百叶窗翅片车辆散热器性能研究

通过数值模拟方法对百叶窗翅片散热器流道中流体的流动和传热性能进行研究,将数值模拟结果与文献实验关联式计算结果进行对比,验证了数值模拟方法的正确性。将百叶窗翅片散热器的翅片间距与百叶窗间距两者关联起来,分析了其比值Fp/Lp和百叶窗倾角对于百叶窗翅片流道传热和压降性能的影响。而后分析了百叶窗翅片结构参数对于百叶窗流道间流体流动效率的影响。研究表明,百叶窗翅片的传热系数和压降随着Re数的增大而增大,随着百叶窗翅片间距与百叶窗间距比值Fp/Lp的增大而减小,随着百叶窗倾角的增大而增大。流动效率随着Re数的增大而增大,随着百叶窗翅片间距与百叶窗间距比值的增大而减小,随着百叶窗倾角的增大而增大。     

散热器空气侧百叶窗翅片结构参数优化

对散热器空气侧的百叶窗翅片建立三维流固耦合的模型,运用Laminar方法进行数值模拟,结果表明传热与压降特性与实验关联式吻合较好,模型得以验证;为进一步阐明汽车内散热器空气侧的强化传热翅片的性能,分别考察了不同的翅片高度、窗翅高度、翅片厚度和翅片节距等结构参数对传热系数和压降的影响,得到了一组综合性能较好的百叶窗翅片结构参数。     

平直翅片热管散热器的正交数值模拟优化

文中以平直翅片热管散热器为研究对象,研究了翅片厚度、翅片间距、翅片高度、翅片宽度和热管直径 5 个结构参数对翅片换热性能和阻力特性的影响,采用正交实验设计的方法设计了上述结构参数的 15 个组合方案,利用 CFD 数值模拟的方法对每个组合方案下翅片的流动换热性能进行了模拟。以努塞尔数 Nu 、阻力系数f、传热性能综合评价指标(Performance Evaluation Criteria, PEC)作为评价指标,在每个评价指标下利用极差分析挑选出性能最优的组合方案。 该方法能快速获得散热器结构的优化方案,并分析出主要影响因素,对工程应用有一定的指导意义。 结果表明:影响 Nu 和 f 的最主要因素是热管直径,影响 PEC 的最主要因素是翅片厚度。 对于本文研究的散热器,其最优参数组合方案为:翅片厚度为 0. 6 mm,翅片间距为 2. 2 mm,热管直径为 6 mm,翅片高度为 65 mm,翅片宽度为 28 mm。     

新型百叶窗翅片对流换热特性研究

百叶窗翅片广泛应用在紧凑式换热器中,基于传统矩形百叶窗结构,提出两种新型矩/梭形百叶窗翅片,利用FLUENT软件对不同结构的百叶窗翅片流场、温度场进行模拟分析,对比不同结构百叶窗翅片的传热和阻力特性。研究表明,由于流道变截面的影响,使得梭形百叶窗和矩/梭形百叶窗有较高流速的流体冲刷加热管壁面,从而梭形百叶窗和矩/梭形百叶窗传热效果增强,其综合性能均优于矩形百叶窗,矩/梭（2/1）形百叶窗传热j因子相对较高,综合性能较好。     

Thermal characteristics of louvered fins with a low-reynolds number flow

A heat recovery system is crucial for the effective use of energy where heat rejection from production processes is unavoidable and must be reused. The response of the louvered fins to the low-Reynolds number hot gas is yet to be reported in the literature for the application of a heat exchanger on low-speed hot plume arising from heat sources in production processes. This study focuses on the effects of the louvered fin heat exchanger’s design parameters, which include the louver pitch and louver angle, on the convective heat transfer, which defines the thermal interaction between the hot, buoyant, naturally-induced air and the louvered fins. The resulting Colburn factors (j) are compared with those derived under forced convection with a similar range of low Reynolds number (233 to 1024). All experiments are done on a 15:1 scaled-up model. The fin aspect ratios between the fin spacing and louver pitch are set at 0.75, 1, and 1.5, while the louver angles are set at 18°, 23°, 30°, 35°, and 40°. The Colburn factor strongly depends on the louver angle, especially at the lower range of the Reynolds number. The decreasing aspect ratio induces more hot buoyant air into the louver-formed channels, increasing the heat transfer rate. When the fin angle increases towards 30°, a larger Colburn factor is produced. However, the heat transfer characteristic drops as the angle goes beyond 30°. The highest j for the low speed flow is attained when the louver angle is 30° and the fin aspect ratio is 1.     

