• Title/Summary/Keyword: Water atomization

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Pulverized Coal Particle Presence Inside CWM Droplet (CWM 방울안의 미분탄 존재)

  • 김종호;김성준
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.14 no.5
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    • pp.1211-1221
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    • 1990
  • The purpose of this study is to get experimental data on the distribution of CWM (Coal- Water Mixture) droplets size and the presence of pulverized coal particles inside CWM droplets. Atomization of CWM is done by Twin-Fluid Atomizer. The operational parameters are atomizing air pressure, coal particle loading, mean size of pulverized coal particles and sampling positions across spray. Th data analysis is initiated by Impression Sampling Method(Magnesium Oxide Technique) and Photo-technique and counting works are followed. Experimental work induces following research results. The variation of particle loadings in slurry makes no appreciable effects on the mean size of CWM droplets. It is evident that atomizing air pressure has very strong effect on the atomization of slurry. The mean size of atomized fuel droplets is dramatically reduced with the increasing air pressure. The population ratio of droplets without coal particles to total number of droplets is decreased as atomizing air pressure or loading rises and the same trend is obtained as the mean size of coal particles becomes smaller but a certain tendency of coal particle presence inside droplets could not be found from the change of sampling positions.

Matrix Modification for Graphite Furnace Atomic Absorption Spectrophotometric Determination of Volatile Elements (Ⅰ). Determination of Trace Lead by Graphite Furnace Atomization (휘발성 원소들의 원자흡수 분광분석을 위한 매트릭스 개선에 관한 연구 (제 1 보). 흑연로 원자화에 의한 흔적량 납의 정량)

  • Choi, Jong Moon;Choi, Ho Sung;Kim, Young Sang
    • Journal of the Korean Chemical Society
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    • v.39 no.3
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    • pp.204-212
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    • 1995
  • The graphite furnace atomic absorption spectrophotometric determination of trace lead in water samples was studied using matrix modifiers. In order to modify the sample matrix, the type and optimum amount of the modifier were investigated with a given concentration of Pb solution. In fact, if the matrix is not modified, lead has low ashing and atomization temperatures as to give a low absorbance with bad reproducibility because of its volatility. Therefore, optimum modifiers should be used to stabilize the atomization. In this work, the ashing and atomization temperatures were raised from 400 and $1800^{\circ}C$, to 1,000 and $2000^{\circ}C$, by the addition of palladium to 50 ng/mL lead solution as a modifier. The concentration of palladium was 5.0 ${\mu}g/mL$ in the modified solution. Furthermore, if 1.5 ${\mu}g/mL$ of aluminum was mixed with the palladium modifier as an auxiliary modifier, the ashing temperature could be increased $150^{\circ}C$ additionally. With such a treatment, the sensitivity was improved more than 5 times of the solution unmodified and the reproducible results of less than 5% RSD were obtained in the samples of university's waste water and pipe-washing tap water. It could be concluded that this procedure was quantitative in the determination of trace lead from the recoveries of more than 88% obtained in the samples in which a given amount of lead was spiked.

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Numerical Simulations on Combustion Considering Propellant Droplet Atomization and Evaporation of 500 N Class Hydrogen Peroxide / Kerosene Rocket Engine (500 N급 과산화수소/케로신 로켓엔진의 추진제 액적 분무와 증발을 고려한 연소 수치해석)

  • Ha, Seong-Up;Lee, Seon-Mi;Moon, In-Sang;Lee, Soo-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.10
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    • pp.862-871
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    • 2012
  • The numerical simulations on 500-N class rocket engine using 96% hydrogen peroxide and kerosene have been conducted, considering atomization, evaporation, mixing and combustion of its propellants. The grid containing 1/6 part of combustion chamber has been generated and it is assumed that 3 kinds of liquid-phase propellants (kerosene, hydrogen peroxide and water) were injected as hollow cone spray pattern, using Rosin-Rammler function for distribution of droplet diameter. For the calculation of combustion the eddy-dissipation model was applied. Owing to small size of combustion chamber and large specific heat / latent heat of hydrogen peroxide and water the propulsion characteristics were highly influenced by the size of droplet particles, and in this analysis the engine with droplet particles of 30 micron in average has shown the best propulsion performance.

