transfer coefficient was measured at the saturation temperature of 48°C with mass fluxes of 50–380 kg/(m²s) and heat fluxes of 3–12 kW/m². The values of experimental heat transfer coefficient results are compared with the predicted values from the existing correlations in the literature, and a new condensation heat transfer coefficient correlation is proposed.     

双向进气对于G-M型单级脉冲管制冷机性能影响的实验研究

根据Redebaugh相位分析理论,建立了双向进气对于G-M型脉冲管制冷机性能影响的数学模型,在此基础上提出了制冷机性能优化的若干措施。同时建立了单级G-M型脉冲管制冷机性能实验系统,通过改进小孔阀的开度,优化旋转阀的进气频率和双向进气的开度,使系统性能得到了明显的改善。     

小流量涡流管特性的实验研究

本文用实验方法研究了小流量涡流管制冷的特性。实验中分别对入口压力和工质等因素对涡流管特性的影响进 行研究。在实验中发现了涡流管冷端制热和热端制冷的反常现象,并对其进行了解释。     

微细管内超临界二氧化碳冷却换热研究

本文对超临界二氧化碳在微细管内冷却对流换热进行数值模拟研究,分析不同流动方向和管径大小对超临界二氧化碳对流换热的影响,考察管内局部流体温度、管壁温度以及无量纲温度分布的变化。湍流模型采用低雷诺数YS模型。研究表明,在LPV范围比较大的截面,超临界二氧化碳局部换热系数达到最大值,同时管内传热受流动方向和管径的影响均较大。     

细圆管内超临界二氧化碳对流换热的实验研究

本文对超临界压力二氧化碳在内径为1 mm的竖直细圆管中的对流换热进行了实验研究.分析了流体的热流密度、进口温度、质量流量以及流动方向对超临界压力二氧化碳对流换热的影响.实验研究发现,热流密度、进口温度、质量流量以及浮升力对细圆管内对流换热的影响很大,对流换热系数在准临界温度附近存在峰值.在加热的前半段向上流动的对流换热强于向下流动,在加热的后半段则相反.随着热流密度与质量流量比值的不断增加,向上流动与向下流动对流换热强弱转换的交点不断向流体进口方向推移,并且向上流动的壁面温度出现峰值,发生换热恶化,而向下流动则没有出现换热恶化.     

竖直圆管中超临界压力CO2对流换热实验研究

本文对超临界压力CO2在竖直加热圆管内的对流换热进行了实验研究,比较了不同流向、不同热流密度等对流动和换热的影响。实验结果表明,管内径为2mm时,在低进口Re条件下,由于浮升力影响导致层流向湍流提前转变, 对流换热增强;与向上流动相比,向下流动更易由层流转变为湍流;向下流动的换热要强于向上流动,表明浮升力对换热有很大影响。对于管内径为0．27 mm的微细圆管,当进口Re高于104时,浮升力的影响可以忽略,对流换热系数的变化完全由物性的变化尤其是cp的变化导致。     

涡流管能量分离过程实验研究

利用涡流管部分轴线温度测量实验装置,考虑到进气压力和涡流室结构对涡流管能量分离过程的影响,针对不同进气压力和不同涡流室结构的涡流管部分轴线温度分布进行了实验研究。根据实测结果,得到了进气压力及涡流室几何结构对涡流管部分轴线温度分布的影响曲线。在此基础上,根据实验结果并结合热力学原理对涡流管制冷的物理行为作了分析。结果表明:涡流导致涡流室中心区域气流膨胀是涡流管产生制冷效应的一个重要原因。     

Experimental investigation of the effect of nozzle numbers on Ranque–Hilsch vortex tube performance

The present study investigates the effects of the orifice nozzle number and the inlet pressure experimentally on the cooling performance of the counter flow-type vortex tube. The energy generation has been conducted using a stream-tek generator (model GNMD-KIT) with different numbers of nozzles (2, 3, and 6), an aspect ratio of 1:6, and an inner diameter of 7.5 mm. In the experiments, for each of the orifices, inlet pressures have been adjusted from 200–600 kPa. The energy separation investigated here focuses on the cold temperature difference and coefficient of performance for cooling. The experimental results concluded in this article prove that the greatest effect of nozzle number is for three nozzles, and hence, that nozzle number could affect the energy separation efficiently. A comparison of the present experiments with other published works has been conducted. An analytical study of the characteristics equation has been carried out to evaluate the best correlation of the ratio of cold temperature difference to the inlet temperature as a function of pressure, cold mass fraction, and nozzle number.     

