energies Article Spray Formation of a Liquid Carbon Dioxide-Water Mixture at Elevated Pressures Hakduck Kim, Changyeon Kim, Heechang Lim and Juhun Song * School of Mechanical Engineering, Pusan National University, Busan 46241, Korea; [email protected] (H.K.); [email protected] (C.K.); [email protected] (H.L.) * Correspondence: [email protected]; Tel.: +82-51-510-7330; Fax: +82-51-512-5236 Academic Editor: Mehrdad Massoudi Received: 6 September 2016; Accepted: 8 November 2016; Published: 14 November 2016 Abstract: Liquid carbon dioxide-assisted (LCO2 -assisted) atomization can be used in coal-water slurry gasification plants to prevent the agglomeration of coal particles. It is essential to understand the atomization behavior of the water-LCO2 mixture leaving the injector nozzle under various conditions, including the CO2 blending ratio, injection pressure, and chamber pressure. In this study, the flash-atomization behavior of a water-LCO2 mixture was evaluated with regard to the spray angle and penetration length during a throttling process. The injector nozzle was mounted downstream of a high-pressure spray-visualization system. Based on the results, the optimal condition for the effective transport of coal particles was proposed. Keywords: coal gasification; flash atomization; liquid carbon dioxide (LCO2 ); water-LCO2 mixture; solubility 1. Introduction Pressurized entrained flow gasification is a promising technology for the conversion of low-grade fuels to high-quality synthetic fuels, e.g., hydrogen and synthetic natural gas. High gasification efficiencies using liquid fuels or slurries can only be achieved through the generation of a fine homogenous spray at a high chamber pressure [1]. During coal-water slurry (CWS) gasification, there is a tendency for the coal particles to agglomerate within individual droplets while the water is evaporating; the agglomerates are then dried out and undergo thermal decomposition in the flame. The resulting coal-particle size distribution (p.s.d.) is determined to a greater degree by the size distribution of the atomized fuel spray than by the initial particle size of the coal. Large particles formed through agglomeration have increased burnout times and produce large fly ash particles [2]. A potential method for obtaining finer spray droplets is CO2 -assisted atomization. The effect of disruptive or flash atomization in reducing the p.s.d. of droplets was evaluated. The CO2 is dissolved into the fuel by injection into the line between the pump and the fuel nozzle. During the pressure release in the atomizing nozzle, the dissolved CO2 changes to the gaseous phase and disrupts the coal-water mixture droplets. Pure liquid CO2 (LCO2 ) has a different impact on the atomization at the injector nozzle when a LCO2 slurry is sprayed [3]. Compared with the conventional spray pattern of H2 O, LCO2 produces effective breakup, leading to smaller liquid droplets, because of its lower viscosity and higher momentum flux. This helps to transport coal particles more uniformly inside the gasifier. This feature of better dispersion is attractive because it requires less heat release from partial combustion and thus less oxygen supply to the coal gasifiers. However, the effect of the blending ratio of LCO2 in the water on the atomization behavior has not been examined. In a study on the spray formation of pure LCO2 [4], CO2 was expanded through a nozzle from a high pressure to an atmospheric pressure. The flash atomization and breakup mechanisms of LCO2 Energies 2016, 9, 948; doi:10.3390/en9110948 www.mdpi.com/journal/energies Energies 2016, 9, 948 2 of 11 were examined using different liquid contents controlled by the degree of superheat. Under certain conditions, the LCO2 experienced a sudden pressure drop below the saturation pressure. LCO2 with Energies 2016, 9, 948 2 of 11 different levels of superheat produced different behaviors of flashing sprays and snow-particle formation. Lee et al. found that sprays in flash-boiling conditions were atomized by bubble growth, were examined using different liquid contents controlled by the degree of superheat. Under certain resulting in a smaller droplet size than that generated by aerodynamic force alone [5]. Liu et al. used conditions, the LCO 2 experienced a sudden pressure drop below the saturation pressure. LCO2 with the laser-diffraction method to determine p.s.d. behaviors of the spray [6]. different levels of superheat produced the different of flashing sprays and snow-particle Engelmeier et al. [7] used a pure carbon dioxide jet for cutting applications where carbon dioxide formation. Lee et al. found that sprays in flash-boiling conditions were atomized by bubble growth, resulting inand a smaller droplet size than that generated aerodynamic forceis alone [5]. Liudownstream et al. used of is compressed expanded via a sapphire nozzle. Aby pressure chamber installed the laser-diffraction method to determine the p.s.d. of thethe spray [6]. the orifice to keep the post-expansion conditions above triple-point pressure of carbon dioxide. Engelmeier that et al. carbon [7] used dioxide a pure carbon dioxide jet for cutting where carbon dioxide They demonstrated has to be expanded to anapplications environment of increased pressure is compressed and expanded via a sapphire nozzle. A pressure chamber is installed downstream of and thus increase the liquid fraction to improve the impact of the jet. the orifice to keep the post-expansion conditions above the triple-point pressure of carbon dioxide. Reverchon et al. reported that the solubilization of amount of supercritical CO2 in liquid solution They demonstrated that carbon dioxide has to be expanded to an environment of increased pressure could produce various powders with controllable size and distributions that are useful in several and thus increase the liquid fraction to