• 제목/요약/키워드: Combustion Visualization

검색결과 219건 처리시간 0.028초

초음속 연소 실험을 위한 연소식 공기 가열기 출구 유동 조건 실험 연구 (A Study on the Flow Conditions of the Combustion Air Heater Outlet for the Supersonic Combustion Experiment)

  • 이은성;한형석;이재혁;최정열
    • 한국추진공학회지
    • /
    • 제26권1호
    • /
    • pp.88-97
    • /
    • 2022
  • 본 연구에서는 직접 연결식 초음속 연소기의 지상 시험 장치에 고온, 고압 공기 공급을 위한 연소식 공기 가열기를 설계 및 제작하였으며, 목표 설계점 만족 여부를 검증하기 위한 실험을 수행하였다. 연소식 공기 가열기 노즐 출구의 상부 경계, 하부 경계 및 중앙에 쐐기를 설치하여 마하수가 2.0 수준을 만족하는 것을 확인하였으며, 연소실 내부 압력 또한 설계점과 비교하여 만족할만한 수준으로 나타났다. 온도의 경우 열전대의 노출되는 정도와 느린 응답 특성에 의해 측정된 온도의 편차가 크게 나타났다. 이후 연소식 공기 가열기 후방에 격리부를 연결하고 동일한 방법으로 마하수를 측정하였으며, 격리부 출구 중앙의 마하수는 1.8~1.9 정도로 소폭 감소하였다.

단기통 디젤엔진에서 함정용 디젤유의 전·후 분사시기가 연소 및 배출가스 특성에 미치는 영향 (Effect of pre-post injection timing of diesel fuel for naval vessel on the combustion and emission characteristics in an optically-accessible single cylinder diesel engine)

  • 이형민
    • Journal of Advanced Marine Engineering and Technology
    • /
    • 제38권7호
    • /
    • pp.868-876
    • /
    • 2014
  • 본 논문에서는 함정에 탑재된 추진용 엔진에 사용되는 디젤연료(MDO)의 분사상태를 가시화가 가능한 단기통 디젤엔진에 적용시켜 전 후 분사시기에 따른 연소특성, 일산화탄소(CO) 및 탄화수소(HC) 배출특성을 규명하고, 연소과정의 가시화를 통하여 연소특성을 분석하는데 초점을 두었다. 전 분사시기가 주 분사시기 쪽으로 지연될수록 실린더 내부 평균유효압력($P_{me}$) 및 최고압력($P_m$)은 상승했으나, 주 분사의 방열율은 저감되고, 일산화탄소 및 탄화수소의 발생량 또한 감소하였다. 후 분사시기가 빨라질 경우 주 분사에 의해 형성된 고온, 고압 하에서 연소가 이루어짐에 따라 실린더 내부 평균유효압력 및 최고압력은 증가하였고, 일산화탄소 및 탄화수소 배출수준 또한 증가하였다. 연소과정을 분석한 결과, 전 분사시기가 늦어질수록 주 분사 시 발생되는 착화지연은 매우 짧아지며, 화염강도는 매우 상승하였다. 분사시기에 관계없이 후 분사 시 착화지연 현상은 발생하지 않았으며, 후 분사시기가 늦어질수록 화염의 강도는 점점 떨어졌다.

연소실 압력변동이 화염안정화와 배출특성에 미치는 영향 (Influence of changing Combustor Pressure on Flame Stabilization and Emission Charncteristics)

  • 김종률;최경민;김덕줄
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2007년도 춘계학술대회B
    • /
    • pp.2354-2359
    • /
    • 2007
  • Influence of changing combustor pressure on flame stabilization and emission index in the swirl-stabilized flame was investigated. The combustor pressure was controlled by suction fan at combustor exit. Pressure index ($P^{\ast}$=Pabs/Patm), where Pabs and Patm indicated the absolute pressure and atmosphere pressure, respectively, was controlled in the range of 0.7${\sim}$1.3 for each equivalence ratio conditions. The flammable limits of swirl flames were largely influenced by changing combustor pressure and they showed similar tendency with laminar flames. NOx emission index decreased with decreasing pressure index for overall equivalence ratio conditions. R.m.s. of pressure fluctuations is increased with decreasing combustor pressure. This flame fluctuation caused incomplete combustion, hence CO emission index increased. These oscillating flames were measured by simultaneous $CH^{\ast}$ chemiluminescence time-series visualization and pressure fluctuation measurement.

  • PDF

직분식 가솔린기관 인젝터의 연료 분무 특성 (Fuel Spray Characteristics of GDI Injector)

  • 권상일;이창식
    • 한국연소학회:학술대회논문집
    • /
    • 한국연소학회 2000년도 제21회 KOSCO SYMPOSIUM 논문집
    • /
    • pp.194-201
    • /
    • 2000
  • This paper is intended to analyze the macroscopic behavior and transient atomization characteristics of the high-pressure gasoline injector in direct-injection gasoline engine. The global spray behavior of fuel injector was visualized by shadowgraph technique. Time-resolved droplet axial and radial velocity components and droplet diameter were measured at many probe positions in both axial and radial directions by a two-component phase Doppler particle analyzer (PDPA). In order to obtain the influence of fuel injection pressure, the macroscopic visualization and experiment of particle measurement on the fuel spray were investigated at 3,5 and 7 MPa of injection pressure under different surrounding pressure in the spray chamber. The results of this work show that the fuel injection pressure of gasoline injector in GDI engine has influence upon the mean droplet diameter, mean velocity of spray droplet, the spray tip penetration, and spray width under the elevated ambient pressure.

