• 한국연소학회:학술대회논문집
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• 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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• pp.109-112
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• 2015

This article describes a cellular instability and laminar burning velocity of simulated synthetic natural gas(SNG) including 3% hydrogen. In this study, experimental apparatus is employed using cylindrical bomb combustor, and investigation is carried out with high speed camera and Schlieren system. The cellular instability is caused by the buoyancy, hydrodynamic instability. Unstretched burning velocity can be determined by extrapolated stretch rate of zero point from measured results. These results were also compared with numerical calculation by Chemkin package with GRI 3.0, USC-II, WANG, C3 Fuel mechanism. As an experimental conditions, equivalence ratios was adjusted from 0.8 to 1.3. From results of this work, the one was found that the cellular instability has occurred by effect of thermal expansion rate and flame thickness. As the other results, unstretched laminar burning velocity was best coincided with GRI 3.0 mechanism.

• 한국자동차공학회논문집
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• 제12권1호
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• pp.55-60
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• 2004

Residual gas acts as a diluent which results in reducing the in-cylinder temperature as well as the flame speed, significantly affecting fuel economy, NOx emissions and combustion stability. Therefore it is important to determine the residual gas fraction as a function of the engine operating parameters accurately. However, the determination of the residual gas fraction is very sophisticated due to the unsteady state of induction and exhaust process. There has been little work toward the development of a generally applicable model for quantitative predictions of residual gas fraction. In this paper, a simple model for calculating the residual gas fraction in SI engines was suggested. The amount of fresh air was evaluated through AFR and fuel consumption. After this, from the intake temperature and pressure, the amount of total cylinder-charging gas was estimated. The residual gas fraction was derived by comparing the total charging and fresh air. This results coincide with measured EGR value very well.

• 한국자동차공학회논문집
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• 제12권1호
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• pp.10-16
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• 2004

The Homogeneous Charge Compression Ignition (HCCI) engine has advantage for reducing the NOx and P.M. simultaneously. Therefore, HCCI engine is receiving attention as a low emission diesel engine concept. This study was carried out to investigate the characteristics of combustion and exhaust emission for operating conditions in a direct injection type of HCCI engines such as supercharged and naturally aspirated using diesel fuel and additive. From the experimental result, we found that cool flame was always appeared and also it was difficult to control combustion characteristics by changing the injection timing in HCCI. In addition, at the lean air-fuel ratio and high speed range, it was observed that charging air pressure, additive or increasing intake air temperature is effective to increase combustion performance and reduce exhaust emission. We concluded that chemical reaction by the increasing intake air temperature or additive without physical improvement has limitation for reduction of exhaust emission.

• 오토저널
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• 제5권4호
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• pp.47-61
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• 1983

In this paper the simulation of a thermodynamic power cycle for a 4-stroke, single-cylinder, spark-ignition engine was studied. In this simulation the cylinder volume was restricted to two zones, a burnt and an unburnt zone, and the convective heat transfer from cylinder contents to surroundings was considered. The chemical species in burnt gas considered was 12 species including H$_{2}$O, H$_{2}$, OH, H, N$_{2}$, NO, N, CO$_{2}$, CO, $O_{2}$, O and Ar. Using this model, computer program for compression, ignition and expansion processes was composed and pressure, temperature and composition of cylinder gas at each crank angle were computed. The composition of CO$_{2}$, CO, $O_{2}$ in the burnt gas when exhaust valve opens, the maximum temperature, the maximum flame speed and the combustion duration were also computed as a function of equivalence ratio. The relation between burnt mass fraction and burnt volume fraction was also computed.

• Tribology and Lubricants
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• 제25권1호
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• pp.66-72
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• 2009

Al-based composites reinforced with SiC particulate were fabricated using a thermal spray process, and dry sliding wear behavior of the composites was investigated. Pre-mixed Al and SiC powders were sprayed on an A16061 substrate by flame spraying, and dry sliding wear test were performed under various sliding speed and applied load conditions against ${Al_2}{O_3}$ ball. Wear behavior of the composites was studied by using scanning electron microscope (SEM), energy dispersive X-ray spectroscopy (EDX) and X-ray diffraction (XRD). And build-up mechanism of MML on the worn surface of the composites was examined. It was revealed that these MML was formed of debris from the contact surface of the composites and effected to wear behavior of the composites protecting the contact surface of the composites.

• Composites Research
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• 제27권4호
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• pp.123-129
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• 2014

세라믹 기지 복합재료는 세라믹 기지에 고 용융 온도, 낮은 밀도, 고 탄성과 강도를 가진 탄화물, 질화물, 보론화물, 산화물 등의 강화재료를 끼워 넣어 파괴 인성을 높인 것이다. 이들 소재는 우주 비행체의 열 차폐 시스템, 또 고온의 가스 터빈의 연소실, 터빈 블레이드, 고정자(Stator) 베인 등의 부품에 사용되며, 버너와 화염 유지기(Flame holder), 고온 가스 덕트에는 산화 CMC가 사용되고 있고, 극심한 열 충격이 일어나는 브레이크 디스크나 시스템의 부품, 그리고 슬라이드 베어링 부품에도 활용되고 있다. 이러한 CMC에 대한 연구 개발은 미국의 우주 비행체 활용 목적을 비롯하여, 미국, 일본, 유럽에서의 초고속항공기와 가스 터빈용, 그리고 핵 융합용 등의 목적으로 국방과 에너지 산업과 같은 전략적 분야의 활용을 목표로 개발되고 있다.

