STUDY OF HYDRODYNAMICS FEATURES IN THE APPARATUSES WITH MOVABLE NOZZLE


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Apparatuses for the heat and mass transfer processes must be designed so that they have a maximum contact sur- face. Classification of heat-mass exchange apparatuses provides geometric features of the apparatus and the hydrodynamic condition they create. However, the main trend which remains dominant in the design of such apparatus is to create a thin film of liquid on the surface of the nozzle. The work was aimed at choosing the solution in which the MN of the heat-mass exchange apparatuses can be used to implement the contact handling process of gases and liquids with density values clarification of the nozzle elements (ρnе) and the column dynamic height (Нст) and obtain the specified calculated dependences which describe the hydrody- namics and mass transfer in the apparatuses with a movable nozzle, that is to create bases for engineering calculations. Research methods were theoretical study and experimental studies on heat and mass transfer devices with movable nozzle. The best ranger for mass transfer processes implementation is that of ρneІІ (ρ = 200-700 kg/m3), which is distin- guished by a wide working area according to wg, acceptable values of fluid withdrawal and a relatively small dynamic layer height. Within the described mode, we can distinguish the area wg @ 4.7-6.0 m/s, where there is no dependence of Hp on wg. Specified calculated dependence obtained which describes the hydrodynamics and heat and mass transfer in the apparatuses with a movable nozzle.