improve the impact of the jet. fine-particle production processes Supercriticalof dissolved-gas atomization is an solution atomization Reverchon et al. reported that[8]. the solubilization amount of supercritical CO2 in liquid process in which carbon dioxide at a temperature and pressure above its critical point is used as the could produce various powders with controllable size and distributions that are useful in several atomizing gas [9].production It relies onprocesses dissolved[8]. COSupercritical from water to form bubbles. Therefore, this fine-particle dissolved-gas atomization is an atomization 2 gas emerging process in which carbon a temperature and pressure above its criticalquantities point is used the technique applies only to a dioxide limitedatrange of liquids that can hold significant of as dissolved atomizing gas [9].mean It relies on dissolved CO2was gas emerging from water by to form bubbles. release Therefore, gas. As a result, the droplet diameter mainly influenced the sudden of this the CO2 techniquein applies only to a limited range of liquids that can hold significant quantities of dissolved gas dissolved the water. gas. As a result, the mean droplet diameter was mainly influenced by the sudden release of the CO2 In general, the dissolved gas at the exit orifice nucleates to form gas bubbles, as in effervescent gas dissolved in the water. atomization, and can rapidly evaporate by flashing as well [10]. The result shows that the mean droplet In general, the dissolved gas at the exit orifice nucleates to form gas bubbles, as in effervescent diameter is mainly influenced by the sudden release of the gas dissolved in the liquid. However, the atomization, and can rapidly evaporate by flashing as well [10]. The result shows that the mean behavior of the waterisspray altered by the of dissolved LCOdissolved 2 was not droplet diameter mainly influenced byatomization the sudden release of the gas in experimentally the liquid. evaluated in our That is, thealtered spray characteristics of the water-LCO 2 mixture However, theprevious behavior work. of the water spray by the atomization of dissolved LCO 2 was notmust be studied. experimentally evaluated in our previous work. That is, the spray characteristics of the water-LCO2 mixture must be studied. In this study, the spray patterns of a water-LCO2 mixture were examined during a throttling In this study, the a water-LCOof 2 mixture were examined during a throttling process. The injector nozzlespray was patterns mountedofdownstream a high-pressure flashing-spray system, while process. The injector nozzle was mounted downstream of a high-pressure flashing-spray system, the downstream pressure was controlled by a back-pressure regulator. A high-speed shadowgraph while the downstream pressure was controlled by a back-pressure regulator. A high-speed apparatus was used to evaluate the CO2 -assisted atomization process. shadowgraph apparatus was used to evaluate the CO2-assisted atomization process. 2. Experimental Setup 2. Experimental Setup Figure 1 presents a schematic of the high-pressure spray-visualization system used in this study. Figure 1 presents a schematic of the high-pressure spray-visualization system used in this study. It consisted of an chamber block,and and a downstream chamber (vessel). It consisted of upstream an upstream chamber(vessel), (vessel), aa middle middle block, a downstream chamber (vessel). ThereThere was was an optical quartz window on the middle block and the two chambers, enabling an optical quartz window on the middle block and the two chambers, enabling the the visualization of the behavior inside the nozzle andand at the of the The The window visualization offlashing-spray the flashing-spray behavior inside the nozzle at exit the exit of nozzle. the nozzle. ◦ window was designed to withstand at a peak temperature of 80 °C, and a was designed to withstand pressures uppressures to 100 barupattoa 100 peakbar temperature of 80 C, and a pressure-relief was installed to prevent pressure rises beyond this limit. valvepressure-relief was installedvalve to prevent pressure rises beyond this limit. Figure 1.1.Schematic experimentalsetup. setup. Figure Schematic of of experimental Energies 2016, 9, 948 Energies 2016, 9, 948 3 of 11 3 of 11 A A saturated saturated mixture mixture of of CO CO22 was wasachieved achievedby by adjusting adjusting the the temperature temperature and and mass mass of of solid solid CO CO22 (SCO (SCO22).).Different Differentchamber chambertemperatures temperatureswere wereachieved achievedwith withthe theuse useofofaaconstant-temperature constant-temperaturebath. bath. As shown in inFigure Figure1, 1, nozzle installed between the middle block the downstream As shown thethe nozzle waswas installed between the middle block and theand downstream chamber. chamber. was long 300 mm with an internal of 0.4 mm. Two different materials werefor used It was 300Itmm withlong an internal diameterdiameter of 0.4 mm. Two different materials were used the for the nozzles. Somemade were of made of transparent enabling the visualization thepattern flow pattern nozzles. Some were transparent Pyrex,Pyrex, enabling the visualization of the of flow inside inside the nozzle. This wasfor useful for examining either action capillary action or flash-boiling behavior.a the nozzle. This was useful examining either capillary or flash-boiling behavior. However, However, a copper was used for purposes other than internal visualization. A data-acquisition copper nozzle was nozzle used for purposes other than internal visualization. A data-acquisition system was system was utilized to monitor the temperature and pressure inside the chambers, and a flow utilized to monitor the temperature and pressure inside the chambers, and a flow controller unit was controller unitthe was usedon to and turnoff thepneumatically. valves