• 한국구조물진단유지관리공학회 논문집
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• 제12권1호
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• pp.193-202
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• 2008

본 논문은 분사식 FRP의 압축 구속효과와 휨 보강 효과 및 분사식 FRP의 반발률에 대한 실험적 연구이다. 분사식 FRP란 레진과 짧게 잘려진 섬유를 고압의 공기에 의해 적용면에 분사하여 보강하는 기법이다. 분사식 FRP의 구속 및 휨 보강 효과를 알아보기 위하여 원주형 공시체와 휨 공시체를 제작하여 FRP를 분사하여 보강하였고, 보강 재료로 유리섬유와 폴리에스테르 수지를 사용하였다. 최적의 보강 조건을 알기 위해 섬유 길이, 보강 두께, 섬유 혼입비, 콘크리트 강도에 따른 실험을 실시하였고, 분사식 FRP 보강법을 섬유 매트에 의한 보강법과 비교하였다. 또한, 분사식 FRP의 반발률 역시 평가하였다. 실험을 통하여 분사식 FRP의 최적 조건을 결정하였다. 본 연구의 분사식 FRP 보강은 유리 섬유 매트에 의한 보강법 이상의 성능을 발휘하였다.

• Tribology and Lubricants
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• 제31권4호
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• pp.148-156
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• 2015

In the study, a design process for ensuring optimal clearance in a fuel injection pump(FIP) is suggested. Structure analysis and hydrodynamic lubrication analysis are performed to determine the optimal clearance. The FIP is simulated using Hypermesh, Abaqus 6.12 to evaluate the reduction of clearance when the maximum supply pressure is applied. The reduction in clearance is caused by the difference in the deformations between the barrel and plunger. When the deformation of the plunger is larger than that of the barrel, a reduction in clearance at the head part occurs. On the other hand, the maximum clearance reduction equals the maximum deformation in the stem part, because the deformation of barrel does not occur in this region. The clearance of FIP should be designed to be larger than maximum reduction of clearance in order to avoid contact between the plunger and barrel. In addition, the two-dimensional Reynolds equation is used to evaluate lubrication characteristics with variations of viscosity, clearance and nozzle for a laminar, incompressible, unsteady state flow. The equation is discretized using the finite difference method. The lubrication characteristics of FIP are investigated by comparing film parameter, which is the ratio of the minimum film thickness and surface roughness. The optimal clearance of FIP is to be designed by considering the maximum reduction in clearance, lubrication characteristics, machining limits and tolerance of clearance.

• 한국항공우주학회지
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• 제39권5호
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• pp.416-423
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• 2011

본 연구는 주유동의 흐름과 동일한 방향으로 2차 유동을 분사하여 주유동의 방향을 제어하는, 동축류 유체역학적 추력방향제어기법에 관한 연구이다. 이는 유체역학 특징인 코안다 효과를 이용하는 기술이다. 주유동의 전압력은 설계노즐의 과팽창 조건인 300~790 kPa 이며 이차유동의 제어유동압력( 120~200 kPa )에 따른 제트편향각, 세부유동특성, 제어노즐 후방에서의 충격파에 따른 추력편향특성에 대하여 수치적, 실험적 연구를 수행하였다. 이를 바탕으로 초음속 제트유동의 방향을 변화시킬 수 있는 제어유동의 작동한계(0.15 < PR < 0.4)를 도출하였다.

• 전기화학회지
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• 제13권3호
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• pp.193-197
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• 2010

In terms of the system efficiency, it is very useful to apply the ejector into the fuel recirculation system of a fuel cell system since the ejector needs no parasitic power to operate. Since the conventional automotive fuel cell use hydrogen and air as their fuel, the only hydrogen is needed to be recirculated for the better fuel efficiency. On the other hand, the submarine fuel cell needs both hydrogen and oxygen recirculation systems because the submarine drives under the sea. In particular, the cathodic recirculation has to meet the tougher target since the oxygen based pressurized stack generally used in the submarine applications generates the significant amount of the water in the stack during the operation. Namely, the oxygen utilization has designed less than 50% in the whole operating range for the better exhausting of the generated waters. And thereby in terms of the oxygen utilization, the entrainment ratio of the ejector should be more than 1 within the whole operating range. However, the conventional ejector using a constant nozzle can not afford to satisfy the mentioned critical requirement. To overcome the problem, the dual-ejector and its control strategy are designed. The performance of the proposed dual-ejector is verified by the experiments based on the real operating conditions of the target submarine system. Furthermore, the proposed design method can be used for the other fuel recirculation system of a large-scale fuel cell system with the critical requirement of the fuel utilization.

