矩形截面螺旋通道内气液两相流局部含气率分布实验研究

应用电导探针测量技术,对矩形截面螺旋通道内气液两相流局部含气率进行实验研究。在不同的气相折算速度下,应用电导探针测量了弹状流弹单元的长度,并与可视化方法进行对比,验证了电导探针的可靠性,并为信号处理选择合适的阈值。分别在泡状流、弹状流及环状流三种流型的条件下,分析了气相与液相折算速度对局部含气率分布的影响。实验结果发现,螺旋通道气液两相局部含气率呈非对称的抛物线形分布,这种非对称性受流型和液相折算速度的影响。     

气液两相流破口泄漏的相分离实验研究

为研究气液两相流体通过破口泄漏时的相分离规律,设计了新型泄漏测量装置,在空气-水两相流实验环道上开展了实验研究.实验测量段水平布置,管径为40mm,采用直径为2.5mm的圆孔模拟破口.实验中出现的气液两相流流型包括波状流、环状流以及弹状流.结果发现气液两相流体通过管壁破口时会发生严重的相分离现象,相分离程度主要受小孔方位、流型等因素的影响.在环状流型下,由于周向液膜分布的不均匀性,随着小孔位置偏离管壁底部,进入小孔的液相逐渐减少,气相逐渐增多;在分层的波状流型下,当破口位于管壁顶部时,在小孔两侧差压较大时由于伯奴利效应,液相也会进入破口;由于弹状流独特的流动特性,在液塞来临时,破口两侧压力急剧增加,从而导致弹状流型下进入管壁破口的液相远大于其它流型.     

对称分支并行微通道中气液两相流的均匀性规律

采用高速摄像系统研究了对称分支形并行微通道内气液两相流及弹状气泡均匀性规律。实验中分别采用含0.3% SDS的甘油-水溶液与氮气作为液相和气相。观察到弹状流和泡状流两种流型,作出了由两相操作条件构成的流型图及流型转变线。结果表明,气泡非均匀性主要由两微通道内流体之间的相互作用、下游通道中流体动力学的反馈作用以及通道制造误差造成。随液相黏度增大,气泡均匀性变好;在高液相流量以及低气相压力下操作,气泡尺寸分布更易达到均匀。基于压力降守恒原理和微通道内气液两相流阻力模型,构建了两通道中气泡尺寸的预测模型。     

对称分支并行微通道中气液两相流的均匀性规律

采用高速摄像系统研究了对称分支形并行微通道内气液两相流及弹状气泡均匀性规律。实验中分别采用含0.3%SDS的甘油-水溶液与氮气作为液相和气相。观察到弹状流和泡状流两种流型,作出了由两相操作条件构成的流型图及流型转变线。结果表明,气泡非均匀性主要由两微通道内流体之间的相互作用、下游通道中流体动力学的反馈作用以及通道制造误差造成。随液相黏度增大,气泡均匀性变好;在高液相流量以及低气相压力下操作,气泡尺寸分布更易达到均匀。基于压力降守恒原理和微通道内气液两相流阻力模型,构建了两通道中气泡尺寸的预测模型。     

无泄漏的管壳式换热器壳侧局部含气率的研究

在常温常压下 ,应用电导探针对无泄漏的TEMA -E型管壳式换热器壳侧气液两相流的局部含气率进行了测量 ,研究发现在壳侧错流区折流板的迎流面和背流面附近 ,气液分布有着明显的差异 ,而且两者均不等同于错流区中心区域的气液分布。通过对局部含气率的加权体积积分得到了体积平均含气率 ,并采用马蒂内利参数及全液相佛鲁德数进行关联 ,得到的关联式与实验数据较吻合     

壁面润湿性对微通道内二氧化碳-水两相流流动及传质性能的影响

在1 mm×1 mm矩形截面下微通道内,以二氧化碳-水为工作流体,研究壁面润湿性和气液表观流速对气-液两相流型和气液传质的影响,并研究了气、液表观流速对弹状流流体力学性质的影响。在亲水微通道中观测到了泡状流、泡状-弹状流、弹状流;在疏水微通道中观测到了非对称弹状流、拉长的非对称弹状流、分层流。实验表明亲水微通道中弹状流区域下气泡长度大体上随气相表观流速的增大而增大,随液相表观流速的增大而减小;液弹长度大体上随气相表观流速的增大而减小,随液相表观流速的增大先增大后减小;液侧体积传质系数k_La均随气、液相表观流速的增大而增大,随通道壁面润湿性的增强而增大。     