on and off pneumatically. used to turn valves Water–LCO Water–LCO22 mixtures mixtureswith withdifferent different percentages percentages LCO LCO22were wereprepared prepared for for blending. blending. A Awater waterisis first filled in upper chamber upto the desired volume, which is determined by water blending ratio first filled in upper chamber upto the desired volume, which is determined by water blending ratio on on basis of volume. Then, a solid 2 is poured with desired volume percent. As a result, the CO 2 thethe basis of volume. Then, a solid COCO is poured with desired volume percent. As a result, the CO 2 2 in in liquid vapor phase is made with water as it reaches temperature at equilibrium. liquid andand vapor phase is made with water as it reaches ambientambient temperature at equilibrium. Before the Before test, isthe mixture is agitated stirringanunit. Therefore, an efficient, continuous test, thethe mixture agitated by stirring unit. by Therefore, efficient, continuous solubilization of CO2 solubilization of CO2 in liquidThe solution allowed. The liquid CO 2 exists as layer above the water in the liquid solution is the allowed. liquidisCO exists as layer above the water layer, indicating low 2 layer, indicating low miscibility of CO 2 with water. This separation is clearly observed in the inset of miscibility of CO2 with water. This separation is clearly observed in the inset of Figure 1. In addition, Figure In addition, droplets COwater. 2 are found in the During this process, neither1.droplets nor neither particles of CO2nor areparticles found inofthe During thiswater. process, the total volume the total volumeremained of the mixture remained constant. effect ratio of thewas blending ratio was investigated of the mixture constant. The effect of theThe blending investigated at two different at two different the upstream and downstream and 65/40gas bar. Nitrogen pressures of the pressures upstream of and downstream chambers: 85/60chambers: and 65/4085/60 bar. Nitrogen was used as gas waswhen used aaspressure a filler when a pressure beyond the saturation pressure was necessary. a filler increase beyondincrease the saturation pressure was necessary. Figure a schematic p-T p-T diagram of theof global multiphase behaviorbehavior of carbonofdioxideFigure22illustrates illustrates a schematic diagram the global multiphase carbon water between 273 and 310 K as can be determined from the literature data [11,12]. In the figure, dioxide-water between 273 and 310 K as can be determined from the literature data [11,12]. In the three-phase line connects all p, T coordinates where two liquid phases (aphases water-rich liquid L1 and a figure, three-phase line connects all p, T coordinates where two liquid (a water-rich liquid carbon dioxide-rich liquid L2) coexist with a carbon dioxide-rich vapor V. The pressure at L1L2V L1 and a carbon dioxide-rich liquid L2) coexist with a carbon dioxide-rich vapor V. The pressure at equilibrium is close to line, the liquid and vaporand curve of pure CO but always below the L1L2V equilibrium is two-phase close to two-phase line, the liquid vapor curve of2, pure CO2 , but always vapor pure CO Because this similarity of the three-phase line andline two-phase line at below pressure the vaporofpressure of2.pure CO2 .ofBecause of this similarity of the three-phase and two-phase ◦ tested ranges of pressure and temperature (25 °C), pressure release from 85 to 60 bar has higher line at tested ranges of pressure and temperature (25 C), pressure release from 85 to 60 bar has higher presence presence of of CO CO22-rich -richliquid(L2) liquid(L2)than thanCO CO22-rich -richvapor(V) vapor(V)since sinceititisislocated locatedwell wellover overthe the three-phase three-phase equilibrium line. In contrast, pressure release from 65 to 40 bar experiences a phase transition equilibrium line. In contrast, pressure release from 65 to 40 bar experiences a phase transition from from the the CO CO22-rich -rich liquid(L2) liquid(L2) to to the the CO CO22-rich -rich vapor(V) vapor(V) phase. phase. The Thedetailed detailedproperties propertiesofofthe the two two pure pure components, components, water water and and LCO LCO2,2,are arelisted listedin inTable Table 1. 1. Figure Figure2. 2.Schematic Schematicof ofspray spraytest testcondition conditionmapping mappingin in P–T P–T diagram diagram of of CO CO22-water -watermixture mixture[12]. [12]. Energies 2016, 9, 948 4 of 11 Table 1. Properties of CO2 and water used in the experiment. Fluids Water CO2 Vapor pressure at 298 K (kPa) Density (mol/L) at 298 K and 64 bar Viscosity (mPa·s) at 298 K and 64 bar 3 55.5 0.89 6400 16.2 (liquid) 0.057 (liquid) The constant pressure of the lower chamber was attained using a backpressure regulator mounted downstream of the lower chamber. Without the regulator, the pressure in the lower chamber would have increased as the liquid flow filled the lower chamber, thereby compressing the gas. The dimensions of the high-pressure flashing-spray system are listed in Table 2. The visualization region in the lower chamber was provided by an optical window with a diameter of 5 cm. It was desirable to fit most of the spray penetration into this visualization region for all the pressure conditions tested in this study. Thus, wetting of the chamber bottom by spray plumes should be prevented. For this reason, we selected a nozzle with a relatively high ratio of length to diameter, as previously mentioned. Table 2. Dimensions of high-pressure flashing-spray system. Parameters Description chamber shape chamber diameter/length chamber volume capillary nozzle inner diameter capillary nozzle length Cylinder 5 cm/13.4 cm 260 cm3 0.4 mm 300 mm A shadowgraph technique was employed to examine the flashing-spray patterns of the LCO2 and its mixture with water. During the throttling process across the nozzle, a high-speed camera was used to record consecutive images at a frame rate of 1/40,000 frames per second. Meanwhile, the pressure difference was measured to verify the downstream pressure controlled by the back-pressure regulator. 