多喷嘴射流式分离器内气固流动特性的数值模拟

基于商用软件Fluent 6.3.26,采用雷诺应力模型及DPM离散相模型并结合理论分析,对基于喷嘴造旋的射流式分离器内两相流动特性进行了模拟计算,得到了较为全面的两相流动规律与细节.结果显示,分离器内部切向速度峰值可达160 m·s^-1,自由涡区的切向速度约为130 m·s^-1,旋流强度明显高于传统旋风单管;沿轴向下,下行流流量逐次减少,其中稳流体顶部下行流降低最为明显,下行流减少致使颗粒卷入内旋流概率增加,分离效果下降;分离器内部局部存在顶部贴壁射流、射流区二次流及灰斗口旋涡流等次级流动;分离器压降约为27.43 kPa,喷嘴区内外旋流能耗分别为4.57 kPa(21.8%)、5.76 kPa(27.6%),稳流体区内外旋流能耗分别为5.85 kPa(27.6%)、4.01 kPa(18.9%);分离器对应的切割粒径较小,约为1.6 μm,极限粒径约为10 μm,符合工业应用要求;基于所建颗粒受力模型及模拟条件下,分离空间可分离的临界粒径为1～2 μm,3 μm及以上颗粒的逃逸浓度小于 0.15 g·m^-3,满足下游烟机对气流的净化要求.     

旋流数为1.0的强旋湍流两相流动的PDPA实验

采用相位多普勒颗粒测速仪 (PDPA)对旋流数为 1 0的轴向和切向进风的圆柱形旋风筒内强旋湍流气粒两相流动进行了测量研究 ,并与旋流数为 0 47、 1 5和 2 0 8的实验结果进行了对比分析 ,指出了旋流数变化对两相流场及两相湍流特性的影响 .     

新型旋风分级器流场特性及颗粒分级性能

针对传统旋风分级器分级效率较低的难题,本文设计了一种中部进风、顶部重力进料式新型旋风分级器,利用数值模拟和试验手段对其流场特征及分级性能进行了研究。模拟结果表明,新型旋风分级器内存在若干旋涡,主气流进入分级器后形成由上、下两个旋涡构成的主分级流场,上部旋涡均为上行气流,下部旋涡为切流返转形式;二次气流形成的细颗粒淘洗旋涡具有近壁面处高转速、中心区快速上升的特点,最大轴向速度达16.5m/s,可强化对边壁处浓集颗粒的剪切分散和淘洗作用,对主分级流场切向速度影响较小,但可使其轴向速度值最大增加100%,这将缩短细颗粒的停留时间;主分级流场与淘洗流场相互作用形成分区流动,具有较明显的动态边界,为粗、细颗粒的定向分离提供了力场基础。试验表明,二次气量占比约20%,主、二次气流气速分别为14m/s和20m/s时,牛顿分级效率可达88%,分级精度指数K值最小为1.84,此时新型旋风分级器具有较高的分级精度。     

旋风管分离器流场模拟研究

旋风管作为多管式旋风分离器的主要元件,已经成为气固两相分离的重要研究对象,主要用于处理气量较大且对分离效率要求较高的工况。本文采用大涡模拟的方法考察了分离器内切向与轴向速度分布形态的影响。模拟结果表明：在一定程度上加长排气管的插入深度对分离效率的提升是有益的;旋风管筒体太长对分离效率的提高作用不大;增大排气管直径有助于降低降压。     

Optimizing swirl in compact uniflow cyclones

This paper presents an experimental examination of the velocity field distribution in the separation chamber of a uniflow cyclone with closed particle outlet to evaluate the swirl characteristics in the vortex finder region based on stereoscopic particle image velocimetry. A cold flow model with a closed particle outlet was used to assess different angles of attack and core size ratios at typical Reynolds numbers for the separation of low loaded gas-solid flows. The focus of the study was on the relationship between swirl strength as well as performance data. At higher angles, the parabolic swirl strength distribution changed to a region with constant high acceleration of the particles in the separation zone. Integral and differential swirl numbers were correlated with the ratio of tangential to radial velocity and to the calculated cut size diameter. At low angles of attack, implying a strong redirection of flow perpendicular toward the main flow direction and small core size ratios, defined by the radial distance between hub and tip, the local differential swirl number can be more than twice as large as in the base configuration. Yet, the integral swirl number hardly changed. The velocity fields showed mean tangential to radial velocity ratios ranging from 0.73 to 6.85 at swirl vane angles of 15 ^° –60 ^° ; core size ratios between 0.125 and 0.625 at vortex finder diameter were measured and calculated cut size diameters between 10 and 90 μm were derived. This data provides the foundation for further validation studies and the development of new design criteria. © 2018 American Institute of Chemical Engineers AIChE J, 65: 766–776, 2019     

