• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2005년도 춘계학술대회
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• pp.630-633
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• 2005

Some gases can be formed into hydrate by physical combination with water under appropriate temperature and pressure condition. Besides them, it was found that the pore size of the sediments can affect the formation and dissociation of hydrate. In this study, formation temperatures of carbon dioxide and methane hydrate have been measured using isobaric method to investigate the effects of flow rates of gases on formation condition of hydrate in porous rock samples. The flow rates of gases were controlled using a mass flow controller. To minimize Memory effect, system temperature increased for the dissociation of gas hydrates and re-established the initial saturation. The results show that the formation temperature of hydrate decreases with increasing the injection flow rate of gas. This indicates that the velocity of gas in porous media may act as kinds of inhibitor for the formation of hydrate.

• Nuclear Engineering and Technology
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• 제35권3호
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• pp.226-233
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• 2003

The discharge characteristics of a prototype ion source was investigated, which was developed and upgraded for the NBI (Neutral Beam Injection) heating system of KSTAR (Korea Superconducting Tokamak Advanced Research). The ion source was designed for the arc discharge of magnetic bucket chamber with multi-pole cusp fields. The ion source was discharged by the emission-limited mode with the control of filament heating voltage. The maximum ion density was 4 times larger than the previous discharge controlled by a space-charge-limited mode with fully heated filament. The plasma (ion) density and arc current were proportional to the filament voltage, but the discharge efficiency was inversely proportional to the operating pressure of hydrogen gas. The maximum ion density and arc current were obtained with constant arc voltage ($80{\sim}100V$), as $8{\times}10^{11}cm^{-3}$ and 1200 A, respectively. The estimated maximum beam current was about 35 A, extracted by the accelerating voltage of 80kV.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.75-78
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• 2004

Various jet engines (Turbine engine family and RAM Jet engine) have been developed for high speed aircrafts. but their application to hypersonic flight is restricted by principle problems such as increase of total pressure loss and thermal stress. Therefore, the development of next generation propulsion system for hypersonic aircraft is a very important subject in the aerospace engineering field, SCRAM Jet engine based on a key technology, Supersonic Combustion. is supposed as the best choice for the hypersonic flight. Since Supersonic Combustion requires both rapid ignition and stable flame holding within supersonic air stream, much attention have to be given on the mixing state between air stream and fuel flow. However. the wider diffusion of fuel is expected with less total pressure loss in the supersonic air stream. So. in this study the direction of fuel injection is inclined 30 degree to downstream and the total pressure of jet is controlled for lower penetration height than thickness of boundary layer. Under these flow configuration both streams, fuel and supersonic air stream, would not mix enough. To spread fuel wider into supersonic air an aerodynamic force, baroclinic torque, is adopted. Baroclinic torque is generated by a spatial misalignment between pressure gradient (shock wave plane) and density gradient (mixing layer). A wedge is installed in downstream of injector orifice to induce an oblique shock. The schlieren optical visualization from side transparent wall and the total pressure measurement at exit cross section of combustor estimate how mixing is enhanced by the incidence of shock wave into supersonic boundary layer composed by fuel and air. In this study non-combustionable helium gas is injected with total pressure 0.66㎫ instead of flammable fuel to clarify mixing process. Mach number 1.8. total pressure O.5㎫, total temperature 288K are set up for supersonic air stream.

• 한국자동차공학회논문집
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• 제15권6호
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• pp.1-8
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• 2007

Minimizing the cylinder wear and the consumption rate of cylinder oil in a large two-stroke marine diesel engine is of great economic importance. In Korea, authors first developed a motor-driven cylinder lubricator for a Wartsila Switzerland large two-stroke diesel engine. The characteristic of the developed product is that can control automatically the oil feed rate with a load fluctuation by the motor drive and the offset cam. For manufacturing the reliable and useful products, however, it is necessary to investigate further characteristics and to improve performances as a cylinder lubricator. In this study, the effects of pump motor speed, plunger stroke and cylinder back pressure on oil feed rate, maximum discharge and delivery pressures are experimentally investigated by using the electronically controlled quill injection system and distributer in the developed cylinder lubricator. It is found that the oil feed rates of electronic control and mechanical type quills with the in-cylinder back pressure are differently characterized by the role of accumulator, the viscous resistance of contact area, etc. It can be also shown that the maximum discharge pressure of the electronic control quill is lower than the mechanical type one but the maximum discharge pressure difference of two types decreased as plunger stroke is small, and the maximum delivery pressures of two types increased as plunger stroke, motor speed and back pressure are elevated but the maximum delivery pressure of mechanical type is higher than the one of electronic control type.

• 한국음향학회지
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• 제35권3호
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• pp.208-215
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• 2016

엔진 연소 거동을 제어 및 개선하기 위하여, 연소실 내의 압력에 대한 다양한 연구가 지속적으로 수행되고 있다. 이 논문에서는 연소실 내의 압력을 통하여 디젤엔진의 연소음 레벨을 추정하였으며 이를 연소음 지수라고 정의하였다. 연소음 지수는 연소실 내의 압력신호를 고속 푸리에 변환을 통하여 계산하였으며 그 유효성을 검증하였다. 검증된 연소음 지수를 기반으로 한 제어기가 개발되었으며 차량에 탑재하였다. 연소음 지수의 목표 값을 만족시키기 위하여 일부의 분사변수를 제어하였으며 차량 연소음이 특정 주파수 영역에서 4.0 dB(A)까지 개선되었다.