• 한국추진공학회지
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• 제20권6호
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• pp.83-90
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• 2016

이중 모드 램젯 엔진 모델의 램젯 모드 연소 시험을 수행하였다. 엔진 모델은 흡입구, 연소기 및 노즐로 이루어졌다. 로켓 기반 복합 사이클 엔진에 사용하는 것을 전제로 큰 후향 계단을 가지는 형상을 선택하였다. 시험은 마하 5, 고도 24 km 조건에서 수행하였다. 연료를 카울면과 바닥면에 분산하여 다중 분사를 한 경우에 안정적인 연소를 달성할 수 있었다. 또한 연료 당량비를 카울면에서 0.5, 바닥면에서 0.5로 하여 총 당량비 1.0으로 한 경우에 연소기 내부에서 열질식이 발생하여 유동이 아음속으로 조성되는 램젯 모드로 운전됨을 확인하였다.

• 한국화재소방학회논문지
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• 제32권1호
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• pp.76-80
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• 2018

본 연구는 바닥의 형태가 오목한 이동형 소방용수 저장탱크의 수직 벽면에 작용하는 동수력을 분석하고자 수행하였다. 이를 위해 용수 공급 노즐의 위치 및 높이에 따라 다양하게 낙하한 용수로 인해 발생한 자유 수면의 출렁임을 수치 모의실험 하였다. 이때, 자유 수면의 출렁임과 수직 벽면에서의 파의 오름을 수치 모의실험하기 위해 선형 Peregrine 모델을 이용하였다. 그 결과, 벽면에서 자유 수면의 출렁임이 증폭되는 현상을 관찰할 수 있었다. 따라서 이동형 소방용수 저장탱크의 안정적인 구조를 확보하기 위해 바닥이 오목한 지형에서 사용할 경우는 소방용수 공급방법에 주의해야 함을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 1999년도 제13회 학술강연논문집
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• pp.33-33
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• 1999

The Coanda effect is the tendency for a fluid jet to atach itself to an adjacent surface and follow its contour without causing an appreciable flow separation. The jet is pulled onto the surface by the low pressure region which develops as entrainment pumps fluid from the region between the jet and the surface. Then the jet is held to the wall surface by the resulting radial pressure gradient which balance the inertial resistance of the jet to turning. The jet may attach to the surface and may be deflected through more than 180 dog, when the radius of the Coanda surface is sufficiently large compared to the height of the exhaust nozzle. However, if the radius of curvature is small, the jet turns through a smaller angle, or may not attach to the surface at all. In general, the limitations in size and weight of a device will limit the radius of the deflection surface. Thus much effort has been paid to improve the jet deflection in a variety of engineering fields. The Coanda effect has long been applied to improve aerodynamic characteristics, such as the drag/lift ratio of flight body, the engine exhaust plume thrust vectoring, and the aerofoil/wing circulation control. During the energy crisis of the seventies, the Coanda jet was applied to reduce vehicle drag and led to drag reductions of as much as about 30% for a trailer configuration. Recently a variety of industrial applications are exploiting another characteristics of the Coanda jets, mainly the enhanced turbulence levels and entrainment compared with conventional jet flows. Various industrial burners and combustors are based upon this principle. If the curvature of the Coanda surface is too great or the operating pressure too high, the jet flow will break away completely from the surface. This could have catastrophic consequences for a burner or combustor. Detailed understanding of the Coanda jet flow is essential to refine the design to maximize the enhanced entrainment in these applications.