新型气液逆流撞击洗涤喷嘴的优化

针对一种新型气液逆流撞击式洗涤喷嘴,通过冷模实验,采用溶氧法考察了不同结构喷嘴的气液两相传质性能。结合解析率及流型变化,考察了喷嘴出口直径、切向进液口倾角、旋流室收敛段锥角、切向进液口直径、喷口长度5个参数对传质的影响,确定了优选喷嘴的结构尺寸,分析了该优选喷嘴在不同操作条件下(气速、表观液气比和轴切比)的传质效果。结果表明,优选喷嘴在轴切比为0.4~0.6且气速较高时传质效果较好。     

蜗壳式旋风分离器内气相流场非轴对称特性分析

采用Fluent软件对蜗壳式旋风分离器内气相流场进行了数值模拟,并在此基础上对流场的非轴对称特性进行了机理分析。蜗壳式旋风分离器入口结构的非轴对称以及气相旋流的不稳定性造成了气流的旋转中心与旋风分离器的几何中心不重合,从而导致了气相流场三维速度的非轴对称分布以及速度分量由于基准不同而产生的大小和方向变化。环形空间流场的非轴对称性主要是非轴对称入口结构影响的结果,分离空间流场的非轴对称性主要是旋流的不稳定性造成的。根据Rayleigh准则,旋风分离器内旋流流场的不稳定性是固有的,提高流场的旋流数可使流场的不稳定性降低,流场的非轴对称性降低。入口速度的变化不影响旋流数,也不影响流场的非轴对称性,但增加入口截面积比或减小量纲1升气管内径均可提高流场的旋流数,使流场的非轴对称性降低。旋风分离器的非轴对称性可以用角动量参量来描述。     

Study of the influence of vane angle on flow, gas species, temperature, and char burnout in a 200 MWe lignite-fired boiler

We measured various operational parameters of a 200-MW_e, wall-fired, lignite utility boiler under various outer secondary air vane angles. The parameters measured were gas temperature, gas species concentrations, char burnout, and component release rates (C, H and N). Cold air experiments of a single burner were conducted in the laboratory. A double swirl flow pulverized-coal burner has a single ring recirculation zone that forms in the secondary air region in the burner. By decreasing vane angles, maximum values of radial velocity, tangential velocity and turbulence intensity all increase. Moreover, swirl intensity of air flow and recirculation zone size increase. Concomitantly, in the central region of the burner, decreasing the vane angles of outer secondary air increases gas temperatures, CO concentrations, char burnout and component release rates of C, H, and N, while O₂ and NO_x concentrations decrease, and an early ignition of pulverized-coal occurs. Meanwhile, in the secondary air region of the burner, conditions are similar except that NO_x mean concentrations are reversed showing instead an increase. In the side wall region, gas temperatures increase, O₂ and NO_x concentrations decrease, but CO concentrations vary only slightly.     

催化裂化再生器树枝状气体分布器喷嘴的射流特性

在催化裂化装置中再生器底部通常设置有树枝状管式气体分布器,通过分布器上的喷嘴分布气体。但在实际运行过程中喷嘴常出现布气不均和磨损问题,影响其自身的布气性能和使用寿命。为此,在二维床实验装置上针对喷嘴的射流特性进行了实验研究。实验物料为FCC催化剂颗粒,喷嘴出口气速范围为30～70 m·s^-1,喷嘴喷射角度范围为0°～67.5°。实验用摄影观察法测量喷嘴射流的射流长度和附近的流场流态。实验结果表明射流长度随喷嘴气速和喷射角度的增大而变长。射流气体在向上翻转过程中,在树枝状管式气体分布器两分支管之间产生旋转涡流现象,旋转涡流的大小与喷嘴出口气速和安装角度有密切关系。最后基于实验数据,建立了喷嘴射流长度的计算模型。     

A heat transfer relation for swirl flow in a vortex tube

An experimental investigation was made to study the heat transfer behavior of a water-cooled vortex tube with air as the working medium. The vortex flow was generated by leading the compressed air to enter the vortex tube tangentially. The pressures of the inlet air were 300 to 500 kPa gauge. For each of these inlet pressures, the heat transfer performance of the vortex tube was studied at different cold mass flow ratios. New experimental data are presented. An empirical correlation for the prediction of the air-side Nusselt number is established. It was shown that the air-side Nusselt number for the swirl flow in this vortex tube can be up to 30 times higher than that for a flow without swirl in the same tube.     

