• Title/Summary/Keyword: Swirl injector

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Spray Structures and Vaporizing Characteristics of a GDI Fuel Spray

  • Park, Dong-Seok;Park, Gyung-Min;Kim, Duck-Jool
    • Journal of Mechanical Science and Technology
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    • v.16 no.7
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    • pp.999-1008
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    • 2002
  • The spray structures and distribution characteristics of liquid and vapor phases in non-evaporating and evaporating Gasoline Direct Injection (GDI) fuel sprays were investigated using Laser Induced Exciplex Fluorescence (LIEF) technique. Dopants were 2% fluorobenzene and 9% DEMA (diethyl-methyl-amine) in 89% solution of hexane by volume. In order to study internal structure of the spray, droplet size and velocity under non-evaporating condition were measured by Phase Doppler Anemometry (PDA). Liquid and vapor phases were visualized at different moments after the start of injection. Experimental results showed that the spray could be divided into two regions by the fluorescence intensity of liquid phase: cone and mixing regions. Moreover, vortex flow of vapor phase was found in the mixing region. About 5㎛ diameter droplets were mostly distributed in the vortex flow region. Higher concentration of vapor phase due to vaporization of these droplets was distributed in this region. Particularly, higher concentration of vapor phase and lower one were balanced within the measurement area at 2ms after the start of injection.

A Numerical Study on Combustion Characteristics of Single Cylinder Engine Fueled with DME (DME를 사용한 단기통 엔진의 연소특성에 관한 수치해석적 연구)

  • Kim, Hyun-Chul;Kang, Woo;Na, Byung-Chul;Kim, Myung-Hwan
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.4
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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.

Spray Characteristics for Specified Regions of High Pressure Swirl Injcetor in Gasoline Direct Injection Engine (가솔린 직접분사식 고압선회 분사기의 분무 영역별 분무 특성 고찰)

  • Song, Bhum-Keun;Kim, Won-Tae;Kang, Shin-Jae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.27 no.1
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    • pp.9-16
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    • 2003
  • According as the industry was developed, the pollution of the environment and atmosphere rose up to the surface. So, the focus is now concentrated on the engines of affinity for nature. And the investigators make more effort to the improvement in the performance of engines, depending to the prices of oil and the anxiety about the exhaustion of the fossil fuel go up. So the GDI engines head up for these necessities. In this experimental study, the spray flow characteristics for a commercial injector equipped in the present GDI engine were investigated, which had a strong influence on the engine performance and emissions. The experiment was performed at the injection pressures of 1, 3, 5 and 7MPa under the atmospheric condition. A PDPA system was used to specify the flow characteristics of the spray. Also, the global spray behavior classified into three regions as leading, main spray and vortex cloud region, was analyzed by using a visualization system. And the regions were compared with each other.

A Study on the Performance of Diesel Automobile Engine with Ultrasonic Fule Supply System(III) (On the case of Turbo-charging Diesel Engine) (초음파 연료공급장치용 디젤자동차의 성능 향상에 관한 연구(III) (과급 디젤기관에 대하여))

  • 최두석;이흥영;류정인
    • Transactions of the Korean Society of Automotive Engineers
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    • v.3 no.4
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    • pp.12-18
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    • 1995
  • To improve the performance of diesel automobile engine, we designed new fuel supply system named ultrasonic fuel supply system. The performance test of diesel automobile engine carried out to examine possibility of practical use of ultrasonic fuel supply system to test engine. This paper deals with the comparative results of performance test of diesel automobile engine in terms of smoke, HC, SFC, PS, thermal, efficiency, torque. Following are obtained result. 1) In naturally aspirated diesel engine, when we use ultrasonic fuel supply system output, fuel consumptions are improved and exhaust gas reduced significantly. 2) In turbo-charging diesel engine both using of ultrasonic fuel supply system and using of conventional injector, engine performance and exhaust gas temperature are almost constant. 3) In turbo-charging diesel engine, when we use ultrasonic fuel supply system, NOx are emitted approximately 3.5% higher than total average. 4) In turbo-charging diesel engine, when we use ultrasonic fuel supply system, smoke and CO are 17% and 11.8% improved respectively.

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CHARACTERISTICS OF WALL IMPINGEMENT AT ELEVATED TEMPERATURE CONDITIONS ON GDI SPRAY

  • Park, J.;Im, K.S.;Kim, H.;Lai, M.C.
    • International Journal of Automotive Technology
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    • v.5 no.3
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    • pp.155-164
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    • 2004
  • The direct injection gasoline spray-wall interaction was characterized inside a heated pressurized chamber using various visualization techniques, including high-speed laser-sheet macroscopic and microscopic movies up to 25,000 frames per second, shadowgraph, and double-spark particle image velocimetry. Two hollow cone high-pressure swirl injectors having different cone angles were used to inject gasoline onto a heated plate at two different impingement angles. Based on the visualization results, the overall transient spray impingement structure, fuel film formation, and preliminary droplet size and velocity were analyzed. The results show that upward spray vortex inside the spray is more obvious at elevated temperature condition, particularly for the wide-cone-angle injector, due to the vaporization of small droplets and decreased air density. Film build-up on the surface is clearly observed at both ambient and elevated temperature, especially for narrow cone spray. Vapor phase appears at both ambient and elevated temperature conditions, particularly in the toroidal vortex and impingement plume. More rapid impingement and faster horizontal spread after impingement are observed for elevated temperature conditions. Droplet rebounding and film break-up are clearly observed. Post-impingement droplets are significantly smaller than pre-impingement droplets with a more horizontal velocity component regardless of the wall temperature and impingement angle condition.

