• Title/Summary/Keyword: Swiller

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Behavior Characteristics of Swirl-Twin Spray with Changing Swirl Angle (선회각도변화에 따른 2유체 선회분무의 거동특성)

  • Kang, Wan-Bong;Cha, Keun-Jong;Kim, Duck-Jool
    • Proceedings of the KSME Conference
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    • 2000.04b
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    • pp.943-948
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    • 2000
  • The Twin-fluid Swirl Nozzles are used in many parts of the industry to produce homogeneous spray. This study is to investigate the effects of outer air swiller and inner water swiller on atomization of liquid.. The experiment was carried out with increasing air-flow rate at constant liquid-flow rate and with changing outer air swiller angle and inner water swiller angle. A Particle Dynamics Analyzer(PDA) was used to measure drop size, mean and ms values of axial velocity, number density and Sauter mean diameter(SMD). The axial mean velocity and SMD of droplets were measured along the center line and radial directions. It was found that the higher air flow-rate resulted in the smaller Sauter mean diameter of liquid spray and the higher axial mean velocity of droplets. This experimental results will be conveniently used for the preliminary design stage of twin-fluid nozzle development.

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Effect of Internal Swirler Angle and Swirl Chamber Aspect Ratio of Nozzle on Spray Characteristics (노즐 내부 스월러각과 스월실 형상비 변화가 분무특성에 미치는 영향)

  • Kim, Y.J.;Jung, H.C.;Jung, J.W.;Kim, D.J.
    • Journal of ILASS-Korea
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    • v.8 no.4
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    • pp.39-45
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    • 2003
  • The Objective of this study is to investigate the effect of internal swiller angle and swirl chamber aspect ratio of nozzle on spray characteristics for application of spray system in micro fabrication process. The macro-spray characterictics such as the spray angle and breakup process were obtained by photographs illustrating atomization. The micro-spray characteristics such as droplet size and axial velocity were measured by using PDA with swirler angle and swirl chamber aspect ratio. The swiller angles were $13.5^{\circ},\;27^{\circ},\;and\;40.5^{\circ}$. The swirl chamber aspect ratios were 1.2, 1.6, and 2.0. It was found that the smaller swirl chamber aspect ratio was, the larger axial velocity and drop size were.

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A Study on Improvement of Etching Characteristics by Spray Characteristics Analysis with Nozzle Geometries in Wet Etching Process (습식 에칭공정에서 노즐 형상에 따른 분무특성 분석을 통한 에칭특성의 향상에 관한 연구)

  • Jung, Ji-Won;Kim, Duck-Jool
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.7
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    • pp.842-849
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    • 2004
  • The objective of this work is to study the improvement of etching characteristics in wet etching process. The etching characteristics such as etching factor were investigated under different etching conditions and compared with the spray characteristics. The spray characteristics of nozzle with different geometries such as swirler angle and swirl chamber aspect ratio were analyzed by using PDA system to predict the effect of the spray characteristics on the etching factor. The swirler angles were 49,5$^{\circ}$, 63$^{\circ}$ and 76.5$^{\circ}$. The swirl chamber aspect ratios were 1.2, 1.6 and 2.0. It was found that the etching factor was correlated with the spray characteristics and also the smaller swiller angle, the larger etching factor became.

Performance Test of A Reverse-Annular Type Combustor (TS2) for APU (보조동력장치용 환형 역류형 연소기 (TS2) 성능 시험)

  • Ko, Young-Sung;Han, Yeoung-Min;Lee, Kang-Yeop;Yang, Soo-Seok;Lee, Dae-Sung
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.26 no.6
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    • pp.805-810
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    • 2002
  • Development of a small gas-turbine combustor for 100㎾ class APU(Auxiliary Power Unit) has been performed. This combustor is a reverse-annular type and has a tangential swiller in the liner head to improve the fuel/air mixing and flame stability. Three main and three pilot fuel injectors of the simplex pressure-swirl type are used. The performance target at the design condition includes a turbine inlet temperature of l170k, a combustion efficiency of 99%, a pattern factor of 30%, and an engine durability of 3000 hours. Under developing the combustor, we conducted the performance test of our first prototype(TS1) with some variants. As a result of the test, the performance targets of the combustor are satisfied except that the pattern factor is about 4% higher than the target value. Therefore, the second prototype(TS2) was redesigned and the performance test was conducted with the critical focus on the pattern factor and the exit mean temperature. We adopted TS2 four variants to check the improvement of the pattern factor. As a result, the pattern factors of several variants were satisfied with the performance target. Finally, the TS2A variant was chosen as a final combustor fur our APU model.