不同旋流数下湍流气粒两相流动特性的PDPA实验研究

利用相位多普勒仪 (PDPA)系统研究了不同旋流数下突扩旋风筒内气粒两相湍流特性的变化规律 .在相同的进口形状和总风量的条件下 ,分别测量了旋流数为 0、 0 .5和 1.0时气相和颗粒相的轴向、切向的平均速度和脉动速度 .结果表明 :旋流数的变化对轴向速度的分布和切向速度的似固核 -位涡结构 ,以及两相脉动速度和两相湍流各向异性都有比较明显的规律性影响 ;总体上 ,旋流对两相湍流起抑制作用 ,但随旋流数的增大 ,两相湍流脉动及其各向异性都有先减弱 ,后来又有所增大的趋势     

旋风分离器内气相旋转流不稳定性的实验研究

旋风分离器内气相旋转流具有较强的不稳定性,其表现形式是旋转流的旋转中心围绕几何中心的偏心摆动,导致流场的瞬时速度随时间发生脉动变化。这种旋流的不稳定特性难以用时均流场参数进行描述,需要用动态流场参数描述,为此采用热线风速仪测量了?300 mm旋风分离器内瞬时切向速度随时间的变化。实验结果表明瞬时切向速度是由气体湍流形成的高频脉动和旋转流偏心摆动形成的低频脉动两部分叠加构成,据此探讨了旋转流摆动形成的机制。瞬时切向速度的低频脉动来源于刚性涡的偏心摆动,脉动幅值与偏心距成正比。通过瞬时切向速度频域建立了旋转流的摆动频率与入口速度、筒体直径和排气管直径的计算模型。     

旋风分离器内气相旋转流不稳定性的实验研究

旋风分离器内气相旋转流具有较强的不稳定性,其表现形式是旋转流的旋转中心围绕几何中心的偏心摆动,导致流场的瞬时速度随时间发生脉动变化。这种旋流的不稳定特性难以用时均流场参数进行描述,需要用动态流场参数描述,为此采用热线风速仪测量了?300 mm旋风分离器内瞬时切向速度随时间的变化。实验结果表明瞬时切向速度是由气体湍流形成的高频脉动和旋转流偏心摆动形成的低频脉动两部分叠加构成,据此探讨了旋转流摆动形成的机制。瞬时切向速度的低频脉动来源于刚性涡的偏心摆动,脉动幅值与偏心距成正比。通过瞬时切向速度频域建立了旋转流的摆动频率与入口速度、筒体直径和排气管直径的计算模型。     

Theoretical and experimental studies of confined vortex flow

A study of the air flow characteristics is reported for a vortex chamber 122 cm in diameter consisting of an upper cylindrical section 61 cm high and of a lower conical section 108 cm high. Measurements were made with a five-channel pressure probe of the radial profiles of tangential and axial velocities, with varying inlet air velocity and axial distance from the top of the chamber. Measurements of the static pressure profiles were made simultaneously. Finally, the angle of flow of the air entering through the single tangential inlet could be adjusted, and its effects on the flow recorded. From these results and from a theoretical analysis, generalized expressions for the tangential velocity profiles were obtained for the two regions of flow, forced-vortex and quasi-free vortex, which prevail in a confined vortex chamber, as a function of the entrance air velocity and of the radius at the point considered only. The angle of entering air was found to have no effect on the tangential velocity and only a minor effect on the static pressure distribution. The outlet diameter of the chamber was found to have a large effect on the profile of the axial velocities, reflecting the influence of the chamber static pressure on the latter.     

