• Title/Summary/Keyword: Swirl type injector

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Study on the Spray Behavior from Swirl and Fan Spray Type Gasoline Injectors Impinging on the Constant Temperature Flat Plate (스월형 및 팬스프레이형 고압직분식 가솔린 분사기의 상온 평판에서의 분무 충돌 특성에 관한 연구)

  • Kim, Chong-Min;Kang, Shin-Jae;Kim, Man-Young
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.2
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    • pp.100-106
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    • 2006
  • The behavior of spray impinging on the inclined constant temperature flat plate was experimentally investigated. To clarify the wall effect of a high pressure DISI injector, a relative angle of the inclined wall to a spray axis was varied. Spray penetration along the wall was observed optically and it was compared with that of a Fan spray type and Swirl type spray. To evaluate various spray motion quantitatively, a spray path penetration which describe the development of a spray tip along the wall was newly introduced. To observe the structure of an impinging spray, it was visualized by a controlled stroboscope light and its visualized image was captured on an CCD camera. Using the digital image of impinging spray $H_x$ and $R_x$ was extracted to clarify the structure of impinging spray. The main parameter of the relative position of the wall was the inclined angle which was defined as the angle was varied from $0^{\circ}$ (vertical impingement) to $60^{\circ}$ at the same condition.

Numerical Study on Swirl Coaxial Injectors with Different Recess Lengths (리세스 길이가 다른 동축 와류형 분사기들에 대한 수치해석)

  • Lee, Bom;Yoon, Wonjae;Yoon, Youngbin;Ahn, Kyubok
    • Journal of ILASS-Korea
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    • v.23 no.2
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    • pp.49-57
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    • 2018
  • Numerical study under single-injection on bi-swirl coaxial injectors with different recess lengths was performed using ANSYS Fluent. The bi-swirl coaxial injectors which consisted of inner closed-type and outer open-type swirl injectors, had three different recess lengths. By changing mass flow rates, numerical simulation was repeated using the Reynolds stress BSL turbulent model. The numerical results such as discharge coefficient and spray angle were compared with previous experimental data and were found to be approximately matched well with them, irrespective of recess length. Quantitative data which was hard to be measured from experiments, were successfully obtained through the present numerical study.

A Numerical Analysis on the Characteristics of Spray by Swirl Injector in Gas Turbine Combustor (가스터빈연소기에서 스월 인젝터의 분무특성에 관한 연구)

  • 이성혁;유홍선;이인섭;홍성국
    • Journal of the Korean Society of Safety
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    • v.15 no.3
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    • pp.30-39
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    • 2000
  • The present paper deals with the numerical simulation for the spray characteristics with swirling turbulent flows and dilution flows from swirl injectors in a simplified can type of gas turbine combustor. The main objective is to investigate the characteristics of swirling turbulent flows with dilution flows and to provide the qualitative results for the spray characteristics such as the droplet distribution and Sauter Mean Diameter(SMD). The gas-phase equations based on Eulerian approach were discretized by Finite Volume Method, together with SIMPLE algorithm and the Reynolds -Stress-Model. The liquid-phase equations based on Lagrangian method were used to predict the droplet behavior. The results of preliminary test are generally in good agreement with experimental data, and show that the anisotropy exists in the primary zone due to swirl velocity and injected air from primary injector, and then gradually decays due to turbulent mixing and consequently near-isotropy occurs in the region between primary and dilution zones. For the spray characteristics, it is indicated that the swirling flows of primary jet region increase the droplet atomization. In addition, it is showed that the swirling flows at the inlet region lead the air-fuel mixture to be distributed near the igniter and can significantly affect the spray behavior in the primary jet region.

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Diesel Engine Intake Port Analysis Using Reverse-engineering Technique (리버스 엔지니어링을 통한 디젤엔진 흡기포트의 성능 비교)

  • Kim, Chang-Su;Park, Sung-Young
    • Transactions of the Korean Society of Automotive Engineers
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    • v.23 no.5
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    • pp.502-507
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    • 2015
  • In this paper, we built a three-dimensional model by applying reverse engineering techniques on targeting the intake port of 2900cc class diesel engine before that three-dimensional design technique is applied. The performance of the intake port is predicted and analysed using the computational flow analysis. Flow Coefficient and Swirl Ratio have been analyzed for two intake port models. One is the intake port for the diesel engine with plunger-type fuel system, and the other is for the diesel engine with CRDI fuel system. Computational result shows that the Flow Coefficient of the intake port with CRDI fuel system is increased upto 10 percentage compared with that with plunger-type. Also, the intake port with plunger-type has high Swirl Ratio at high valve lift, and the intake port with CRDI fuel system has high Swirl Ratio at relatively low valve lift. It is believed that because of high performance of the fuel injector, the intake port with CRDI fuel system is designed for more air amount and not much swirl flow at high valve lift. However, high swirl flow is required at low valve lift for initial fuel and air mixing. The result of this study may be useful for the re-manufacturing industry of automotive parts.