3. Results and Discussion 3.1. Effect of Water-Blending Ratio in Water-LCO2 Mixture In a previous work [3], spray patterns under three different levels of upstream pressure (pressure difference) were observed using a high-speed camera: 65/40, 75/50, and 85/60 bar. At 65/40 bar, the internal flashing due to bubble formation caused a wider spray angle and shallower penetration length among three sprays. This is sometimes called a “bowl spray” and involves a high level of flash-atomization, which is an effective breakup mechanism of the liquid column, due to a burst of bubbles. A phenomenon similar to the bowl spray was observed with an increasing degree of superheat by Lin et al. [4] and Park et al. [13]. In contrast, a narrower spray angle and deeper penetration were observed at 85/60 bar, where the flash boiling is absent because of the liquid abundance. This is considered a normal jet spray. This difference is caused by the higher velocity of the liquid flow inside the nozzle orifice. At the same pressure of 65/40 bar, the same nozzle length and diameter were used. The spray of H2 O was not fully developed compared with that of LCO2 . Such weak atomization is expected because of the low velocity and higher surface tension occurring when the H2 O flows with a high viscosity inside the nozzle. This breakup mode is similar to the Rayleigh-type breakup mode observed in the experiment of Dechelette et al. [14], which is the main atomization zone of high-viscosity CWSs. However, the behavior of water sprays altered by the addition of LCO2 was not experimentally evaluated in our previous work. Energies 2016, 9, 948 5 of 11 Energies 2016, 9, 948 5 of 11 Figure 3 shows the effect of the water fraction blended in the water-LCO2 mixture on the spray pattern atFigure 65/403bar. Thethe amount water the mixture was while the total shows effect ofofthe waterinfraction blended in increased the water-LCO 2 mixture on volume the sprayof the pattern 65/40 bar. The amount of water the mixture increased while the total of thewater, mixture wasatmaintained. Water contents of in 0 and 100 volwas % correspond to pure LCOvolume 2 and pure mixture was Water contents of conditions 0 and 100 volare % correspond to pure LCO2 and pure respectively. Themaintained. spray patterns under both similar to past observations, as water, previously respectively. The spraycontent patternsincreased under both are similar past observations, previously mentioned. As the water toconditions 75%, the spray angletoincreased slightly,asfrom 8.5◦ to 9.8◦ mentioned. As the water content increased to 75%, the spray angle increased slightly, from 8.5° 9.8° was ◦ and then to 12.3 . Subsequently, it decreased to zero when the water content reached 100%.toThis and then to 12.3°. Subsequently, it decreased to zero when the water content reached 100%. This was because of the increased dissolution of LCO2 when water content in the mixture is high. The high because of the increased dissolution of LCO2 when water content in the mixture is high. The high content of dissolved CO2 can evolve gaseous CO2 and thereby create the flash or disruptive boiling content of dissolved CO 2 can evolve gaseous CO2 and thereby create the flash or disruptive boiling during a pressure release. during a pressure release. (a) (b) (c) (d) (e) Figure 3. Effect of water fraction blended in water-LCO2 mixture on spray pattern at 65/40 bar: (a) 0%; (b) 5%; (c) 25%; (d) 75%; and (e) 100% of water fraction. Energies 2016, 2016, 9, 9, 948 948 Energies of 11 11 66 of Figure 3. Effect of water fraction blended in water-LCO2 mixture on spray pattern at 65/40 bar: (a) 0%; (b) 5%; 5%; (c) (c) 25%; 25%; (d) (d) 75%; 75%; and and (e) (e) 100% 100% of of water water fraction. fraction. (b) Figure 3. 948 Effect of water fraction blended in water-LCO2 mixture on spray pattern at 65/40 bar: (a) 0%;6 of 11 Energies 2016, 9, A similar similartrend trendwas wasobserved observedwhen when dissolved CO 2 content increased in the the water-CO 2 mixture A dissolved CO increased in the water-CO [2]. 2 content 2 mixture A similar trend was observed when dissolved CO 2 content increased in water-CO 2 mixture [2]. Better atomization was achieved by the increased flash boiling of CO 2dissolved dissolved in mixture. Better atomization was achieved by the increased flash boiling of CO in the [2]. Better atomization was achieved by the increased flash boiling of CO2 2 dissolved in the mixture. The solubility solubility of of CO ininwater water was fixed once pressure and temperature are are given in the the data. For of CO CO222in waterwas was fixed once pressure and temperature given in data. the data. The fixed once pressure and temperature are given in For ◦ example, 2.5 mol mol % is obtained obtained for constant constant solubility at 65 65 bar bar and 25 °C °C in 25 the predicted predicted results of of For example, 2.5 % mol % is obtained for constant solubility atand 65 bar and C in the predicted example, 2.5 is for solubility at 25 in the results Larryn W. Diamond et al. [11]. When water makes up 75% of the mixture, absolute amounts soluble results of Larryn W. Diamond et al. [11]. When water makes up 75% of the mixture, absolute amounts Larryn W. Diamond et al. [11]. When water makes up 75% of the mixture, absolute amounts soluble in the the water water become higher compared to the the case case of 25% despite having thehaving same solubility. solubility. Therefore, soluble in the water higher become higher compared toof the case of 25% despite the same Therefore, solubility. in become compared to 25% despite having the same higher soluble soluble CO22soluble amountCO contribute