微通道气液两相流型及界面面积测定

以氢氧化钠水溶液及纯二氧化碳气体为工质,研究了石英玻璃微通道中的气液两相流流型及两相界面面积.实验中可清晰分辨的流型为弹状流(Slug),弹状-环状流(Slug-annular)及搅拌流(Churn),由实验观测的结果建立了相应的流型图并与Triplett实验结果进行了比较,结果表明高液相表观流速对流型转换影响较大.在微通道中可以实现比较高的气液两相界面面积,实验范围内气液两相界面面积高达5 070 m2/m3.两相界面面积随气相表观流速的增加而增加,而液相表观流速对两相界面面积的影响则不显著.相对于弹状流区域,在弹状-环状流及搅拌流区域可以实现比较高的传质界面面积.搅拌流区域气液两相界面面积可以采用气液表观雷诺数进行很好关联,其绝对平均偏差仅为3.76%.     

矩形截面螺旋管内气液两相流型转换数值模拟

采用CLSVOF(coupled level set and volume of fluid method)方法,以空气和水为介质对矩形截面螺旋管内气液两相流动进行数值模拟,气相折算速度U_G为0.1～2.5 m·s^-1,液相折算速度U_L为0.09～4.5 m·s^-1.研究螺旋直径、螺旋升角对流型转换边界的影响,并绘制了不同螺旋直径、不同螺旋升角下的流型图.数值结果表明,与传统VOF方法相比,CLSVOF可以得到更精确的相界面;随着螺旋升角的增加,塞状流向泡状流的转换边界向U_L减小的方向进行,但是幅度很小,塞状流向弹状流的转换边界向U_L减小的方向进行;随着螺旋直径的增加,塞状流向泡状流的转换边界向U_L减小的方向进行,塞状流向弹状流的转换边界向U_L减小、U_G增大的方向进行;与Murai流型图相比,流型转换边界有所差异.     

弹状流液弹区含气率分布的试验研究

采用光纤探针法和高速摄影法对垂直上升气液两相弹状流的液弹区含气率分布进行了试验研究,测试管径为15 mm。一种基于机器学习的图像处理技术用来识别气液两相界面,通过搭建气泡边界提取的神经网路系统,使用构建的气泡边界数据库对模型进行多次迭代训练,该方法可以有效地识别多种复杂类型的气泡边界。试验得到了弹状流液弹区的径向含气率分布曲线,结果表明,壁峰分布是液弹区含气率分布的主要形式,其中泰勒气泡的尾迹效应对分布形式有重要影响,尾迹的旋涡中心和含气率分布的峰值相对应。针对弹状流液弹区径向含气率分布的两个主要特征——中心局部含气率和壁峰位置,分别提出了相应的预测公式,且与本文的试验数据吻合良好。     

起伏振动垂直上升管气液两相流截面含气率分析与计算

起伏振动下气液两相流含气率的准确预测对漂浮核电站的安全稳定运行有重要意义。实验研究了不同振动和流动工况下垂直上升管气液两相流的含气率特性。结果表明,起伏振动对泡状流下的含气率影响比较明显,对弹状流、搅混流和环状流的影响较弱。整体来看,起伏振动导致泡状流的含气率增加,其他三种流型下的含气率减小。对静止管道内常用的含气率计算模型进行评价,发现现有含气率计算模型比较适用于起伏振动下含气率的计算,但对泡状流和弹状流下含气率的预测误差较大。考虑振动的影响,引入了液相Froude数,建立了考虑流型的含气率计算关系式,显著提高了起伏振动下含气率的预测准确度。     

Influence of impeller diameter on local gas dispersion properties in a sparged multi-impeller stirred tank☆

