• 대한기계학회논문집B
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• 제20권8호
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• pp.2626-2636
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• 1996

A study of soot deposition and reentrainment was carried out both theoretically and experimentally to understand behavior of soot formed by incomplete combustion in a diesel engine. Theoretically, soot deposition on engine cylinder wall and/or piston head was studied with a stagnation point flow approximation. Soot reentrainment occurred upon exhaust gas blowdown was also studied by assuming a long-normal shear velocity distribution. Experimentally, a LPG$O_2/N_2$ flame impinging on a disk, produced by a concentric tubular burner, was chosen as deposition configuration and a shear flow unit with compressed air was installed for the study of reentrainment. For selected flame configuration, soot deposition measurements were conducted and showed that the dominant deposition mechanism was thermophoresis. Distributions of gas temperature and soot number density were estimated by combining data obtained by a B-type thermocouple with a thermophoretic transport theory. Disk temperature distributions were directly measured using a K-type thermocouple. Soot size and morphology were estimated from a TEM photograph. Ratios of soot deposit to reentrained amount were measured for a wide range of shear flow velocities, which showed that the reentrainment model was reasonable.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2009년도 추계학술대회
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• pp.861-865
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• 2009

지금까지 자동차에서의 기술 개발이 엔진 성능과 같은 기계 중점적으로 이루어졌다면 최근에는 전자제어장치(ECU, Electronic Control Unit)를 활용하여 안전, 편의성, 비용 등을 개선하는 전자적 측면의 기술 개발이 활발하게 진행이 되고 있다. 또한, 자동차에 대한 소비자들의 선호가 빠른 속도로 변함에 따라 모델수가 다양해지고 첨단 서비스 개발로 인해 요구되는 소프트웨어의 복잡도가 크게 증가되었다. 이 같은 변화로 자동차 제조비용에서 소프트웨어 개발비용이 상당한 비중을 차지하게 되었고 자동차 업계는 이를 대응하기 위하여 응용 소프트웨어를 모듈별로 재사용할 수 있고 다른 제어장치에도 쉽게 이식할 수 있도록 자동차용 임베디드 시스템의 표준인 OSEK/VDX를 제정하였다.[8] 본고에서는 위의에서 언급한 급변하는 환경을 대응하기 위한 대안으로 제시된 OSEK/VDX표준을 살펴보고, 실제 OSEK/VDX를 이용한 실시간 OS구조에 대하여 알아보자 한다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2018년도 춘계학술대회
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• pp.162-163
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• 2018

해양환경 및 배출가스 규제로 지금까지와는 다른 새로운 연료공급시스템을 적용하게 되는 LNG 추진 선박의 경우 초기 설계 단계에서 위해도 평가가 수행된다. 위해도 평가는 위험에 대한 분석과 평가를 체계적으로 가능하게 하는 일련의 논리적인 단계이다. LNG 연료추진선박은 크게 LNG Tank, Fuel Gas Supply System, Bunkering Manifold, LNG Engine으로 구성되며 이는 해당 선박의 특성, 크기, 항로, 운항거리, 사용엔진 등에 따라 구성요소가 달라지므로 각각의 선박에 대한 위험 요소가 달라지며, 위해도 분석 또한 달라진다. 본 연구에서는 LNG를 연료로 하는 선박들의 시스템에 대해 고찰하고, 실제 위험도 평가가 진행된 몇 가지 사례 선박들의 위해도 평가에 대한 분석을 하고자 한다.

• 한국전산유체공학회지
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• 제13권2호
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• pp.48-54
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• 2008

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 추계 학술대회논문집
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• pp.227-231
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• 2007

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication and ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2001년도 Proceedings ICPE 01 2001 International Conference on Power Electronics
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• pp.281-285
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• 2001

This paper proposes a snubber circuit for flying capacitor multilevel inverter and converter. The proposed snubber circuit makes use of Undeland snubber as basic snubber unit. It has such an advantage of Undeland snubber used in the two-level inverter. Compared with conventional RLD/RCD snubber for multilevel inverter and converter, the proposed snubber keeps such good features as fewer number of components, reduction of voltage stress of main switching devices due to low overvoltage, and improved efficiency of system due to low snubber loss. In this paper. the proposed snubber is applied to three-level flying capacitor inverter and its feature is demonstrated by computer simulation and experimental result.

• 한국산학기술학회:학술대회논문집
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• 한국산학기술학회 2009년도 추계학술발표논문집
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• pp.279-282
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• 2009

Motohawk ECU(Engine Control Unit)에 의한 가솔린기관의 연료분사제어 알고리즘 연구를 통하여 연비를 절감할 수 있는 방안을 연구한다. 실제 차량엔진 ECU는 캘리브레이션 이외의 제어 알고리즘을 변경하여 구현하기가 쉽지 않으므로 상기의 프로토타입 ECU를 활용하여 연료분사제어 로직을 변경해가면서 연료분사와 관련된 여러가지 파라메터의 연구가 가능하다. 또한 프로그래밍은 Matlab과 Simulink로 구현할 수 있어서 최적연비를 얻기 위한 로직의 구현을 실시간으로 할 수 있으며 차량의 특성상 프로그램의 임베딩이 가능하여야 하므로 이러한 목적에 프로토타입 ECU에 의한 로직개발은 많은 장점이 있다. 이러한 ECU를 활용하여 여러 가지 제어 변수에 의한 최적화된 연료분사 로직의 설계 및 미치는 영향을 평가한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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• pp.166-172
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• 1998

In contrast to the conventional intake manifold of steel or aluminum material, the lst natural frequency range of plastic intake manifold becomes very lower to ca. 40Hz. That causes negative effects on the engine control unit installed inside the throttle body. In this paper, support design concepts to increase the natural frequency range larger than max. 200Hz are suggested based on the vibration analysis results using finite-element method. In conclusion, it is shown that the vibration level can be reduced most effectively by the installation of the neck support bracket between the throttle body and the plenum chamber.

• 한국자동차공학회논문집
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• 제6권1호
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• pp.205-212
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• 1998

In this study, the effects of water vapor in inlet air on combustion efficiency, general performance, knock characteristics and emission gas concentration were investig- ated through the experiments of combustion and vibration analyses, emission gas analysis by changing water vapor quantity in inlet air with temperature and humidity auto control unit. With partial vapor pressure increase, the brake torque at wide open throttle status decreased and the average ignition delay angle increased, IMEP (indicated mean effective pressured using the integral and 3rd derivatives of filtered cylinder pressure as knock intensity, which matched well with the method of frequency power spectrum of block vibration signal. Water vapor in intake air had influence on the spark knock sensitivity. With the increase of water vapor content in intake air NOx emission was decreased and HC emission was increased.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2005년도 추계학술대회 논문집
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• pp.1021-1027
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• 2005

The Diesel Multiple Units (DMU) is a successful mass transportation system, that is being, continuously, on demand by train operators and railway authorities around the globe. One of its advantages is the fact that a diesel engine, along with the correct propulsion and control equipment, could also be used on either Electrified or Non-Electrified Railway Lines. Currently, there are almost 12,000 DM Units being used worldwide and the demand is on the increase. This paper describes the special features as well as the advantages/disadvantages of the different types of the DMUs according to the propulsion systems that are employed, to help establish a trend in the DMU market.