热端管长度对涡流管性能影响的实验研究

研究了不同热端管长度情况下涡流管的能量分离性能。实验中,采用纯度为99.99%二氧化碳为工质,进口压力为0.4 MPa。实验发现,在相同进口压力下,随着热端管长度的增加,涡流管制冷效应呈现先增大后减小的趋势,热端管长度为125 mm时具有最佳制冷温度效应,制热效应逐渐增大。同一管长时,轴向Z=12.5—50 mm壁温变化剧烈,热端出口附近壁面温度受回流影响较大,冷流率越大受回流影响越大。冷流率0.6、0.7时壁温随着管长的增大呈现先增大后减小的趋势,冷流率0.8时各管长壁温差别较小。     

涡流管的入口压力对其性能影响的研究北大核心CSCD

针对涡流管的性能优化问题,需要研究各个参数及结构部件对其制冷、制热能力的影响,并寻求最佳的运行工况。本文搭建了开式实验系统,采用自制的六流道喷嘴,以二氧化碳气体为工质,研究了入口压力和冷流率对涡流管能量分离性能的影响。结果表明:涡流管的制冷、制热效应均随入口压力的增大呈现先增大后减小的趋势,在入口压力为0.4 MPa,冷流率为0.4时具有最佳制冷效应,冷流率为0.9时,具有最佳制热效应;冷流率为0.2~0.5时,涡流管热端管壁面温度随冷流率的增大呈现逐渐升高的趋势,冷流率为0.6~0.9时,壁面温度在出现壁面最高温度点后有所下降,并且冷流率越大壁面温度下降越明显。     

冷孔板孔径及进口压力对涡流管性能影响的实验研究北大核心CSCD

针对涡流管大量应用于制冷系统中,对涡流管的各项参数进行研究,寻求最佳制冷工况及参数。本文自行设计涡流管实验样机,搭建开式的涡流管实验台,以CO2为工质,在不同的进口压力(0.2~0.6 MPa)、不同的冷流率(0.2~0.9)工况下研究了5种冷孔板孔径(1.5~3.5 mm)的涡流管性能,分析冷孔板孔径对涡流管性能的影响情况。研究表明:制冷、制热效应均在0.4MPa达到峰值后出现下降,在冷孔板孔径为2.5 mm时获得最佳制冷效应29.3℃、制热温度效应37.9℃,且获得最佳制冷量及制冷性能。     

冷孔板孔径及进口压力对涡流管性能影响的实验研究北大核心CSCD

针对涡流管大量应用于制冷系统中,对涡流管的各项参数进行研究,寻求最佳制冷工况及参数。本文自行设计涡流管实验样机,搭建开式的涡流管实验台,以CO2为工质,在不同的进口压力(0.2~0.6 MPa)、不同的冷流率(0.2~0.9)工况下研究了5种冷孔板孔径(1.5~3.5 mm)的涡流管性能,分析冷孔板孔径对涡流管性能的影响情况。研究表明:制冷、制热效应均在0.4MPa达到峰值后出现下降,在冷孔板孔径为2.5 mm时获得最佳制冷效应29.3℃、制热温度效应37.9℃,且获得最佳制冷量及制冷性能。     

热端管长度对涡流管流场影响的数值模拟研究

以理想CO_2气体为工质,采用Standard k-ε湍流模型,对涡流管能量分离效应进行数值模拟,分析了管内流体流场的分布以及内旋流与外旋流分离界面的分布。在此基础上,探究了进口温度为298.15 K、进口压力为6.5 MPa、冷流率为0.1时,热端管长度对涡流管内流场分布以及能量分离性能的影响。模拟结果表明:热端管长度在100～200 mm范围内变化时,随着热端管长度的增大,轴向上:轴向速度逐渐增大,切向速度逐渐减小、径向上:轴向速度会出现运动方向相反的情况,切向速度先增大后减小,制冷温度效应呈现先增大后减小的趋势。     

热端管长度对涡流管性能影响的试验研究

涡流管具有结构简单、无运动部件、价格低廉、可靠性高等优点,但管内发生的能量转换却极为复杂。本文以压缩空气为工作介质,对涡流管能量分离特性进行试验研究,获得涡流管制冷、制热效应随热端管长度、冷端流率之间的关系。研究结果表明,热端管长度越长,六流道喷嘴涡流管的制冷、制热效应越好,获得最大制冷效应时的冷端流率越大。     