CFD analysis of fin tube heat exchanger with a pair of delta winglet vortex generators

Among tubular heat exchangers, fin-tube types are the most widely used in refrigeration and air-conditioning equipment. Efforts to enhance the performance of these heat exchangers included variations in the fin shape from a plain fin to a slit and louver type. In the context of heat transfer augmentation, the performance of vortex generators has also been investigated. Delta winglet vortex generators have recently attracted research interest, partly due to experimental data showing that their addition to fin-tube heat exchangers considerably reduces pressure loss at heat transfer capacity of nearly the same level. The efficiency of the delta winglet vortex generators widely varies depending on their size and shape, as well as the locations where they are implemented. In this paper, the flow field around delta winglet vortex generators in a common flow up arrangement was analyzed in terms of flow characteristics and heat transfer using computational fluid dynamics methods. Flow mixing due to vortices and delayed separation due to acceleration influence the overall fin performance. The fin with delta winglet vortex generators exhibited a pressure loss lower than that of a plain fin, and the heat transfer performance was enhanced at high air velocity or Reynolds number.     

水冷盘式制动器散热结构优化

为提高水冷盘式制动器散热性能,基于强化对流传热原理,通过添加扰流柱对制动器散热结构进行优化,设计了4种扰流柱散热结构,运用CFD方法模拟制动盘流固耦合传热过程,采用Fluent软件进行热流固耦合仿真计算,获得制动盘温度特性和换热特性以及流动阻力特性,并使用综合性能评价因子对不同扰流柱散热结构进行评价。结果表明:通过在安装盘水槽内添加扰流柱可以有效地提高水冷盘式制动器的散热效果;在相同的工作条件下,正三角形扰流柱散热结构的盘面温度最低,平均努塞尔数与流动阻力最高,其综合散热性能较圆形、椭圆形以及水滴形扰流柱散热结构分别提高了3.4%,2.4%和4.4%,较无扰流柱散热结构提高了6.7%,正三角形扰流柱散热结构具有更好的综合散热性能。研究结果为水冷盘式制动器散热结构的优化设计提供了参考。     

Numerical analysis of the flow and heat transfer characteristics for forced convection-radiation in entrance region of an internally finned tubes

The flow and heat transfer characteristics of combined forced convection and radiation in the entrance region of internally finned tubes are investigated numerically in this paper. The uniform flow is considered for an inlet flow condition. A three dimensional parabolic problem is solved by a marching-type procedure envolving a series of two dimensional elliptic problems in the cross-stream plane. The SIMPLER-algorithm and Raithby's pressure-velocity coupling method are employed to analyze the flow and heat transfer characteristics. For the calculation of radiative heat transfer, the P₁-approximation and the weighted sum of gray gases method (WSGGM) are used. The effects of fin height, number of fins, optical thickness, reference temperature, and Planck number on the flow and heat transfer characteristics are examined. It was found that the effect of fin-height on the heat transfer characteristic is more dominant than that of number of fins. The present results show that the optimal non-dimensional fin height and number of fins are 0.4 and 16, respectively.     

ICEPAK在三相PWM变流器模块散热分析中的应用

散热器的设计和散热分析是三相PWM变流器设计的关键技术.本文利用CFD软件ICEPAK分析了三相PWM变流器模块的散热性能,探讨了影响散热性能的各个因素.结果表明:散热器的换热系数随着风速的增大而增大,压力系数则越来越小.散热器的肋片数以及肋片厚度的增加导致流通面积变小,压力系数增大,换热系数逐渐增大.     

