• Title/Summary/Keyword: Gas Atomization

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An Experimental Study on Conversion of Reducing Agent from Aqueous Urea Solutions under Low Reaction Temperature (저온 반응장에서 요소 수용액의 환원제 전환에 관한 실험적 연구)

  • Ku, Kun Woo;Hong, Jung Goo
    • Journal of ILASS-Korea
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    • v.20 no.1
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    • pp.20-27
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    • 2015
  • Urea-SCR which is one of the aftertreatment technologies for reducing the NOx emission is widely used. An experimental study was performed to investigate urea decomposition under various thermo-fluid conditions, with different temperatures and velocities of inflow gas, and urea solution quantities. 40 wt. % aqueous urea solutions were used in this study. The inflow gas conditions were similar to the exhaust conditions of a large marine engine. The spray performance of urea solution injector was identical under all experimental conditions. The conversion efficiency of $NH_3$ was larger than that of HNCO under all experimental conditions, unlike for the theoretical thermolysis reaction.

CFD Simulation of SMD Distribution of Diesel Sprays Injected from a Common Rail Injector According to Compression Ratio of Combustion Chamber (커먼레일 인젝터로부터 분사되는 디젤 분무의 연소실 압축비 변화에 따른 SMD 분포의 CFD 시뮬레이션)

  • Lee, Choong Hoon
    • Journal of ILASS-Korea
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    • v.19 no.3
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    • pp.123-129
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    • 2014
  • A diesel spray overall SMD (Sauter mean diameter) in a spray chamber was simulated with CFD by varying the compression ratio in the spray chamber from 18:1 to 100:1. The gas densities of the spray chambers for the compression ratios of 18:1 and 100:1 were 17.97 and $74.8kg/m^3$, respectively. Standard KIVA-3V code was used for the CFD simulation. Various fuel injection patterns such as single injection, pilot injection and split injection were used for the CFD simulation. Fuel injection pressures for the simulated diesel sprays are 90 and 120 MPa. As the compression ratio increases, the CFD simulated SMD was decreased, which was generally in agreement with previous experimental studies.

Numerical Study of Combustion Characteristics in CNG DI Engine using Gaseous Sphere Injection Model (기체구 분사 모델을 이용한 CNG DI 엔진의 연소특성 수치해석)

  • Choi, Mingi
    • Journal of ILASS-Korea
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    • v.24 no.4
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    • pp.171-177
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    • 2019
  • This paper describes numerical study of combustion characteristics in CNG(compressed natural gas) DI(direct injection) engine using gaseous sphere injection model. Simulations were conducted using KIVA-3V Release 2 code. Gaseous sphere injection model, which is modified model of liquid fuel injection, was used to simulate the CNG direct injection. Until now, a very fine mesh smaller than the injector nozzle has been required to resolve the gas-jet inflow boundary. However, the gaseous sphere injection model simulates gaseous fuel injection using a coarse mesh. This model injects gaseous spheres as in liquid fuel injection and the gaseous spheres evaporate together without the latent heat of evaporation. Therefore, it does not require a very fine mesh and reduce calculation time. Combustion simulation were performed under various injection timings and injection pressures.

Observations on the Near-Nozzle Behavior of an Unsteady Fuel Spray (노즐부근에서의 비정상분무 거동)

  • 구자예;정흥철
    • Transactions of the Korean Society of Automotive Engineers
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    • v.2 no.4
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    • pp.100-111
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    • 1994
  • Observations on the near-nozzle behavior of an unsteady fuel spray through single cylindrical hole nozzle were made by phase Doopler anemometer and microphotographs. At the edge of the spray, droplet velocity peaked during needle opening and closing. Droplet sizes tended to be small on the edge of spray. The near-nozzle spray angle taken from the microphotographs was time-dependent, even though it increased with gas-to-liquid density ratio as expected. The near-nozzle spray angle was the greatest on the initial stage and decreased to a relatively constant value after about one third of the total injection duration regardless of the ambient gas conditions, even in the near-vaccum condition. The wider near-nozzle spray angle in the early stage is due to the flow characteristics inside the nozzle rather than aerodynamic interactions. However, once the spray was established, aerodynamic interactions are essential in the near-nozzle atomization.

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Numerical Study of Ignition and Combustion Process of a Diesel Spray (Diesel spray의 점화와 연소 특성 해석)

  • 김용모;권영동;김후중;김세원
    • Transactions of the Korean Society of Automotive Engineers
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    • v.5 no.1
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    • pp.15-26
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    • 1997
  • The present study is mainly motivated to numerically simulate the autoignition and combustion process of a diesel spray in RCM and effects of design parameters on combustion and engine performance in the DI diesel engine using EGR. In case of the burning spray in RCM, special emphasis is given to the autoignition process coupled with the fluid mechanics and chemical reaction. Computations are carried out for a wide range of operating condition in terms of temperature, concentration of oxygen and carbon dioxide of the intake gas in the DI diesel engine. Numerical results indicate that the mixing process along the edges of spray jet has a crucial role for autoignition and combustion process. Temperature and concentration of O2 and CO2 of intake gas significantly influence the combustion characteristics and engine performance in the diesel/EGR environment.

