• 제목/요약/키워드: Jet Width

검색결과 151건 처리시간 0.032초

Jet 폭기 시스템의 순환유량에 따른 산소전달 특성 및 순산소 적용성 검토 (Oxygen Transfer Characteristics & Pure Oxygen Application Study on Circulation Flow Rate of the JLB (Jet Loop Bioreactor))

  • 박노백;송용효;박준규;전항배
    • 한국물환경학회지
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    • 제25권6호
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    • pp.896-901
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    • 2009
  • In this study, in order to apply the air and pure oxygen in the Jet Loop Reactor (JLB) in which the oxygen transfer rate is high, differentiate the operation mode according to each air flowrate and liquid flowrate and investigate the oxygen transfer characteristic, an experiment was carried out. The oxygen concentration with the air flowrate ($Q_g$) and liquid flowrate ($Q_L$) was identical but the oxygen transfer coefficient ($K_L{\cdot}a$) is linear depending on degree of two factors. The width of an increase is small in $0.1min^{-1}$ when the air flowrate is 0.2 L/min with increasing the liquid flowrate. Whereas, the increment was exposed to be very high for $1.5min^{-1}$ when the air flowrate was 5 L/min. In the experiments using the pure oxygen, it was 30 mg/L of oxygen concentration finally and it was 3.5 times than using the air. But the time reached the saturated concentration was similar to using the air, and $K_L{\cdot}a$ was similar to using the air too. Analysis between two independent variable and oxygen transfer of the correlation is the same model like $K_L{\cdot}a={0.0161Q_L}^{1.5371}{Q_g}^{0.5433}$ using with coefficient non linear regression analysis. It was resulted that the liquid flowrate were approximately three times than air flowrate on effect to oxygen transfer rate.

삼차원(三次元) 수분류(水噴流)의 충돌(衝突) 압력(壓力) 분포(分布) 특성(特性)에 관(關)한 연구(硏究) (A Study on the Characteristic of Impinging Pressure Distribution in the Three Dimensional Impinging Water Jet)

  • 이종수;최국광
    • 태양에너지
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    • 제18권3호
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    • pp.217-228
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    • 1998
  • 축류비가 5이고 형상비가 7인 장방형(長方形) 노즐을 사용하여 연직 상향의 3차원 자유 충돌 수분류계를 구성하였다. 수평 충돌판에 상향의 장방형 충돌수분류가 충돌할 때, 보조수를 동반하지 않은 단일수분류 및 보조수를 동반하는 수분류에 대하여 노즐-충돌판 사이의 거리, 노즐출구 속도를 변수로하여 노즐의 긴변 방향과 짧은 변 방향에 대하여 전압 및 정압 분포를 측정하였다. 이때 충돌판상에서 정압이 영이 되는 국소 위치까지의 거리인 충돌 반폭을 구하고, 최고 압력을 나타내는 정체점을 기준으로 무차원 정압 분포식을 제시하였다. 또한 각 실험조건에서 정체점상에서의 충돌속도를 구하였으며, 충돌속도는 노즐-전열면간 거리가 증가함에 따라 감소하며 그 감쇄율은 삼차원 자유 분류의 특성감쇄 영역의 유동 특성을 갖는다.

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유기EL 잉크 점성에 따른 잉크젯 분사 특성 (The Viscosity Dependency of the Organic Electroluminescent Diode On Ink-Jetting Characteristics)

  • 강경태;김명기;김혜진;황준영;강희석;박문수
    • 반도체디스플레이기술학회지
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    • 제4권2호
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    • pp.21-24
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    • 2005
  • Ink-jetting characteristics of pulse width and pulse amplitude for a piezoelectric ink jet printer driver have been mapped with various polymer EL ink. In this study, the jetting characteristics have been classified into 4 regime; no Jetting, unstable jetting, stable jetting, and spraying, and the importance of fluid viscosity on the scope of the stable jetting regime has been emphasized. The relation between jetting speed and the width and amplitude of driving signal has also been investigated and the effect of the speed on the jetting characteristics has been discussed.

