• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.3026-3031
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• 2008

In conventional closed-loop crankcase ventilation systems, the lubrication oil had to be re-circulated to the intake manifold, in the form of oil mist mixed with the blow-by gas. This blow-by gas containing the engine lubricant oil affects on the engine problems and the exhaust emissions. A high-efficient oil separator is required to minimize consumption of engine oil and reduce harmful emissions. In the conventional oil separator of CI engines, it has good oil separation performance even though separator design is simple, due to lots of the blow-by gas. As the emission regulation becomes severe, the oil separator for SI engines is also required. But in SI engines, separator design should be optimized, due to small size of oil particles and little amount of blow-by gas. In this study, oil separation performance classified by diameter of oil mist in cylinder head cover internal model which has three cyclones and two baffle plates for SI engine is calculated with CFD methodology.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제31회 추계학술대회논문집
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• pp.133-136
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• 2008

본 연구는 추진제를 공급하는 터보펌프와 연계한 연료 과농 가스발생기의 연소 특성에 관한 것이다. 총 5회의 연소시험이 안정적으로 실시되었다. 가스발생기의 압력 형성은 터보펌프로부터 추진제 공급유량에 따라 연동하였다. 터보펌프를 가스발생기 가스로 직접 구동하는 폐회로 시험에서도 안정적인 작동 성능을 보여주었다. 연소 가스의 온도 형성은 이전 시험 결과와 비슷한 양상을 보였다. 실제 작동 연소 압력 변경을 위해 장착한 오리피스는 압력 섭동 저감에 효과적이었으나 45 bar 이하의 저압에서는 단품 시험 시와 동일한 압력 섭동 특성을 보여주었다.

• Journal of Advanced Marine Engineering and Technology
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• 제35권6호
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• pp.765-772
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• 2011

본 연구에서는 선박 전원용 SOFC 시스템에 대한 HIL(Hardware-In-the-Loop)을 구축하기 위하여 실시간 코드 생성이 가능한 연료전지 시스템 모델을 개발을 하였다. 또한, 메탄을 연료로 사용한 내부개질형 500kW급 고체산화물형 연료전지 시스템에서 연료전지 스택으로 공급되는 애노드와 캐소드 공급가스의 온도 차이를 최소화하기 위하여 연료전지 스택 배기가스의 유량 분배, 연료 및 공기 공급 유량, 공급 공기 온도의 영향이 애노드 및 캐소드 공급 가스의 온도 특성과 연료전지 스택 출력 및 시스템 효율 등에 미치는 영향에 관하여 검토하였다. 그 결과 터빈 출구에 위치한 3-Way 밸브의 위치가 0.839에서 애노드와 캐소드 공급 가스 온도가 약 830K에서 동일하게 유지됨을 알 수 있었다. 또한, 애노드와 캐소드 공급 가스 온도를 높이기 위해서는 연료전지 스택 및 시스템 효율을 충분히 고려하여 메탄 공급 유량을 최적화하는 프로세스가 필요함을 알 수 있었다.

• 한국정보통신학회논문지
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• 제22권7호
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• pp.949-955
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• 2018

HIL 시뮬레이션은 복잡한 실시간 임베디드 시스템을 개발하고 테스트하는 데 사용되는 기법이다. HIL 테스트는 해양플랜트와 같은 고부가가치 선박인 LNGC의 PMS 성능 검증을 위한 효율적인 플랫폼이 된다. 그러나 국내 조선소를 비롯한 연구기관에서 스스로 HIL 테스트를 수행하기에는 시간이 필요하다. 이 문제를 해결하기 위해, 본 연구는 전력 공급 장치 / 소비 장치, 제어콘솔, MSBD 로 구성된 FPGA 기반의 PMS-HIL 시뮬레이터를 제안한다. 제안된 HIL시뮬레이션 플랫폼은 실제 장비 데이터를 사용하였고, PMS의 부하 공유 테스트를 수행하였다. 제안된 시스템은 대칭, 비대칭 및 고정 부하분배를 통해 검증하였고 공장수락시험 대체 가능성을 보여 준다. 또한 향후 에너지관리시스템 개발을 비롯한 선박 자동화 및 자율운항을 위한 추가 시스템 개발 시 많은 도움을 줄 것으로 사료된다.

• 한국수소및신에너지학회논문집
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• 제30권3호
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• pp.282-288
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• 2019

When liquefied natural gas (LNG) is vaporized to form natural gas for industrial and household consumption, a tremendous amount of cold energy is transferred from LNG to seawater as a part of the phase-change process. This heat exchange loop is not only a waste of cold energy, but causes thermal pollution to coastal fishery areas by dumping the cold energy into the sea. This project describes an innovative new design for reclaiming cold energy for use by cold storage warehouses (operating in the 35 to $62^{\circ}C$ range). Conventionally, warehouse cooling is done by mechanical refrigeration systems that consume large amounts of electricity for the maintenance of low temperatures. Here, a closed loop LNG heat exchange system was designed (by simulator) to replace mechanical or vapor-compression refrigeration systems. The software PRO II with PROVISION V9.4 was used to simulate LNG cold energy, gas re-liquefaction, and the vaporized process under various conditions. The effects on sensible and latent heats from changes to the array type of heat exchangers have been investigated, as well as an examination of the optimum.