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A Study on the Characteristics of an Evaporating Diesel Spary Using LIEF Technique (LIEF법을 이용한 증발 디젤 분무의 특성에 관한 연구)

  • Kim, Y.R.;Kim, M.S.;Cho, H.;Min, K.D.
    • Journal of ILASS-Korea
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    • v.7 no.3
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    • pp.18-23
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    • 2002
  • An evaporating diesel spray of a common rail lnjector was visualized by LIEF technique. This technique makes it possible to separate the vapor and liquid phase images. The experiment was conducted in a constant volume vessel to make a high temperature and high pressure condition. Three images(vapor and liquid phase images from LIEF and a liquid phase image from Mie scattering) were taken simultaneously in one spray event. The major experimental parameters are the injection pressure and the ambient gas pressure. Also, a relative SMD distribution in a liquid phase was obtained by the ratio of the intensities of the fluorescence and the Mie scattering. The results show that the injection pressure and the ambient gas pressure have a close relation with the spray development and air-fuel muting process.

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Flame Stabilization and Control in Gas Turbine Combustor (가스터어빈 연소기의 화염 안정화와 제어)

  • Choi, G.M.
    • Journal of ILASS-Korea
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    • v.8 no.4
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    • pp.24-30
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    • 2003
  • This paper presents the characteristics of lifted height and flame length from non-premixed jet flames in highly preheated air to investigate the detail combustion mechanism in the gas turbine or HCCI engine, etc. Special attention was paid to the effect of preheated air temperature, oxygen concentration and fuel injection flow rate on flame length and lifted hight. By using highly preheated air, stable flames were formed even in low oxygen concentration condition. The lifted height increased with decreasing preheated air temperature, where the flame length showed opposed phenomena. The flamelet model, which is thought to have very thin flamelet, is difficult to applicable to the present flame conditions which is formed In low oxygen concentration in highly preheated air.

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Fuel Spray Characteristics in the High Pressure Injection Process (고압분사 시 연료분무 특성에 관한 연구)

  • Ahn, J.H.;Kim, H.M.;Shin, M.C.;Kim, S.W.
    • Journal of ILASS-Korea
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    • v.8 no.4
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    • pp.31-38
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    • 2003
  • Constant volume combustion chamber has been designed to investigate diesel spray characteristics with Common-Rail injection system to realize high pressure injection. In this study, two methods of measurements, Schlieren shadowgraphy and Mie scattering imaging method ate applied experimentally to study spray form and liquid phase zone in high pressure, high temperature conditions. Diesel fuel is injected at the point which ignited mixture gas is completely burned. The effect of injection pressure, injector hole diameter, ambient gas temperature and density are investigated experimentally.

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Mechanical Properties of Al-Ti Base Alloys Processed Via Rapid Solidification and Mechanical Alloying (급냉응고 및 기계적 합금화된 Al-Ti계 합금의 기계적 성질)

  • 최철진
    • Journal of Powder Materials
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    • v.2 no.1
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    • pp.36-43
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    • 1995
  • Rapidly solidified and mechanically alloyed Al-Ti base alloys were prepared by gas atomization and attritor milling separately. The gas atomized and the mechanically alloyed powders were consolidated after preheating at $450^{\circ}C$, and then heat treated isochronally for 1 hour to observe the microstructures and to investigate the mechanical properties. Stable phases of precipitates in the Al-Ti-Si and the Al-Ti-Zr alloys were identified as DO22-$(Al,Si)_3Ti$ and $Do_{23}-Al_3(Ti, Zr)$ each. Among the alloys, the mechanically alloyed Al-l0Ti-2Si alloy showed superior thermal stability and mechanical properties at elevated temperature. The additions of third elements, such as Si and Zr, to Al-Ti alloys seemed to improve the mechnical properties remarkably by stabilizing the microstructure and the precipitate phases in the consolidated alloys.

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Flame Transfer Function Modeling in a Gas Turbine Partially-premixed Combustor with Equivalence Ratio Modulation (가스터빈 부분 예혼합 연소기에서 당량비 섭동에 대한 화염전달함수 모델링)

  • Kim, Jihwan;Kim, Daesik
    • Journal of ILASS-Korea
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    • v.22 no.2
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    • pp.55-61
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    • 2017
  • This study has investigated the relationship between heat release fluctuations and the flow perturbations in a partially premixed gas turbine combustor using a commercial CFD code. Special focus of the current work is placed on the effect of equivalence ratio on the flame dynamics in a partially-premixed system. As the first step for this combustion dynamics study in the non-perfectly premixed combustor, flame behaviors are modeled and then compared with measured results under both steady and unsteady conditions. The calculated results of the flame transfer function with equivalence ratio fluctuation are found to well capture the main qualitative characteristics of the combustion dynamics for the partially-premixed flames.