Fuel Distribution Characteristics in a Swirl Type GDI Engine (스월형 GDI 엔진의 연료분포특성 연구)

  • 김기성;박상규
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2002.05a
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    • pp.49-59
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    • 2002
  • For the purpose of helping development of a GDI(Gasoline Direct Injection) engine, the spray behaviors and fuel distributions were investigated in a single cylinder GDI engine. The experimental engine is a swirl type GBI engine with a SCV(Swirl Control Valve). PLIF(Planar Laser Induced Fluorescence) system with KrF Excimer laser was used for the measurement of the fuel distributions. The effects of SCV opening angle and the Injector specifications, such as the spray cone angle and the offset an91e on the fuel distributions characteristics were investigated. As a result, it was found that the SCV opening angle had a great effect on the fuel distributions in the late stage of compression process by changing flow fields in the combustion chamber.

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Combustion Performance Tests of Sub-scale Combustor for Liquid Rocket Engine (다종의 축소형 고압연소기 연소성능시험)

  • Kim Seung-Han;Seo Seonghyeon;Moon Il-Yoon;Seol Woo-Seok;Cho Gwang-Rae;Han Yeoung-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.259-264
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    • 2004
  • The critical component of combustor having high combustion efficiency for high performance liquid rocket engine is injector. The results of design and hot firing tests of six sub-scale combustors which have respectively an impinging type injector(1ea.), an bi-propellant swirl closed injector(1ea.), and hi-propellant swirl mixed injector(4ea.) were described in this paper. The combustion test were successfully performed. The combustion efficiency have higher value than predicted value and high frequency combustion instability does not occur.

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An Experimental Study on the Spray Behaviors of Swirl and Slit Injector to Direct Injection Spark Injection Engine (DISI 엔진용 스월인젝터와 슬릿인젝터의 분무 거동에 관한 연구)

  • Lee Changhee;Lee Kihyung;Choi Youngjong
    • Transactions of the Korean Society of Automotive Engineers
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    • v.13 no.1
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    • pp.19-27
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    • 2005
  • The spray characteristics of DISI injector has a great role in engine efficiency and emission. Thus, many researchers have been studied to investigate the spray characteristics of hollow cone type and slit type injector which are used in DISI engine. In this study, we tried to provide spray parameters which effect on the spray characteristics such as injection pressure, ambient pressure and ambient temperature. In addition, we calculated $t_b\;and\;t_c$ to investigate the break up mechanism of test injectors and also obtained $C_v$ to evaluate the spray characteristics. From this study, As the ambient pressure increases in case of slit injector, $C_v$ decreases.

The Experimental Study on the Interaction of Dual Orifice Type Swirl Injectors (이중선회 분무간의 상호작용에 관한 실험적 연구)

  • Kim, H.J.;Park, B.S.;Kim, H.Y.;Chung, J.T.
    • 한국연소학회:학술대회논문집
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    • 2001.06a
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    • pp.119-126
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    • 2001
  • The effects of injection pressure and the distance between injectors on the droplet distribution characteristics of liquid spray for dual orifice type swirl injectors were experimentally investigated. The SMD distributions, volume concentration and Rosin- Rammler variation N of liquid spray droplets for water and a fuel were measured by using the laser diffraction particle sizer. The results of present study show that SMD decreases and spray angle increases as the injection pressure increases. The interaction of sprays from two injectors gives more uniform SMD distribution in the radial direction. As the distance between two injectors increases, SMD that is measured in the interacting region increases. The effect of viscosity on the droplet distribution in the interacting region is greater than the that of surface tension of liquid.

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Aspects of Mixture Formation in a Swirl Type GDI Engine (스월형 GDI 엔진의 연료혼합특성 연구)

  • 김기성;박상규
    • Journal of Advanced Marine Engineering and Technology
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    • v.27 no.2
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    • pp.260-271
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    • 2003
  • For the Purpose of understanding the mixing phenomena of a GDI(Gasoline Direct Injection) engine, the spray behaviors and fuel distributions were investigated in a single cylinder transparent GDI engine. The experimental engine is a swirl type GDI engine with a SCV(Swirl Control Valve). PLIF(Planar Laser Induced Fluorescence) system with KrF Excimer laser was used for the measurement of the fuel distributions. The effects of SCV opening angles and the injector specifications on the fuel distribution characteristics were investigated. As a result, it was found that the SCV opening angle had a great effect on the fuel distributions in the late stage of compression process by changing the flow fields in the combustion chamber.

An Optimization of the Combustion Parameters for Reducing Exhaust Emissions in a Direct Injection Diesel Engine (직접분사식 디젤기관 배기배출물 저감을 위한 연소인자의 최적화)

  • 주봉철;노병준;김규철;이삼구
    • Transactions of the Korean Society of Automotive Engineers
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    • v.8 no.5
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    • pp.78-85
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    • 2000
  • This study is to develop the diesel engine which has 6 cylinder natural aspiration direct injection type of 7.4$\ell$ with high performance, low emissions and low fuel consumption Finally the developed engine meets Korean `98 exhaust emission regulation for the city bus of heavy duty diesel engine by optimizing the various combustion parameters affecting performance and exhaust emissions. Combustion parameters are the swirl ratio of intake ports, the profile of injection pump`s cam affecting injection pressure, the design features of piston bowl of injection pump`s cam affecting injection pressure, the design features of piston bowl of combustion chamber and injector`s hole size. Through experimental analysis, various combustion parameters are optimized and the results are as follows; the swirl ratio is 2.20, the profile of injection pump`s cam is concave and re-entrant ratio, inner diameter of piston bowl and hole diameter of injector is 0.88,$\psi$64.0mm and $\psi$0.25mm respectively.

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