• Title/Summary/Keyword: Burner Distance

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An Experimental Study on Heat Transfer Characteristics of Synthetic Gas($H_2/CO$)Air Premixed Flames in an Impinging Jet Burner - Part 1 : Stretched Lift-off Flames (충돌제트 버너에서 합성가스($H_2/CO$) 공기 예혼합 화염의 열전달 특성에 관한 실험적 연구 - Part 1 : 스트레치된 부상 화염)

  • Kang, Ki-Joong;Jo, Joon-Ik;Lee, Kee-Man
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.453-456
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    • 2011
  • An experimental investigation of the heat transfer characteristics of stretched premixed flames using Synthetic gas has been performed. Hydrogen and carbon mon-oxide which could be extracted from coal gasification process are the main fuel of synthetic-gas. Heat flux at the stagnation point was increased as global strainrate was increased, then the heat flux was decreased when a global strainrate reached a sudden point. Heat flux at the stagnation point is also affected by nozzle to impingement distance. Heat flux was increased as nozzle to impingement place distance was increased. This study is a foundation study of practical use of secondary gases from coals.

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A Study on the Combustion Characteristics of Annular Swirl Jet (環狀旋回噴流의 燃燒特性에 관한 硏究)

  • 이창식
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.7 no.4
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    • pp.410-416
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    • 1983
  • This study presents the combustion characteristics and flame structure of annular swirling flow when there were changes the equivalence ratio and swirl number of swirling jet of fuelair mixture. The conclusions of this study are as follows; During the investigations in which the change of equivalence ratio and swirl number were studied, three basic shapes of flame were observed in this study. Visible flame lengths of swirling jet results in the decrease with increasing of swirl number and air-fuel ratio of mixture. Radial distribution of flame temperature with strong swirl is higher than that of weak swirl at the same equivalence ratio of mixture. The angle of spread of the annular jet increases with the increase of swirl number. When the swirl intensity is increased in a jet, the decay of concentration of carbon dioxide is decreased with the distance from nozzle exit of burner.

Characteristics of Catalytically Supported Combustion for Gas Turbine Catalytic Combustor;Effects of the inlet shape of catalytic burner (가스터빈용 촉매 연소기를 위한 촉매-화염 복합 연소 특성연구;촉매버너 입구 형상의 영향)

  • Lee, Kyung-Won;Chung, Nam-Jo;Ryu, In-Soo;Cho, Sung-June;Seo, Yong-Seog;Kang, Sung-Kyu;Song, Kwang-Sup;Chun, Kwang-Min
    • 한국연소학회:학술대회논문집
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    • 2002.11a
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    • pp.71-79
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    • 2002
  • The characteristics of the catalytically supported combustion with Pd and Pd/Pt based catalyst using the bench-scaled high pressure combustor have been investigated up to 5atm. This study aimed to investigate combustion characteristics of the stable flame attached to the exit of catalyst bed and NOx emissions with respect to the position of axial and radial direction in the combustor. NOx emissions were increased along the axial distance after the catalyst bed exit and radially decreased from the center to the wall of the combustor. At the higher pressure, the NOx emission decreased slightly due to the lower flame temperature in the combustor at the high pressure.

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Effect of the CO Tube insert for Emission Characteristics in a Compact Combustion Chamber (컴팩트 연소실 내 CO튜브 삽입에 따른 오염물질 배출특성)

  • Lee, Jae-Park;Kim, Jong-Min;Lee, Seung-Ro;Jang, Gi-Hyun;Lee, Chang-Eon
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 2010.04a
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    • pp.66-71
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    • 2010
  • This study was the effect of CO tube insert for NOx and CO emission characteristics in a compact combustion chamber. In detail, NOx and CO emission characteristics with changing of distance due to inserting the CO tube between the burner and the main heat exchanger were investigated. For this study, the commercial program, FLUENT, and the GRI 2.11 detail reaction mechanism were used for the numerical study and a simple model heat exchanger was tested for the experimental study. As results, when the CO tube was inserted between the burner and the main heat exchanger, it was verified the simultaneous NOx and CO reduction method because of increasing the residence time and decreasing the flame temperature.

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A Study on the Particle Behavior in Turbulent Pulverized Coal Flame (난류 미분탄화염 내 입자거동에 관한 연구)

  • Hwang, Seung-Min
    • Journal of Korean Society of Environmental Engineers
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    • v.32 no.12
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    • pp.1111-1118
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    • 2010
  • Combustion measurements based on optical techniques have recently become of major interest as tools not only for clarifying the combustion mechanism but also for validating the computational results for the combustion fields. In this study, the particle behavior in turbulent pulverized coal flame are investigated using advanced optical diagnostics. A laboratory-scale pulverized coal combustion burner is specially fabricated as open type in order to apply various optical measurement techniques. The detailed particle behavior is performed by LDV (laser Doppler velocimetry) and SDPA (shadow Doppler particle analyzer). It is observed that the particle mean diameter increase as the distance from burner increases, and this is found to be caused by the decrease of small particles' diameter and increase of large particles' diameter. This is because of result in the char reaction and the particle swelling due to devolatilization, respectively. The size-classified streamwise velocities of pulverized coal particles in the central region of the jet show the same magnitude, whereas those in the outer region are different depending on the particle size. The results show that the velocity and size-classified diameter of the pulverized coal particles in the flame can be measured well by SDPA.

