简析钎焊渗层螺旋翅片管省煤器

本介绍了一种新型省煤器，即钎焊渗层螺旋翅片管省煤器。这种新型省煤器具有较高的传热效率，可有效地解决磨损问题，提高锅炉平均工作时间，是传统省煤器的理想换代产品。     

钎焊渗层螺旋翅片管省煤器

介绍了一种新型省煤器 ,即钎焊渗层螺旋翅片管省煤器。这种新型省煤器具有较高的传热效率 ,可有效地解决磨损问题 ,提高锅炉使用率 ,是传统省煤器的理想换代产品     

镍基渗层管表面实现珠状凝结的研究

对镍基渗层管的强化冷凝换热进行了对比实验研究，并对渗层组织促成珠状凝结的机理进行了分析和讨论，为渗层管在强化冷凝换热领域中的开发与应用提供了依据。图8表2参8     

镍基渗层螺旋翅片式省煤器在410t/h煤粉炉上的应用

齐鲁石化热电厂410t／h煤粉锅炉原下级省煤器为光管式省煤器，运行中存在烟气阻力大、磨损严重以及换热效果差等问题，导致泄漏频繁，产品使用寿命短，检修工作量大，影响锅炉热效率。更换镍基渗层螺旋翅片式省煤器后，烟气阻力大、磨损严重现象明显改善，换热效果充分加强，运行周期大大延长，锅炉热效率显著提高。     

螺旋翅片管防磨和防积灰特性的试验研究

应用三维颗粒动态分析仪（PDA）对气固两相流绕流螺旋翅片管进行了防磨和防积灰的实验研究。实验结果表明在翅片之间，固相颗粒密度和主流速度呈抛物线规律分布。颗粒密度和速度的这种分布规律降低了固体颗粒对翅片壁面的撞击能量，从而减轻了翅片和基管的磨损。随着来流速度和来流密度的提高，迎风面区域磨损加剧，其他区域基本不受影响。实验数据还表明，螺旋翅片的导流作用使得迎风面的滞点处产生一个轴向速度，这和光管有着本质的区别。此速度的存在有利于减轻积灰。     

H型鳍片管的传热与流动特性试验研究

H型鳍片管是一种新型高效强化传热管。对一定结构的H型鳍片管与螺旋翅片管换热器进行了比较性半工业试验研究,得到了H型鳍片管换热与阻力准则关系式,并与相同结构参数的螺旋翅片管进行比较。根据实验结果得出:H型鳍片管换热与阻力特性均优于同结构参数的螺旋翅片管。     

波纹内翅片管内空气强化传热特性的研究

研究了一种波纹内翅片管的换热特性，得出了所测参数范围内沿程温度及换热系数分布特点，并比较了相同管径的内翅片波纹管和光管的综合换热效果，结果表明：高Re数时管子与翅片间的接触热阻对传热性能有较大影响；波纹内翅片管的综合换热效果强于光管，而且在低流速下换热强化效果更加明显。     

高压给水加热器采用小螺旋角的内外螺旋三角翅片管强化传热的试验研究

通过确切了解电站高压加热器的传热性能和特殊的设备要求，设计并加工出小螺旋角的内外螺旋三角翅片管用于强化其传热性能。基础实验表明，在实验的条件下，立式小螺旋角的内外螺旋三角翅片管的总传热系数比光滑管提高６３％－９５％，其中管外冷凝换热系数是同条件下光滑管的３．５－４倍，管内的对流换热系数也比光滑管提高了１８％。同螺旋槽等比较可知，立式小螺旋角的内餐螺旋三角翅片管的总换热系数比螺旋槽提高４％－２７％，     

螺旋翅片管省煤器抗磨性能的研究

采用数值模拟技术对错列布置光管及螺旋翅片管、顺列螺旋翅片管的双相流场进行了数值模拟,分析了不同结构、不同排列方式的省煤器的抗磨性能.分析了翅片结构对颗粒运动与流场的影响,指出翅片的存在使烟气中的大颗粒飞灰较难碰撞到基管的表面,增强了省煤器的抗磨损能力.     