Theoretical and experimental studies of confined vortex flow

A study of the air flow characteristics is reported for a vortex chamber 122 cm in diameter consisting of an upper cylindrical section 61 cm high and of a lower conical section 108 cm high. Measurements were made with a five-channel pressure probe of the radial profiles of tangential and axial velocities, with varying inlet air velocity and axial distance from the top of the chamber. Measurements of the static pressure profiles were made simultaneously. Finally, the angle of flow of the air entering through the single tangential inlet could be adjusted, and its effects on the flow recorded. From these results and from a theoretical analysis, generalized expressions for the tangential velocity profiles were obtained for the two regions of flow, forced-vortex and quasi-free vortex, which prevail in a confined vortex chamber, as a function of the entrance air velocity and of the radius at the point considered only. The angle of entering air was found to have no effect on the tangential velocity and only a minor effect on the static pressure distribution. The outlet diameter of the chamber was found to have a large effect on the profile of the axial velocities, reflecting the influence of the chamber static pressure on the later.     

分级进风燃烧室内旋流反应流的湍流特性

This paper presents an experimental investigation of the turbulent reacting flow in a swirl combustor with staged air injection. The air injected into the combustor is composed of the primary swirling jet and the secondary non-swirling jet. A three dimension-laser particle dynamic analyzer （PDA） was employed to measure the instantaneous gas velocity. The probability density functions （PDF） for the instantaneous gas axial and tangential velocities at each measuring location, as well as the radial profiles of the root mean square of fluctuating gas axial and tangential velocities and the second-order moment for the fluctuating gas axial and tangential velocities are obtained. The measured results delineate the turbulence properties of the swirling reacting flow under the conditions of staged combustion.     

Measurements of flow characteristics in a confined vortex flow

A study of air flow patterns by hot-wire anemometry is reported for a vortex chamber consisting of an upper cylindrical section 122 cm in diameter and 61 cm high and a conical bottom section 122 cm high. Quantitative data are presented for flow angles, profiles of mean tangential and axial velocities, and radial distributions of tangential and axial intensities of turbulence as a function of air entrance velocities of 1.6, 2.4 and 3.2 m/s, and axial distance from the top of the chamber. In general, the quantitative results confirm the theoretical predictions and the experimental trends reported in the literature. In particular, they fully support the conclusion that the flow pattern is relatively insensitive to the entrance volumetric flow rate. A generalized correlation is presented for the axial velocity distribution. Preliminary correlations are also presented for the tangential velocity distributions in the core and in the annular region of the vortex near the wall. These were found to be functions of the axial location and of the air entrance velocity.     

基于临界分流理论的气液两相流均匀分配器

提出了一种新型气液两相流分配器,主要由旋流叶片、整流器、分流喷嘴以及分配腔室组成。通过采用“流型调整”与“临界分流”控制相分离。为研究不同分流比下的分配特征,设计了2喷嘴和4喷嘴两种分配结构。建立了气液两相流数值模型,模拟了气液两相流在分配器内流动特性。在气液两相流实验环道上进行了测试,气相折算速度范围为5.0～25.0 m·s^-1,液相折算速度范围为0.012～0.14 m·s^-1,实验中出现的流型包括波浪流、段塞流以及环状流。结果表明,在临界分流条件下,气液相分流系数主要取决于与侧支管相连通的分流喷嘴数目与总喷嘴数目的比值,不受流型、气液流速等参数波动的影响。对于2喷嘴分配器分流系数接近理论值0.5,对于4喷嘴气液分流系数约为0.25。     

蜗壳式旋风分离器全空间三维时均流场的结构

采用激光多普勒测速系统（LDV）对蜗壳式旋风分离器全空间内三维湍流的时均流场进行了实验测定与分析,重点讨论了灰斗、环形空间和排气管的流场特点.分离空间内时均流场是外侧准自由涡与内侧准强制涡的典型结构.环形空间的入口部位有多个纵向二次涡,其他大部分空间顶部出现纵向二次环流,切向速度和径向速度的分布呈现非轴对称性,入口气量沿高度分布不均匀.灰斗的顶部也存在纵向二次环流.排气管内轴向速度分布与分离空间内的分布形态迥异.     

直切式旋风分离器内气相流场的实验研究和数值分析

采用实验测量与数值模拟相结合的方法对直切式旋风分离器内气相流动的三维流场进行了研究。雷诺应力湍流模型对流场的计算与五孔球探针的测量结果基本相符。实验测量与数值模拟的研究结果表明,环形空间的流场呈现明显的非轴对称性,切向速度在0°方位最大,在300°方位最小;分离空间基本呈轴对称性,流场稳定,有利于颗粒分离;排气管内仍存在较强的旋转,产生较大的能耗。