• 대한기계학회논문집B
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• 제21권4호
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• pp.473-485
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• 1997

Detailed experimental study has been made of air blast kerosene spray flames with and without swirl in combustion air flow. Phase-Doppler detect technique is used to measure Sauter mean diameter, axial component mean and rms velocity, size-velocity correlation, and number density. These measurements are obtained for both nonreacting and reacting cases under several stable flame conditions. The results show that the introduction of swirl to the combustion air modifies the spatial distribution of droplet size, velocity, and number density, and thus alters the flame structure. However, due to the weak swirl intensity, the overall structure of swirling flames are essentially same as that of nonswirling flames. Physical model of structure of air blast atomized spray flames is projected to show that spray flames are composed of three distinct regions: the two-phase mixture region, the main reaction and the intermittent combustion region. Near the atomizer, two phase mixture of droplet and air is formed in the core region. This dense spray region is characterized by high droplet number density and the strong convective effect. There follows the main combustion region where the main flame penetrates within the spray boundary. Main reaction region of these flames are governed by internal group combustion mode. Finally there exists the intermittent combustion region where local group burning or isolated droplet burning occurs.

• 한국자동차공학회논문집
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• 제12권2호
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• pp.32-38
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• 2004

This study was performed to investigate the behavior of liquid and vapor phase of fuel mixtures with different piston cavity diameters in a optically accessible engine. The conventional engine was modified as Central Injected DI gasoline engine with swirl motion. Two dimensional spray fluorescence images of liquid and vapor phase were acquired to analyze spray behavior and fuel distribution inside of cylinder using exciplex fluorescence method. Piston cavity geometries were set by Type S, M and L. The results obtained are as follows. In the spray formation after SOI, the cone angle and width of the spray were decreased at late injection timing. With a fuel injection timing of BTDC $180^{\circ}C$, fuel was not greatly affected in a piston cavity but generally distributed as homogeneous mixture in the cylinder. With a fuel injection timings of BTDC $90{\circ}C$ and $60^{\circ}C$, fuel mixture was widely distributed in near the cavity center. As a injection timing was late in the compression stroke, residual width of fuel mixture was narrow in proportion to piston cavity.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.5-8
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• 2010

본 논문에서 연구하고자 하는 분사기는 다단 연소 사이클 엔진 연소기에 적용하는 분사기이다. 본 분사기에서 연료는 접선홀을 통해 와류 형상으로 분무되며, 예연소기에서 생성된 산화제 과잉 가스는 중앙에서 jet의 형태로 공급된다. 이러한 기체-액체 분사기의 상압/고압환경에서의 분무특성 및 분사기의 리세스에 따른 분무특성의 차이를 알아보았다. 이러한 결과들은 향후 다단 연소 사이클 엔진 개발의 기본 데이터로 활용될 수 있을 것이다.

• 한국자동차공학회논문집
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• 제17권4호
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• pp.79-85
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• 2009

Low temperature combustion regime for the simultaneous reduction of nitrogen oxides ($NO_x$) and paticulate matter (PM) is demonstrated in single cylinder engine at various operating parameters, such as EGR rate, injection timing, EGR temperature, amount of fuel and swirl rate. Low temperature combustion is accomplished by high exhaust gas recirculation (EGR) rate in this study. Generally, the emission of $NO_x$ almost completely disappears and PM significantly increases in the first decreasing regime of oxygen concentration but after peaking about 10~12% oxygen concentration, PM then decreases regardless of fuel injection quantity. Low temperature combustion regime was extended by low EGR temperature, high injection pressure and low amount of fuel.

• 에너지공학
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• 제22권2호
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• pp.96-104
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• 2013

석탄가스화 기술은 청정석탄에너지 기술 중에서 아주 중요한 대안으로 인식되고 있으며, 이에 전 세계적으로 차세대 석탄가스화기라고 할 수 있는 고효율 저비용 석탄가스화기를 개발하고 있다. 본 연구에서도 이러한 목적의 달성을 위하여 저비용으로 구현이 가능한 컴팩트 석탄가스화기를 개발하고 있으며, 다수개의 공급부로 이루어진 일체형 이중선회형 버너를 개발하였다. 개발된 버너의 가스화 운전조건을 확보하기 위하여 미분탄 분배기와 함께 기존의 석탄가스화기 몸체에 설치하여 가스화 실험을 수행하였다. 인도네시아산 아역청탄인 ABK 탄을 사용하여 1.5톤/일의 파일럿 규모로 $6.4{\sim}7.2kg/cm^2$, $1170{\sim}1300^{\circ}C$ 조건에서 운전을 수행하였다. 우선 성능평가보다는 안정적인 가스화기 운전조건을 확보하는데 중점을 두었다. 그 결과, 안정적인 운전조건에서 탄소전환율은 84.0%, 냉가스 효율 52.1%를 확보할 수 있었다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 1998년도 제17회 KOSCI SYMPOSIUM 논문집
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• pp.79-84
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• 1998

In this paper we show design and operation of 1MWth pulverized coal combustion test facility. The test facility is consists of coal feeding system, furnace and flue gas treatment system. The furnace is equipped with a top-fired burner in order to avoid influence of gravity on the coal particles. There are two part of vertical(VP) and horizontal pass(HP) at furnace. We can measure temperature and species of coal flames in vertical pass. Also, there is horizontally arranged section where investigation regarding corrosion and deposit formation will be carried out. The burner of combustor was externally air staging burner(EASB) type made by IFRF. The pulverized high bituminous(Blair athol) coal from Australia was used as fuel, and the particle size less than 80 ${\mu}m$ was 83.4%. Overall excess air ratio was 1.2.