• 대한기계학회논문집B
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• 제22권9호
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• pp.1317-1324
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• 1998

In general, DI gasoline engine has the advantages of higher power output, higher thermal efficiency, higher EGR tolerance and lower emissions due to the operation characteristics of increased volumetric efficiency, compression ratio and ultra-lean combustion scheme. In order to apply the concept of stratified charge into direct injection gasoline engine, some kinds of methodologies have been adapted in various papers. In this study, a reflector was adapted around the injector nozzle to apply the concept of stratified charge combustion which leads the air-fuel mixture to be rich near spark plug. Therefore, the mixture near the spark plug is locally rich to ignite while the lean mixture is wholly introduced into the combustion chamber. The characteristics of combustion is analyzed with the variations of fuel injection pressure and load in a stratified -charge direct injection single cylinder gasoline engine. The obtained results are summarized as follows ; 1. The MBT spark timing approached to TDC with the increase of load on account of the increase of evaporation energy, but has little relation with fuel injection pressure. 2. The stratification effects are apparent with the increase of injection pressure. It is considered by the development of secondary diffusive combustion and the increase of heat release of same region, but proceed rapidly than diesel engine. Especially, in the case of high pressure injection (l70bar) and high load (3.0kgf m), the diffusive combustion parts are developed excessively and results in the decrease of peak pressure than in the case of middle load. 3. The index of engine stability, COVimep value, is drastically decreased with the increase of load. 4. To get better performance of DI gasoline engine development, staged optimizaion must be needed such as injection pressure, reflector, intake swirl, injection timing, chamber shape, ignition system and so on. In this study, the I50bar injection pressure is appeared as the optimum.

• 한국생산제조학회지
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• 제25권2호
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• pp.124-131
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• 2016

Several research works for finding and optimizing the methods of dispensing high viscosity phosphor used in the fabrication of white LED's are currently in progress. High viscosity phosphor dispensing with a high accuracy is crucial because the dispensing rate and uniformity directly affect parameters such as the CIE chromaticity diagram, color temperature and luminous flux of white LED's. This study presents a novel method of dispensing high viscosity phosphor using electrohydrodynamic printing. The dispensing rate was optimized less than 0.01 mg phosphor using experiments and optimizing the process parameters including the standoff distance from the nozzle to the substrate, ink supply pressure, and multi-step pulsed waveform magnitude ratio. The dispensing rate was measured by dispensing 20 dots using drop-on-demand with the optimized parameters, and the experiments were repeated 10 times to maximize the data accuracy. The average dispensing rate that can be reliably used for high viscosity phosphor dispensing was 0.0052 mg.

• 청정기술
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• 제18권4호
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• pp.410-418
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• 2012

선택적 촉매환원(selective catalytic reduction, SCR) 시스템에서 사용되는 환원제의 효용성을 극대화하기 위해 적용되는 암모니아주입관(ammonia injection gun, AIG) 성능은 유량의 분배, 공기분배다기관(air distribution manifold, ADM)의 배치 그리고 노즐의 배열 및 형상 등에 의해 영향을 받는다. 본 연구에서는 전산유체역학(computational fluid dynamics, CFD) 기법을 이용하여 AIG 성능의 지표가 되는 토출 유량 균일도를 통계적인 수치로 표현하여 관련된 설계인자들과 SCR 시스템의 성능 사이의 상관관계를 평가하고자 하였다. 관내 유동에서 일어나는 유체역학적인 현상의 영향으로 AIG에 대한 공급유량이 증가할 때 각 노즐에서의 토출 유량의 균일도는 감소하는 해석결과를 얻었으며 헤더로부터 가까울수록 분지관으로의 유량분배율이 낮아짐과 동시에 헤더에 가까운 노즐일수록 토출유량이 적어지는 현상을 파악하였다. 각 분지관에 대해 유입 면적대비 노즐의 총 면적비가 0.5 미만일 때 토출 유량의 균일도와 분지관의 유량분배가 매우 균일해지는 것으로 파악되었다.