  • PDF

초희박 연소를 실현하기 위한 플라즈마 제트의 개발 (A Development of Plasma Jet to Realize Ultra Lean Burn)

  • 오병진;박정서;김문헌
    • 한국자동차공학회논문집
    • /
    • 제6권1호
    • /
    • pp.213-221
    • /
    • 1998
  • The investigation regarding the ignition system of a plasma jet explored by using a constant volume vessel. The purpose of this study is to elucidate relation between the characteristics of the configuration and jet ejection of plasma jet plug, when the sub energy were supplied at plasma jet ignition system. From the results of a visualization by the schlieren system, the jut ejection for plasma jet ignition are depended on the jet plug configuration and sub energy, but the configuration of plasma jet plug is more influenced than the sub energy on the plasma jet ejection. And the plasma jet ignition strongly influences upon the combustion enhancement than the conventional spark ignition.

  • PDF

초음속 유동장 내 평판/cavity를 이용한 연료-공기 혼합의 실험적 연구 (Experimental Study on Fuel-Air Mixing Using Flat Plate/Cavity in Supersonic Flow)

  • 김정우;정은주;김채형;정인석
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
    • /
    • pp.319-322
    • /
    • 2006
  • 초음속 연소가 성공하려면 1 ms의 시간 안에 충분한 연료-공기 혼합이 이루어져야 한다. 본 실험은 마하 1.92유동에서 헬륨을 수직 분사하여 연료-공기 혼합이 어떻게 이루어지는지 살펴보았다. 평판과 공동 두 가지 모델로 실험을 수행하였고, 슐리렌 가시화를 통해 사진을 찍었다. 압력은 초음속 덕트 내에서 충격파가 어떻게 생성되는지에 영향이 많았고, 침투 거리는 J가 커질수록 두꺼워졌다. 공동이 있는 경우 평판일 때보다 침투 거리가 더 컸다.

  • PDF

가솔린 직접분사식 고압 슬릿 노즐의 팬형 분무 특성 고찰 (Fan-shaped Spray Characteristics of High Pressure Slit Nozzle in a Gasoline Direct Injection Engine)

  • 송범근;김종민;강신재
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2003년도 춘계학술대회
    • /
    • pp.2239-2244
    • /
    • 2003
  • A new stratified charge combustion system has been introduced and developed for GDI engines. Before this new GDI system, the stratified mixture was formed by a high pressure swirl injector. But, the special feature of new system is employed of a thin fan-shaped fuel spray formed by a slit type nozzle. Also, this system has been adopted a shell-shaped piston cavity. We made high pressure gasoline injection system and investigated the fan-shaped spray characteristics such as spray tip penetration, spray angle, SMD and velocities of droplets using PDPA(Phase Doppler Particle Analyzer) system and spray visualization system to obtain the concept of the new design and the fundamental data for the next generation GDI system. The experiment was performed at the injection pressures of 5 and 9MPa under the atmospheric condition.

  • PDF

Spray Characteristics of Dimethyl Ether(DME) Fuel Compared to Various Diesel Fuels

  • Lee, Seang-Wock;Kim, Duk-Sang;Cho, Yong-Seok
    • 한국분무공학회지
    • /
    • 제13권2호
    • /
    • pp.65-72
    • /
    • 2008
  • It is recognized that alternative fuel such as dimethyl ether (DME) has better combustion polluting characteristics than diesel fuel, even though the cetane number of DME is almost the same as that of diesel. Characteristics of DME spray were observed experimentally under various ambient conditions using a constant volume chamber and a common-rail injection system. N-dodecane and LPG fuel sprays were also observed under same conditions of DME spray. Using spray images from backlight scattering and Mie scattering, characteristics of fuel sprays such as penetration and spray volume were visualized and quantitatively measured. The measurements showed that the penetration of early period decreased remarkably, because evaporation of alternative fuels became prosperous by the influence of flash boiling phenomenon under the condition of the low temperature and pressure compared with n-dodecane. The penetration of DME and LPG spray received the influence of temperature more largely in comparison with low density, because the specific surface area increased by atomizing in high density.

  • PDF

2유체 정전분무의 액체 미립화 및 분무 특성 (Liquid Atomization and Spray Characteristics in Electrostatic Spray of Twin Fluids)

  • 김정헌;배충식
    • 대한기계학회논문집B
    • /
    • 제25권11호
    • /
    • pp.1552-1560
    • /
    • 2001
  • This paper presents the experimental results of a study undertaken to develop an electrostatic spray system for a combustion application. The characteristics of the liquid atomization and the droplet dispersion in the electrostatic spray of twin fluids were investigated by the optical measurement techniques. The processes associated with the break-up of charged jets were also observed using the laser sheet visualization. The diameter and velocity of droplets were simultaneously measured using the phase Doppler measurement technique. The electrostatic atomization of the liquid fuel depended primarily on the charging voltage and the flow rate, but the dispersion of droplets depended significantly on the aerodynamic flow. Aerodynamic influences on the liquid atomization decreased with an increase of the charging voltage. Consequently, the liquid atomization and the droplet dispersion could be independently controlled using the electrostatic and aerodynamic mechanisms.

튜브내 고압수소가스 누출에 따른 자발점화 현상 유동가시화 연구 (Self-ignition of high-pressure hydrogen gas released into tube)

  • 김용련;이형진;김세환;정인석
    • 한국연소학회:학술대회논문집
    • /
    • 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
    • /
    • pp.247-248
    • /
    • 2012
  • Unidentified self-ignitions were reported when the high-pressure hydrogen gas suddenly leaked out. This paper presents a flow visualization study to investigate the self-ignition mechanism in a test tube how the ignition process is initiated and the flame propagates with measurement of a number of pressure and light sensors installed in the tube supported the analysis of the self-ignition. The test result showed the location of the self-ignition taken place and critical static pressure at the boundary layer for self-ignition.

  • PDF