• Title/Summary/Keyword: Combustion Characteristics Velocity

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Characteristics of In-cylinder Steady Flow using PIV for Different Intake Port Geometries in a 4-valve Gasoline Engine (PIV에 의한 4밸브 가솔린기관의 흡기포트 형상에 따른 정상유동 해석)

  • 조규백;전충환;장영준;강건용
    • Transactions of the Korean Society of Automotive Engineers
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    • v.5 no.5
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    • pp.188-196
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    • 1997
  • Many researchers have developed the measurement technique of in-cylinder flow characteristics and found the effect of intake port geometries on engine performance. The flow characteristics of four-valve cylinder head were examined in a steady flow rig for different intake ports. Tumble intensity of intake configurations with different entry angles were quantified with a tumble meter. The velocity and angular momentum distributions in the tumble adaptor were measured under steady conditions with PIV(Particle Image Velocimetry). We have obtained the results that flow structure becomes complicated by valve interference at low valve lift. As the valve interferences were reducing and the flow pattern changed to large vortex structure with tumble direction, intake ports with different entry angles have different tumble centers. Tumble eccentricity of intake port with low entry angle was large, so that the port had relatively much angular momentum compared to others which was expected to improve combustion performance.

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A Study on the Propriety of Ultrasonic Atomization Apparatus for the Gasoline Engine (l) - In the Case of the Atomization of Fual - (가솔린 기관용 초음파 미립화장치의 타당성에 관한 연구 (I) - 연료 미립화를 중심으로 -)

  • 조규상
    • Journal of the korean Society of Automotive Engineers
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    • v.9 no.4
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    • pp.41-49
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    • 1987
  • It is an experimental study to improve the characteristics of combustion and exhaust emission gas in the gasoline engine. These characteristics are influenced by the fuel droplet size. To improve these characteristics, we make the ultrasonic atomization apparatus, and compare with the commercial carburetor. The results obtained are as follows: 1. Maximum atomization quantity is obtained by the vibrator of resonancy frequency 1.65MHz in the ultrasonic atomization apparatus. 2. With ultrasonic atomization apparatus, more than 99% of atomization rate can be obtained regardless of intake air temperature, velocity, and air-fuel ratio. 3. Atomization rate of the commercial carburetor increases with the air-fuel ratio and intake air temperature. 4. Difference of atomization rate between the ultrasonic atomization apparatus and the commercial carburetor increases with decreasing air-fuel ratio. 5. Droplet size is about 1-5.mu.m at the ultrasonic atomization apparatus, and 80-150.mu.m at the commercial carburetor, which indicates the ultrasonic atomization apparatus is excellent in atomization.

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Study on Lean-Premixed Combustion Characteristics of Dual-Stage Burner (이중 연료 분사구조를 갖는 희박-예혼합 버너의 연소특성 연구)

  • Jang, Jae Hwan;Cho, Ju Hyeong;Kim, Han Seok;Lee, Sang Min;Kim, Min Kuk;Ahn, Kook Young
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.1
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    • pp.51-57
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    • 2013
  • This study aims to experimentally investigate the combustion characteristics of a lean premixed swirl-stabilized burner with dual-stage fuel injection arrays. The results show that a variation in the fuel distribution to fuel stages 1 (upstream) and 2 (downstream) produces a noticeable change in the NOx and CO emissions. Reducing the confined ratio, defined as the ratio of the nozzle exit diameter to the liner diameter, may reduce NOx and CO emissions owing to reduced combustion loading and longer residence time, respectively. A nozzle exit velocity of 30 m/s shows the optimum characteristics in terms of NOx and CO emissions and flame stability: increasing or decreasing the nozzle exit velocity leads to a degradation in emissions or flame stability, respectively.