Improvement of Deposition Performance of Ultrasonic Spray Pyrolysis Deposition System through Atomizer Shape Modification (분무장치 형상 변경을 통한 초음파 열분해 증착 시스템의 증착 성능 개선)

  • Kim, Kyu-Eon;Lee, Jae-Hoo;Jeon, Jae-Keon;Park, Sung-Hwan;Lee, Chibum
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.24 no.4
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    • pp.469-474
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    • 2015
  • In ultrasonic spray pyrolysis deposition, a precursor solution is evaporated by an ultrasonic atomizer, then gas-carried into a furnace where the solute is separated from the water vapor. After condensation, polymerization, and nucleation, the solute oxide forms a thin film. To improve the deposition efficiency, the ultrasonic atomizer was studied to optimize the evaporated gas flow. The vat cover was redesigned, using three versions with different inlet factors being tested through a computational fluid dynamic analysis as well as a water evaporation experiment. The atomization rate with a hemispherical cover with a $30^{\circ}$ inlet was found to be 2.4 times higher than that with the original. This improvement was verified with fluorine-doped tin oxide spray pyrolysis deposition. The film obtained with the modified vat cover was 2.4 times thicker than that obtained with the original vat cover.

An Experimental Study on the Drop Size of a Twin-Fluid Swirl Jet Nozzle (이유체 선회분사 노즐의 액적크기에 관한 실험적 연구)

  • Oh, J.H.;Kim, W.T.;Kang, S.J.;Rho, B.J.
    • Journal of ILASS-Korea
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    • v.1 no.1
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    • pp.21-27
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    • 1996
  • This experimental study was to investigate spray angles and drop sizes in an external mixed twin-fluid swirl jet nozzle. Twin-fluid swirl jet nozzle with swirlers designed four swirl angles such as $0^{\circ},\;22.5^{\circ},\;45^{\circ},\;64.2^{\circ}$ was employed. A PDA system was utilized for the measurement of drop size and mean velocity. Water and air were used as the working fluids in this experiment. The mass flow rate of water was fixed as 0.03 kg/min, and air flow rates were controlled to have the air/liquid mass ratio from 1.0 to 6.0. As a result, swirl angle controlled to spray angles and drop sizes. It was found that swirl angle was increased with spray angle and with decreased SMD. However, the effect of swirl angle was reduced at large air/liquid mass ratio(Mr=6.0).

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Development of an external twin-fluid nozzle for Selective Catalytic Reduction (선택적 촉매 환원법을 위한 외부 혼합형 이유체 노즐 개발에 대한 실험적 연구)

  • Park, J.K.;Lee, C.W.
    • Journal of ILASS-Korea
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    • v.9 no.2
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    • pp.24-33
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    • 2004
  • The effect of the working fluid flow conditions and nozzle geometry on the spray performance of a twin-fluid nozzle used in Selective Catalytic Reduction is investigated experimentally. The liquid pressure is varied in the range of 0.3atm to 1.5atm and the air pressure is varied from the 0.5atm to 3.0atm. relative position between liquid nozzle(internal nozzle) and air nozzle(external nozzle) tip changes front 1mm inside the air nozzle to 1mm outside the air nozzle. The orifice diameter of the air nozzle is varied with 5mm. 6mm and 7mm. Spray visualization is realized with CCD-Camera. SMD(Sauter Mean Diameter) and mean particle velocities are measured by PDPA(Phase Doppler Particle Analyzer) under various experimental conditions. The measuring point is 300mm away from the nozzle tip in the downstream spray. The experimental results are that spray angle is depended air flow rate because nozzle diameter, air pressure and nozzle tip relative positions are related air flow rate. SMD is depended air flow rate and water flow rate. Also, SMD is increased when water flow rate is bigger. SMD is decreased when Air flow rate is bigger.

