• Title/Summary/Keyword: Atomizer

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An Experimental Study on the Characteristic of Sprays and Spray Flames by Twin-Fluid Atomizer (2유체 분사노즐을 이용한 분무 및 연소특성에 관한 실험적 연구)

  • 백민수;오상헌
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.2
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    • pp.548-558
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    • 1995
  • An experimental investigation has been conducted to study the spray and combustion characteristics using the air-assisted twin fluid atomizer. Axial mean and fluctuating velocity components as well as drop-size distributions in non-reaction spray were measured with a nonintrusive phase doppler technique. Droplet number density distributions were also visualized using high speed CCD camera. Locations of spray and flame boundaries are obtained by direct photographic method. It is confirmed that at the fixed fuel flow rate, the increase of the atomizing air flow causes improvements on both spray and combustion characteristics under stable flame conditions. Internal group combustion modes where flame is located inside the spray boundary are observed to exist in the upstream region of higher droplet number density.

A study on the Characteristics of the Blowing type Rotary Burner (송풍형 로터리 버너의 특성 연구)

  • Choi Y. H.;Kim K. H.;Yoon S. J.
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.303-306
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    • 2002
  • Liquid atomization by means of a spinning cup is widely used as a device for combustion, in cooling and spray drying. In this study, the blowing type rotary atomizer was experimental carried out the investigations on the characteristics of the blowing type rotary atomizer which is an air flow energy of blower instead of an electric motor most commonly used to a driven energy. The analysis on the rotary cup speed, air velocity with the blower conditions was performed and also the drop size was measured using LDPA. It was tried to analyzed on air-nozzle size and liquid flowrate as the result. It was found that the increase of the relative velocity between liquid and air improve significantly atomization liquid, and decrease of the liquid flowrate improved the maximum drop size though the mean drop size is really the same.

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The Spray Characteristics of Simplex Atomizer under Various Shroud Air Conditions with Swirl Flow (쉬라우드 공기의 선회 유동 특성 변화에 따른 심플렉스 연료 노즐의 분무 특성)

  • Lee, D.H.;Lee, K.Y.;Choi, S.M.
    • Journal of ILASS-Korea
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    • v.9 no.3
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    • pp.35-41
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    • 2004
  • The spray characteristics were investigated to study the effect of shroud air with swirl flow on simplex type fuel injector for gas turbine combustor. The spray tests using PDA(Phase Doppler Anemometry) technique were conducted to compare the performance of simplex atomizer with $0^{\circ},\;40^{\circ},\;50^{\circ}$ swirled-shroud air conditions. In this study. we found that the injector with strong swirled-shroud air has the better atomization Performance compared with weaker swirled and non-swirled conditions.

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Modeling of Nozzle Flow Inside a Y-JET Twin-Fluid Atomizer (Y-JET 2-유체 분무노즐 내부유동의 모델링)

  • In, Wang-Kee;Lee, Sang-Yong;Song, Si-Hong
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.17 no.7 s.94
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    • pp.1841-1850
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    • 1993
  • A simplified one-dimensional analysis has been performed to predict the local pressure distributions in Y-Jet twin-fluid atomizers. Fluid compressibility was considered both in the gas(air) and two-phase(mixing) ports. The annular-mist flow model was adopted to analyze the flow in the mixing port. A series of experiments also has been performed; the results show that the air flow rate increases and the liquid flow rate decreases with the increase of the air injection pressure and/or with the decrease of the liquid injection pressure. From the measured injection pressures and flow rates, the appropriate constants for the correlations of the pressure loss coefficients and the rate of drop entrainment were decided. The local pressures inside the nozzle by prediction reasonably agree with those by the experiments.

Combustion and Atomization Characteristics of Swirl-Stabilized Spray Burner (선회 분무 연소기의 분무 및 연소특성 분석)

  • Yoon, S.P.;Ahn, J.H.;Kim, Y.M.;Kim, S.W.
    • Proceedings of the KSME Conference
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    • 2000.04b
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    • pp.434-440
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    • 2000
  • The atomization characteristics of air-assist atomizer which is surrounded by a coflowing airstream is investigated. The air-assist, coflow air stream had swirl imparted to them in the same direction with 45 degree's angle swillers. The fuel and air entered the combustor at ambient temperature and the combustor was operated in an unconfined environment. Diesel fuel was used for all the experiments. Drop size and mean velocity are reported for certain distances downstream from the nozzle. The droplet size and velocity measurements were performed using a two-component phase/Doppler particle analyzer and velocity profiles across the entire flowfield are presented.

