三分螺旋折流板换热器壳侧流场温度场模拟

建立了三分螺旋折流板换热器壳侧流动与传热的数学模型,对其流场、温度场和压力场的数值模拟结果在多个纵剖面和横切片上进行了展示。可见在螺旋通道的轴心和靠近壳体的折流板外缘区域局部速度较高,在折流板背流面呈现出有利于强化掺混作用的回流区,流道内几乎没有流动死区;壳侧流体温度为稳步均匀下降趋势,并呈现从圆周的外缘向轴心方向逐渐递减;而压力场则呈现明显的周期性和阶梯性。     

椭圆管连续螺旋折流板换热器布管方式对壳侧传热和阻力性能的影响

以椭圆管连续螺旋折流板换热器作为研究对象,提出了三角形横置和竖置与同心圆环状和发散状四种布管方式,用ANSYS CFX进行数值模拟,并采用三场协同原理分析其壳侧综合性能。结果表明:同心圆环状布管流场最易形成旋转流动,壳侧压降最小;以三场协同原理作为评价标准得出,同心圆环状布管综合性能最优,其它依次是三角形竖置布管、三角形横置布管、同心发散状布管。     

双螺旋与中间搭接螺旋折流板换热器性能研究

采用数值模拟方法研究了40°螺旋角时螺旋折流板换热器双螺旋和中间搭接两种折流板布置形式对壳程性能与螺旋流动的影响,并与30°和40°螺旋角时单螺旋连续搭接结构的进行了对比.结果表明,40°螺旋角时双螺旋和中间搭接结构会强化壳程流体的螺旋流动,使同流量下壳程换热系数与压降增加,但同压降下的换热系数显著下降且均低于30°螺...     

双壳程连续螺旋折流板换热器的数值模拟

本文提出了一种新型的双壳程连续螺旋折流板换热器。采用数值模拟方法对双壳程、单壳程连续螺折流板换热器,以及弓形折流板换热器壳侧流动与传热持性进行了对比研究。结果表明,同质量流量和对流换热系数近似相等的情况下,双壳程连续螺旋折流板换热器壳程压降比弓形折流板换热器低17.7%～23.5%,同质量流量和壳程压降近似相等的情况下,其对流换热系数比单壳程连续螺旋折流板换热器高7.1%～12.6%。     

连续螺旋折流板蒸发器壳侧流动换热数值模拟研究

本文对相同几何尺寸的连续螺旋折流板蒸发器与传统弓形折流板蒸发器进行对比性的数值模拟研究,结果表明:在相同壳侧体积流量和折流板数条件下,连续螺旋折流板蒸发器的传热因子和摩擦因子约是弓形折流板的1/3和1/4;当以换热因子和摩擦因子比值评价蒸发器综合性能时,连续螺旋折流板蒸发器比弓形折流板蒸发器提高57%;当最小流通截面流...     

组合式多壳程螺旋折流板管壳式换热器数值模拟研究

本文采用数值模拟方法对内壳程为非连续螺旋折流板的组合式螺旋折流板和单壳程弓形折流板管壳式换热器壳侧流动换热特性进行对比研究,结果表明:相同壳程质量流量和相同换热量条件下,组合式两壳程螺旋折流板换热器的压损比弓形折流板换热器降低14.6%;相同壳程质量流量条件下,组合式两壳程螺旋折流板换热器单位压降下换热量比弓形折流板换热器提高10.8%.     

弓形折流板换热器中折流板对换热器性能的影响

本文采用Bell-Delaware换热器设计方法研究了传统弓形折流板换热器加热轻油时在不同管束排列角度下,改变换热器壳侧折流板间距以及改变折流板的窗口高度对管壳式换热器的壳体内径、换热管数目、壳侧换热系数及壳侧压降的影响.     

螺旋折流板换热器层流流动与换热的数值模拟

应用多孔介质和分布阻力模型对一螺旋折流板管壳式换热器的壳侧层流流动与换热进行了三维数值模拟,并与该换热器的实验研究结果进行了对比分析,符合程度良好.证明了该方法能有效地模拟螺旋折流板换热器的流动和换热特性.     

螺旋折流板换热器流动与换热特性的试验分析

对螺旋折流板换热器的流动及换热特性进行了试验研究与分析.结果表明,当保持螺旋周期为定值时,在相同流量下和相同壳径下,螺旋折流板换热器的壳侧压降随螺旋角增大而减小,且远低于弓形折流板的管壳式换热器;壳径减 小时,压降增加明显.相同Re下,螺旋折流板换热器的壳侧换热系数低于弓形折流板,在螺旋角为40°时达到最大值.相同流量下,螺旋折流板管壳式换热器单位压降和单位泵功下的换热系数均高于弓形折流板管壳式换热器.     

变截面折流杆换热器的流动与传热分析

本文在折流杆换热器的基础上,采用数值计算的方法,以水为流动介质,对不同折流杆间隔的折流杆式换热器进行流动与传热特性的分析。同时,本文设计了一种新型的变截面折流杆式换热器,对换热器进行优化,结果表明,变截面折流杆换热器比等截面折流杆换热器的综合性能最多高13%～14%。     

折流杆换热器的数值模拟及优化设计

在折流杆换热器的基础上,以水为流动介质,采用数值计算的方法,对不同折流杆杆型与间隔组合的折流杆式换热器进行流动与传热特性的分析.结果表明,折流杆杆型为椭圆杆,折流杆间隔为120 mm时,性能最好.     