• 한국화재소방학회논문지
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• 제17권4호
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• pp.111-116
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• 2003

가로, 세로, 높이가 각각 100cm, 60cm, 45cm로 내용적이 $270\ell$인 폭발 용기를 이용하여 불균일 농도 상태의 LPG-공기 혼합가스의 폭발특성을 측정하였다. 폭발은 vented-explosion과 closed explosion의 조건에서 실시하였다. 실험의 변수로는 점화원의 위치, 노즐직경 및 유속으로, 시료가스를 주입하는 노즐의 직경과 유속을 변화시키면서 용기 내에서의 불균일 혼합정도를 조절하였다. 폭발압력은 strain형 압력센사를 사용하여 측정하였고 폭발화염의 거동은 비디오카메라로 측정하여 분석하였다. 실험결과 유속과 가스 주입 시간이 용기 내 가스 혼합에 중요한 요소임을 알 수 있었으며, 불균일 정도가 심화될 수록 폭발압력과 압력상승속도가 감소하였으나 용기 내 폭발화염의 체류시간은 크게 증가하였으며 이로 인하여 가스 폭발 후 화재로의 전이 위험성이 증가함을 알 수 있었다.

• Journal of Advanced Marine Engineering and Technology
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• 제37권6호
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• pp.611-616
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• 2013

선박운항의 경제성, 효율성 및 편리성을 높이면서 친환경적인 선박에 대한 연구가 지속적으로 추진되고 있는데, 그 중 한 예로 전자제어식 디젤엔진의 개발을 들 수 있다. 그러나 전자제어식 엔진으로 추진되는 선박은 안전성과 신뢰성이 우려되고 있어 이들을 선박에 널리 보급하는데 어려움을 겪고 있다. 본 연구에서는 이러한 문제를 해결하기 위하여 전자제어식과 캠구동식 연료분사시스템을 탑재하고 있는 선박의 주기관을 이용하여 시스템별 배기성능을 비교 분석하였다. 그 결과 전자제어식의 경제적 운항 모드에서는 캠구동식과 비슷한 배기특성을 나타내었지만, 유해가스 저배출 모드의 100% 부하상태에서는 NOx를 100ppm 이상, HC의 경우 50% 부하상태에서는 10~20ppm을, 25% 부하상태에서는 35~40ppm을 캠구동식에 비해 저감시킨다. 연료소비율에 있어서는 25% 부하상태에서 압축압력을 캠 구동식에 비해 200bar 이상 증가시킨 700bar로 유지할 때 7g/kWh 정도 저감되었다.

• Steel and Composite Structures
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• 제42권5호
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• pp.591-598
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• 2022

The article deals with the possibilities of vibration stimulation. Based on the stability analysis, a multi-scale approach with a modified whole-building model is implemented. The motion equation is configured for a controlled bridge with a MDOF (multiple dynamic degrees of freedom) Tuned Mass Damper (M-TMD) system, and a combination of welding, excitation, and control effects is used with its advanced packages and commercial software submodel. Because the design of high-performance and efficient structural systems has been of interest to practical engineers, systematic methods of structural and functional synthesis of control systems must be used in many applications. The smart method can be stabilized by properly controlling the high frequency injection limits. The simulation results illustrate that the multiple modeling method used is consistent with the accuracy and high computational efficiency. The M-TMD system, even with moderate reductions in critical pressure, can significantly suppress overall feedback on an unregulated design.

• 항공우주시스템공학회지
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• 제14권5호
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• pp.66-72
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• 2020

본 연구에서는 증기발생기 내부로 냉각수 공급 시 화염에 의한 냉각수 분사 노즐 손상이 없도록, 초반 냉각수 공급량을 늘리는 방안에 대한 연구를 진행하였다. 초기 증기발생기 시험 시 벤추리만 사용하여 유량을 제어하였는데, 초반 유량 안정화 구간 동안 연소실 내부로 냉각수 공급이 되지 않아 냉각수 노즐의 손상이 발생하였다. 이를 해결하기 위해 벤추리와 오리피스를 병렬로 구성하여, 초반 공급 유량을 늘림으로써 냉각수 매니폴드와 연소실 사이 차압을 형성시켜 냉각수를 공급하였다. 수류시험을 통해 벤추리와 오리피스 공급 시퀀스를 확립하였으며, 최종 검증을 위해 연소실험을 진행하였다. 실험 결과 연소 초반 지속적으로 냉각수를 공급하는 것을 확인하였으며, 냉각수 노즐 손상 없이 성공적으로 실험을 수행하였다.

• Nuclear Engineering and Technology
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• 제41권10호
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• pp.1263-1274
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• 2009

Several experimental tests to simulate a reflood phase of a cold-leg LBLOCA of the APR1400 have been performed using the ATLAS facility. This paper describes the related experimental results with respect to the thermal-hydraulic behavior in the core and the system-core interactions during the reflood phase of the cold-leg LBLOCA conditions. The present descriptions will be focused on the LB-CL-09, LB-CL-11, LB-CL-14, and LB-CL-15 tests performed using the ATLAS. The LB-CL-09 is an integral effect test with conservative boundary condition; the LB-CL-11 and -14 are integral effect tests with realistic boundary conditions, and the LB-CL-15 is a separated effect test. The objectives of these tests are to investigate the thermal-hydraulic behavior during an entire reflood phase and to provide reliable experimental data for validating the LBLOCA analysis methodology for the APR1400. The initial and boundary conditions were obtained by applying scaling ratios to the MARS simulation results for the LBLOCA scenario of the APR1400. The ECC water flow rate from the safety injection tanks and the decay heat were simulated from the start of the reflood phase. The simulated core power was controlled to be 1.2 times that of the ANS-73 decay heat curve for LB-CL-09 and 1.02 times that of the ANS-79 decay curve for LB-CL-11, -14, and -15. The simulated ECC water flow rate from the high pressure safety injection pump was 0.32 kg/s. The present experimental data showed that the cladding temperature behavior is closely related to the collapsed water level in the core and the downcomer.