翅片结构对超汽化结构换热性能影响的研究

基于计算流体动力学软件ANSYS CFX，利用非均相流欧拉-欧拉模型耦合RPI(伦斯勒理工大学)沸腾模型开展超汽化冷却结构的过冷沸腾两相流模拟，比较不同翅片结构对超汽化结构换热性能的影响。研究发现在高热流量条件下三角形翅片结构的换热性能优于矩形翅片结构：其中顺流4×3 三角形翅片结构总体换热性能最好；矩形4×3 翅片结构受流速影响较大，由于翅片的阻碍作用使得流速越来越低，换热性能越来越差；逆流4×3 三角形翅片结构由于其翅片间的腔小，并且逆流翅片对主流的破坏使得腔内流体保持着很大的湍度，所以翅片区有很好的换热性能，但由于逆流翅片对流体阻碍作用大，小槽内流体速度越来越低，使得远离翅片区的侧边换热性能逐渐变差。     

浮升力对管内水过冷流动沸腾传热特性的影响研究

基于已知的2087组水的过冷流动沸腾传热实验数据,通过努塞尔数(Nu)和格拉晓夫数(Gr)的关系探讨了不同流动方向和加热方式下浮升力对过冷流动沸腾传热性能的影响。对上壁面单边加热水平矩形管内过冷流动沸腾传热进行了实验研究。实验结果表明,向上的浮升力阻碍了气泡向流体中的扩散,使得传热恶化。在增加流速、增大压力和减小过冷度的条件下,Nu均随Gr增加,使过冷流动沸腾传热得到强化。     

Experimental investigation of heat transfer from different pin fin in a rectangular channel

In this study, the effect of both hexagonal pin fins (HPFs) and cylindrical pin fins (CPFs) into the rectangular channel on heat transfer augmentation, Nusselt number and friction factor were experimentally investigated. In planning of the experiments, different Reynolds number, pin fin array, pin fin geometry and the ratio of the distance between pin fin spacing (s) to the pin fin hydraulic diameter (s/D_h) were chosen as the design parameters. Air was used as the fluid. The Reynolds number, based on the channel hydraulic diameter of the rectangular channel, was varied from 3188 to 19531. In the experiments, the heating plate was made of stainless steel foil. The foil was electrically heated by means of a high current DC power supply to provide a constantly heated flux surface. The heat transfer results were obtained using the infrared thermal imaging technique. The heat transfer results of the hexagonal pin fins (HPFs) and cylindrical pin fins (CPFs) are compared with those of a smooth plate. Best heat transfer performance was obtained with the hexagonal pin fins. The maximum thermal performance factor ((?), was obtained as Re = 3188, staggered array, s/D_h = 0, ? = 2.28.     

基于(火积)耗散率最小的复杂肋片对流换热构形优化

基于构形理论, 以基于(火积)耗散率定义的当量热阻最小为优化目标对复杂肋片进行构形优化, 得到同时考虑肋片导热和对流换热(火积)耗散性能的肋片最优构形, 并比较不同形状和不同优化目标下的肋片最优构形. 结果表明: 存在最佳单元级直肋、中部空腔以及肋片末梢高度和长度比使得复杂肋片当量热阻取得三重最小值. 当量热阻最小的复杂肋片最优构形与T-Y形肋片最优构形相比, 复杂肋片结构使得肋片整体传热性能大大提高. 当肋片传热为二维传热且根部较宽时, 肋片根部温度越不均匀, 当量热阻最小和最大热阻最小的复杂肋片最优构形差别越大. 在保证热安全性的前提下, 工程上对肋片进行优化设计时可选择当量热阻最小的肋片构形设计方案以降低其平均传热温差、提高整体传热性能. 本文从传热优化角度为复杂肋片的优化设计提供了参考.     