一种新型相变散热器设计

对于短时或间歇性工作的大功率电子设备,特别是工作在临近空间的电子设备,利用相变材料进行散热是一种比较有效的冷却方式。但常用的相变材料导热系数比较低,必须采取各种措施强化相变材料的导热性能。文中在分析相变散热器中强化传热措施的基础上,针对小型轻量相变散热器的设计要求,设计了一种易于加工的内嵌螺旋形翅片的相变散热器。通过对散热器进行简化,计算了翅片间距。加热实验证明,所设计的新型相变散热器能很好地满足设计要求,螺旋形翅片能明显增强相变材料的导热性能,改善相变散热器的内部温度均匀性。     

A study on thermal fluid flow of magnetron cooling for microwave oven

A numerical study has been conducted on thermal dissipation fin shape of the magnetron of a microwave oven. The main focus of the study was on reducing the bypass away from cooling air around cooling fins and enhancing the heat transfer around cylindrical anode body with numerical investigation on louver, slit, dimple and bending shape. To optimize the location and the shape of the elliptical dimple, RSM(DOE) was adopted to enhance the thermal dissipation from the cylindrical anode of magnetron. The flow separation around the anode was delayed due to optimized dimple numerically and verified by experimental study. The enhancement of the fin cooling was utilized for cost reduction of the cooling fin by reducing the thickness of the fin from 0.6 mm to 0.5 mm, resulting in weight saving by 16.7 %.

     

锯齿形翅片散热器风冷性能试验研究

文中从试验的角度研究了锯齿形翅片散热器的风冷性能。锯齿形翅片散热器具有结构复杂、不易仿真实施的特点。文中系统介绍了锯齿形风冷散热器的典型结构形式以及风冷性能测试系统原理、性能和测试分析结果,从试验实测的角度研究了锯齿形翅片散热器的应用选型及其与散热量、风量、风压等的关系,分析了翅片参数(翅高、翅宽、翅片节距)对散热性能的影响,对电子产品散热的风冷设计具有较高的参考价值。     

气动发动机排气冷量在内燃机冷却系统中的回收利用研究

针对气动发动机排气的低温特性,提出了利用气动发动机排气冷却内燃机散热器的技术方案。通过初步试验,获得了气动发动机在不同转速下的排气流量和温度特性。基于初步试验结果,建立了气动发动机排气与内燃机冷却水的热交换模型,并进行了仿真计算,得到了不同水泵流量下,热水流经换热器的进出口温差以及换热量。研究结果表明,换热器进出口热水温差、换热量随着气动发动机转速的升高而增大;随水泵流量的增加,热水流经换热器进出口的温差逐渐减小,换热量增大,但各个水泵流量下的换热量相差较小,当发动机转速为700r／min时,温差增加值及换热量的增加值均为最小;随着气动发动机转速增加,气动发动机排气的冷量炯变化范围很小,回收指数逐渐上升,冷量回收效果变好。     

新型同轴套管式换热器强化传热研究

同轴套管式地热能开采技术是用于中深层地热能开采的有效方式。为了增强同轴套管式换热器的换热效率,提出了一种带螺旋翅片的新型同轴套管式换热器。基于有限体积法,对比分析新型与普通型同轴套管式换热器的换热性能,得到螺旋翅片结构对换热性能的影响,揭示其强化传热机理。结果表明：通过增加螺旋翅片的翅高或减小螺旋翅片的螺距,可有效增强同轴套管式换热器内流体流动的湍流动能,达到提高换热性能的目的;与普通光滑管换热器相比,翅高为19 mm,螺距为300 mm的新型换热器在雷诺数为27000时,努赛尔数提高了35.5%,摩擦系数提高了91%,热性能系数达到最高1.093;增加翅片和减小螺距都可以增加采出温度和采热功率,翅高为19 mm,螺距为300 mm换热器较光滑管换热器采热温度提高了5.4 K,采热功率提高了32.4%。为高效同轴套管式换热器设计提供了理论依据。     

带有强化冷凝段的热管散热器三维温度场数值模拟分析

为了解决高热流密度器件的散热问题而设计一种带有强化冷凝段的热管散热器,模拟不同的运行工况,对其散热效果进行了数值计算,并与其他类型的热管散热器进行了比较。结果表明:新型散热器由于热管设计结构的改变,使其换热温差增大,而且使散热器底板的均温效果更好,可以有效地降低高热流密度器件的工作温度。     