• International Journal of Automotive Technology
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• 제6권4호
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• pp.323-332
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• 2005

A cylindrical constant volume combustion chamber was used to investigate the flow characteristics at the spark electrode gap and the combustion characteristics of a homogeneous charged methane-air mixture under various overall charge pressures, excess air ratios and ignition times. The flow characteristics, including the mean velocity and turbulence intensity, were analyzed with a hot wire anemometer. Combustion pressure development measured by piezoelectric pressure transducer, a flame propagation image acquired by ICCD camera and exhaust emissions measured by 2-valve gas chromatography were used to investigate effects of initial pressures, excess air ratios and ignition times on the combustion characteristics. It was found that the mean velocity and turbulence intensity had the maximum value around 200-300 ms and then decreased gradually to a near-zero value after 3000 ms and that the combustion duration was shorten and the flame speed and laminar burning velocity had the highest value under the condition of an excess air ratio of 1.1, an overall charge pressure of 0.15 MPa and an ignition time of 300 ms in the present study. The $CO_2$ concentration was proportional to the ignition time and overall charge pressure, the $CO_2$ concentration was proportional to the excess air ratio, and the UHC concentration was inversely proportional to the ignition time and overall charge pressure.

• 한국항행학회논문지
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• 제17권1호
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• pp.107-114
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• 2013

본 논문에서는 무인항공기 터보제트 엔진의 가속도를 제어하는 제어기를 제안한다. 압축기 회전 속도를 추정하기 위해 고이득 관측기를 사용하고 퍼지 추론 기법과 PID 제어 알고리즘을 적용하는 터보제트 엔진 제어기를 설계한다. 터보제트 엔진의 가 감속 시 서지현상과 flame-out 현상을 방지하기 위해 연료 유량 제어 입력을 퍼지 PID 제어기로 생성한다. 기준 가속도를 설정하고 연료유량 제어를 퍼지추론에 의해 정하도록 한다. 제안된 제어기의 성능을 확인하기 위해 MATLAB을 사용한 컴퓨터 시뮬레이션을 수행하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제31권1호
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• pp.26-33
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• 2007

The intake swirl motion, as one of dominant effects for an engine combustion. is very effective for turbulence enhancement during the compression process in the cylinder of 2-valve engine. Because the combustion flame speed is determined by the turbulence that is mainly generated from the mean flow of the charge air motion in intake port system. This paper describes the experimental results of swirl flow and combustion characteristics by using the oil spot method and back-scattering Laser Doppler velocimeter (LDV) in 2-valve single cylinder transparent LPG engine using the liquid phase LPG injection. For this. various intake port configurations were developed by using the flow box system and swirl ratios for different intake port configurations were determined by impulse swirl meter in a steady flow rig test. And the effects of intake swirl ratio on combustion characteristics in an LPG engine were analyzed with some analysis parameters that is swirl ratio. mean flow coefficient, swirl mean velocity fuel conversion efficiency. combustion duration and cyclic variations of indicated mean effective pressure(IMEP). As these research results, we found that the intake port configuration with swirl ratio of 2.0 that has a reasonable lean combustion stability is very suitable to an $11{\ell}$ heavy-duty LPG engine with liquid phase fuel injection system. It also has a better mean flow coefficient of 0.34 to develope a stable flame kernel and to produce high performance. This research expects to clarify major factor that effects on the design of intake port efficiently with the optimized swirl ratio for the heavy duty LPG engine.

• 한국화재소방학회논문지
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• 제26권2호
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• pp.90-96
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• 2012

외장재에 의한 수직화재확산은 확산속도가 구획화재에 비해 매우 빨라 이에 대한 화재의 특성 분석이 요구된다. 본 연구에서는 건물 외부에서 발생한 화재가 연소 확대되면서 수직으로 상승하여 개구부를 통해 유입되는 화재의 성상에 대해서 외장재로 널리 사용되는 심재가 폴리에틸렌인 일반 알루미늄복합패널에 대해 화재시뮬레이션을 적용하여 연구하였다. 그 결과, 수직확산화염은 화재초기에 2층까지 상승하는 데는 약 135초가 걸렸지만 10층까지는 470초, 최고층인 30층까지 상승하는 데는 711초에 도달하는 것으로 분석되어 고층부로 갈수록 난류 및 외장재 설치공간의 연돌효과에 의해서 급격히 확대되는 것을 알 수 있었다. 이러한 연구 결과로 외장재가 설치된 건축물의 화재 시 개구부를 통한 화재는 동시다발적으로 그 건물의 내부에 확대되는 심각성을 확인할 수 있었다.