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Method of Setting Nozzle Intervals at the Finishing Scale Breaker

  • Park, Jong-Wook;Kim, Sung-Cho;Park, Jin-Won
    • Journal of Mechanical Science and Technology
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    • 제17권6호
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    • pp.870-878
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    • 2003
  • The scale is removed from the strip by high pressure hydraulic descaling at the FSB (Finishing Scale Breaker). Recently, the spray height of nozzle has a trend to be shorter for the purpose of increasing the impact pressure by the high pressure water jet. Here, the nozzle intervals should be decided after considering the impact pressure and the temperature distribution on the strip. In other words, the minimum of impact pressure at the overlap of spray influences the surface grade of the strip due to scale and the overlap distance of the spray affects the temperature variation in the direction of the width of strip. In the present study, the impact pressure of the high pressure water jet is measured by the hydraulic descaling system and calculated with regard to the lead angle of 15$^{\circ}$ and the offset angle of 15$^{\circ}$, and then the temperature distribution and the temperature variation are calculated at the overlap distances of 0 mm, 10 mm, 20 mm, and 30 mm, respectively. The method of setting nozzle intervals is shown by utilizing these results.

이중제트에서 노즐과 노즐사이의 각도 변화에 따른 유동 특성 (The Flow Characteristics with Variation of Nozzle-to-nozzle Angles on Unventilated Dual Jests)

  • 김동건;김문경;윤순현
    • Journal of Advanced Marine Engineering and Technology
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    • 제32권8호
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    • pp.1231-1239
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    • 2008
  • The characteristics of flow on unventilated dual jets was experimentally investigated. The two nozzles each with an aspect ratio of 20 were separated by 6 nozzle widths. Reynolds number based on nozzle width was set to 5,000 by nozzle exit velocity. All measurements were made over a range of nozzle-to-nozzle angles from $0^{\circ}$ to $25^{\circ}$. The particle image velocimetry and pressure transducer were employed to measure turbulent velocity components and mean static pressure, respectively. It was shown that a recirculation zone with sub-atmospheric static pressure was bounded by the inner shear layers of the individual jets and the nozzles plated. As nozzle-to-nozzle inclined angles were decreased, it was found that the spanwise turbulent intensity is greater than the streamwise turbulent intensity in the merging region. In the combined region, the velocity of dual jets agree well with that of single jet, but the turbulence intensity of dual jets not agree with that of single jet.

\ulcorner㈎\ulcorner의한 세굴깊이의 실험적 예측에 대한 고찰 (Examination on the Experimental Prediction of Scour Depths Caused by Jets)

  • 손광익;윤세의
    • 한국수자원학회논문집
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    • 제30권6호
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    • pp.743-751
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    • 1997
  • 본 연구에서는 수직 또는 경사 에 의한 세굴에 대한 과거 연구결과의 종합적인 분석 및 재검토를 통하여 현재까지의 실험에 대한 문제점 파악 및 앞으로의 연구방향을 모색하며 과거 여러 연구자들의 실험적 연구중 약 500개의 실험자료를 이용하여 범용성있는 실험적 예측공식을 제시하였다. 예측세굴깊이는 하류수심 Ht와 평형하상으로부터의 세굴깊이 Hs의 합으로 표현할 수 있었으며 세굴지배인지는 하상입자의 크기, 단위폭당 유량, 그리고 상하류수면 차로 단순화시킬 수 있었으며 ${\gamma}$=0.941란 높은 상관관계를 보이는 경험적 세굴예측공식을 유도하였다. 유도하였다.

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A MECHANISM OF DEEP WELD PENETRATION IN GAS TUNGSTEN ARC WELDGING WITH ACTIVATING FLUX

  • Manabu Tanaka;Hidenori Terasaki;Masao Ushio;John J. Lowke;Yang, Chun-Li
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.76-81
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    • 2002
  • The dramatic increase in the depth of a weld bead penetration has been demonstrated by welding a stainless steel in GTA (Gas-Tungsten-Arc) process with activating flux which consists of oxides and halides. However, there is no commonly agreed mechanism fer the effect of flux on the process. In order to make clear the mechanism, each behavior of the arc md the weld pool in GTA process with activating flux is observed in comparison with a conventional GTA process. A constricted anode root is shown in GTA process with the activating flux, whereas a diffuse anode root is shown in the conventional process. These anode roots are related strongly to metal vapor from the weld pool and the metal vapor is also related to temperature distributions on the weld pool surface. Furthermore, it is suggested that a balance between the Marangoni force and the drag force of the cathode jet should dominate the direction of re-circulatory flow in the weld pool. The electromagnetic force encourages the inward re-circulatory flow due to the constricted anode root in the case with flux. The difference in flow direction in the weld pool changes the geometry or depth/width ratio of weld bead penetration.