微型汽车散热器百叶窗翅片高度的优化设计

为了得到更合理的微型汽车散热器的百叶窗翅片结构,采用Fluent软件,对散热器翅片进行了数值分析.通过修改其关键尺寸(翅片高度),得到了不同高度下散热器翅片的阻力因子f和散热因子j,并引入无量纲参数j/f1/3来评价其综合性能.优化结果是当翅片高度为8.94mm时,综合性能最佳.     

车用小通道平行流换热器传热流动试验与分析

小通道平行流换热器是燃料电池汽车的主要散热部件。吸收了电堆废热的冷却液(50%乙二醇溶液),流过小通道换热管,由换热器外侧空气冷却。在进液温度、进风温度、冷却液流量以及风速变化的试验工况下,测试了换热器的传热流动性能。引入量纲一参数k,评估了各工况参数对换热量、阻力影响的强弱。接着,分析液侧努谢尔数Nu和摩阻系数f随雷诺数Re的变化趋势,结果显示:在小通道内(当量直径D=2.685 mm),冷却液从层流到湍流的转浪点Re_c=1 750,介于微尺度与常规尺度的临界值之间。在此基础上,通过多元回归法,拟合得到层流和湍流的液侧换热系数,摩阻系数的关联式,以及空气侧阻力f_a公式。Nu和f的计算值与试验值误差分别在[-7.06%,5.93%]和[-3.95%,4.11%]内,f_a的误差在[-2.22%,3.62%]内。基于这些关联式,建立数学模型,可在广泛多变的运行条件下,对换热器的运行性能进行理论预测和评估。     

Development of friction model for offset strip fin with separated viscous and inertial resistances

To predict the flow resistance of a compact heat exchanger with an offset strip fin, a large number of correlations have been developed and these correlations have been well used in the engineering field. Recently, three-dimensional computational analysis has been frequently used for the design and verification of heat exchangers. To improve the accuracy of three-dimensional numerical analysis and reduce the resources used for the analysis, the fins of compact heat exchangers are assumed to be a porous medium generally. To predict the flow resistance of an offset strip fin assumed to be a porous medium, the resistance must be separated into viscous and inertial resistances. However, the correlations developed so far for the offset strip fin have not been able to distinguish between these resistance types. In this paper, we propose a new friction model that can represent the flow resistance of an offset strip fin as the sum of the viscous and inertial resistances. The new friction correlation model has a maximum error of 10 % compared to existing correlation models. In addition, using the new friction model, the permeability and the Ergun constant for offset strip fins are defined as functions of offset strip fin parameters. Therefore, when predicting the flow resistance of a compact heat exchanger with an offset strip fin using three-dimensional numerical analysis, viscous and inertial resistances can be defined without additional calculations or tests for a porous medium approach.

     

基于Icepak的注塑机控制器散热翅片的优化

针对某公司的一款注塑机控制器的翅片散热问题,运用CFD软件Icepak对散热器的翅片厚度和高度进行了数值模拟和仿真分析,通过对比优化前后的散热效果,采用优化后的翅片厚度和高度获得了满足散热要求的翅片结构。结果表明：翅片厚度为lmm高度为8mm时,翅片散热效果得到强化,有效地降低了CPU的中心温度。     

基于Fluent的压裂车液压油散的翅片散热优化

随着压裂技术水平的提高和油气井的大规模开发，低功率压裂泵已逐步淘汰。大功率、超高压、大排量和智能化已成为国内外压裂车的主要特点。当满足这些条件时，压裂车散热器便不可避免地需要具有高散热效率。基于工程传热学，对液压油散进行几何模型和数学模型的构建，分析了压裂车液压油散的内部结构。利用 Fluent对不同的隔板间距和不同翅片厚度和节距的液压油散模型进行了仿真分析，并运用MATLAB对数据进行插值拟合处理，最终提出了一种提高压裂车油散的散热效率结构。