• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.202-206
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• 2009

고속회전 연료분사시스템의 분무특성을 연구하였다. 분무특성에 영향을 주는 직렬식 분무오리피스의 직경을 각각 1mm, 2mm, 3mm, 4mm, 5mm와 분무오리피스 수를 3개, 6개, 12개로 변화시켜가며 분무특성 연구를 수행하였다. PDPA 측정 시스템을 이용하여 분무입자의 크기와 속도, 분무분포 등을 측정하였고, 고속카메라를 이용하여 분무가시화를 수행하였다. 실험결과, 분무오리피스로부터 분출된 단일 액주의 길이는 회전속도에 의해 제어되며, 분무입자의 크기(SMD)는 분무오리피스의 직경과 수가 증가함에 따라 작아지는 경향을 보였다. 결국 분무입자의 크기를 제어하는 기본 메커니즘은 분무 오리피스내의 액막의 두께에 의해 결정됨을 알 수 있었다.

• 대한기계학회논문집
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• 제17권9호
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• pp.2294-2303
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• 1993

This paper investigated the characteristics of the turbulent incompressible flow past the orifice ring in an axi-symmetric pipe. The flow field was the turbulent pulsatile flow for Reynolds number of $2{\times}10^{5}$ which was defined based on the maximum velocity and the pipe diameter at the inlet, with oscillating frequence $(f_{os})=1/4{\pi}$ which was considered as quasi-steady state frequence. In the present investigation, finite analytic method was used to solve the governing equations in Navier Stokes and turbulent transport formulations. Particularly at high Reynolds number and low oscillation frequency, the effects of orifice ring on the flow were numerically investigated. The separation zone behind the orifice ring during the acceleration phase was found to be decreased. However, during the deceleration phase, the separation behind the orifice ring for pulsatile flow continuously grow to a size even larger than that in steady flow. The pressure drop in steady flow was found to be constant and always positive while for pulsatile flow the pressure drop change with time. And large turbulent kinetic energy, dissipation rate were found to be located in the region where the flow passes through the orifics ring. The maximum turbulent kinetic energy, generally occurs along the shear layer where the velocity gradient is large.

• 설비공학논문집
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• 제25권6호
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• pp.317-323
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• 2013

A multi-perforated tube indicates the existence of multiple holes of various shapes on the surface of a long cylinder-type or rectangular tube, and a hole installed on the surface is called an orifice, as it is relatively small in size, compared with the surface area of the tube. In this study, the flow characteristics of a circular multi-perforated tube with many orifices on the surface were investigated experimentally and numerically. The volume flowrate issuing from each orifice, discharge angle, effective flow area ratio, and the flow fields around the orifices were measured and visualized, with the variation of the orifice area ratio, at the same blockage ratio. The volume flowrate distributions along the flow direction of the multi-perforated tube tends to be more uniform, as larger orifices were positioned at the inlet side of the multi-perforated tube, compared with no orifice area change along the flow direction.

• 대한기계학회논문집B
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• 제27권2호
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• pp.197-205
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• 2003

A cascade impactor is a multistage impaction device used to separate airborne particles into aerodynamic size classes. A micro-orifice impactor uses micro-orifice nozzles to extend the cut sizes of the lower stages to as small as 0.05 ${\mu}{\textrm}{m}$ in diameter without resorting to low pressures or creating excessive pressure drops across the impactor stages. In this work, the phenomenon of particle clogging in micro-orifice nozzles was experimentally investigated for a commercial micro-orifice uniform deposit impactor (MOUDI). It was observed, using an optical microscope, that the micro-orifice nozzles of the final stages were partially clogged due to particle deposition during the aerosol sampling. Therefore the pressure drops across the nozzles were higher than the nominal values given by the manufacturer. To examine the effect of particle clogging in micro-orifice nozzles, the particle collection efficiency of the MOUDI was evaluated using an electrical method for fine particles with diameters in the range of 0.1-0.6 ${\mu}{\textrm}{m}$. The monodisperse liquid dioctyl sebacate (DOS) particles were used as test aerosols. A faraday cage was employed to measure the low-level current of the charged particles upstream and downstream of each stage. It was found that the collection efficiency curves shifted to correspond to smaller orifice sizes, and the 50-% cutoff sizes were much smaller than those given by the manufacturer for the three stages with nozzles less than 400 ${\mu}{\textrm}{m}$ in diameter.

