• 제목/요약/키워드: Flame configuration

검색결과 123건 처리시간 0.03초

층류제트 화염의 노즐직경에 따른 안정화 메커니즘과 화염형상에 관한 연구 (A Study on the Flame Configuration and Flame Stability Mechanism with a Nozzle Diameter of Laminar Lifted Jet Flame)

  • 김태권;김경호;하지수
    • Journal of Advanced Marine Engineering and Technology
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    • 제35권2호
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    • pp.204-215
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    • 2011
  • 화염 안정성은 층류부상화염의 중요한 메커니즘 중 하나이며 화염전파속도는 화염안정화를 평가하기 위한 척도가 된다. Bilger는 삼지점을 기준으로 혼합분율과 화염의 형상에 관계된 삼지화염의 화염 전파속도 및 안정화 메키니즘을 제시하였다. 그러나 동축류 작은 노즐을 이용한 실험과 수치해석에서는 화염이 형성되고 소화되는 전 과정을 상세히 관찰 할 수는 없었다. 본 논문에서는 노즐 직경에 따른 화염거동과 화염 형상 및 안정화 메커니즘에 대하여 세분화하였다. 본 논문의 결과로 노즐에 따른 삼지화염의 거동과 삼지화염전파, 화염면 전파 및 평면화염의 존재 등을 구분하였다. 그리고 삼지화염전파 거동에 있어서 열린삼지화염전파 및 닫힌 삼지화염전파 거동에 대해 구분하였다.

다수 비예혼합 화염의 안정화 특성 (Stability Enhancement by the Interaction of Diffusion Flames)

  • 김진선;이병준
    • 대한기계학회논문집B
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    • 제27권10호
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    • pp.1420-1426
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    • 2003
  • The stability of turbulent nonpremixed interacting flames is investigated in terms of nozzle configuration shapes and kind of fuels. Four nozzle arrangements - cross 5, matrix 8, matrix 9 and circle 8 nozzles - are used in the experiment. There are many parameters affecting flame stability in multi-nozzle flames such as nozzle separation distance, fuel flowrates and nozzle configuration etc. Key factors to enhance blowout limit are the nozzle configuration and the existence of center nozzle. Even nozzle exit velocity equal 204 m/s, flame is not extinguished when there is not a center nozzle and s/d=15.3∼27.6 in matrix-8 and circular-8 configurations. At these conditions, recirculation of burnt gas is related with stability augmentation. Fuel mole fraction measurements using laser induced fluorescence reveal lifted flame base is not located at the stoichiometric contour.

수소 예혼합 난류전파화염의 화염형상 특성에 미치는 불활성 가스의 영향 (Influence of Inert Gas on the Configuration Characteristics of Premixed Turbulent Propagating Flames of Hydrogen Mixtures)

  • 나까하라마사야;키도히로유끼;김준효
    • Journal of Advanced Marine Engineering and Technology
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    • 제28권4호
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    • pp.632-640
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    • 2004
  • The purpose of this study is to clarify the influence of inert gas on the configuration characteristics of premixed turbulent propagating flames of hydrogen mixtures. Inert gas is changed to $N_2$, Ar, $CO_2$ and He keeping the laminar burning velocity of mixtures nearly the same value. A laser tomography technique was used to obtain the flame shape, and quantitative analyses were performed. The result shows that in the wrinkled laminar flame region, the surface area of turbulent flame is slightly dependent on the equivalence ratio and the kind of inert gas. It is also shown the region of convex part of flame toward the unburned gas is greater than that of toward the burned gas regardless of the kind of inert gas.

반밀폐 연소공간 내 동축관 형상에 따른 DME-공기 확산화염의 안정화 특성 (Stabilization Characteristics of DME-Air Diffusion Flames Depending on the Configuration of the Fuel-Air Tubes in Half Closed Combustion Spaces)

  • 김고태;김남일
    • 대한기계학회논문집B
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    • 제33권11호
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    • pp.916-923
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    • 2009
  • The effects of configuration of fuel and air tubes on the flame stabilization were experimentally investigated in half-closed combustors. Flame behaviors and stabilities of methane, propane, and DME flames were compared by changing tube diameters and the locations of the fuel and air tubes. It was found that flammability limits are significantly affected by the outlet boundary condition, which disturbs compositions of burned and unburned mixtures near the flame base. And it was found that there exist critical inner tube heights, over which flame stability is determined only by the fuel flow rate. Conclusively, flame stabilization is governed by the flame propagation velocity in an ordinary mixing flow and the non-uniform mixture concentration in the combustion space which is affected by flow recirculation and the combustor configuration. The compositions of $NO_x$ and CO were compared to know basic characteristics of methane, propane, and DME flames.

비예혼합 튜브형상내 화염셀의 거동에 대한 수치 해석적 연구 (A Numerical Study of the Flame Cell Dynamics in Opposed Nonpremixed Tubular Configuration)

  • 박현수;유춘상
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.175-178
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    • 2014
  • The flame cell dynamics in 2-D opposed nonpremixed tubular configuration was investigated using high-fidelity numerical simulations. The diffusive-thermal instability occurs as the $Damk{\ddot{o}}hler$ number, Da, approaches the 1-D extinction limit of the tubular flames and several flame cells are generated depending on Da, and flame radius. In general, the number of flame cells are found close to the largest wave number from the linear stability analysis. It was also found from the displacement speed analysis that during the local flame extinction and cell formation, negative edge flame speed is observed due to small gain from reaction compared to large loss from diffusion.

