• 한국신재생에너지학회:학술대회논문집
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• 2005.11a
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• pp.60-75
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• 2005

천연가스차량이 배출하는 미연 탄화수소 중 약 80%이상이 메탄으로 구성 되어있다. 메탄은 그 자체로 유독성 물질은 아니지만 이산화탄소와 더불어 지구온난화를 유발하는 온실가스로 향후 강력한 규제가 예상되는 물질로 이를 저감하는 기술 개발이 이루어져야하나 연료 특성상 이를 줄이는데 어려움이 있다. 최근 연구에 의하면 천연가스엔진에 수소를 일정량(15%이상) 첨가할 경우 배출가스 및 성능 이 상당량 개선되는 결과를 보이고 있다. 이는 종래 천연가스 연소의 문제점인 지연된 화염 전파 속도를 수소 연료를 첨가함에 따라 화염 전파속도를 촉진시켜 적정한 연소를 야기 시켜 미연탄화수소 배출이 줄어들고 열효율도 향상되는 결과를 보이고 있다. 이와 같이 수소와 천연가스연료의 각각의 장점을 활용한 Hy-thane 엔진을 개발할 경우 무공해엔진에 근접한 초 저공해 동력장치 개발이 가능하며 이에 대한 상용화 측면에서 산업용 발전기, GEHP, 차량용 엔진 등 활용도가 크기 때문에 그 개발이 절실히 필요하다고 할 수 있다. 따라서 본 과제에서는 이중연료를 사용하는 수소-천연가스 기관을 개발하고 이를 효과적으로 제어할 수 있는 제어시스템을 개발하여, 기관효율 향상과 배기가스저감을 이루었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2001.04a
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• pp.35-38
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• 2001

The aerothermodynamic characteristics of SCRamjet engine for the airbreathing populsion system of the next generation flight vehicle are described. As the flow is passing by, combustion caused the total pressure loss and the Mach number decrease, but nozzle exit velocity is large enough to produce net thrust. To simulate supersonic combustion test, preliminary design of ground-based blowdown type supersonic combustion tunnel is attained. Minimum allowable operating pressure and mass flow rate are calculated for the design Mach number of 2.5 at the test section of a supersonic combustion tunnel.

• Journal of Advanced Marine Engineering and Technology
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• v.17 no.5
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• pp.33-43
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• 1993

Recent marine propulsion diesel engines tend to become slower in speed and longer in stroke for the higher engine efficiency, and in these long stroke and slow speed engines the digital governors are highly recommended to be used. But, in the present digital governors only the feedback of the engine rpm-signal is used for the engine speed control and it does not work so effectively when the load variation is large. In this paper, a new method is proposed to improve the speed control performance in a diesel engine, by adding the torque feedback loop to the present digital governor which uses the rpm feedback PID controller only. And also a method is proposed to adjust the parameters of the PID controller optimally.

• Journal of Advanced Marine Engineering and Technology
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• v.24 no.4
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• pp.435-440
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• 2000

The speed control system of diesel engine is considerably nonlinear. Therefore, a countermeasure such as gain scheduling used to be incorporated to compensate this nonlinearity. On the other hand, it is said that fuzzy control is very robust against nonlinearity. But it is difficult to get a satisfactory response with only fuzzy control in real system. In this paper authors design a fuzzy-PI controller for the speed control of Medium diesel engine and carry out experiments with dedicate system implemented by Intel 80916KC to real diesel engine, Deawoo MAN 6Cyl., 1800rpm driving 3$\psi$220V, 150KW generator. We confirm the effectiveness of proposed control system.

• Journal of Advanced Marine Engineering and Technology
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• v.26 no.6
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• pp.638-645
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• 2002

This paper presents a scheme for integrating PID control, gain scheduling and emerging techniques in the field of artificial intelligence, such as fuzzy logic and genetic algorithms for the speed control of a marine diesel engine. At first, local PID controllers are designed based on a local model obtained at each speed mode, whose parameters are optimally tuned using a real-coded genetic algorithm. Then, fuzzy "if-then" rules combine the local controllers as a consequence part to implement fuzzy gain scheduling. To demonstrate the performance of the proposed fuzzy PID controller on overall operating conditions, a set of simulation works on B'||'&'||'W's 4L80MC diesel engine are carried out.t.

• Journal of Advanced Marine Engineering and Technology
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• v.39 no.6
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• pp.642-648
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• 2015

Recently, there have been many studies pertaining to reducing energy consumption on ships. As part of those studies, the energy consumption of ships can be reduced by understanding and controlling the varying loads, excluding fixed loads. In existing ships, engine room fans are usually operated based on the actual experience of the crew without any special guidelines. To realize energy reduction, we investigate the characteristics of engine-room fans, and we propose an energy-management system called the engine room fan control system (ERFCS) and the ERFCS algorithm. The ERFCS controls the fan speed depending on the temperature and pressure, where one to four fans are operated depending on changes in the load. In addition, the minimum rotation speed of the engine-room fan was limited to 50% to prevent the surging phenomenon, which is due to fan damage or low pressure resulting from mechanical friction or heating at low fan speeds. We develop a fan control system simulation model using LabVIEW that is based on the proposed algorithm and ISO 8861. Finally, we perform simulations to confirm that operation of the proposed fan control system is possible using only 46.4% of the power required by the existing method.

• Journal of Fisheries and Marine Sciences Education
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• v.7 no.2
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• pp.201-206
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• 1995

• Proceedings of the Korean Society of Fisheries Technology Conference
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• 1994.06c
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• pp.52-63
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• 1994

• Life and Agrochemicals
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• v.26 no.3 s.206
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• pp.28-31
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• 2005

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.12-12
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• 1998

무기체계의 추진체로서 고체 로켓트 추진기관이 제작의 용이성, 구조의 간단성, 이에 따른 저렴한 제작비, 그리고 고 신뢰도 확보가능 등의 여러 장점으로 대부분의 현존 전술 유도무기에 채택되어 사용되어 오고 있으나 대응, 방어 무기체계의 빠른 발전으로 이에 따른 새로운 추진기관의 유도무기체제가 요구되고 있다. 램제트 기관은 공기흡입추진기관으로 상대적으로 높은 비추력(1000-2000s)과 추력 중량비(∼20)을 가지며, 이로 인해 기존의 로켓 엔진에 비해 4-5배의 성능을 낼 수 있으며, 초음속 장거리 비행에 적합하다며, 또한 높은 속도영역까지 운용가능하고 구조가 비교적 간단하다.