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Introduction. The defining feature of heat and mass transfer processes, which occurs in the three-phase flows, is the interaction phase, which determines the value of the interfacial surface. Therefore, apparatuses for the heat and mass transfer processes must be designed so that they have a maximum contact surface. Classification of heat- mass exchange apparatuses (HMEA) provides geometric features of the apparatus and the hydrodynamic condition they create. However, the main trend which remains domi- nant in the design of such apparatus is to create a thin film of liquid on the surface of the nozzle. Apparatuses with a movable nozzle (AMN) were developed in relation to the implementation process of dedusting and degassing and absorption in a number of countries: Canada, the USA, Germany, Japan, CIS- countries [1; 2]. AMN advantages over other types of contact devices, which determined their widespread occurrence: steady operation in the polluted environments of self-cleaning nozzle surfaces and walls of casing, low sensitivity of the device characteristics to sudden load fluctuations of gas and liquid; indiscriminateness to the initial liquid distribution, which is important for industrial AMN; high lateral uniformity simplifying scalability; a wide range of workload (in [3-7] a value ql up to 200 m3/(m2×h is reported) and wg up to 8 m/s at an empty AMN intersection); high intensity of exchange processes in the layer; constructive design simplicity; compactness; low weight and cost of the nozzle. So far published information about the interaction of the three phases in the HMEA varies by the difference in the representation quality and experimental data discrepancies in all major aspects of the movable layers behaviour, so that its practical use in the engineering cal- culations is complicated. The study of the quite complex “gas-liquid-solid” system behaviour remains largely ex- perimental. Prospects of AMN use for evaporative water cooling require special consideration. AMN is ad- visable to apply for the organization of such mass transfer processes in which the main resistance of mass transfer is focused in the gas phase, typical for the process of evaporation cooling in the cooling towers [4]. Therefore, the work was aimed at choosing the solution in which the MN of the HMEA can be used to implement the contact handling process of gases and liquids with density values clarification of the nozzle elements (ρne) and the column dynamic height (Нdh) and obtain the specified calculated dependences which describe the hy- drodynamics and mass transfer in AMN, that is to create bases for engineering calculations [8-12]. Studying of evaporative water cooling processes was carried. Studying of evaporative water cooling proc- esses was carried on a laboratory model using different nozzle elements (see table). From a scientific and practical point of view, the issue concerning the nature of the transit of nozzle layer from a stationary to a moving condition seems important. The issue is complex and poorly studied. Typical modes of movable nozzles (MN) behaviour in the apparatuses are shown in fig. 1. Fixed layer porosity does not depend on the load of the gas and the liquid. Traditionally, the critical transition velocity (w0, w0') is determined by visual pseudo- fluidization curve analysis that is described by the dependence D р = (wg, ql). We conducted its specification by constructing selective Lа (wg, ql) under the following conditions: Нdh = 0,1 m, dne = 0,04 m, ρ = 300 kg/m3, ql = 15 m3/(m2h) (fig. 2). Studied nozzle elements characteristics № NE type Nozzle material Geometry rne, kg/m3 Note dne, mm 1 dne Foamed polypropylene 40.1 248 Commercialization of elements 2 40.3 305 3 36.6 335 4 35.6 367 5 dne Empty celluloid ball which is partly filled with water 37.1 100-1000 in increments of 100 units Size rne for the empty element 91 kg/m3 Подпись: НhdПодпись: НhdПодпись: НhdFig. 1. Typical AMN modes: a - stationary; b - stationary nozzle flooding; c - initial pseudo-fluidization; d - developed pseudo-fluidization Рис. 1. Характерные режимы АПН: а - стационарный; б - захлебывание стационарной насадки; в - начальное псевдоожижение; г - развитое псевдоожижение Speed wg is given to the empty column crossing; fixed (1, a) and initially compacted layer of nozzle elements (1, b) having the ability to expand is considered. Value wg *: wотр - the maximum speed at which the curves coincide Δp for fixed and movable layers; wз - the beginning of stationary nozzle flooding; wo, wo' - the beginning of pseudo-fluidization; w1 - the beginning of active pseudo- fluidization; wi - inversion beginning. Let us specify some definitions through the variety of existing formula- We found that the elements with ρne < 200 kg/m3 transferred to a moving state, bypassing flooding in a sta- tionary state, for ρne > 200 kg/m3 pseudo-fluidization is carried out in pseudo-stationary flooding condition of the extending layer; for ρne > 700 kg/m3 this pattern per- sists for larger values of Hp, and the part of liquid is taken outside of the layer and placed on top of its upper limit as the layer of foam with thickness Hn over 0.02 meters. Gas and liquid layer load effecting movable nozzles tions for w *: w corresponds to the intensive growth Δp, retaining ability Н = 0.1 m is shown in fig. 3. g з dh Подпись: Нпlayer turbidity, foam formation atop of the layer (partially