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다수 난류 비예혼합 화염의 상호작용에 관한 연구 (The Stability of Turbulent Interacting Flames)

  • 김진선;이병준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집A
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    • pp.453-458
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    • 2001
  • The stability of turbulent nonpremixed interacting flames is investigated in terms of nozzle configuration shapes which depend on the existence of the center nozzles. Six nozzle arrangements which are cross 4, 5, 8, 9, square 8 and circular 8 nozzles are used for the experiment. Those are arranged to see the effect of the center nozzle out of multi-nozzle. There are many parameters that affect flame stability in multi-nozzle flame such as nozzle separation distance, fuel flowrates and nozzle configuration, but the most important factor is the existence of nozzles in the center area from the nozzle arrangement. As the number of nozzle in the area is reduced, more air can be entrained into the center of flame base and then tag flame is formed. In the case of circular 8 nozzles, blowout flowrates are above 5.4 times compared with that of single equivalent area nozzle.

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피스톤 형상이 연소와 화염전파에 미치는 영향 (The Effect of Piston Configuration on Combustion and Flame Propagation)

  • 지명석;강기영
    • 한국산업융합학회 논문집
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    • 제22권5호
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    • pp.511-517
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    • 2019
  • Two type pistons which had different configuration were made to find out the effects on combustion and flame propagation. Flame propagation speed was obtained by use of the cylinder head gasket ionization probe. Ionization Probe voltage output and flame propagation speed were increased according to the air fuel mixture ratio increase. Exhaust direction flame propagation speed was fastest in combustion chamber and next was front direction, rear direction and intake direction cause of tumbling motion in cylinder. In case of remove the valve pocket in piston, average flame propagation speed changed slowly and spark timing was advanced. Also emission was decreased.

LIIM(Laser-Induced Ion Mobility) 계측을 이용한 매연 나노입자 측정 (Measurement of Soot Nano-Particle Using LIIM(Laser-Induced Ion Mobility))

  • 이의주
    • 대한기계학회논문집B
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    • 제28권9호
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    • pp.1110-1116
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    • 2004
  • Experimental measurements of laser-induced ion mobility(LIIM) were performed for ethene/air premixed flames operated near the soot inception point. Soot was ionized using a pulsed laser operated at 532 nm. The ionization signal was collected with a tungsten electrode located in the post-flame region. ionization signals were collected using both a single electrode and dual electrode configuration. Prior LIIM studies have focused on the use of a single biased electrode to generate the electric field, with the burner head serving as the path to ground. In many practical combustion systems, a path to ground is not readily available. To apply the LIIM diagnostic to these geometries, a dual electrode geometry must be employed. The influence of electrode configuration, flame equivalence ratio, and flame height on ionization signal detection was determined. The efficacy of the LIIM diagnostic to detect soot inception in the post-flame region of a premixed flame using a dual electrode configuration was investigated. For the different dual electrode configurations tested, the dual parallel electrode geometry was observed to be most sensitive to detect the soot inception point in a premixed flame.

수소를 첨가한 탄화수소 혼합기의 난류연소 특성에 관한 실험적 연구 (An Experimental Study on the Turbulent Combustion Characteristics of Hydrocarbon Mixtures by Hydrogen Addition)

  • 김준효;한원희;키도히로유끼
    • 한국자동차공학회논문집
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    • 제11권6호
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    • pp.65-72
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    • 2003
  • In order to clarify turbulent combustion characteristics of hydrocarbon mixtures by hydrogen addition, turbulent burning velocities in a constant volume vessel were measured for both lean and rich hydrocarbon mixtures. Moreover, the configuration characteristics of turbulent flame was investigated in the wrinkled laminar flame region. A laser tomography technique was used to obtain the images of turbulent flame, and quantitative analyses were performed. As a result, the characteristics of turbulent burning velocity was shown a distinct difference with the addition rate of hydrogen between lean and rich mixtures. On the other hand, the obtained tomograms showed that the surface area of turbulent flame depends almost only on the turbulence intensity.

상호작용하는 부상화염의 특성에 관한 연구 (Characteristics of Interacting Lifted Flames)

  • 이승;이병준
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.1-8
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    • 2000
  • The effects of nozzle arrangements, nozzle distances and fuel flowrates on the flame stabilities such as flame length, liftoff height and blowout characteristics are investigated experimentally. Three nozzle arrangements - diamond 4 nozzle, linear 5 nozzle, cross 5 nozzle- are used. Flame interactions result in the increase of the blowout flowrates and constant turbulent liftoff heights. The flames separated about 10 nozzle diameters are sustained as nozzle attached flames to the higher fuel flowrates than the other separation cases. Normally flames are extinguished at the lifted states. Blowout flowrates are affected by the nozzle configuration, nozzle seperation distance. Blowout flowrates for the diamond- or cross- shaped nozzle arrangements are parabolic function of nozzle distances. Maximum blowout flowrates for the 5 nozzle configuration case except linear one is about 2.9 times that of single equivalent nozzle case. Turbulent liftoff heights are not function of flowrates for the interacting flames.

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