tocontribute higher flash flash spray asflash waterspray content increases in the theincreases mixture. Therefore, higher tospray higher as increases water content 2 amount higher CO amount contribute to higher as water content in mixture. However, this trend is not consistent with the results of supercritical dissolved-gas atomization [9]. in the mixture. However, trend iswith not the consistent the results dissolved-gas of supercritical dissolved-gas However, this trend is notthis consistent results with of supercritical atomization [9]. The cone cone half-angle half-angle was reported for aawas wide range of offor gas-to-liquid ratios (GLRs). The The cone cone half angle atomization [9]. Thewas cone half-angle reported a wide range of (GLRs). gas-to-liquid ratios (GLRs). The reported for wide range gas-to-liquid ratios half angle ◦decreases ◦increased. is approximately 13° at a low GLR and to 4° when the GLR is This is attributed The cone half angle is approximately 13 at a low GLR and decreases to 4 when the GLR is increased. is approximately 13° at a low GLR and decreases to 4° when the GLR is increased. This is attributed to differences differences in the the experimental apparatus and method. method. This is attributed to differences in the experimental apparatus and method. to in experimental apparatus and Figures444and and 5 show the change in the spray angle and penetration penetration length, respectively, respectively, Figures 5 show the change in the spray angle penetration length, respectively, according and 5 show the change in the spray and angle and length, according to the water fraction. The information was derived from the images of Figure 3. image, In the the to the water fraction. The information was derived from the images of Figure 3. In the spray according to the water fraction. The information was derived from the images of Figure 3. In spray image, two lines are drawn and intersected at the nozzle tip. The angle between two lines is two lines are drawn and are intersected at theintersected nozzle tip. at The between twoangle lines between is carefully measured spray image, two lines drawn and theangle nozzle tip. The two lines is carefully measured for spray spray horizontal angle. We We line identified horizontal line of spray sprayline tip and normal to vertical vertical line for spray angle. We identified of spray tip normal to of vertical measured distance carefully measured for angle. identified horizontal line tip normal to line and measured distance from nozzle tip to this line. This is used for penetration length. The data at aa frommeasured nozzle tipdistance to this line. is used penetration The data at a water content of zero and fromThis nozzle tip tofor this line. This islength. used for penetration length. The data at water contentin ofthese zero are are excluded in thesecontent plots. As As the water waterthe content increased, the spray angle angle and are excluded plots. As thein water increased, sprayincreased, angle andthe penetration length water content of zero excluded these plots. the content spray and penetration length increased to 75 wt % and then decreased. At 75% water blend condition, higher increased to 75 wt % and then decreased. At 75% water blend condition, higher penetration length penetration length increased to 75 wt % and then decreased. At 75% water blend condition, higher penetration length and angle angle were observed, observed, indicating a higher higher degree ofcase flashof spray. Inflash the case case of and angle were observed, indicating a higherindicating degree of aflash spray. In the higher spray, penetration length and were degree of flash spray. In the of higher flash flash spray, droplet droplet size becomes smallerTherefore, and more more droplet uniform. Therefore,quickly dropletand evaporates droplet size becomes smaller and more uniform. evaporates particle higher spray, size becomes smaller and uniform. Therefore, droplet evaporates quickly and particle would agglomerate less. Based on this observation, a water content of 75 wt % % would Based on this observation, water of 75 wt % appears to of be 75 optimal quicklyagglomerate and particleless. would agglomerate less. Basedaon this content observation, a water content wt appears to be optimal for the effective transport of coal particles by improving the spray quality. for the effective transport of coal particles by improving the spraybyquality. appears to be optimal for the effective transport of coal particles improving the spray quality. Figure 4. 4. Change Change in in spray spray angle angle with with respect respectto towater waterfraction fractionat at65/40 65/40 bar. bar. Figure bar. fraction at 65/40 Figure 5. 5. Change in in penetration penetration length length with with respect respect to to water water fraction fraction at at 65/40 65/40 bar. bar. Figure Figure 5. Change Change in penetration length with respect to water fraction at 65/40 bar. Energies 2016, 9, 948 Energies 2016, 9, 948 Energies 2016, 9, 948 7 of 11 7 of 11 7 of 11 3.2. Effect of Injection Pressure 3.2. Effect of Injection Pressure The spray characteristics were observed observed for for aa higher higher injection injection pressure pressure of of 85/60 85/60 bar. Figure 6 The spray characteristics were observed for a higher injection pressure of 85/60 bar. Figure 6 water-blending ratio ratio of of the the water-CO water-CO22 mixture on the spray angle at 85/60 85/60 bar. shows the effect of the water-blending bar. shows the effect water-blending ratio oftothe 2 mixture on the spray angle at 85/60 bar. The variation of of thethe spray angle with respect thewater-CO water fraction as the water content increased was The variation of the spray angle with respect to the water fraction as the water content increased was 65/40 bar. 65/40 bar. similar to that at 65/40 