A Parametric Study on Combustion Stability Characteristics of Fuel-rich Gas Generators (설계 인자에 따른 연료 과농 가스발생기의 연소 안정성 특성 연구)

  • Ahn Kyu-Bok;Moon Il-Yoon;Seo Seong-Hyeon;Han Yeoung-Min;Choi Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.171-176
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    • 2006
  • An experimental study on a fuel-rich gas generator was carried out. Thirty seven double-swirl injectors with recess number of 1.5 were distributed and installed in the injector head, which significantly influences the combustion performance. In the paper, the characteristics of combustion stability are inspected by the parametric varations such as changing length and diameter of a combustion chamber and installing a turbulence ring. The experimental results show that as a resonant frequency took place in a high region, the amplitude of the dynamic pressure generally diminished, however, the combustion instability could not be suppressed perfectly.

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Study for combustion characteristic according to the O/F ratio of low thrust rocket engine using green propellant (친환경 추진제를 사용하는 저추력 엑체로켓엔진의 혼합비에 따른 연소 특성)

  • Jeon, Jun-Su;Kim, Young-Mun;Hwang, O-Sik;Ko, Young-Sung;Kim, Yoo;Kim, Sun-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.134-137
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    • 2009
  • Combustion tests of a low thrust rocket engine was performed to get combustion characteristics, which used a high concentrated hydrogen peroxide and kerosene as the oxidizer and fuel. The engine consisted of multi injector(six coaxial swirl injectors), chamber, nozzle and catalyst ignition system. The test was carried out by changing O/F ratio from 3.8 to 11.0. The experimental results showed that combustion efficiency was highest at O/F ratio from 5 to 6 and pressure fluctuations of all the range were lower than 5%.

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Design of Hydrogen Peroxide/Kerosene Ignitor and Ignition Characteristic according to Operation Condition (친환경 추진제를 사용하는 액체로켓엔진 점화기의 설계 및 운용 조건이 점화 특성에 미치는 영향)

  • Hwang, Oh-Sik;Kim, Tae-Woan;Jeon, Jun-Su;Ko, Young-Sung;Kim, Yoo;Kim, Sun-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.74-77
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    • 2009
  • Ignition performance tests were performed to develop a catalytic ignitor which used hydrogen peroxide and kerosene. Ignition characteristics were investigated by exit area of the catalytic bed, shape of kerosene injector and lead time of purge gas. The results showed that exit area of catalytic bed must be enough for non chocking condition and kerosene must be sprayed with swirl in the middle of catalytic bed. Also in case without preheating of catalytic bed, hydrogen peroxide must be leaded by 3sec, and purge gas must be supplied simultaneously or lately with kerosene.

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Spray Characteristics of Simplex Swirl Injector with Low Hydrodynamic Disturbance Generated by Pressure Fluctuation in Feed Line (축방향 압력섭동에 의해 발생되는 저주파 수력학적 교란이 단일 스월 인젝터에 미치는 영향 분석)

  • Khil, Tae-Ock;Kim, Sung-Hyuk;Kim, Hyeon-Sung;Yoon, Young-Bin
    • Journal of ILASS-Korea
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    • v.12 no.1
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    • pp.1-10
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    • 2007
  • The low frequency combustion instability phenomena generated by pressure drop oscillation such as propellant shake in feed line are studied. To generate the flowrate oscillation by the pressure pulsation up to 400Hz without flow discontinuities and cavitations, a hydrodynamic mechanical pulsator of rotating disk type was produced. Injection pressure conditions are 5, 7 and 9 bar and pressure fluctuation frequency conditions are 0, 4, 6 and 8 Hz. When the injection pressure was oscillated by a mechanical pulsator, the spray shape was pulsated regularly. During the pulsated state of the spray with a mechanical pulsator, the spray characteristics, such as spray angle and liquid film thickness in orifice exit, were measured and compared with those in steady state without a mechanical pulsator. Though the mean injection pressure was fixed in the steady and fluctuating state, there were some differences in all measured values, i.e. liquid film thickness and spray cone angle, between both states.

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Average Droplet Size Distribution of a GDI Spray by Simultaneous Fluorescence/Scattering Image Technique (형과/산란광 동시 측정에 의한 GDI 분무의 평균 입경 분포에 관한 연구)

  • Gwak, Su-Min;Ryu, Gyeong-Hun;Choe, Dong-Seok;Kim, Deok-Jul
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.6
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    • pp.868-875
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    • 2001
  • The objective of this study is to investigate the average droplet size distributions of a GDI spray by simultaneous fluorescence/scattering image technique. GDI engine is recently very popular because of high engine efficiency and low emissions. However, the injectors must have good spray characteristics because the fuel is directly injected into the cylinder. The fuel mixtures used in this study were 2% of fluorobenzene, 9% of DEMA(diethyl-methyl-amine) and 89% of hexane by volume. The system for obtaining 2-D fluorescence/scattering images of fuel spray was constituted of a laser sheet, a doubling prism, optical filters, and an ICCD camera. Using the ratio of the fluorescence to the scattering intensities, SMD distributions were obtained. SMD measured by the technique was compared with that obtained by PDA. It was found that average droplet size was bigger at spray center in the early stage of injection and at the outer periphery of the spray in the late stage of injection.