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두 개의 평행한 평면 제트의 실험적 연구 (Experimental Investigation of Two Parallel Plane Jets)

  • 김동건;윤순현
    • 대한기계학회논문집B
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    • 제29권2호
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    • pp.214-223
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    • 2005
  • The characteristics of flow on two parallel plane jets was experimentally investigated. The two nozzles each with an aspect ratio of 20 were separated by 6 nozzle widths. Reynolds number based on nozzle width was set to 5,000 by nozzle exit velocity. The particle image velocimetry and pressure transducer were employed to measure turbulent velocity components and mean static pressure, respectively. In case of unventilated parallel plane jets, it was shown that a recirculation zone with sub-atmospheric static pressure was bounded by the inner shear layers of the individual jets and the nozzles plated. There was no recirculation zone in the ventilated parallel plane jets. It was found that the spanwise turbulent intensities of unventilated jets were higher than those of ventilated jets because of the interaction of jets, and the streamwise turbulent intensities of ventilated jets were higher than those of unventilated jets because of the effect of entrainment.

피에조 잉크젯 헤드의 음향파 거동의 수치 해석 (Numerical Simulation of Hydro-Acoustic Flow in Piezo Inkjet Print Head)

  • 이유섭;위상권;오세영;정재우
    • 대한기계학회논문집B
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    • 제31권1호
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    • pp.51-61
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    • 2007
  • This paper presents numerical and theoretical studies of acoustic wave interactions in slightly compressible liquids within piezoelectrically driven inkjet print heads. The interconnected flow channels may cause jet crosstalk, resulting in poor printing quality. It should be reduced by modifying the channel structure with the acoustic wave interactions considered. Compressible gas flow driven by the sudden movement of a top wall in the channel is calculated using Flow3D and is validated with the narrow gap theory. Limited compressibility model of the Flow3D is employed to calculate pressure waves of slightly compressible ink flow. It is found that reducing restrictor width can damp out the jet crosstalk by inhibiting the pressure wave propagation. The degree of crosstalk has been quantified using the maximum values of cross-correlations between neighboring channels and a critical channel dimension for acceptable crosstalk has been proposed. This finding is verified by drop visualization experiments using silicon-micromachined piezo inkjet print heads that are fabricated by our group.

An optimum design study of interlacing nozzle by using Computational Fluid Dynamics

  • Juraeva Makhsuda;Ryu Kyung-Jin;Kim Sang-Dug;Song Dong-Joo
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 PARALLEL CFD 2006
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    • pp.395-397
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    • 2006
  • Air interlacing serves to protect the yarn against damage, strengthens inter-filament compactness or cohesion, and ensures fabric consistency. The air interlacing nozzle is used to introduce intermittent nips to a filament yarn so as to improve its performance in textile processing. The effect of various interlacing nozzle geometries on the interlacing process was studied. The geometries of interlacing nozzles with single or multiple air inlets located across the width of yarn channels are investigated. The basis case is the yarn channel, with a perpendicular main air inlet in the middle. Other cases have main air inlets, slightly inclined double sub air inlets, The yarn channel cross sectional shapes are either semicircular or rectangular shapes. The compressed impinging jet from the main air inlet hole hits the opposing bottom wall of the yarn channel, is divided into two branches, joins with the compressed air coming out from sub air inlet at the bottom and creates two free jets at both ends of the yarn channel. The compressed air movement in the cross-section consists of two opposing directional vortices. The CFD-FASTRAN flow parallel solver was used to perform steady simulations of impinging jet flow inside of the interlace nozzles. The vortical structure and the flow pattern such as pressure contour, particle traces, velocity vector plots inside of interlace nozzle geometry are discussed in this pater.

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