• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2009.06a
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• pp.170-170
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• 2009

aerosol deposition method(ADM)은 에어로졸화 된 고상의 원료분말을 노즐을 통해 분사시켜 소결과정을 거치지 않고도 상온에서 고밀도 후막을 제조할 수 있으며, 세라믹, 고분자, 금속 등의 다양한 코팅이 가능하다. 본 연구에서는 ADM들 이용하여 세라믹 후막 및 세라믹-폴리머 복합체 후막을 제조하였고 60 mm 노즐을 이용하여 대면적 세라믹 후막 성장도 시도되었다. 세라믹 후막의 원료로는 낮은 유전율과 우수한 품질계수를 갖는 $Al_2O_3$ 분말과 AlN의 분말이 사용되었으며, 세라믹에 비하여 높은 탄성과 1,500~2,000의 품질계수를 갖는 테프론(teflon) 분말이 세라믹과의 복합체 후막성장에 사용되었다. 세라믹-폴리머 복합체의 경우, 폴리머의 함유량에 따라 후막 내부의 결정립 크기가 20 때의 평균 결정립을 갚는 세라믹 후막에 비해 최대 10배 정도까지 증가하는 것을 확인할 수 있었으며, 이에 따라 후막에서의 유전특성 및 전기적인 특성, 열전도도, 투과율이 크게 변화하는 것을 확인할 수 있었다. 본 연구에서는 이러한 물성 변화에 대한 원인 고찰을 위하여 후막의 미세구조 및 화학조성 등에 다양한 분석이 이루어졌으며, 상온에서 성막되는 후막의 고분자 기판으로의 응용을 위한 최적의 공정조건을 제시하고자 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.11
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• pp.849-859
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• 2020

The semi-empirical equation and commercial computational tool were used to predict the base drag of a guided missile with free-stream Mach numbers and chamber pressures, and the results were generally agree each other. Differences in flow characteristics and base drags were observed with over/under expansion conditions by the nozzle. Under the over-expansion condition, the base pressure decreased as the expansion fan was generated at upper region of the base, and base pressure decreased further with increasing free-stream Mach number as the expansion becomes strong. Under the under-expansion conditions, a shock wave was generated around the base by the influence of the nozzle flow, which increased the base pressure, and the effect increased as the chamber pressure increased. Under the same chamber pressure condition, as the free-stream Mach number increases, the characteristic that the base pressure decreases as the shock wave generated at the base moves downstream was observed.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.30 no.6 s.249
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• pp.553-559
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• 2006

Most diesel injector, which is currently used in high-pressure common rail fuel injection system of diesel engine, is driven by the solenoid coil energy for its needle movement. The main disadvantage of this solenoid-driven injector is a high power consumption, high power loss through solenoid coil and relatively fixed needle response's problem. In this study, a prototype piezo-driven injector, as a new injector mechanism driven by piezoelectric energy based on the concept of inverse piezo-electric effect, has been designed and fabricated to know the effect of piezo-driven injection processes on the diesel spray structure and internal nozzle flow. Firstly we investigated the spray characteristics in a constant volume chamber pressurized by nitrogen gas using the back diffusion light illumination method for high-speed temporal photography and also analyzed the inside nozzle flow by a fully transient simulation with cavitation model using VOF(volume of fraction) method. The numerical calculation has been performed to simulate the cavitating flow of 3-dimensional real size single hole nozzle along the injection duration. Results were compared between a conventional solenoid-driven injector and piezo-driven injector, both equipped with the same micro-sac multi-hole injection nozzle. The experimental results show that the piezo-driven injector has short injection delay and a faster spray development and produces higher injection velocity than the solenoid-driven injector. And the predicted simulation results with the degree of cavitation's generation inside nozzle for faster needle response In a piezo-driven injector were reflected to spray development in agreement with the experimental spray images.