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The Effect of Bluff-Body Shapes on the Drop Size and Flame Temperature (Bluff-Body형상이 연료액적크기와 화염온도에 미치는 영향)

  • Hwang, Sang-Ho;Cha, Keun-Jong;Kim, Duck-Jool
    • Proceedings of the KSME Conference
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    • 2000.04b
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    • pp.937-942
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    • 2000
  • The characteristics of spray combustion and dropsize of spray through twin-fluid atomizer was experimentally investigated. The distribution of flame temperature have an effect on the generation of NOx. To investigate there effects, flame temperature with different spray shape was observed. The spray shape was varied by various bluff-bodys. Mean temperature were measured by thermocouple respectively, and NOx concentration was measure by NOx analyser. Distribution of droplet sizes were measured by PMAS. The result showed that the flame with wide distribution has lower temperature and lower NOx emission compared with narrow.

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Numerical Simulation on Flow and Heat Transfer in a Gas Atomizer (가스분무장치에서 열유동 특성에 관한 전산해석)

  • 이성연
    • Journal of Powder Materials
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    • v.4 no.1
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    • pp.55-62
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    • 1997
  • Flow and heat transfer characteristics of gas, and trajectories and cooling characteristics of droplets/particles in a gas atomizer were investigated by a numerical simulation using FLUENT code. Among several kinds of solution method, the k-$\varepsilon$ turbulent model, power-law scheme, SIMPLE algorithm is adopted in this study. Momentum and heat exchange between a continuous phase(gas) and a dispersed phase(particle) were taken into account. Particle trajectories are simulated using the Lagrangian method, and Rosin-Rammler formula is used for the particle size distribution. Streamlines, velocities and pressures of gas, and trajectories, velocities and cooling rates of particles have been investigated for the various gas inlet conditions. Small but very intensive recirculation is found just below the melt orifice, and this recirculation seems to cause the liquid metal to spread radially. Particle trajectory depends on the particle size, the location of particle formation and the turbulent motion of gas. Small particle cools down rapidly, while large diameter particles solidify slowly, and this is mainly due to the differences in thermal inertia.

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Experimental and Numerical Study on Characteristics of Air-assisted Spray and Spray Flames (2유체 분무의 연소특성에 관한 실험 및 수치 해석적 연구)

  • Kim, Dong-Il;Oh, Sang-Huen
    • Journal of the Korean Society of Combustion
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    • v.3 no.2
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    • pp.51-63
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    • 1998
  • Air-assisted atomizer flames are investigated numerically to study spray structures in nonburning and burning conditions based on experimental data. A PDA is used to measure droplet size, velocity, and number density for both nonburning and burning spray. Computations utilize time-averaged gas-phase equations and $k-{\varepsilon}$ turbulence model for simplicity. The major features of the liquid-phase model are that a SSF approach is used to represent the effect of gas-phase turbulence on droplet trajectories and vaporization, an infinite-diffusion model is employed to represent the transient liquid-phase process. Computation and experiment results show that the droplet acceleration and evaporation proceed quickly in near the atomizer, characterizing high number densities and a strong convective effect. The primary combustion zone, however, is dorminated by the gas phase reaction and exhibits a sheath combustion.

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Spray characteristics and nozzle design experiment to twin-fluid atomizer (이유체 분무기의 분무특성 및 노즐설계 실험)

  • Jeong, Jin-Do;Ji, Pyeong-Sam
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.6
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    • pp.1941-1947
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    • 1996
  • Droplet size measurement technique was established for the sprayed viscous fluid by virtue of the installation of the sprayed-droplet size measurement system employing light scattering method. Atomization test results showed that the mean droplet size of the sprayed viscous fluid is decreased with the increase of the mass ratio of air to fuel and in case of the same air/fuel ratio, also with the increase of viscous fluid flow rate, and is increased with the distance from atomizer tip. Basic design data for the manufacture of external-mixing type, Y-Jet type, and internal-mixing type atomizers was acquired from the atomization tests.

Experimental and Numerical Study on the Air-assist Atomizer Spray Droplets (2유체 분무 액적의 거동에 관한 실험 및 수치 해석적 연구)

  • Kim, D.I.;Oh, S.H.
    • Journal of ILASS-Korea
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    • v.3 no.4
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    • pp.65-76
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    • 1998
  • An experimental and numerical study of a spray flow is performed to investigate the spray characteristics using an air-assisted atomizer. A Partical Dynamic Analyzer(PDA) is used to measure SMD, dmp velocity, and drop number density whose the initial conditions have considerable effect on the numerical results. The measured experimental data have been used to asses the accuracy of model predictions. Numerical investigation is made with the Eulerian - Lagrangian formulism. Turbulent dispersion effects using a Monte-Carlo method, turbulent modulation effect and entrainment of air are also numerically simulated. Results show that the numerical predictions of SSF(Stochastic Separated Flow) analysis yielded reasonable agreement with the experimental data. However, the model calculations for small drops produced the inconsistent numerical results due to the effect of surrounding air entrainment.

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