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Atomization of Annular Liquid Sheet with Core Air Flow - SMD Variation with Gas/Liquid Injection Velocity (중심 공기류를 이용한 환상 액막 미립화에 관한 연구-기/액 분사유속에 따른 입경 변화 고찰)

  • Choi, Chul-Jin;Lee, Sang-Yong
    • Proceedings of the KSME Conference
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    • 2001.06e
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    • pp.131-135
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    • 2001
  • The atomization characteristics of an annular liquid (water) sheet of small radius with a core gas (air) flow were studied. Different sizes of annular gaps (0.2, 0.4 and 0.8 mm) were tested to find the effect of liquid sheet thickness on SMD. The inner diameter of the gas port for the core gas flow was 4 mm. Cross-section averaged SMD was measured for various liquid and gas velocities. Regions of the SMD decrease with the increase of the liquid velocity always existed regardless of the liquid sheet thickness. This attributes to the transition of the flow patterns of spray and also to the aerodynamic interaction between the atomizing gas and the ripples on the liquid sheet surface.

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An Experimental Study on the Atomization Characteristics of a Two-Phase Turbulent Jet of Liquid Sheet Type Co-Axial Nozzle (액막형 동축노즐의 2상 난류분사의 미립화 특성에 관한 실험적 연구)

  • 노병준;강신재;오제하
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.6
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    • pp.1529-1538
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    • 1995
  • In this study, a liquid sheet type co-axial nozzle has been used to investigate the turbulent atomization characteristics which could result in the experimental data to be used in designing a jet nozzle with high performance. Image processing technique and immersion sampling method were employed to measure droplet size. In atomizing characteristics, droplet size distributions and absolute droplet sizes, SMD(Sauter Mean Diameter) have been investigated in the wide ranges of flow field depending upon the air-water mass ratios. And the comparisons between the present data and the semi-empirical curves have been conducted semi-empirical correlation for SMD has been derived in the present analysis.

Atomization Characteristics of a Double Impinging F-0-0-F Type Injector with Four Streams for Liquid Rockets

  • Kang, Shin-Jae;Rho, Byung-Joon;Oh, Je-Ha;Kwon, Ki-Chul
    • Journal of Mechanical Science and Technology
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    • v.14 no.4
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    • pp.466-476
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    • 2000
  • This paper presents atomization characteristics of a double impinging F -0-0- F type injector with four streams. A phase Doppler particle analyzer was employed to measure the droplet-size and water was used as the inert simulant liquid instead of reactive propellant liquids. The droplet mean diameter (SMD) and size distribution were measured to investigate the effects of the momentum ratio and pressure drop variations. This experimental results can be used during the preliminary design stage of a impinging stream type injector for liquid rockets.

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Effects of Propellant Phases on Atmospheric Spray Characteristics of a Pintle Injector for Throttleable Rocket Engines (가변 추력용 핀틀 분사기에서 추진제 상에 따른 상압분무 특성)

  • Yu, Kijeong;Son, Min;Radhakrishnan, Kanmaniraja;Kim, Heuy Dong;Koo, Jaye
    • Journal of ILASS-Korea
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    • v.21 no.1
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    • pp.13-19
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    • 2016
  • Atmospheric spray characteristics were experimentally compared between liquid-gas and liquid-liquid sprays of a pintle injector. In order to study spray characteristics, water and air were used as the simulants and the visualization technic was adopted. Spray images were acquired by using a backlight method by a high-resolution CMOS camera. As a result, when the pintle opening distance increased, liquid sheets became unstabled and fluttering droplets increased. In the liquid-gas case, the breakup performance increased as the pressure of gas injected from the annular orifice increased. In the liquid-liquid case, atomization efficiency decreased as the pressure of liquid injected from the annular orifice increased. Spray angles presented a similar trend between two cases. At the same momentum ratio, the spray angle of liquid-liquid case was lower than the angle of liquid-gas case.