PCS换热器螺旋结构强化换热数值研究

为了优化非能动热量导出系统（PCS）的设计,提高其换热性能,从而进一步提高PCS系统设计的安全性和先进性,采用数值分析的方法对光管、螺旋扁管和螺旋翅片管的冷凝传热特性进行研究。结果显示：在高含量不凝气条件下,螺旋翅片管的换热性能最强,螺旋扁管次之,光管最差。研究表明,PCS换热器采用螺旋翅片管能够强化换热效果。     

椭圆翅片管空冷器流动传热特性的研究

用稳态的恒壁温法对3个椭圆翅片管空冷器和1个圆翅片管空冷器的传热和阻力特性进行了研究,得到空冷器空气侧的传热与阻力性能,在相同的迎风面流速下,椭圆翅片管比圆翅片管空气侧换热系数约大3－7倍;在相同的换热系数下,椭圆翅片管比圆翅片管的压降低。     

连续型与锯齿型螺旋翅片管翅片效率计算与分析

介绍了烟气换热领域常用的两类高频焊钢质螺旋翅片管.指出目前存在多种连续型与锯齿型高频焊螺旋翅片管翅片效率计算方法,不便于同类换热实验结果的相互比较.通过深入分析与计算比较,对连续型与锯齿型高频焊螺旋翅片管分别给出了建议的翅片效率计算方法,供相关的工程设计及实验研究选用.两种管型的翅片效率比较表明,锯齿翅片的翅片效率较高,提高的幅度随翅片高度增大而增大.     

Comparison of Heat Transfer and Pressure Drop for the Helically Baffled Heat Exchanger Combined with Three-Dimensional and Two-Dimensional Finned Tubes

Experiments were performed to compare the shell-side heat transfer coefficient and pressure drop of a helically baffled heat exchanger with petal-shaped finned tubes to those of low-finned tubes for oil cooling using water as a coolant. The experimental results showed that for the heat exchanger with petal-shaped finned tubes, the shell-side heat transfer coefficients were augmented by 28–48%, yet the shell-side pressure drops were reduced by 35–75% at the same volumetric flow rates of oil. The possible mechanisms responsible for this heat transfer enhancement were analyzed for helically baffled heat exchanger combined with petal-shaped finned tubes.     

径向错列翅片管内凝结对流换热数值模拟分析

采用数值模拟方法,对径向错列翅片管内含不凝结气体水蒸气的凝结对流换热及阻力特性进行了综合分析。将编写的自定义函数(UDF)导入ANSYS FLUENT软件,对新型强化管传热性能和阻力性能进行了数值模拟,并根据管长方向壁面上蒸汽质量分数的变化情况,讨论分析了凝结过程中翅片管传热性能的变化规律。分析结果表明:与光管相比,内翅片管的强化传热效果随翅数增多、翅片换热接触面积增大而更加显著;另一方面,翅片管的流动阻力相应增大,对管路换热产生不良影响。在所研究翅型范围内16翅y=2x~2型翅片管综合强化换热效果更优;此外随着换热过程的持续,蒸汽凝结逐渐放缓;入口速度增大导致水蒸气凝结不充分,对换热效果的提升有一定制约。     