整流器对涡流管能量分离性能影响的研究

设计加工了不同叶片角度的导流叶片形涡流管整流器。搭建了涡流管性能研究实验台。对整流器及其叶片角度对涡流管能量分离性能的影响，整流器对涡流管的长径比的影响进行了实验研究，并将白行设计加工的带有上述整流器的涡流管与ARTX公司生产的同类型涡流管进行了对比实验。实验结果表明：在涡流管末端加装上述整流器后，在冷流率为50％～80％时，涡流管的单位制冷量比不装整流器的涡流管提高了12％～44％；在实验研究的角度范围内，冷流率小于70％时，整流器叶片角度越大，制冷效果越好；加装整流器后，将涡流管的长径比由10．8降低到4．6，并且保持制冷效应不变；上述带整流器的涡流管在冷流率大于60％时，其制冷效应好于ARTX公司的同类型涡流管。     

工业机柜涡流管制冷装置性能试验研究

介绍了工业机柜涡流管制冷装置试验台;对实验结果进行了分析,分析表明,涡流管的入口温度越低,其制冷性能越好,制热性能越差,对涡流管的分离效应影响不大;涡流管的入口压力越高,涡流管表现出更好的制冷性能、制冷效应、制热性能和制热效应,其分离效应也增强;热阀开度K=1时,涡流管有最好的制冷性能和制冷效应;热阀开度K=2时,涡流管有最好的制热性能和制热效应;热阀开度K=1和K=2时都有较高的分离效应.     

涡流室直径对涡流管性能的影响

以高压气体为工质,对配有不同涡流室内径的涡流管冷热分离效应进行数值模拟研究,并获得了不同结构的涡流管随冷流比变化的制冷制热结果,以及等熵效率曲线。研究表明,随着冷流比的增加,涡流管制冷温差逐渐减小,制热温差逐渐增大,而等熵效率逐渐减小。当冷流比为0.28左右时,涡流管能获得最大的单位制冷量。通常装有较大涡流室的涡流管能获得更好能量分离效果。     

带排液结构的涡流管的性能实验

设计了带排液结构的涡流管的基本结构并搭建了性能研究实验平台,以空气为介质,研究长径比、排液口位置、排液间隙、可凝组分浓度对涡流管性能的影响。实验结果表明:在实验所进行的冷流率范围内,制热效应随着冷流率的增加而逐渐增大,制冷效应则存在极大值;随着长径比的增加,温度效率的极值有所增大,但是当长径比达到一定的数值后,温度效率和制冷效率增加的幅度显著减小;排液口位置的改变对于涡流管温度效率和湿气脱除率的影响不大;排液间隙的存在对涡流管的冷热分离性能有影响,间隙为1 mm时湿气脱除率最小;随着可凝组分浓度的增加,湿气脱除率逐渐增大,但增大的趋势逐渐趋于平缓。     

冷端孔径对涡流管性能影响的实验研究

本文搭建了涡流管性能实验台,研究了不同冷端孔口直径的涡流管实验样机的性能。当进口压力为0.3~0.5 MPa时,分析了冷端孔径对冷端温降特性、制冷量特性、等熵温度效率特性及COP特性的影响。结果表明:冷端孔口直径对涡流管性能有很大影响,存在一个使涡流管冷端温降及制冷量均达到最大值的最佳冷端孔口直径,在本文设计的涡流管几何尺寸条件下,最佳冷端孔口直径为5 mm,最佳冷端孔口直径与热端直径比为0.5。     

六流道喷嘴涡流管能量分离特性的研究

涡流管具有结构简单、无运动部件、价格低廉、可靠性高等优点，但管内发生的能量转换却极为复杂。以压缩空气为工作介质，对涡流管能量分离特性进行了实验研究，获得了涡流管制冷、制热效应随入口压力、冷端流率之间的关系，研究结果表明，进口压力越高，六流道喷嘴涡流管的制冷、制热效应越好，但获得最大制冷、制热效应时的冷端流率均有减小的趋势。     

Determining of gas type in counter flow vortex tube using pairwise fisher score attribute reduction method

This paper focused on the determining of gas types in counter flow type vortex tubes. In the present study, four different gas types including air, oxygen, nitrogen, and argon in the vortex tube with different inlet pressures and nozzle numbers have been used. The main aims of this paper are to investigate the correlations between gas types and input parameters comprising nozzle numbers, inlet pressures, inlet mass flow rate, temperature of cold outlet, temperature of hot outlet, and cold mass fraction and to select the most important attributes using correlation based attribute reduction and pairwise fisher score attribute reduction (PFSAR). After attribute reduction methods applied to dataset, k-nearest neighbor and C4.5 decision tree classifiers have been used to determine the gas type in the RHVT. The results have demonstrated that the PFSAR is a robust and efficient method in the reduction of attributes belonging to vortex tube.     