水蒸汽在水平三维微肋管内的凝结换热及阻力特性

本文以水蒸汽为工质对水平三维微肋管内凝结换热及阻力特性进行了实验研究．与光管和二维管相比，在相同条件下，实验中效果最好的T3管全长平均凝结换热系数分别提高了113％～410％和20％～65％，同时，与二维管相比流动阻力增加较小，最大值不超过6．3％．比较另两种管型（T1，T2管）也证明三维管以较小的流阻增加为代价换取了明显的强化效果．     

渐缩型锥形脉管制冷机的二维数值研究

本文开发了二维可压缩交变流动的SIMPLEC计算程序,对渐缩型锥形脉管制冷机进行了二维数值研究,研究了锥度对脉管制冷机性能的影响。数值计算结果表明,对渐缩型锥形脉管,存在一最佳锥度,此时的制冷效果最好,当锥度大于最佳锥度时,制冷效果反而变差。另外本文还从脉管内流场的分布及二次流的角度揭示了锥形脉管能提高制冷机性能的原因及内在机理。一定锥度下的锥形脉管不但可以改变脉管内二次流的大小,还改变了脉管内二次流的分布情况,使脉管冷热端的二次流分布变得不均匀。这是一定锥度下的锥形脉管可以改善脉管制冷机制冷效果的主要原因。     

扁平管外蛇形翅片空间的流动换热性能数值模拟

扁平管外纤焊蛇形翅片是直接空冷凝汽器翅片管的一种常见形式,研究扁平管外蛇行翅片空间的空气流速和温度分布规律,对指导直接空冷凝汽器的设计和运行具有重要意义.针对不同空冷凝汽器管束夹角、不同空气温度以及不同空气入口流速,分别对空气侧流场和温度场进行了数值模拟,得到了空冷器外流场和温度场,以及对流换热Nu和摩擦系数f随Re和空冷器夹角的变化规律.数值模拟结果表明,不同的空冷器管束夹角显著影响其流动和换热特性,夹角越大,凝汽器空冷效果越好.     

微型蒸气压缩制冷系统实验研究

该制冷系统由微型回转式压缩机、管带式换热器和毛细管等组成,制冷剂为R134a。单机重2.21kg,体积210mm×140mm×160mm。2.0kg锂电池确保系统150min内持续提供73.6W冷量。利用空气焓差台测量压缩机转速、蒸发器进风温度和送风量等参数对于系统性能的影响。实验结果确定了影响性能的主要因素,且表明主动调节可使系统满足不同的制冷量和冷却温度要求。     

Flames in narrow circular tubes

We examine an axi-symmetric deflagration located in a tube with thermally active walls. It is noted that the flame-in-tube configuration defines a classical edge-flame, a flame in a shear flow for which there is a water-shed solution for a critical value of the Damköhler number (D), ignition front solutions for larger values of D, and failure wave solutions for smaller values. We examine semi-infinite tubes with a heat flux imposed at the tube wall ends, to simulate experiments reported in the 30th Symposium. We identify parameters for which stable solutions are obtained at certain flow rates, but unstable solutions are generated at higher flow rates, followed by stable solutions at still higher flow rates. These solutions are consistent with the experimental record. Instability leads either to regular oscillations or to a violent process characterized by quenching and re-ignition.     

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Cryostat thermal shield (CTS) of China Fusion Engineering Test Reactor (CFETR) is designed with 304LN stainless steel being selected as the CTS material. The CTS is divided into 16 sectors with each sector encompassing 20 sub-sectors, the corresponding cooling tubes are arranged on each sub-sector of the CTS panel sector, and liquid helium is selected as the coolant. The thermal analysis of the designed CTS structure is performed based on FLUENT, and the temperature distribution of the CTS panel and the pressure difference between the inlet and outlet of the cooling pipeline are obtained. The results show that the temperature of the CTS panel and the pressure difference between the inlet and outlet of the cooling tubes are within a reasonable range, which verifies the rationality of the layout of the cooling pipeline, and it provides reference for optimal design of the CTS.