bar. However, However, the angle was 15°–21°, 15◦ –21◦ , which is far larger than that at 65/40 bar. similar to that at 65/40 bar. However, the angle was 15°–21°, which is far larger than that at 65/40 bar. This can can be be explained explained by by the the reduced reduced evolution evolution of of gaseous gaseousCO CO22 in in the the water water droplet. droplet. Dissolved Dissolved CO CO22 This This can be explained by the reduced evolution of gaseous CO2 in ◦the water droplet. Dissolved CO2 has aa higher than vapor vapor pressure pressure at at the the temperature temperature of of 25 25 °C has higher pressure pressure than C and and is is likely likely to to remain remain aa liquid. liquid. has a higher pressure than vapor pressure at the temperature of 25 °C and is likely to remain a liquid. Therefore, the the addition addition of of liquid liquid CO CO22 provides where the the Therefore, provides less less viscosity viscosity for for the the mixture mixture than than for for water, water, where Therefore, the addition of liquid CO2 provides less viscosity for the mixture than for water, where the velocity and andthus thusthe the momentum increase. can increase the spray angle despite theamount lower velocity momentum increase. ThisThis can increase the spray angle despite the lower velocity and thus the momentum increase. This can increase the spray angle despite the lower amount of flash The boiling. The presence liquid in the jetimportant was also important the usedioxide of carbon of flash boiling. presence of liquid of in the jet was also for the usefor of carbon in amount of flash boiling. The presence of liquid in the jet was also important for the use of carbon dioxide applications in cutting applications jets containing andshowed liquid showed almost no effect cutting [7]. While[7]. jetsWhile containing only gas only and gas liquid almost no effect on the dioxide in cutting applications [7]. While jets containing only gas and liquid showed almost no effect on the selected samples, the impact increased dramatically with the presence of liquid. selected samples, the impact increased dramatically with the presence of liquid. on the selected samples, the impact increased dramatically with the presence of liquid. Figure 6. 6. Effect Effect of of water-blending water-blending ratio ratio in in water-CO water-CO2 mixture mixture on on spray spray angle angle at at 85/60 85/60 bar. Figure bar. Figure 6. Effect of water-blending ratio in water-CO22 mixture on spray angle at 85/60 bar. The images in Figure 7 compare the effects of the water fraction and the injection pressure on The images images in in Figure Figure 77 compare compare the the effects effects of of the water water fraction fraction and and the the injection injection pressure pressure on on The the spray pattern of the water-CO2 mixture. They confirm that the spray angle increases with the the spray pattern of the water-CO mixture. They confirm that the spray angle increases with the the spray pattern 22 mixture. They confirm that the spray angle increases with the injection pressure and has little dependence on the water-blending ratio. Compared with the 65/40injection pressure water-blending ratio. Compared with the the 65/40-bar injection pressure and andhas haslittle littledependence dependenceononthe the water-blending ratio. Compared with 65/40bar condition, less flash boiling was apparent at 85/60 bar. condition, less flash boiling was apparent at 85/60 bar. bar condition, less flash boiling was apparent at 85/60 bar. (a) (a) (b) (b) Figure 7. Cont. Energies 2016, 9, 948 8 of 11 Energies 2016, 9, 948 Energies 2016, 9, 948 8 of 11 8 of 11 (c) (c) (d) (d) Figure of effects effectsofofwater waterfraction fractionand and injection pressure spray pattern of waterFigure 7. 7. Comparison Comparison of injection pressure on on spray pattern of water-CO 2 Figure 7. Comparison of effects of water fraction and injection pressure on spray pattern of water2 mixture: (a) 25% at 65/40 bar; (b) 75% at 65/40 bar; (c) 25% at 85/60 bar; and (d) 75% at 85/60 bar CO mixture: (a) 25% at 65/40 bar; (b) 75% at 65/40 bar; (c) 25% at 85/60 bar; and (d) 75% at 85/60 bar. CO2 mixture: (a) 25% at 65/40 bar; (b) 75% at 65/40 bar; (c) 25% at 85/60 bar; and (d) 75% at 85/60 bar Figure 8 shows the dependence of the distribution of the liquid-droplet size on the degree of Figure of of thethe distribution of the liquid-droplet size on of flash Figure88shows showsthe thedependence dependence distribution of the liquid-droplet sizethe ondegree the degree of flash boiling. A conventional image-analysis technique was employed to obtain the droplet-size boiling. A conventional image-analysis techniquetechnique was employed to obtain the flash boiling. A conventional image-analysis was employed todroplet-size obtain the distribution. droplet-size distribution. The results show that the mean diameter of the liquid spray at 65/40 bar was 150 μm. The results show that theshow meanthat diameter of the liquidof spray at 65/40 baratwas 150bar µm. However, distribution. The results the mean diameter the liquid spray 65/40 was 150 μm. However, the higher pressure of 85/60 bar yielded a larger droplet of 300 μm with a larger deviation the higher pressure of 85/60 bar yielded a larger droplet of 300 µm with a larger deviation from However, the higher pressure of 85/60 bar yielded a larger droplet of 300 μm with a larger deviation from the mean diameter. A similar trend in the droplet-size distribution was observed by Xiao et al. the mean diameter. A similar trendtrend in theindroplet-size distribution was observed by Xiao et al. et [15], from the mean diameter. A similar the droplet-size distribution was observed by Xiao al. [15], who demonstrated that the addition of CO2 in diesel spray produced a far more uniform droplet who that the of COof in diesel spray produced a far