• 한국화재소방학회논문지
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• 제29권5호
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• pp.29-33
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• 2015

본 연구에서는 노즐의 형상변화에 따라서 방사유량, 살수분포 그리고 액적크기를 측정하였다. 이를 위해서 중심부 직경이 6.0 mm이고 반지름 방향 방사각도가 $142^{\circ}$와 $148^{\circ}$인 이중 구조의 미세 물분무 노즐(LPN142, LPN148) 형상을 제작하여 UL2167 시험규격에 의해서 살수분포와 분사거리의 관계를 정량화하였다. Hellium-Neon 레이져에 의한 광학적 분석 방법을 적용하여 방사유량 변화에 따라서 웨버 수와 액적 크기 그리고 방사각도에 관한 경험식을 구하였으며, 전달 방정식의 주요인자인 소멸 항과 액적크기의 상관관계를 분석하였다. 그 결과 이중 구조의 미세 물분무 노즐은 최소허용 유량범위가 결정된 경우 작동압력, 분사거리, 액적 직경을 예측하여 화재특성을 분석함으로써 노즐 선정이 가능할 것으로 사료된다.

• 한국터널지하공간학회 논문집
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• 제23권6호
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• pp.589-604
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• 2021

워터젯 암반 굴착공법은 물과 연마재만을 사용하는 친환경 및 비접촉식 굴착방법으로 다양한 장점을 가지고 있다. 최근에는 기존 천공 공법의 문제점을 보완하고 분진 방지, 소음 저하 등의 이유로 워터젯 공법의 활용이 증가하고 있다. 워터젯 굴착효율을 증대시키기 위해서는 복수의 노즐을 운용하는 것이 유리하다. 복수의 노즐을 사용할 경우, 노즐 운용방법에 따른 굴착성능과 형상을 분석하는 것이 필수적이다. 본 연구에서는 노즐각, 노즐 간 수평거리, 이격거리를 노즐 운용변수로 정의하고 굴착성능과 형상을 분석하였다. 실험결과, 노즐각과 이격거리가 증가할 때 굴착깊이는 감소하였고 유효 굴착깊이는 증가하는 경향을 보였다. 또한, 실험결과를 바탕으로 노즐 삽입에 필요한 굴착형상 기준을 제안하고 기준에 따른 최적 노즐 운용변수를 도출하였다. 본 연구결과는 향후 암반 천공용 다중 워터젯 노즐 개발 시 유용한 기초연구로 활용될 것으로 기대된다.

• 한국분무공학회지
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• 제16권1호
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• pp.27-36
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• 2011

The impact force on the single and overlap region of twin spray was experimentally evaluated using visualization method in full cone type swirl nozzle spray. Visualization of spray was conducted to obtain the spray angle and breakup process. The photography/imaging technique, based on Particle Image Velocimetry (PIV) using high-speed camera, was adopted for the direct observation of droplet motion and axial velocity measurement, respectively. Droplet size was measured by Particle Motion Analyze System (PMAS). The purpose of this study is to provide fundamental information of spray characteristics, such as impact force, for higher etching factor in the practical wet etching system. It was found that the spray angle, axial velocity and impact force were increased with increasing the nozzle pressure while droplet size decreased with increasing the nozzle pressure. Droplet size increased as the distance from nozzle tip was decreased. The impact force of twin spray in the overlap region was about 63.29, 67.02, 52.41% higher than that of single spray at 40, 50 and 60 mm of nozzle pitch, respectively. Also, the nozzle pitch was one of the important factors in the twin spray characteristics.

• 한국기계가공학회지
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• 제17권3호
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• pp.120-126
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• 2018

In the present study, the multi-nozzle electrospinning process is investigated for the fabrication of uniform polymer nanofiber mats. Electrospinning has been one of the simple and efficient methods to manufacture polymer nanofibers and their mats. Although a typical electrospinning has many advantages such as simple system and operation, various materials, and cost-effectiveness, a relatively low productivity prevents it from being used in practical applications. Thus, the multi-nozzle electrospinning system with the adjustable nozzle position and rotating drum collector is designed and produced in this study. In particular, the effects of the inter-nozzle distance and spatial arrangement of nozzles on the uniformity of the electrospun nanofibers are investigated. With this multi-nozzle electrospinning process, the maximum flow rate of the supplied polymer solution for a uniform electrospinning increases, which indicates the enhanced productivity.

• 대한기계학회논문집B
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• 제25권6호
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• pp.751-757
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• 2001

An experimental study of impinging jet-flow structure has been carried out for a fully developed single circular jet impingement cooling on a flat plate, and the effect of the wall thickness at nozzle exit edge is investigated. Impinging jet flow structures have been measured by Laser-Doppler Velocimeter to interpret the heat transfer results presented previously by Yoon et al.(sup)(10) The peaks of heat transfer rate are observed near the nozzle edge owing to the radial acceleration of jet flow when the nozzle locates close to the impingement plate. The growth of the velocity fluctuations in the wall jet flow is induced by the vortices which originate in the jet shear layer, and consequently the radial distribution of local Nusselt numbers has a secondary peak at the certain radial position. As a wall of circular pipe nozzle becomes thicker for small nozzle-to-target distance, the entrainment can be inhibited, consequently, the acceleration of wall jet flow is reduced and the heat transfer rate decreases.