Experimental investigation of vortex tube refrigerator with a divergent hot tube

Energy separation performance of vortex tube can be improved by using a divergent hot tube. Experiments are carried out to investigate the influence of the geometrical parameters on vortex tube refrigeration capacity by using nitrogen as the working fluid. In this work, the parameters are focused on the divergence angle of hot tube, length of divergent hot tube and number of nozzle intakes. Experimental results present that there is an optimum angle for obtaining the highest refrigeration performance, and 4° is the optimal candidate under our experimental conditions. Divergent tube length which exceeds a critical length has slight effect on the refrigeration capacity. The critical length to diameter ratio is L/D = 12 in our experiment. Increasing number of nozzle intakes increases the sensitivity of temperature reduction and can obtain the highest possible temperature reduction. Moreover, similarity relations for the prediction of the cold exit stream are presented and confirmed by the experimental data.     

Experimental investigation of performance of hot cascade type Ranque-Hilsch vortex tube and exergy analysis

In this study, three Ranque-Hilsch vortex tubes were used, which have 9 mm inside diameter and length/diameter ratio was 15. Their performances were examined as one of the classical RHVT and other was hot cascade type RHVT. Performance analysis was according to temperature difference between the hot outlet and the inlet (ΔT_hot.). The ΔT_hot values of hot cascade type Ranque-Hilsch vortex tubes were greater than the ΔT_hot values of classical RHVT, which were determined experimentally. The total inlet exergy, total outlet exergy, total lost exergy and exergy efficiency of hot stream were investigated by using experimental data. In both the classical RHVT and hot cascade type RHVT, it was found that as fraction of cold flow increases the total lost exergy decreases. It was also found that, the hot cascade type RHVT more exergy efficiency of hot outlet than the classical RHVT. Excess ΔT_hot value of hot cascade type Ranque-Hilsch vortex tube causes the excess exergy efficiency of hot outlet.     

进气温度与压力对锥形涡流管性能的影响

以氮气为工质,对锥形涡流管能量分离特性进行了实验研究,结果表明入口气流温度对锥形涡流管的工作性能影响较小.进气压力越高,能量分离性能越强,不同压力下都在冷气流率约0.2时,可得到最大制冷效应和制冷效率,冷气流率约为0.5时,可获得最大制热效应.升高压力可提高锥形涡流管的能量分离性能,但提高幅度逐渐减小,当压力升高到一定...     

Numerical investigation of gas species and energy separation in the Ranque-Hilsch vortex tube using real gas model

A three dimensional Computational Fluid Dynamics (CFD) model is used to investigate the phenomena of energy and species separation in a vortex tube (VT) with compressed air at normal atmospheric temperature and cryogenic temperature as the working fluid. In this work the NIST real gas model is used for the first time to accurately compute the thermodynamic and transport properties of air inside the VT. CFD simulations are carried out using the perfect gas law as well. The computed performance curves (hot and cold outlet temperatures versus hot outlet mass fraction) at normal atmospheric temperature obtained with both the real gas model and the perfect gas law are compared with the experimental results. The separation of air into its main components, i.e. oxygen and nitrogen is observed, although the separation effect is very small. The magnitudes of both the energy separation and the species separation at cryogenic temperature were found to be smaller than those at normal atmospheric temperature.     

内调相型脉管制冷机的理论分析

对内调相型脉管制冷机进行热力学理论分析.内调相型脉管制冷机的特点是两个冷头在脉管热端通过针阀串联,两边脉管内的压力和流量耦合,通过调节各自的输入压力相位来主动调节脉管冷端流量与压力的相位差,输入压力相位由一个具有双出口的旋转阀来实现.分析表明,该调相方法可使脉管冷端流量与压力同相,从而使制冷量最大,而且相比于传统的小孔加气库型和双向进气型脉管制冷机,其制冷效率大大提高.该结构省却了体积较大的气库,结构更加紧凑.