• Fire Science and Engineering
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• v.16 no.4
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• pp.33-43
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• 2002

To analyze the effect of fire plume on the characteristics of air flow and $CO_2$, extinguishant transfer when extinguishant is injected into a closed space similar to a marine engine room with fire plume, a numerical simulation on a space was performed. Flow fields and $CO_2$, concentration fields are calculated according with the variation of the location of nozzles. In all cases excepting the case of all nozzles located in the right side of ceiling, an counterclockwise & clockwise recirculation flow was found in the region of the right and left side of the nozzle on the second floor and such a recirculation flow greatly affected mass transfer and the diffusion process of $CO_2$, extinguishant. In the region of the first floor with fire plume, the diffusion process of $CO_2$, extinguishant was in agreement with the extension process of recirculation flow. It is considered that the result of this study can be useful to designing the arrangement of nozzles for the $CO_2$ fire fighting equipments in a marine engine room.

• Journal of Bio-Environment Control
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• v.20 no.4
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• pp.394-398
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• 2011

The effect of two-fluid fogging system on the control of Bemisia tabaci in tomato cultivation was evaluated in a greenhouse. The number of Bemisia tabaci was decreased by 87% from the fog treatment for 7 days. During the fog treatment, the mean daily temperature was decreased by $2^{\circ}C$ and the mean daily relative humidity was increased by 3~4% as compared to the non-treatment. The reduction of Bemisia tabaci in the treatment might not be resulted from the differences in temperature and humidity in the greenhouse. The sound coming from the two-fluid fogging system did not affect when it was operated without water inside. Therefore it was concluded that water droplets coming out the nozzle reduced the growth and the movement of whiteflies because the suspension of tiny water droplets were attached on the skin of whiteflies.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.10
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• pp.1025-1031
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• 2011

Autoignition characteristic is an important parameter for designing diesel or PCCI engines. In particular, diesel spray flames are lifted from the nozzle and the initial flame is formed by an autoignition phenomenon. The lifted nature of diesel spray flames influences soot formation, since air will be entrained into the spray core by the entrainment of air between the nozzle region and the lifted flame base. The objective of the present study was to identify the effect of heat loss on the ignition delay time by adopting a coflow jet as a model problem. Methane ($CH_4$), ethylene ($C_2H_4$), ethane ($C_2H_6$), propene ($C_3H_6$), propane ($C_3H_8$), and normal butane (n-$C_4H_{10}$) fuels were injected into high temperature air, and the liftoff height was measured experimentally. As the result, a correlation was determined between the liftoff height of the autoignited lifted flame and the ignition delay time considering the heat loss to the atmosphere.

• Journal of the Korean Society of Propulsion Engineers
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• v.4 no.3
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• pp.11-18
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• 2000

When supersonic underexpanded jets are exhausted from the nozzle, complex shock cell configurations such as barrel shock, expansion fan, Mach disc, and exhaust-gas jet boundary are appeared repetitively. The shock cell is smeared by turbulence dissipation and disappeared in long distance from the nozzle. When underexpanded jet is suddenly impinged on a flat plate, it forms very complex flow structure. In this paper, we solve compressible Wavier-Stokes equation adapting finite volume method to obtain jet impingement flow structure and compare calculated data with experimental ones. It is shown that numerical simulation data are in good agreement with experimental one in a short distance between nozzle exit and flat plate and little influence of underexpanded ratio is appeared in jet impingement now distribution.

• The KSFM Journal of Fluid Machinery
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• v.18 no.2
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• pp.60-66
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• 2015

Conjugate heat transfer analysis was performed to investigate the flow and cooling performance of the high pressure turbine nozzle of gas turbine engine. The CHT code was verified by comparison between CFD results and experimental results of C3X vane. The combination of k-${\omega}$ based SST turbulence model and transition model was used to solve the flow and thermal field of the fluid zone and the material property of CMSX-4 was applied to the solid zone. The turbine nozzle has two internal cooling channels and each channel has a complex cooling configurations, such as the film cooling, jet impingement, pedestal and rib turbulator. The parabolic temperature profile was given to the inlet condition of the nozzle to simulate the combustor exit condition. The flow characteristics were analyzed by comparing with uncooled nozzle vane. The Mach number around the vane increased due to the increase of coolant mass flow flowed in the main flow passage. The maximum cooling effectiveness (91 %) at the vane surface is located in the middle of pressure side which is effected by the film cooling and the rib turbulrator. The region of the minimum cooling effectiveness (44.8 %) was positioned at the leading edge. And the results show that the TBC layer increases the average cooling effectiveness up to 18 %.