more uniform droplet size [15], demonstrated who demonstrated thataddition the addition CO 2 in diesel spray produced a far more uniform droplet size because of the flash separation of CO2 2 from the liquid. The finer and more uniform droplet because of the of flash of CO2 from the liquid.the The finer and droplet confirms the size because theseparation flash separation of CO 2 from liquid. Themore fineruniform and more uniform droplet confirms the strong flash atomization of the spray at 65/40 bar. This condition is favorable, as small strong flash the spray at of 65/40 bar. This condition is favorable, as is small liquid droplets confirms theatomization strong flashofatomization the spray at 65/40 bar. This condition favorable, as small liquid droplets may evaporate quickly and thereby prevent coal agglomeration when coal is present may evaporate quickly and thereby prevent coal agglomeration when coal is present [2]. isThe size liquid droplets may evaporate quickly and thereby prevent coal agglomeration when coal present [2]. The size distribution was measured using the open source software ImageJ. The threshold was distribution measuredwas using the open source ImageJ. The threshold was threshold appropriately [2]. The sizewas distribution measured using thesoftware open source software ImageJ. The was appropriately chosen to identify the droplet particle from the background. Then, a measuring tool chosen to identify the to droplet particle from the background. a measuring was usedtool to appropriately chosen identify the droplet particle from the Then, background. Then, tool a measuring was used to calculate the size of multiple droplets automatically. It is instructive to note the calculate of multiple droplets automatically. is instructive to the limitations of the was usedthe to size calculate the size of multiple dropletsItautomatically. It note is instructive to note the limitations of the shadowgraph technique. Smaller droplets scatter away much less light than large shadowgraph Smaller technique. droplets scatter away much scatter less light thanmuch large less droplets. Therefore, limitations of technique. the shadowgraph Smaller droplets away light than large droplets. Therefore, the smallest droplets in the spray are not detectable with current shadowgraph the smallest droplets the in the spray droplets are not detectable with shadowgraph technique. However, droplets. Therefore, smallest in the spray arecurrent not detectable with current shadowgraph technique. However, this effect may not be significant when determining any difference in injection this effect may not bethis significant when difference in injection pressureinsince it is technique. However, effect may notdetermining be significantany when determining any difference injection pressure since it is present at both pressure conditions. present both it pressure conditions. pressureatsince is present at both pressure conditions. (a) (a) (b) (b) Figure 8. Dependence of atomized liquid droplet distribution on degree of flash boiling at (a) 65/40 Figure 8.8. Dependence Dependence of of atomized atomized liquid liquiddroplet dropletdistribution distributionon ondegree degreeof offlash flashboiling boilingatat(a) (a)65/40 65/40 Figure and (b) 85/60 bar. and (b) 85/60 bar. and (b) 85/60 bar. 3.3. Effect of Chamber Pressure 3.3. Effect of Chamber Pressure Figure 9 shows a series of spray events of LCO2-water mixture at different chamber pressures. Figure 9 shows a series of spray events of LCO2-water mixture at different chamber pressures. As the chamber pressure increased at the same injection pressure, the flow rate decreased, which As the chamber pressure increased at the same injection pressure, the flow rate decreased, which Energies 2016, 9, 948 9 of 11 3.3. Effect of Chamber Pressure Figure 9 shows a series of spray events of LCO2 -water mixture at different chamber pressures. Energies 2016, 9, 948 9 of 11 As the chamber pressure increased at the same injection pressure, the flow rate decreased, which reduced reduced the the spray spray angle angle as as well well as as the thepenetration penetration length. length. This This phenomenon phenomenon was was observed observed in in the the visualization visualization results results of of Jakobs Jakobs et et al. al. [1] [1] and and Johnson Johnson et et al. al. [16]. [16]. The The spray spray angle angle as as aa function function of of the the chamber pressure has been measured for values between 1 and 20 bar [1]. An increase in the chamber chamber pressure has been measured for values between 1 and 20 bar [1]. An increase in the chamber ◦ ◦ pressure pressurefrom from11to to20 20bar barresults resultsin inaadecrease decreasein inthe thewater-spray water-sprayangle anglefrom from36 36°to to24 24°.. An An increased increased chamber pressure appeared to contract the spray, yielding a more dense cloud of droplets compared chamber pressure appeared to contract the spray, yielding a more dense cloud of droplets compared with with the the corresponding correspondingatmospheric atmosphericcase. case. This This was was explained explained by by the the smaller smaller volume volume of of the the entrained entrained air air due due to to the the increased increased pressure. pressure. This This tendency tendencymatches matchesthe thediesel dieselspray sprayreported reportedin in[17]. [17]. (a) (b) (c) (d) Figure 9. 