• 한국자동차공학회논문집
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• 제14권4호
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• pp.39-48
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• 2006

In this research, in order to study the spray, combustion, and emission characteristics of the common rail DME engine, the target engine was disassembled, and 3D CAD file was constructed using a 3D measurement machine and a rapid prototyping machine. Using the obtained 3D geometry, fine moving meshes are generated, and three dimensional non-steady turbulence flow field and combustion phenomenon including spray were numerically analyzed. As a result, IMEP of DME and diesel in medium and high speed revolution showed similar performance. As the DME fuel start to burn in spray area, the vaporized fuel rapidly spreads squish area in low speed revolution. In the case of DME engine, CO and NOx are relatively consistent with experiment results. It was found that the break-up, evaporation, collision model of DME fuel need to be properly adjusted through matching the characteristics of fuel and injector for further improvement.

• 한국추진공학회지
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• 제2권2호
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• pp.24-29
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• 1998

Duplex Type의 2-유체 공기충돌형 Swirl 인젝터의 분무특성을 파악하고자 유체공급압력 0~13kg/$\textrm{cm}^2$ 범위에서 유량계수, 등가 분산각, 질량분포를 실험적으로 구하였다. 일반적으로 기체의 총 유량이 증가할수록 미립화는 촉진되나 반경방향 유량이 많은 경우에 분무형상은 비교적 안정적이었으며, 축방향 보다는 반경방향 선회기가 미립화에 미치는 영향이 컸다. 3kg/$\textrm{cm}^2$을 제외하고는 물 유량이 증가함에 따른 등가 분산각의 변화는 미소하였고, 기체의 유량증가도 마찬가지였다. Patternator를 사용한 질량 분포는 반경방향 기체유량이 증가함에 따라 분포곡선의 최대점은 낮아지면서 더 넓은 영역에 걸쳐 분포하였고, 물 유량의 증가에 따른 질량중심점의 위치는 변화가 없었다.

• 대한조선학회논문집
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• 제55권6호
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• pp.474-481
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• 2018

This paper is to compare by numerical analysis the flow characteristics and propulsion performance of stern with the shape change of K-duct, a pre-swirl duct developed by Korea Research Institute of Ships & Ocean Engineering (KRISO). First, the characteristics of the propeller and the resistance and self-propulsion before and after the attachment of the K-duct to the ship were verified and the validity of the calculation method was confirmed by comparing this result with the model test results. After that, resistance and self-propulsion calculations were performed by the same numerical method when the K-duct was changed into five different shapes. The efficiency of the other five cases was compared using the delivery horsepower in the model scale and the flow characteristics of the stern were analyzed as the velocity and pressure distributions in the area between the duct end and the propeller plane. For the computation, STAR-CCM +, a general-purpose flow analysis program, was used and the Reynolds Averaged Navier-Stokes (RANS) equations were applied. Rigid Body Motion (RBM) method was used for the propeller rotating motion and SST $k-{\omega}$ turbulence model was applied for the turbulence model. As a result, the tangential velocity of the propeller inflow changed according to the position angle change of the stator, and the pressure of the propeller hub and the cap changes. This regulated the propeller hub vortex. It was confirmed that the vortex of the portion where the fixed blade and the duct meet was reduced by blunt change.

• 대한기계학회논문집B
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• 제40권7호
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• pp.417-427
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• 2016

본 논문은 반 쐐기형 연소실에서 포트 형상에 따른 정상유동 특성을 비교한 연구의 첫 번째로 통상적인 충격식 스월측정기 평가위치인 1.75B에서 입자영상유속계로 반 쐐기형 연소실에 직선형 포트와 나선형 포트를 적용하여 평면유속을 측정하고 비교하였다. 속도분포 분석 결과 직선형 포트에서는 밸브리프트 4 mm 이하, 그리고 나선형 포트에서는 2 mm 이하에서 두 개의 스월이 형성되고 이후 리프트가 증가하면 하나의 스월만 관찰된다. 리프트에 따른 유동체계의 천이점이 포트형상에 따라 상이하여 직선형 포트에서는 리프트 4 mm와 5mm를 경계로 유동 특성이 완전히 바뀌는 반면, 나선형 포트에서는 리프트 증가에 따라 점진적 변화만 관찰된다. 또한 모든 포트에서 1.75B 위치에서 편심도는 측정값이 왜곡되지 않는 범위에 들어오지 않고, 특히 직선형 포트의 편심도가 매우 크다. 동시에 포트형상에 관계없이 ISM 평가와 상응하는 실린더 중심 기준의 평균접선속도는 ISM 평가에서 가정한 속도보다 매우 낮고, 속도분포 특성도 ISM 평가의 가정과 매우 다르다.