Experimental Study on the Lift-off Behavior of Tone-excited Propane Jet Diffusion flames (음향 가진 된 프로판 확산 화염의 부상 거동에 관한 실험적 연구)

  • Kim, Seung-Gon;Park, Joeng;Kim, Tea-Kwon;Lee, Kee-Man
    • 한국연소학회:학술대회논문집
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    • 2003.05a
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    • pp.65-73
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    • 2003
  • An experimental study on flame lift-off characteristics of propane jet flame highly diluted with nitrogen has been conducted introducing acoustic forcing with a tube resonant frequency. A flame stability curve is attained according to forcing strength and nozzle exit velocity for $N_2$ diluted flames. Flame lift-off behavior with forcing strength and nozzle exit velocity is globally categorized into three; a well premixed behavior caused by a collapsible mixing for large forcing strength, a coexistent behavior of well-premixed and edge flames interacting with well-organized inner fuel vortices for moderate forcing strengths, and edge flame behavior for small forcing strengths. Special focus is concentrated on the coexistent behavior of the flame base in lifted flame since this may give a hint to a possibility which the flame base behaves like a well-mixed premixed flame in highly turbulent lifted flames. It is also shown that the acoustic forcing to self-pulsating laminar lifted flame affects flame lift-off behavior considerably which is closely related to downstream flow velocity, mixture strength, effective fuel Lewis number, and flame stretch.

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Numerical Simulation of the Mixing and Flow Characteristics in a Micro Cyclone Combustor (마이크로 사이클론 연소기의 혼합 및 유동특성에 관한 수치해석 연구)

  • Oh, Chang-Bo;Choi, Byung-il;Han, Yong-shik;Kim, Myung-bae;Hwang, Cheol-hong
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.1900-1905
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    • 2007
  • A micro cyclone combustor was developed to be used as a heat source of thermoelectric power generator (TPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately. The mixing and flow characteristics in the combustor were investigated numerically. The global equivalence ratio (${\Phi}$), defined using the fuel and air flow rates, was introduced to examine the flow features of the combustor. The mixing of fuel and air inside the combustor could be well understood using the fuel concentration distribution. It was found that the weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$ < 1.0. In addition, it was found that small regions that have a negative axial velocity exist near the fuel injection ports. It is assumed that these negative axial velocity regions can stabilize a flame inside the micro cyclone combustor.

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A Study on the Radial Spray Performance of a Plaint-Jet Twin-Fluid Nozzle (액주형 이류체노즐의 반경반향 분무특성에 관한 연구)

  • 최진철;노병준;강신재
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.3
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    • pp.662-669
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    • 1994
  • In the combustion system, the optimum spray conditions reduce the pollutant emission of exhaust gas and enhance the fuel efficiency. The spray characteristics-the drop size, the drop velocity, the number density and the mass flux, become increasingly important in the design of combustor and in testifying numerical simulation of spray flow in the combustor. The purposes of this study are to clarify the spray characteristics of twin-fluid nozzle and to offer the data for combustor design and the numerical simulation of a spray flow. Spatial drop diameter was measured by immersion sampling method. The mean diameter, size distribution and uniformity of drop were analyzed with variations of air/liquid mass flow ratio. The results show that the SMD increases with the liquid supply flow rate and decreases with the air supply velocity. The radial distribution of SMD shows the larger drops can diffuse farther to the boundary of spray. And the drop size range is found to be wider close to the spray boundary where the maximum SMD locates.

Vibration Characteristics of Lean Premixed Flame Anchored by a Hydrogen Pilot Flame in a Tube (파일롯 화엄에 의해 고정된 관내 예혼합 화염의 진동 특성)