Numerical investigation of heat transfer and pressure drop in enhanced tubes

This study investigates passive heat transfer enhancement techniques to determine the distribution of temperature and static pressure in test tubes, the friction factor, the heat flux, the temperature difference between the inlet and outlet fluid temperatures, the pressure drop penalty and the numerical convective heat transfer coefficient, and then compares the results to the experimental data of Zdaniuk et al. It predicts the single-phase friction factors for the smooth and enhanced tubes by means of the empirical correlations of Blasius and Zdaniuk et al. This study performed calculations on a smooth tube and two helically finned tubes with different geometric parameters also used in the analyses of Zdaniuk et al. It also performed calculations on two corrugated tubes in the simulation study. In Zdaniuk et al.'s experimental setup, the horizontal test section was a 2.74 m long countercurrent flow double tube heat exchanger with the fluid of water flowing in the inner copper tube (15.57–15.64 mm i.d.) and cooling water flowing in the annulus (31.75 mm i.d.). Their test runs were performed at a temperature around 20 °C for cold water flowing in the annulus while Reynolds numbers ranged from 12,000 to 57,000 for the water flowing in the inner tube. A single-phase numerical model having three-dimensional equations is employed with either constant or temperature dependent properties to study the hydrodynamics and thermal behaviors of the flow. The temperature contours are presented for inlet, outlet and fully developed regions of the tube. The variations of the fluid temperature and static pressure along tube length are shown in the paper. The results obtained from a numerical analysis for the helically tubes were validated by various friction factor correlations, such as those found by Blasius and Zdaniuk et al. Then, numerical results were obtained for the two corrugated tubes as a simulation study. The present study found that the average deviation is less than 5% for the friction factors obtained by the Fluent CFD program while Blasius's correlation has the average deviation of less than 10%. The corrugated tubes have a higher heat transfer coefficient than smooth tubes but a lower coefficient than helically finned tubes. The paper also investigates the pressure drop penalty for the heat transfer enhancement.     

滴状翅片管传热及阻力特性的试验研究

对滴状翅片管的传热及阻力性能进行了试验,给出了不同风速、温度下的试验结果。探讨了对流换热系数的分离方法。依据实测的数据,将管外空气横掠管簇的对流换热系数从传热系数中分离了出来。对管外的对流换热特性、阻力特性进行了分析研究,并整理成了无量纲准则式。试验表明滴状翅片管的阻力较小,试件性能达到国际先进水平。     

椭圆钎焊与双金属轧制翅片管传热与阻力性能的试验对比

对椭圆钎焊翅片管和双金属轧制翅片管换热器的传热及阻力性能进行试验对比研究,试验得到了一系列工况下的传热数据与管外空气流动阻力数据,给出了相应的传热系数、流动阻力曲线。从总传热系数中分离出管外空气侧的对流换热系数,得到了具有一定应用价值的管外换热的计算关联式;拟合得到了管外阻力计算关联式。结果表明:椭圆钎焊翅片管比双金属轧制翅片管的传热系数约高9%,管外换热系数约高17%,且管外空气流动阻力约低11%。     

新型轴对称内翅管换热过程的数值模拟

采用数值模拟的方法,对新型整体式轴对称不等高内展翅片换热管的管内流动、换热及阻力特性进行了研究,并将模拟结果分别与实验测量值和光管经验公式计算值进行了比较,结果表明:数值模拟结果与实验测量结果和经验公式计算结果符合得较好;新型内翅片管的强化换热效果最好,其换热系数约为光管的1.67~2.27倍,为中心对称翅片管的1.17~1.35倍;内翅片管的阻力系数是光管的1.44~2.20倍,中心对称和新型内翅片管具有基本相同的阻力系数;8翅和10翅新型内翅片管的综合性能参数较优.     

Heat transfer augmentation in 3D internally finned and microfinned helical tube

Experiments are performed to investigate the single-phase flow and flow-boiling heat transfer augmentation in 3D internally finned and micro-finned helical tubes. The tests for single-phase flow heat transfer augmentation are carried out in helical tubes with a curvature of 0.0663 and a length of 1.15 m, and the examined range of the Reynolds number varies from 1000 to 8500. Within the applied range of Reynolds number, compared with the smooth helical tube, the average heat transfer augmentation ratio for the two finned tubes is 71% and 103%, but associated with a flow resistance increase of 90% and 140%, respectively. A higher fin height gives a higher heat transfer rate and a larger friction flow resistance. The tests for flow-boiling heat transfer are carried out in 3D internally micro-finned helical tube with a curvature of 0.0605 and a length of 0.668 m. Compared with that in the smooth helical tube, the boiling heat transfer coefficient in the 3D internally micro-finned helical tube is increased by 40-120% under varied mass flow rate and wall heat flux conditions, meanwhile, the flow resistance is increased by 18-119%, respectively.