Vertical distributions of local void fraction and bubble size in alr–water dispersion system were measured with a dual conductivity probe in a fully baffled dished base stirred vessel with the diameter T of 0.48 m, holding 0.134 m3 liquid. The impel er combination with a six parabolic blade disk turbine below two down-pumping hy-drofoil propel ers, identified as PDT+2CBY, was used in this study. The effects of the impel er diameter D, rang-ing from 0.30T to 0.40T (corresponding to D/T from 0.30 to 0.40), on the local void fraction and bubble size were investigated by both experimental and CFD simulation methods. At low superficial gas velocity VS of 0.0077 m·s?1, there is no obvious difference in the local void fraction distribution for al systems with different D/T. However, at high superficial gas velocity, the system with a D/T of 0.30 leads to higher local void fraction than systems with other D/T. There is no significant variation in the axial distribution of the Sauter mean bubble size for al the systems with different D/T at the same gas superficial velocity. CFD simulation based on the two-fluid model along with the population balance model (PBM) was used to investigate the effect of the impel er diameter on the gas–liquid flows. The local void fraction predicted by the numerical simulation approach was in reasonable agreement with the experimental data.     

基于丝网探针的螺旋管内气液两相流气泡行为研究

核反应堆蒸汽发生器的传热面由螺旋管束组成。螺旋管的三维螺旋结构使得泡状流和塞状流等气液两相流中的气泡在重力、离心力和浮力等作用下在管道内部呈现不对称的相分布状态,两相滑移速度增大,显著影响换热性能并导致DNB型传热恶化难以预测。实验介质为空气-水,结合自主开发的电导式丝网探针技术并发展先进的数据后处理算法,实现了复杂流场的三维时空重构和离散气泡粒径的精细测量,获得了螺旋管内泡状流和塞状流的截面空泡分布规律。基于研究结果,可根据气泡分布规律对螺旋管道的几何结构进行调整以避免传热恶化,为螺旋管式蒸发器的安全设计提供了基础数据和优化思路。     

基于丝网探针的螺旋管内气液两相流气泡行为研究

核反应堆蒸汽发生器的传热面由螺旋管束组成。螺旋管的三维螺旋结构使得泡状流和塞状流等气液两相流中的气泡在重力、离心力和浮力等作用下在管道内部呈现不对称的相分布状态,两相滑移速度增大,显著影响换热性能并导致DNB型传热恶化难以预测。实验介质为空气-水,结合自主开发的电导式丝网探针技术并发展先进的数据后处理算法,实现了复杂流场的三维时空重构和离散气泡粒径的精细测量,获得了螺旋管内泡状流和塞状流的截面空泡分布规律。基于研究结果,可根据气泡分布规律对螺旋管道的几何结构进行调整以避免传热恶化,为螺旋管式蒸发器的安全设计提供了基础数据和优化思路。     

垂直管内气液两相弹状流含气率研究

In order to investigate the influence of the entrance effect on the spatial distribution of phases, the experiments on gas-liquid two-phase slug flow in a vertical pipe of 0.03m ID were carried out by using optical probes and an EKTAPRO 1000 high speed motion analyzer. It demonstrates that the radial profile of slug flow void fraction is parabolic. Influenced by the falling liquid film, the radial profile curve of liquid slug void fraction in the wake region is also parabolic. Since fully turbulent velocity distribution is built up in the developed region,the void fraction profile in this region is the saddle type. At given superficial liquid velocity, the liquid slug void fraction increases with gas velocity. The radial profiles of liquid slug void fraction at different axial locations are all saddle curves, but void fraction is obviously high around the centerline in the entrance region. The nearer the measuring station is from the entrance, the farther the peak location is away from the wall.     

Bubble flow in trickle beds: investigations using resistive sensors

The local hydrodynamics of co-current gas-liquid down-flow through porous media are investigated in a quasi two-dimensional regular arrangement by means of a network of resistive sensors. The investigations are focused on a liquid continuous flow regime, the dispersed bubble flow, where the gas is divided into elongated bubbles. Due to the variation of the local flow channel orientation and the local void fraction, the average bubble velocity strongly depends on the local geometry. The flow is more coherent in vertical constrictions, compared to all other types of sites, this is probably due to bubble stagnation in the flow channel enlargements. At a given liquid superficial velocities and for sufficiently high superficial gas velocities, the average bubble size is independent of the gas flow rate; it is of the order of magnitude of the volume of the enlargements of the porous medium. The maximum bubble size is about three times its average size, corresponding thus to the coalescence of three average sized bubbles.     