• Smart Media Journal
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• v.8 no.4
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• pp.38-45
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• 2019

When there is a spray flow such as from a pesticide nozzle, winds affect the droplet flow of a rotary-wing drone accompanied by a strong wake, with a severe oscillation. Especially, during forwarding flights or when winds come from the side, compare to a simple hovering flight as the droplet is in the effect of aerodynamic drag force, the effect of spraying region becomes even larger. For this reason, the spraying of pesticides using drones may cause a greater risk of scattering or a difference in droplet dispersion between locations, resulting in a decrease in efficiency. Therefore, through proper numerical modeling and its applied simulation, an indication tool is required applicable for the various flight and atmospheric conditions. In this research, we completed both experiment and numerical analysis for the strong downwash from the rotor and flight velocity of the drone by comparing the probability density function of droplet distribution to build a spraying system that can improve the efficiency when spraying droplets in the pesticide spray drone.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.245-245
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• 2010

최근에 반도체 소자 및 마이크로머신, 바이오센서 등에 사용되는 미세 부품에 대한 연구 개발이 활발히 진행되고 있다. 미세 부품을 제작하기 위한 MEMS 공정은 대표적으로 화학용액을 이용한 습식식각, 플라즈마를 이용한 건식식각 등이 주를 이룬다. Micro blaster는 경도가 강하고 화학적 내성을 가지며 용융점이 높아 반도체 MEMS 공정에 어려움이 있는 기판을 다양한 형태로 식각 할 수 있는 기계적인 식각 공정 기술이라 할 수 있다. Micro blaster의 식각 공정은 고속의 날카로운 입자가 공작물을 타격할 때 입자의 아래에는 고압축응력이 발생하게 되고, 이 고압축 응력에 의하여 소성변형과 탄성변형이 발생된다. 이러한 변형이 발전되어 재료의 파괴 초기값보다 크게 되면 크랙이 발생되고, 점점 더 발전하게 되면 재료의 제거가 일어나는 단계로 이루어진다. 본 연구에서는 micro blaster 장비를 반도체 MEMS 공정에 적용하기 위한 식각 특성에 관하여 확인하였다. Micro blaster 장비와 식각에 사용한 파우더는 COMCO INC. 제품을 사용하였다. Micro blaster를 $Al_2O_3$ 파우더의 입자 크기, 분사 압력, 기판의 종류, 노즐과 기판과의 간격, 반복 횟수, 노즐 이동 속도 등의 공정 조건에 따른 식각 특성에 관하여 분석하였다. 특히 실제 반도체 MEMS 공정에 적용 가능한지 여부를 확인하기 위하여 바이오 PCR-chip을 제작하였다. 먼저 glass 기판과 Si wafer 기판에서의 식각률을 비교 분석하였고, 이 식각률을 바탕으로 바이오 PCR-chip에 사용하게 될 미세 홀과 미세 채널, 그리고 미세 챔버를 형성 하였다. 패턴을 형성하기 위하여 TOK Ordyl 사의 DFR(dry film photoresist:BF-410)을 passivation 막으로 사용하였다. Micro blaster에 사용되는 파우더의 직경이 수${\mu}m$ 이상이기 때문에 $10\;{\mu}m$ 이하의 미세 채널과 미세홀을 형성하기 어려웠지만 현재 반도체 MEMS 공정 기술로 제작 연구되어지고 있는 바이오 PCR-chip을 직접 제작하여 micro blaster를 이용한 반도체 MEMS 공정 기술에 적용 가능함을 확인하였다.