inverted cocurrent). For the fixed layer speed wз is un- changed for specific loadings; for an extending layer wз depends on the porosity and cannot be described by the known dependencies; wo is the minimum gas velocity at which steady vertical oscillations of several adjacent NE are observed; w1 corresponds to the active movement and mixing of NE; wi is the beginning of NE inversion - their concentration near restrictive gates. The latter mode is almost immediately transformed into “upper” NE flooding, which is typical for the fixed layer (fig. 1, b). Value wo' is clearly recorded on vibrocurve La (wg) as a leap ( @ 20 dB or 30 %) and mild stated on fluidization curve (column walls vibroacceleration is defined by the movable nozzles state). Almost constant vibroacceleration level (La = 5.5 wg 0,08 ) corresponds to the stationary layer state. The NE transition to movable state was much more difficult, as compared to the traditional presentation. If wg @ wo' then the described unstable pseudo-stationary NE states are formed during periodic movement of an individual NE (layer alteration with changing porosity) at a constant load. Their duration ranges from tens of seconds to several minutes. The layer structure is changing and fluid retention therein varies, i. e. the wo' value is characterized by a certain range of existence. The width of this range depends on the initial layer density which is determined by NE own weight and the action of external loads and vibrations. For example, for NE with ρne = 300 kg/m3 and dne = 0,037 m, this value is 0.4 m/s. The best range to implement mass transfer processes seems to be that of ρneІІ (ρne = 200-700 kg/m3). Partial fixed layer flooding precedes the beginning of pseudo- fluidization; the nature of the transition determines the entire future behaviour of the system. The speed of the apparatus starting to flood w3 is quite high (≈ 6 m/s); liq- uid withdrawal DGl from the working area is slow until the speed value is w3. This range differs by a wide work area of speed wg, acceptable values of fluid withdrawal DGl and a relatively small dynamic height of the layer Hl. Regarding this area let us consider the characteristic pseudo-fluidization modes: 1. 0 < wg £ 2.0 m/s - Stationary system state with characteristic local restructuring of fixed layer structure and some porosity growth. Linear growth Hl (wg) until the beginning of the pseudo-fluidization speed w0' with the progressive flooding of the fixed reconstructed layer. 2. 2.0 < wg £ 2.5 m/s - Initial pseudo-fluidization mode (transitional mode). There is a characteristic peak Hp by the speed of gas w0' (fig. 3, a) with the consequent restoration to the previous value; the system is unstable, the part of the layer remains stationary and its periodic restructuring occurs. Fluid retention for ql < 5 m3/ (m2×h) (fig. 3, b) in active pseudo-fluidization mode decreases to values which are characteristic of the stationary layer. l This is a border q* for cooling towers with movable nozzle (CTMN) related to layer drainage; here CTMN operation is not feasible, despite the liquid being in the layer for a long time. 3. 2.5 < wg £ 6.0 m/s - Developed pseudo-fluidization mode. The entire nozzle layer is movable, the system is homogeneous. Comparison of system characteristics with the similar mode for the zone ρneІ shows that the new transition patterns to mobility impacted the behaviour of the system as a whole: the initial flooding state is sup- ported. However, it does not further develop with the in- crease of wg to the developed flooding due to a mecha- nism that compensates the layer expansion. This kind of situation when the initial flooding supported in a wide range of wg, provides the possibility of stable AMN op- eration in the high loads mode. Within the described mode, we can distinguish the area wg @ 4.7-6.0 m/s, where there is no dependence of Hl on wg. This new area precedes a sharp increase of Hl. 4. 6.0 < wg £ 8.0 m/s. In fact, that is the previous mode with a sharp increase of flooding component. Con- La, dB 110 ventionally, it can be called a movable layer flooding mode, noting a significant difference from the same mode with a stationary nozzle. Whereas, under the latter condi- tions, the flooding mode means the practical impossibility of further employment, but concerning the apparatuses with a movable nozzle this possibility remains, due to the liquid capacity of the apparatus and very high intensity of the process. Processing of experimental information. The most important hydrodynamic characteristics of cooling towers with movable nozzle (CTMN), which are required for engineering calculations, are critical speeds (w0', w1), pressure loss in the working area ( D p), fluid retention (Hl) and dynamic layer height (HД). This information allows selecting the operating mode of heat-mass exchange apparatus (HMEA), calculating the height of the columns and fan power [13-15]. 