泡罩塔板上气液两相局部统计特性实验测定

以空气、水为工质,用双头电导探针研究了泡罩塔板上局部气液接触情况,得到了泡罩塔内距离塔板高度49mm截面上气液两相局部参数——气含率、气泡速度、比表面积及气泡尺寸的统计规律。结果表明,在泡罩塔板上,同一位置的局部气含率随气量的增加而增大,受液量的影响较小;气泡速度主要分布为0．4～o．6m／s;气液比表面积的值85％在50～200m^-1,但在截面上分布不均匀;气泡Sauter直径为0～40mm,55％分布在5～25mm。     

An experimental study of gas void fraction in dilute alcohol solutions in annular gap bubble columns using a four-point conductivity probe

The influence of alcohol concentration on the gas void fraction in open tube and annular gap bubble columns has been investigated using a vertical column with an internal diameter of 0.102 m, containing a range of concentric inner tubes, which formed an annular gap; the inner tubes had diameter ratios from 0.25 to 0.69. Gas (air) superficial velocities in the range 0.014–0.200 m/s were investigated. Tap water and aqueous solutions of ethanol and isopropanol, with concentrations in the range 8–300 ppm by mass, were used as the working liquids. Radial profiles of the local void fraction were obtained using a four-point conductivity probe and were cross-sectionally averaged to give mean values that were within 12% of the volume-averaged gas void fractions obtained from changes in the aerated level. The presence of alcohol inhibited the coalescence between the bubbles and consequently increased the mean gas void fraction at a given gas superficial velocity in both the open tube and the annular gap bubble columns. This effect also extended the range of homogeneous bubbly flow and delayed the transition to heterogeneous flow. Moreover, isopropanol results gave slightly higher mean void fractions compared to those for ethanol at the same mass fraction, due to their increased carbon chain length. It was shown that the void fraction profiles in the annular gap bubble column were far from uniform, leading to lower mean void fractions than were obtained in an open tube for the same gas superficial velocity and liquid composition.     

常温及热态通气条件下多层桨三相搅拌反应器中局部气含率分布

Vertical distributions of void fraction in gas-liquid and gas-liquid-solid stirred tanks have been measured in a fully baffled dished base vessel of 0.48 m diameter, using a conductivity probe. The impeller configuration (a hollow half elliptical blade dispersing turbine below two up-pumping wide blade hydrofoils, identified as HEDT+2WHU) recommended in previous work has been used in this work. The operating temperatures were 24°C and 81°C, identified as cold and hot respectively. The effects of superficial gas velocity, agitator speed and the corresponding power input on the local void fraction in two-phase systems are investigated and discussed. Results show that the increasing of agitator speed or gas flow rate leads to an increase in local void fraction at the majority of measurement points in both cold and hot systems. However, the uniformity of gas dispersion does not always increase as the rais-ing of agitator speed and power input. In either cold or hot sparged conditions, the two- and three-phase systems have similar vertical profiles for void fraction, with maxima in similar locations; however, the void fractions are significantly lower in hot sparging than with cold. In cold operation the presence of particles leads to a lower void fraction at most points, although the local void fractions increase a little with the addition of solid particles at high temperature, in good agreement with the global gas holdup results, and the possible reasons are discussed in this paper. This work can give a better understanding of the differences between cold-gassed and hot-sparged three phase stirred tanks.     

气升式外环流反应器流体力学参数的轴径向分布

在气升式外环流反应器（Φ 0.09 m×1.8 m）内,利用压差法和双探针电导探头技术考察了不同表观气速下空气-水两相体系中气含率及气泡参数随轴径向位置的变化规律,测得了平均及局部气含率、气泡尺寸及分布、气泡上升速度、气泡频率以及气液相界面积,并从气液流场特征及气泡间相互作用等方面对实验结果作出分析。基于实验数据拟合出局部气含率随表观气速和轴径向位置的关联式。