Study on Heat Transfer Performance of Skin Heat Exchanger

Cooling technology is facing new challenges with the increase of electronic equipment power onboard aircraft. The traditional heat sink based on high-altitude bleed air does not satisfy this increase of cooling demands. In this article, an air/air-type skin heat exchanger is studied for cooling aircraft electronic equipment. It uses outside high-altitude cold air rather than bleed air as a heat sink. This cooling technology can effectively remove the heat load of high-power electronic devices without greatly increasing aircraft performance penalty. To assess its high-altitude heat transfer performance, an experimental prototype was designed and made. Some experiments were conducted on a ground experimental test. The heat transfer criteria formulas were obtained for both the side air in the skin heat exchanger and its convective heat transfer coefficients. Based on these experimental analyses, the heat transfer performances of the skin heat exchanger in a high-altitude cruise condition are deduced when it is assumed to be installed at an unfavorable position and a favorable position, separately. This work tries to provide a technical support for its future onboard application.     

壳管相变蓄热器强化传热实验研究

为了强化相变蓄热器传热性能,本文设计了三种新型壳管相变蓄热器结构,并对其换热性能进行实验研究.结果表明:在蓄热器内部添加分层结构和斜翅片换热性能最高,内部温度达到均匀化的时间随换热单元数增加而增大;换热管道间翅片的添加可有效地强化换热效果,改善蓄热器内部出现的温度严重分层现象,温度分布更加均匀;在研究范围内,换热流体温...     

An Experimental Investigation of Forced Convection Heat Transfer from a Coiled Heat Exchanger Embedded in a Packed Bed

Forced convection heat transfer from a helically coiled heat exchanger embedded in a packed bed of spherical glass particles was investigated experimentally. With dry air at ambient pressure and temperature as a flowing fluid, the effect of particle size, helically coiled heat exchanger diameter, and position was studied for a wide range of Reynolds numbers. It was found that the particle diameter, the helically coiled heat exchanger diameter and position, and the air velocity are of great influence on the convective heat transfer between the helically coiled heat exchanger and air. Results indicated that the heat transfer coefficient increased with increasing the air velocity, increasing helically coiled heat exchanger diameter, and decreasing the particle size. The highest heat transfer coefficients were obtained with the packed-bed particle size of 16 mm and heat exchanger coil diameter of 9.525 mm (1/4 inch) at a Reynolds number range of 1,536 to 4,134 for all used coil positions in the conducted tests. A dimensionless correlation was proposed for Nusselt number as a function of Reynolds number, particle size, coil size, and coil position.     

中空纤维膜换热器传热传质性能的实验研究

中空纤维膜换热器可同时实现传质传热, 该换热器可应用于吸收式制冷系统以改善制冷性能. 为探究该膜换热器在溴化锂吸收式制冷系统的运行工况下的传热传质特性, 搭建中空纤维膜换热器性能测试实验台, 采用控制变量法探究在热侧不同入口溶液流速、温度下该换热器的传热量及膜通量变化规律特性. 结果表明: 在热流体其它参数保持不变的情况下, 中空纤维膜换热器热侧溶液的入口流速由3.05 m/s 增至3.30 m/s 时, 换热器总传热量与膜通量均随之加大, 增幅分别为16.0%和2.2%; 该膜换热器的总传热量在冷侧溶液与热侧溶液入口温差10°C 至15°C 内, 增幅达到18.9%, 而膜通量受膜两侧溶液的入口温差变化影响较小, 增幅仅3.1%. 研究表示: 温度的变化对中空纤维膜换热器的传热传质性能影响更为显著, 而流速的变化对水分子的运动影响较小.     

斜向流换热器壳程流场均匀化研究

传统弓形折流板换热器壳程流体横向流动时存在流动阻力和传热死区大等缺点。为克服上述不足,研究开发了一种新型高效节能的斜向流管壳式换热器,采用导向型折流栅替代传统弓形折流板,倾斜流道内流体斜向冲刷换热管束。考察和对比了斜向流换热器和弓形折流板换热器壳程主流区的流体流速分布和变化规律,证实了导向型折流栅具有显著的控涡均化壳程流场和提高壳程流体整体流速的作用,有助于减小壳程压降,增大有效换热面积,为管壳式换热器结构改良提供了参考依据。     

Experimental and Numerical Investigation of the Effect of Turbulator on Heat Transfer in a Concentric-type Heat Exchanger

This article experimentally and numerically analyzes the effect of turbulators with different geometries (Type I, Type II, Type III, and Type IV) located at the inlet of the inner pipe in a concentric-type heat exchanger. Experiments were performed at parallel-flow conditions in the same and opposite directions to investigate the impact of manufactured turbulators on heat transfer and pressure drop. In the numerical study, ANSYS 12.0 Fluent code program was used, and basic protection equations were solved in the steady-state, three-dimensional, and turbulence-flow conditions. Results were obtained from numerical analysis conducted at different flow values of air (7, 8, 9, 10, 11, and 12 m³/h). The distribution of temperature, velocity, and pressure was demonstrated as a result of numerical analyses. Experimental and numerical results were compared, and it was observed that they were in conformity with each other. When the data obtained from the analyses were examined, the highest heat transfer, pressure drop, and friction factor increase were detected to be in the Type IV turbulator.