9. Series Series of of spray spray events events of of LCO LCO2-water -water mixture mixture reported reported at at different different chamber chamber pressures pressures with with Figure 2 same injection pressure (75 bar): (a) 70 bar; (b) 60 bar; (c) 50 bar; and (d) 30 bar. same injection pressure (75 bar): (a) 70 bar; (b) 60 bar; (c) 50 bar; and (d) 30 bar. Figure 10 shows the temporal variation of two different pressures between the chambers during Figure 10 shows the temporal variation of two different pressures between the chambers during the throttling process. One is the upstream pressure (injection pressure), and the other is the the throttling process. One is the upstream pressure (injection pressure), and the other is the downstream pressure (chamber pressure). The chamber pressure remained constant, indicating the downstream pressure (chamber pressure). The chamber pressure remained constant, indicating proper operation of the back-pressure regulator. The injection pressure in the upper chamber the proper operation of the back-pressure regulator. The injection pressure in the upper chamber experienced a continuous and smooth decay during the throttling process. experienced a continuous and smooth decay during the throttling process. Energies 2016, 9, 948 Energies 2016, 9, 948 Energies 2016, 9, 948 10 of 11 10 of 11 10 of 11 Figure 10. Temporal variation of differential pressure between chambers during the throttling process Figure 10. Temporal variation of differential pressure between chambers during the throttling process at 75/70 bar. bar. at 75/70 75/70 bar. Figure 11 plots the spray angle against the pressure difference. When the chamber pressure is pressure difference. difference. When the chamber pressure is Figure 11 plots the spray angle against the pressure high, the pressure difference is low, which indicates a reduced flow rate. The spray angle remains low, which which indicates indicates aa reduced reduced flow flow rate. rate. The spray angle remains high, the pressure difference is low, low at 13.5°. However, when the chamber pressure decreases, i.e., the pressure difference increases, ◦ 13.5°.. However, when the chamber low at 13.5 chamber pressure decreases, decreases, i.e., the pressure difference increases, increases, the angle is increased to 20°◦ and afterwards it is not changed substantially. The latter is attributed to 20° and afterwards it is not changed substantially. The latter is attributed to the angle is increased to 20 choke flow, where vapor is prevalent in the mixture and therefore the flow rate is limited. flow, where where vapor vapor is is prevalent prevalentin inthe themixture mixtureand andtherefore thereforethe theflow flowrate rateisislimited. limited. choke flow, Figure 11. Variation of spray angle with respect to pressure difference. Figure with respect respect to to pressure pressure difference. difference. Figure 11. 11. Variation Variation of of spray spray angle angle with 4. Conclusions 4. Conclusions 4. Conclusions We investigated the spray characteristics of a mixture of LCO2 and water leaving an injector We investigated the spray characteristics of a mixture of LCO2 and water leaving an injector We investigated the spray characteristics of awas mixture of LCO water leaving an injector 2 and nozzle. The optimal amount of CO 2 in the mixture reported for the spray angle and length. This nozzle. The optimal amount of CO2 in the mixture was reported for the spray angle and length. This nozzle. Thedetermined optimal amount CO2 in the mixture was reported thewater-LCO spray angle and length. value was by theof difference in the solubility of CO2 inforthe 2 mixture. The value was determined by the difference in the solubility of CO2 in the water-LCO2 mixture. The This value was determined by the difference in the solubility of CO in the water-LCO mixture. 2 2 smaller droplets obtained at 65/40 bar indicate the strong flash atomization of the spray compared smaller droplets obtained at 65/40 bar indicate the strong flash atomization of the spray compared The droplets obtained at chamber 65/40 barpressure indicate the strong flash atomization of the spray compared withsmaller 85/60 bar. Changes in the have no significant influence on the spray angle, with 85/60 bar. Changes in the chamber pressure have no significant influence on the spray angle, with 85/60 Changes the chamber pressure have no significant influence on the spray angle, except in thebar. case of a highinchamber pressure. except in the case of a high chamber pressure. except in the case of a high chamber pressure. Acknowledgments: The authors thank the Korean government (MKE) for financial support from the manpower Acknowledgments: The The authors thank the government (MKE) for support from the manpower Acknowledgments: authors This thankwork the Korean Korean government for financial financial from of theKorea manpower program (No. 20144010200780). was supported by a(MKE) National Researchsupport Foundation grant program (No. 20144010200780). 20144010200780). This This work work was was supported supported by by a National Research Foundation of Korea grant (NRF-2016M1A3A1A02005033) funded by the Korean government (MEST). (NRF-2016M1A3A1A02005033) (NRF-2016M1A3A1A02005033) funded funded by by the the Korean Korean government government (MEST). (MEST). Author Contributions: Hakduck Kim and Changyeon Kim performed the spray experiment under the advice Author experiment under thethe advice of Author Contributions: Contributions: Hakduck Hakduck Kim Kimand andChangyeon ChangyeonKim Kimperformed performedthe thespray spray experiment under advice of Juhun Song. Heechang Lim reviewed the experimentaldata dataand andrevised revisedaamanuscript. manuscript.Juhun JuhunSong Song supervised supervised Juhun Song. Heechang Lim reviewed the experimental of Juhun Song. Heechang Lim reviewed the experimental data and revised a manuscript. Juhun Song supervised the research research and and wrote wrote the the manuscript. manuscript. the research and wrote the manuscript. Conflicts Conflicts of of Interest: Interest: The The authors authors declare declare no noconflict conflictof ofinterest. interest. Conflicts of Interest: The authors declare no conflict of interest. References References 1. 1. 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