• Proceedings of the Korean Powder Metallurgy Institute Conference
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• 2006.04a
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• pp.79-80
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• 2006

새로운 급속소결방법인 고주파유도가열 소결법과 펄스전류활성 소결법을 이용하여 습식 볼밀링으로 혼합한 WC-8wt.%Co분말에 60MPa의 압력과 90%의 고주파출력 또는 2800A의 필스전류를 가하여 상대밀도가 98.6% 이상인 초경재료를 2분이내의 짧은 시간에 제조하였다. 초기의 WC분말의 입도가 미세해짐에 따라 고주파유도가열 소결법과 펄스전류활성 소결법 모두 소결시간이 단축되는 경향을 보였으며 그 소결체의 결정립 크기도 감소하였다. 고주파유도가열 소결법으로 제조된 초경합금의 WC 결정립 크기는 초기입도가 증가함에 따라 가각 410, 540, 600, 700 및 850nm으로 측정되었으며. 그 결과를 Fig. 1.에 나타내었다. WC의 초기입도가 $0.5{\mu}m$일 경우 고주파유도가열 소결법과 펄스전류활성 소결법으로 제조된 WC-8wt.%Co 소결체의 경도와 파괴인성은 각각 $1923kg/mm^2$과 $10.5MPa{\cdot}m^{1/2}$ 및 $1947kg/mm^2$과 $10.8MPa{\cdot}m^{1/2}$ 이었다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.5
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• pp.1763-1773
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• 1991

본 연구에서는 포화수증기와 공기의 혼합기내에서 분무수적으로의 열 및 질량 전달률을 계산하기 위하여 수적의 부분혼합모형과 비혼합모형에 대하여 수적내 과도온 도분포의 해석해를 적용성이 보장되면서도 계산상의 어려움이 수반되지 않는 형태로 구하기 위하여 수적내부의 열전도해석에 있어서 적분법을 적용하였다. 적분법으로 얻어지는 과도온도분포의 해는 유한차의 다항식으로 표시되어 비혼합모형인 경우 각시 간 구간의 경계에서의 온도분포가 연속성을 유지하면서 물성치들의 온도에 대한 종속 성이 쉽게 고려되고 계산도 용이한 형태이다. 본 보에서 제시하는 해석결과의 적용 성을 조사하기 위하여 완전혼합모형을 포함하는 세가지 수적모형들에 대한 계산결과들 로부터 얻어진 시간변화에 따른 수적의 무차원 체적평균온도변동을 유효한 실험결과들 과 비교, 검토하였으며, 부분혼합모형에 대하여 혼합기의 압력, 수적의 초기온도, 혼 합기 속에 포함되어 있는 수증기의 체적분율, 수적의 초기크기, 수적의 초기속도 및 분사각도가 주위혼합기로부터 수적으로 전달되는 열 및 질량전달에 미치는 영향을 조] 사하고 도출된 대표적인 검토 결과를 제시하였다.

• Proceedings of the Korean Vacuum Society Conference
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• 2000.02a
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• pp.91-91
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• 2000

a-C:H 혹은 a-SiC:H 박막은 광전소자 및 태양전지 등의 개발에 있어서 중요한 물질이다. 우리는 a-C:H 및 a-SiC:H 박막을 PECVD (plasma-enhanced chemical vapor deposition) 방법으로 증착시키고, 박막의 가열에 따른 스핀밀도의 변화를 ESR (electron spin resonance) 측정을 통하여 조사하였다. PECVD 증착가스는 Ch4, SiH4 가스를 사용하였고, 기판은 Corning 1737glass를 사용하였으며, 기판 온도는 300-40$0^{\circ}C$, 증착 압력은 0.1-0.3 Torr, r.f. 전력은 3-36W 사이에서 변화되었다. ESR 측정은 상온 X-band 영역에서 수행되었고, modulation amplitude는 2.5G, modulation frequency는 100kHz 이었다. a-C:H 혹은 a-SiC:H 박막은 진공상태의 reactor, 혹은 공기중의 furnace 안에서 300-50$0^{\circ}C$ 영역에서 3-8시간 정도 가열되거나, 혹은 상온에서 약 50$0^{\circ}C$ 정도까지 단계적으로 가열되었다. 증착된 a-C:H 박막의 초기 구조는 Raman 측정으로부터 polymer-like Carbon으로 추정되었으며, 300-35$0^{\circ}C$ 가열시 초기 1시간 정도 사이에는 스핀밀도가 증가되었으나, 그 후 8시간 정도까지의 가열의 경우에도 대체로 동일하게 나타났다. 또한 상온으로부터 약 50$0^{\circ}C$까지 단계적으로 온도를 높여주며, 각 단계마다 1시간씩 가열했을 때도 30$0^{\circ}C$ 정도까지는 스핀밀도가 증가하다가 더 높은 온도로 가면서 다시 스핀밀도가 감소함을 볼 수 있었다. 이러한 스핀밀도의 초기 증가 및 감소를 일으키는 메카니즘에 대해서 논의해 볼 것이다.