90 70 50 Нl·102, m Fig. 2. Experimental dependences: 1 - pseudo-fluidization curve Dр = f (wg); 2 - vibrocurve La = f (wg) Рис. 2. Экспериментальные зависимости: 1 - кривая псевдоожижения Dр = f (wg); 2 - виброкривая La = f (wg) Нl,·102, m 3 2 6 4 4 2 2 1 2 4 6 a 0 wg, m/s 10 20 b 50 ql, m3/m2h Fig. 3. Dependence of retaining ability of the movable nozzle on gas and liquid loads at Нdh = 0.1 m: 1 - ρne = 100 kg/m3, 2 - ρne = 500 kg/m3; 3 - ρne = 800 kg/m3; a - Hl = F (wg); b - Hl = f (qg) Рис. 3. Зависимость удерживающей способности слоя подвижной насадки от нагрузок по газу и жидкости при Нdh = 0,1 м: 1 - ρne = 100 кг/м3; 2 - ρne = 500 кг/м3; 3 - ρne = 800 кг/м3; а - Нl = f(wg); б - Нl = f (qg) For non-irrigated layers the equation is obtained: It consists of a dynamic specific NE weight æ gM ne ö and w0dne Arg ç F H ÷ Re0 = n = , (1) è к d ø g where, in order to record the peculiarities of the compressure loss Δpd, that characterize the contribution to the general value of the detained fluid pressure loss and fric- tion due to the elements mixing in the pseudo-fluidized layer: pressed flow of balls with gas stream the stationary layer porosity is used. Equation (1) provides the calculation wo for the layer of balls with diameter of the nozzle elements Dр = Dрd Hd + gM ne , Fk dne = 35...42 mm and density ρen = 90...1000 kg/m3 for Hст > dne. Nozzle irrigation leads to a decrease Dрd = 0,8Н -0,65wg ´ hd ´ ехр(1,85 ×10-3r +1, 56 ×10-2 q + 2,86), (5) of w* (w '), and with the increase of ρ the w ' value ne l g o ne o decreases. With regard to the influence of ql and rне us write down: let where Мne - NE layer mass. The equation is adequate to the experimental data with an average relative error 0.11 and is fair in the ranges: ¢ 4320 ×r-1,21 ×w 0.05 £ Нdh £ 0.2 m; wo < wg £ 4.5 m/s; w0 = ne 0 . 4320r-1,21 + q (-1,25×10-4 rne +0,275) (2) 5 £ ql £ 25 m3/ (m2 × h); 200 £ ρne £ 1000 kg/m3. ne l This equation is fair for 200 £ ρ £ 1000 kg/m 3 and Increase of Нdh leads to the decrease of Dрd , which indine cates pseudo-fluidization quality deterioration. For the 5 £ ql £ 25 m3/(m2·h). For ρne <200 kg/m3 dependence of elements with ρ = 90 kg/m3 the Dр value does not w ' = F (ρ ) appears to be bigger. The w ne d value character- 0 ne 1 depend on w ; for w = w ' the smallest difference of Dр izes the transition to the developed pseudo-fluidization, i. e. to the uniformly pseudo-fluidized layer: g g o d occurs, which was obtained for different densities ρne. w1 = 1, 4 ×w¢0. (3) Heavier NE correspond to the greater value Dрd , which The width of the area of initial pseudo-fluidization sharply increases with ρne growth and the layers of nozzle elements (NE) with density ρne > 500 kg/m3 operate in practice only in this mode. Dynamic height is characterized by a mean value of oscillating movable nozzle (MN) level, and was deter- mined visually. In the stationary state, these oscillations are characterized by constant amplitude: Нd = Нhd + Нhd (wg - w¢0 )´ ´ éë16, 2 exp (-0, 002rne - 70dne ) + 0, 007ql ùû . (4) o ' 3 2 If wg = w ', then value Нd = Нdh. This formula pro- vides a calculation of Нd for dry layer of MN, as well; it is fair in the range of wg = wo - 4.5 m/s; ql £ 25 m /(m ·h); Нdh = 0.5-0.2 m; ρne = 90-1000 kg/m3, dne= 0,035-0,042 m. The gas stream pressure loss value Δp determines the capacity of the electric fan motor (excluding energy consumption for separation and loss in communication). æ Dр ö match physical presentations. For ql < 5 m3/(m2×h) the exponential nature of equation (5) is disturbed. Conclusion. The apparatuses with a movable nozzle are a promising solution of column HMEA, which en- ables operation in the extreme conditions (contaminated environment, sharp fluctuations of loads), increased limit loads, high lateral uniformity of fluid (scaling task simpli- fication), and lack of demands to the flow distribution quality. The best ranger for mass transfer processes implementation is that of ρneІІ (ρen = 200-700 kg/m3), which is distinguished by a wide working area according to wg, acceptable values of fluid withdrawal and a rela- tively small dynamic layer height. Necessary dependencies for engineering calculation were obtained, which determine the critical speed value (w0'), the pressure loss in the working area (Δр) and the dynamic NE layer height (Нд). It remains necessary to study the dynamics of gas- droplet flows in the system to provide for calculation of fluid distribution units, drop moisture separation, envi- ronmental emission and scattering therein, to consider the Traditionally the ratio ç è ÷ Н hd ø is used, but the main MN issues of the applied nature (scale factor, work in long-term inclines and tossing; the accumulation of impurities in the layer characteristic is its dynamic height Нdh. Complex æ Dр ö recirculation liquid, etc. An improved constructive design of devices with the movable nozzle shall be developed. Н ç ÷ è hd ø leads to a distortion of the physical scene, as, References for example, with ρne = 1000 kg/m3 this value exceeds 104 Pa/m. This maximum value corresponds to the weight of the fixed layer NE, where voids are completely filled with liquid. This should result in the inverted cocurrent if losses are greater than 10 Pa/m, which in practice is not observed even at wg > 8 m/s. So it is worthy using Н ç ÷ the specific dynamic pressure loss, i. e. the value æ Dр ö .
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作者简介

V. Danko

Plekhanov Russian University of Economics; Kuban State Technological University

Email: vladislav.danko@mail.ru
360, Severnaya Str., Krasnodar, 350002, Russian Federation; 2, Moskovskaya Str., Krasnodar, 350072, Russian Federation

V. Karnauh

Donetsk National University of Economy and Trade named after Mykhajlo Tugan-Baranovskogo

31, Schorsa Str., Donetsk, 83050

A. Titlov

Odessa National Academy of Food Technologies

112, Kanatnaya Str., Odessa, 65039, Ukraine

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