• 대한기계학회논문집B
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• 제20권6호
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• pp.1994-2004
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• 1996

Numerical calculation was applied to supersonic under-expanded jets, and compared with the results of a linear theory and other experiments. TVD difference scheme was employed to solve 2-dimensional and axisymmetric inviscid Euler equation. This paper aims to explore the effects of angle of divergence and design Mach number of nozzle on the structure of under-expanded jets. The angle of divergence was varied from 0 to 20 deg. The results show that the length of the first cell of the under-expanded jets decreases and Mach disk generates at lower nozzle pressure ratio, if the angle of divergence or design Mach number of nozzle increases. The distance from the nozzle exit to Mach disk in 2-dimensional jets becomes much larger than that of axisymmetric jets, and the widths of the jet boundary and the barrel shock wave are also larger than that of axisymmetric jets. Calculation results indicate that the configuration of the under-expanded jets is strongly dependent on the nozzle pressure ratio.

• 한국분무공학회지
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• 제15권2호
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• pp.74-82
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• 2010

In order to understand the behavior of transient gaseous injection used in an LPG (Liquefied Petroleum Gas) engine, turbulent incompressible transient jets with butane and propane were measured and analyzed at pressures of 1.5 bar and 2.0 bar with injector diameters of 3 mm and 5 mm. Mie-scattering method with a tracer was used, and images were processed to investigate the behavior of butane and propane jets. Distances from the nozzle to transition region were measured as $L_e/d_{inj}$=4.35~19.4, where $L_e$ and $d_{inj}$ indicate respectively a distance from nozzle to transition point and nozzle diameter. Slits and tubes around jet at near-field were introduced to measure the effect of entrainment and the diameter of jet, which revealed that the entrainment of surrounding air is significant for developing jet diameter. When the entrainment is restricted, the behavior of jet became deviating from the baseline. It was found that the virtual origin located outside of a nozzle towards jet tip within the conditions of this work, and its location was estimated as $x_o/d_{inj}$=0.56~7.25, where $x_o$ is a distance from nozzle to virtual origin.

• 한국재료학회지
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• 제24권8호
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• pp.429-433
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• 2014

As the fabrication technology used in FPDs(flat-panel displays) advances, the size of these panels is increasing and the pattern size is decreasing to the um range. Accordingly, a cleaning process during the FPD fabrication process is becoming more important to prevent yield reductions. The purpose of this study is to develop a FPD cleaning system and a cleaning process using a two-phase flow. The FPD cleaning system consists of two parts, one being a cleaning part which includes a two-phase flow nozzle, and the other being a drying part which includes an air-knife and a halogen lamp. To evaluate the particle removal efficiency by means of two-phase flow cleaning, silica particles $1.5{\mu}m$ in size were contaminated onto a six-inch silicon wafer and a four-inch glass wafer. We conducted cleaning processes under various conditions, i.e., DI water and nitrogen gas at different pressures, using a two-phase-flow nozzle with a gap distance between the nozzle and the substrate. The drying efficiency was also tested using the air-knife with a change in the gap distance between the air-knife and the substrate to remove the DI water which remained on the substrate after the two-phase-flow cleaning process. We obtained high efficiency in terms of particle removal as well as good drying efficiency through the optimized conditions of the two-phase-flow cleaning and air-knife processes.

• 한국군사과학기술학회지
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• 제20권6호
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• pp.767-773
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• 2017

Infrared stealth is an important technology for naval ships. This technology helps improve the anti-detection performance and survivability of naval ships. In general, the infrared signature of naval ships are categorized into internal and external heat source. External signature are generated by ship surface heating by solar flux as well as the complicated heat transfer process with the surrounding weather condition. Modern naval ships are equipped with seawater injection nozzles on the outside for nuclear, biological and, chemical, and these nozzles are used to control external signature. Wide nozzle placement intervals and insufficient injection pressure, however, have reduced seawater dispersion area. To address this problem, nozzle installation standards must be established. In this study, an actual-scale experimental system was implemented to provide the evidence for nozzle installation standards in order to reduce the infrared signature of naval ships. In addition, the environmental conditions of the experiment were set up through computational fluid dynamics considering the ocean climate data and naval ship management conditions of South Korea. The dispersion distance was measured using a high-resolution thermography system. The flow rate, pipe pressure, and dispersion distance were analyzed, and the evidence for the installation of seawater injection nozzles and operation performance standards was suggested.

• 한국구조물진단유지관리공학회 논문집
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• 제22권6호
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• pp.157-163
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• 2018

본 연구는 기존에 사용되어 지고 있는 타설 노즐 내부에 블레이드를 설치함으로써 타설 시 시멘트 복합체에 혼입된 섬유의 방향성을 제어하고 동시에 분포도를 향상시키고자 하였다. 블레이드 변수 최적화를 위하여 시멘트계 매트릭스 재료의 유동과 혼입된 섬유의 운동, 노즐간의 상호작용을 고려한 다중물리계 유한요소해석을 수행하였다. 사용되는 섬유길이를 변수로 하여 블레이드의 간격, 길이, 위치를 결정하였다. 내부 블레이드 간격이 섬유길이의 약 1.2~2.4배, 블레이드 길이는 섬유길이의 약 4~8배, 설치 위치는 시멘트 복합체가 도출되는 입구에서부터 섬유길이의 14배 이하일 때 섬유 방향각이 약 $15^{\circ}$이하로 제어되었다. 또한, 본 연구에서 제시된 블레이드형 노즐은 기존의 섬유보강 시멘트 복합체 타설장비와 타설관을 그대로 사용하면서, 탈 부착식으로 제작될 수 있어 사용성과 편의성을 동시에 제공할 수 있을 것으로 판단된다.