• Journal of Aerospace System Engineering
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• v.14 no.5
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• pp.26-32
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• 2020

In this study, a facility was constructed to supply liquid nitrogen to simulate combustion instability in a liquid rocket combustor. The pressurization and supply performances were predicted and verified through different experiments. The liquid nitrogen supply system was composed of a pressurized supply system, and a dome regulator was used to adjust the pressure of the pressurant. A cavitation venturi was used to control the mass flow rate of liquid nitrogen. The condition of liquid nitrogen supply was a mass flow rate of 2.55 kg/s and the venturi inlet pressure was above 100 bar. Based on the initial experiment, it was observed that the predicted amount of the pressurant was not sufficiently supplied and the target pressure was not supplied due to a drop in tank pressure. Through the modification of the established facilities, the target mass flow rate was successfully supplied and the cryogenic liquid nitrogen supply facility was verified.

• Journal of the Mineralogical Society of Korea
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• v.17 no.3
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• pp.267-275
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• 2004

A hydrothermal process was used to synthesize dioctahedral smectite from dickite [$A1_2$$Si_2$$O_{5}$ $(OH)_4$], Dickite was previously activated by heating at $800^{\circ}C$ far 4 hours with $Na_2$$CO_3$. After the heat-treatment, $SiO_2$ was added for stoichiometry, The autoclaving was carried out in closed stainless steel vessel (about 1 liter) at the condition of various temperature, pressure, time etc. High quality smectite could be obtaind by heating at $290^{\circ}C$ under the pressure of 60 kgf/$\textrm{cm}^2$ for 48 hours. This experiment reveals that pH of the solution was an important factor and should be maintained at 10 to 11 for the formation of dioctahedral smectite. The synthesized smectite was identified as Na-beidellite by the treatment of ethylene glycol and Greene-Kelly test.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.34-40
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• 2006

For a cooling performance research of the combustor operated in a extreme environment of a high temperature and high pressure, we accomplished a cooling performance analysis. Generally a heat transfer characteristic in cooling passage is known well experimentally and theoretically, however heat flux in the combustion chamber isn't. In this study, fluid flow combined with heat transfer and thermal structural analysis is accomplished about a combustor nozzle. We tried to analyze the cooling performance with a heat transfer characteristic of a gas and coolant side in the view point of quantity on the mass flow rate to be supplied to the cooling channel. And finally, evaluation on the thermal and structural safety of nozzle wall material was accomplished.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.12
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• pp.729-734
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• 2017

A safety relief valve is a device that relieves excessive pressure in piping lines or tanks and maintains pressure at the appropriate pressure level for use. The (pressure in the) safety valve is directly influenced by the change in the back pressure, depending on whether the vents in the spring bonnet are vented to the atmosphere or to the outlet. The back pressure is divided into the built-up back pressure and the superimposed back pressure, and the back pressure characteristics vary according to the usage conditions. The safety valve used in this study is a Conventional Safety Relief Valve. The blowdown of the safety valve is predicted by establishing the equilibrium equation between the opening force and spring force considering the back pressure characteristics. Its reliability is secured by using CFX17.1. In addition, the safety of the safety valve trim was examined through fluid-structure interaction analysis.

• Journal of Astronomy and Space Sciences
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• v.19 no.3
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• pp.207-214
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• 2002

One of the way to derive design parameters of the fuel feeding system in satellite propulsion system is to analyze unsteady flow of liquid propellant (hydrazine). During steady thruster firing the flow rate is constant: if a thruster valve is abruptly shut down among a set of thrusters, pressure spikes much higher than the initial tank pressure occur. This renders the fuel flow unsteady, and the fluid pressure and flow rate to oscillate. If the pressure spikes are high enough, there are possibilities that propellant explosively decomposes, thruster valves we damaged, and adiabatic detonation of the hydrazine propellant is potentially incurred. Reflected shockwaves could also affect the calibration and operation of the pressure transducers. These necessitate the analysis of unsteady flow in the propulsion system design, and pressure behavior inside the propellant line obtained through some governing parameter variation is presented in this work.

• Journal of the Korea Society for Simulation
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• v.20 no.4
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• pp.49-58
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• 2011

It is required that a developed control system should be verified using simulator in terms of functionality and reliability prior to application to a power plant that is a very critical facility in the industry. In this paper, the control model for turbine bypass system was developed for power plant simulator. In order to develop the control model for turbine bypass system, the tool that can be used to implement turbine bypass control logic was developed based on the turbine bypass control system manual. The developed tool was merged into the simulator development environment. The functionality of the developed tool was verified via the simulation based on the each function block specification. The HP turbine bypass pressure control logic was implemented using the developed tool and was integrated with process models and other control models such as boiler control model, turbine control model and boiler feed water pump turbine control model for 500 MW korean standard type fossil power plant. Finally, the validity of the developed control model was shown via simulation result under the integrated simulation environment.

• Journal of the Korea Institute of Building Construction
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• v.15 no.3
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• pp.291-297
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• 2015

In this study, the evaluation and the analysis of the correlation between rheological properties and pumpability of high performance concrete, C80A which was applied to the height of from 200 m to 350 m in a super tall building, was carried out by measuring pumping pressure and flow rate, testing concrete properties at before and after pumping. As the results, C80A had satisfactory properties of fresh and hardened concrete to the requirements even after pumping and the maximum pumping pressure showed increase of 10~15% at every 50m higher pumping and the average flow rate showed the above $25m^3$ per hour which means proper productivity. Additionally it was verified that pumping pressure and friction factor in pipeline are inversely proportional to slump flow and showed a tendency to increase according to the higher T-500 value.