• Journal of Mechanical Science and Technology
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• 제16권7호
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• pp.1019-1028
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• 2002

The instability of two-phase loop thermosyphons was investigated experimentally and analytically. Three orifice type inserts were used to study the effect of change in the pressure drop in the flow channel of the TLT on the flow instability and temperature fluctuation. It is observed that a decrease in the size of the orifice insert from 3.7 mm (no insert) to 0.71 mm drastically reduced the fluctuation of the temperature, especially at the evaporator section of the TLT. With the orifice type insert of 0.71 mm for the TLT, the overall temperature fluctuation was almost completely eliminated, especially at higher power input to the TLT The analysis based on the Kelvin-Helmholtz instability theory seems to predict reasonable well the loop stability state of the TLT with experimentally determined constant factors.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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• pp.240-243
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• 2008

회전식 연료 노즐의 분무특성을 알기 위해서 고속회전 시험장치를 이용하여 실험적 연구를 수행하였다. 시험장치는 연료공급장치, 고속 회전장치 그리고 아크릴 케이스로 구성되어있다. Injection orifice의 직경 및 개수를 변화시켜가며 분무실험을 수행하였다. 액적의 크기 및 속도는 PDPA(Phase Doppler Particle Analyzer)시스템을 이용하여 측정하였다. 실험결과로부터 Injection orifice의 직경 및 개수변화에 따른 회전식 노즐의 분무특성을 이해 할 수 있었다.

• 설비공학논문집
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• 제14권5호
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• pp.408-414
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• 2002

The instability of two-phase loop thermosyphons (TLTs) was investigated experimentally. Three orifice type inserts were used to study the effect of change in the pressure drop in the flow channel of the TLT on the flow instability and temperature fluctuation. It is observed that a decrease in the size of the orifice insert from 3.7mm (no insert) to 0.71mm drastically reduced the fluctuation of the temperature, especially at the evaporator section of the TLT With the orifice type insert of 0.71 mm for the TLT, the overall temperature fluctuation was almost completely eliminated, especially at higher power input to the TLT.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.258-263
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• 2010

고속회전 시험장치를 이용하여 V 형태의 회전식 연료 노즐의 오리피스 직경에 따른 분사특성을 파악하기 위한 연구를 수행하였다. 시험장치는 고속 회전장치, 연료공급장치, 아크릴 케이스로 구성하였다. 분무 오리피스의 직경과 회전속도를 변화시켜가며 분무실험을 수행하였다. 분무입자의 크기 및 속도 측정은 PDPA(Phase Doppler Particle Analyzer) 시스템을 사용하였고, Nd-Yag Laser를 이용하여 분무특성을 가시화하였다. 실험결과, 분무오리피스의 직경이 커질수록 분무입자의 크기가 작아졌으며, 분무 오리피스의 직경이 2.6mm인 경우 최적의 분무형태를 보였다. 그러나 오리피스의 직경이 이보다 클 경우 분무입자의 크기는 더 이상 감소하지 않았다. 이것은 분무오리피스가 최적의 직경보다 커질 경우 오리피스내의 액막이 균일하게 분포하지 않기 때문으로 판단된다.

• 한국산학기술학회논문지
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• 제20권12호
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• pp.125-130
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• 2019

가스스프링은 그 사용 목적에 따라 다양한 설계가 가능하여 많은 분야에서 사용되고 있고 그 사용량도 계속하여 증가하고 있다. 본 연구에서는 가스스프링을 압축할 경우 반발력을 감소시키고 피스톤이 복귀할 때 저속으로 복귀할 수 있도록 설계된, 오리피스 홀을 갖는 피스톤의 가스스프링 실린더 내부에서의 거동을 전산유체해석을 이용하여 예측해 보았다. 해석결과 가스스프링 내의 초기 가스압을 일정 수준 이상으로 증가시키면 피스톤의 복귀속도가 시간에 따라 감소하지 않고 일정하게 유지됨을 알 수 있었다. 오리피스 홀 사이즈가 피스톤 복귀속도에 미치는 영향을 해석을 통해 알아보았다. 오리피스 홀 사이즈를 줄이게 되면 피스톤 양단의 압력 차가 증가하여 피스톤 전진속도가 감소하게 되고 보다 등속으로 운동하게 됨을 알 수 있었다. 마지막으로 피스톤의 속도가 일정하다는 가정에서 초기 가스압에 따른 피스톤의 복귀속도를 이론적인 방법으로 도출하였고, 여러 초기 가스압에 대한 해석 결과와 비교하였다. 비교결과 이론적으로 도출한 해와 해석결과로부터 얻어진 결과 값이 거의 일치함을 알 수 있었다.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2006년도 전기학술대회논문집
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• pp.67-68
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• 2006

This study suggests a precision flow control system that enables fluid injection of a few grams at a time in a few ms time duration. The fluid injection system suggested here consists of a high pressure fluid pump, a 3 way 3 position directional control valve, an injector and an orifice. The orifice is located between the directional control valve and the injector. By supplying current signal to the directional control valve, the prescribed small amount of fluid can be supplied to a plant through the injector. The control robustness of the suggested system against the disturbances like the pressure change in a plant and the viscosity variation of the injected fluid is secured easily by using an orifice with very small inside diameter and setting the supply pressure with comparatively high value. The control performances of the suggested system are verified by numerical simulations and experiments. The outcomes of this research could be applied to the common rail injection control of lubrication oil for large size marine diesel engines, and other industrial plants.