• 대한기계학회논문집B
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• 제28권4호
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• pp.415-424
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• 2004

Cooling the electronic equipment is one of the major focal points of the design process and the key to successful product launch. The two-phase loop thermosyphone which is a good candidate among many available options was investigated fur cooling of the high power amplifiers. The system is composed of evaporator which contains 6 parallel cold plates, fan cooled condenser, gas-liquid separator, and interconnecting tubes. Experiments were performed for several refrigerant charging values, hs and as a experiment result, the optimum charging value fur this system was proposed. In order to optimize the system design, the operating cycle pressure and inlet/outlet temperatures of evaporator and condenser are measured and analyzed. The effect of the three parameters such as flow rate and temperature of condenser cooling air, and thermal load on the evaporator are investigated. The lower the operating pressure and the cycle temperatures are also better to prevent the leakage of the system. The system invesigated in this paper can be directly used for cooling of a real unmanned wireless communication station.

• 한국항해항만학회지
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• 제38권6호
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• pp.567-575
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• 2014

In recent times, an obvious strategy in liner shipping markets that has come to the fore is slow steaming. Nowadays, most liner shipping companies have decelerated the voyage speed to 15-18 knots on major routes, and some leading liner shipping companies have a plan to reduce it to below 15 knots. Slow steaming is helpful in reducing the operating cost and the amount of greenhouse-gas emissions on a single vessel with lower fuel consumption. However, it also creates various negative effects such as the opportunity cost, additional fixed costs and an in-transit inventory cost on a loop. Hence, the net operating cost on a loop is changing dynamically due to the changes of voyage speed based on various slow steaming effects. The aim of this study is to analyze the slow steaming effects in the liner shipping, and to find the best voyage speed that minimizes the operating cost on a loop. Moreover, this study suggests the recommendable strategy for liner shipping companies. To achieve the aim of this study, a simulation model has been designed using System Dynamics.

• Journal of Astronomy and Space Sciences
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• 제26권1호
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• pp.47-58
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• 2009

In this study, a Hardware-In-the-Loop (HIL) simulator using thrusters is developed to validate the spacecraft attitude system. To control the attitude of the simulator, eight cold gas thrusters are aligned with roll, pitch and yaw axis. Also linear actuators are applied to the HIL simulator for automatic mass balancing to compensate the center of mass offset from the center of rotation. The HIL simulator consists of an embedded computer (Onboard PC) for simulator system control, a wireless adapter for wireless network, a rate gyro sensor to measure 3-axis attitude of the simulator, an inclinometer to measure horizontal attitude, and a battery set to supply power for the simulator independently. For the performance test of the HIL simulator, a bang-bang controller and Pulse-Width Pulse-Frequency (PWPF) modulator are evaluated successfully. The maneuver of 68 deg. in yaw axis is tested for the comparison of the both controllers. The settling time of the bang -bang controller is faster than that of the PWPF modulator by six seconds in the experiment. The required fuel of the PWPF modulator is used as much as 51% of bang-bang controller in the experiment. Overall, the HIL simulator is appropriately developed to validate the control algorithms using thrusters.

• Journal of Electrical Engineering and Technology
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• 제13권2호
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• pp.608-619
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• 2018

As distributed generation (DG) is connected to grid, there is new node-type occurring in distribution network. An efficient algorithm is proposed in this paper to calculate power flow for weakly meshed distribution network with DGs in different load models. The algorithm respectively establishes mathematical models focusing on the wind power, photovoltaic cell, fuel cell, and gas turbine, wherein the different DGs are respectively equivalent to PQ, PI, PQ (V) and PV node-type. When dealing with PV node, the algorithm adopts reactive power compensation device to correct power, and the reactive power allocation principle is proposed to determine reactive power initial value to improve convergence of the algorithm. In addition, when dealing with the weakly meshed network, the proposed algorithm, which builds path matrix based on loop-analysis and establishes incident matrix of node voltage and injection current, possesses good convergence and strong ability to process the loops. The simulation results in IEEE33 and PG&G69 node distribution networks show that with increase of the number of loops, the algorithm's iteration times will decrease, and its convergence performance is stronger. Clearly, it can be effectively used to solve the problem of power flow calculation for weakly meshed distribution network containing different DGs.

• 한국임상수의학회지
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• 제25권6호
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• pp.540-544
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• 2008

Four dogs were presented with the history of progressive abdominal distension and regurgitation. Survey abdominal radiographs revealed gastric dilatation-volvulus (GDV) with a distended, gas-filled stomach and double bubbles. The mean time from onset of clinical signs to presentation to a clinic was 3.25 hours. In three dogs, orogastric tubes were inserted and their stomachs were decompressed. However, we failed to insert the tube in the remaining one dog. Among these four dogs, gastrotomy was performed in two dogs to remove the gastric contents and to decompress the stomach additionally during surgery. The dogs with GDV were treated with belt-loop gastropexy (n=3) or circumcostal gastropexy (n=1) to prevent recurrence. Necrosis of gastric or splenic tissues was not observed during surgical intervention. All four dogs recovered uneventfully, and no recurrence was found in long term follow-up during $1{\sim}3$ years.