微方肋冷却系统的换热特性

采用去离子水为冷却介质,对自行设计的不同结构微方肋散热器内的换热特性进行实验研究,结果表明:在进口温度为20 ℃、进口流量为57.225 L/h、底面平均温度为73.4 ℃时,散热器散热量可达2.83106 W/cm2,可以满足当前高热流密度散热需求;当散热面温度一定时,散热量随着散热器进口流量的增加而增加,但增速随散热器底面温度的增加变缓;努谢尔特数随雷诺数的增加而成幂次方增加,常规针肋结构和微针肋结构换热关系式不满足微方肋散热器特性。为了更好地表达微方肋散热器内的换热特性,拟合了微方肋散热器内对流换热关系式。     

HL-2M 偏滤器超汽化结构冷却性能研究

利用 ANSYS CFX 分析软件对 HL-2M 偏滤器超汽化结构模块方案进行了热工水力分析。研究结果 表明：在流道高度为 6mm 时,翅片高度为 3mm、厚度为 4mm 的超汽化结构排热能力最佳。当超汽化结构偏滤 器表面热流密度为 10MW·m^-2 时,靶板表面最大温度小于 700℃,热沉最大温度小于 300℃,满足排热能力需求和材料许用范围。     

超临界LNG在错列S形翅片微通道的流动传热特性研究

作为一种新型微通道换热器,印刷电路板式换热器(Printed Circuit Heat Exchanger,PCHE)因比表面积大、耐高压和低温、海上适应性强以及便于模块化等特点,近年来逐渐成为浮式LNG接收站和浮式储存及再气化装置的主低温换热器首选.针对改进后的错列S型翅片,对超临界LNG在翅片通道内的流动传热特性展...     

Study of vapor condensation on curvilinear fins under influence of capillary forces and gravity

The problem on film vapor condensation on curvilinear fins is solved numerically with regard to surface tension and gravity. Steam condensation on a fin of optimized and semicircular form was calculated for various inclinations of the fin relative to the direction of gravity vector and the levels of groove flooding. The calculations showed that the average heat transfer coefficient for a semicircular fin slightly decreases with changing the fin position relative to the direction of gravity vector, at that, the “zero” flow point from which the condensate flows in different directions shifts. For an optimized fin, there is no such shift, and the heat transfer coefficient does not practically change. The top of an optimized fin with a large curvature serves as a kind of "barrier" for the flow. The heat transfer coefficients on optimized fins are significantly higher than those on semicircular fins. The amount of the level of groove flooding significantly affects the condensation efficiency as a whole; however, it does not affect the process of condensation on the convex part of fins.     

车用散热器百叶窗翅片结构仿真优化

随着现代发动机技术的进步,发动机功率和性能的提升,也对发动机散热器提出了更高的要求。在兼备良好的散热性能和稳定性的同时,更要求散热器结构紧凑,以实现轻型化。通过对车用发动机管带式散热器的局部翅片和整体散热器进行三维建模,分析百叶窗翅片角度、翅片波距、翅片波高对空气侧压降影响,并对影响散热器散热性能主要因素进行分析。然后采用了多孔介质代替翅片的方法,模拟整体散热器的散热性能,并对比实验结果验证仿真模型准确性。最后拟合仿真数据的总传热系数和空气侧压降系数,建立粒子群算法优化数学模型。在不改变散热器外形尺寸和空气侧压降符合设计标准的情况下,优化散热器的翅片结构。翅片结构优化后,空气侧压降基本不变,散热量提升了11.6%。     

Experimental Study of Wavy Fin Aluminum Plate Fin Heat Exchanger

An experimental study of the air-side thermal hydraulic performance of the aluminum wavy fin in heat exchanger was performed. A series of tests were conducted for 16 wavy fin samples with different geometry parameters. The experimental correlation equations of the wavy fin about the heat transfer and pressure drop are set up using the multiple regression method. The parametric study on the performance of the wavy fins is carried out using the Taguchi method. The study results show that the ratio of the wavy fin amplitude and wavy length is the most important factor that affects the overall thermal hydraulic performance.