  • Guahk, Young-Tae;Oh, Kwang-Chul;Shin, Hyun-Dong
    • 한국연소학회:학술대회논문집
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    • 2004.06a
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    • pp.42-48
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    • 2004
  • Lean laminar premixed propane and methane flames which were anchored by a hydrogen-pilot flame in a tube were investigated experimentally. The flame shapes were observed by varying mean velocity from 10cm/s to 140cm/s and equivalence ratio from 0.45 to 0.8. In this study, behaviors of flames are divided into five regions such as tail-out, flash-back, flickering, stable and vibrating flames with respect to the mean velocity and the equivalence ratio. Although the flames are unstable in both the flickering and the vibrating region, they have different characteristics such as the frequency, sound generation and creation process of flame curvature. The flickering region exists near the flammability limit and the flame flickers in a frequency of about 10Hz. When flame front is bended, the propane flame front is straightened and the methane flame front is bended more by thermo-diffusive instability. In the vibrating region, the flame vibrates emitting audible sound in a frequency of about 100Hz. In the boundary of vibrating region, the vibration of flame changes between two modes such as single frequency vibration and dual frequency vibration. Increase and decrease of vibration in each mode are determined by thermo-acoustic instability.

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Numerical Simulation of the Mixing and Flow Characteristics in a Micro Cyclone Combustor (마이크로 사이클론 연소기의 혼합 및 유동특성에 관한 수치해석 연구)

  • Choi, Byung-ll;Han, Yong-Shik;Kim, Myung-Bae;Hwang, Cheol-Hong;Oh, Chang-Bo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.12
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    • pp.1042-1047
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    • 2007
  • A micro cyclone combustor was developed to be used as a heat source of thermoelectric power generator (TPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately. The mixing and flow characteristics in the combustor were investigated numerically. The global equivalence ratio ($\Phi$), defined using the fuel and air flow rates, was introduced to examine the flow features of the combustor. The mixing of fuel and air inside the combustor could be well understood using the fuel concentration distribution. It was found that the weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$<1.0. In addition, it was found that small regions that have a negative axial velocity exist near the fuel injection ports. It is assumed that these negative axial velocity regions can stabilize a flame inside the micro cyclone combustor.

Design and Analysis a Drive-train for a Parallel-type Hybrid Electric Vehicle (병렬형 하이브리드 자동차의 구동장치 설계 및 해석)

  • Kim, Dong-Hyun;Ahn, Sung-Jun;Choi, Jae-Weon
    • Journal of the Korean Society for Precision Engineering
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    • v.29 no.7
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    • pp.770-777
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    • 2012
  • This paper deals with the design and modal characteristics analysis of a drive-train for a paralleltype hybrid electric vehicle (HEV). The function of the drive-train system (DTS) in the HEV combines or divides the torque and velocity from the internal combustion engine along with the induction motor. The system consists of a compound planetary gear and unit's electromagnetic clutch to provide the operation modes such as Engine Only (EO), Electric Vehicle (EV), and Hybrid Electric Vehicle (HEV) modes. In order to investigate the characteristics of the velocity and torque flow for the system, dynamic models of the HEV with DTS are derived from the prototype DTS. The performance of the derived dynamic models is evaluated by both computer simulations and experiments according to each mode.

Simulation and Model Validation of Combustion in a Wood Pellet Boiler Using Computational Fluid Dynamics (전산유체역학을 이용한 목재펠릿보일러 연소모델 정립 및 검증)

  • Oh, Kwang Cheol;Euh, Seung Hee;Oh, Jae Heun;Kim, Dae Hyun
    • Journal of Energy Engineering
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    • v.23 no.3
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    • pp.203-210
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    • 2014
  • In this study, combustion behaviour were to analyze by comparing experimental data against predicted values. In developing pellet boiler performance, various factors such as combustion chamber shape, input air velocity, the amount of fuel, temperature, and fuel characteristics need to be analyzed. Analytical model using a numerical method is useful to overcome time and cost consuming by practical experiment. By controlling feeding rate of fuel, flue gas composition and temperature distribution obtained form experiment were compared with predicted values using FLUENT(ANSYS, Inc., Southpointe). Measurement were in good agreement with model predictions : with 0.60 % for $CO_2$ 0.73% for $O_2$ when compared with independent data sets.