A Study on Flame Extinction and Edge Flame Oscillation in Counterflow Diffusion Flame (대향류확산화염에서 화염소화와 에지화염진동에 관한 연구)

  • Park, Dae-Geun;Yun, Jin-Han;Park, Jeong;Keel, Sang-In
    • Journal of the Korean Society of Propulsion Engineers
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    • v.13 no.2
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    • pp.64-76
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    • 2009
  • Experimental and numerical studies are conducted on the characteristics of flame extinction and edge flame oscillation in counterflow diffusion flames. The characteristics of flame extinction and edge flame oscillation are well described varying burner diameter, separation distance between two burners, global strain rate, and velocity ratio. It is verified numerically and experimentally that radial conduction heat loss significantly contributes to flame extinction and edge flame oscillation at low strain rate flames in zero- and micro-gravity. It is also shown that for appropriately small burner diameters flame extinction modes are grouped into four and these are significantly attributed to excessive radial conduction heat loss. The edge flame oscillation can be characterized well by one curve with Strouhal number and Peclet number.

Numerical Study on the Flow and Combustion Characteristics in Swirl-Premix Burners (스월 예혼합 버너의 유동 및 연소특성에 관한 수치적 연구)

  • Lim, Jun-Seok;Lee, Jong-Hyeok;Baek, Gwang-Min;Cho, Ju-Hyeong;Kim, Han-Seok;Sohn, Chae-Hoon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.1
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    • pp.103-110
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    • 2012
  • The flow field, fuel-air mixing, and behaviors of turbulent flames have been investigated using the large eddy simulation (LES) numerical technique in a premixed swirl combustor equipped with EV double cone burners. Recirculation zones are generated by the swirl burner, and lean premixed flames are formed within a distance of 0.2 m from the tip of the burner. NOx emission of 0.46 ppm is predicted at 1 atm and an air/fuel ratio of 38.7. However, most of the CO generated in a flame front continues to be oxidized as it moves toward the exit, and CO emission of 5.45 ppm is predicted at the exit. The NOx emission can be reduced by decreasing the pressure and air/fuel ratio. The characteristics of NOx emission have been investigated through RANS simulations for various fuel injection types, and it is found thereby that five-lance-hole injection produces the lowest NOx emission rate.

Combustion Characteristics of CH4 Nonpremixed Flame with Recession Distance (메탄 비예혼합 화염의 후퇴거리에 따른 연소특성)

  • Kim, Jun-Hee;Ku, Kun-Woo;Hong, Jung-Goo;Lee, Choong-Won;Kim, In-Su;Cheong, In-Mo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.3
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    • pp.285-291
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    • 2012
  • A lot of research on the stability of nonpremixed flames has focused on the fuel-nozzle and quarl geometries. Of the work carried out, only a small amount has focused on the stability of the nonpremixed flame according to the recession distance and air-nozzle geometry. Therefore, in this study, a coaxial-diffusion-type gas burner with a swirler is designed for the systematic investigation of the combustion characteristics of a $CH_4$ flame depending on the recession distance and secondary air-nozzle geometry. 1st air is flowed through the swirler, and 2nd air is flowed through each nozzle. It is shown that the secondary air velocity greatly influences the flame length and shape. There is an optimum recession distance for each nozzle for the best combustion efficiency. In this study, it is shown that the optimized recession distance is nearly half the outer diameter of the air-supply nozzle.

Thermophoretic deposition of soot particles in laminar diffusion flame along a solid wall in microgravity (미소중력환경에서의 고체벽면근방 층류확산염내 매연입자의 열영동 부착)

  • Choi, Jae-Hyuk;Osamu, Fujita;Chung, Suk-Ho
    • 한국연소학회:학술대회논문집
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    • 2007.05a
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    • pp.19-24
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    • 2007
  • The deposition behavior of soot particles in a diffusion flame along a solid wall was examined experimentally by getting rid of the effect of natural convection utilizing microgravity environment. The microgravity environment was realized by using a drop tower facility. The fuel for the flame was an ethylene ($C_2H_4$) and the surrounding oxygen concentration 35% with the surrounding air velocity of $V_a$=2.5, 5, and 10 cm/s. Laser extinction method was adopted to measure the soot volume fraction distribution between the flame and burner wall. The results show that observation of soot deposition in normal flame was difficult from buoyancy and the relative position of flame and solid surface changes with time. The soot particle distribution region moves closer to the surface of the wall as the surrounding air velocity is increased. And the experiments determined the trace of the maximum soot concentration line. It was found that the distance between soot line and flame line is around 5 mm. That is, the soot particle near the flame zone tends to move away from flame zone because of thermophoretic force and to concentrate at a certain narrow area inside of the flame, finally, to adhere the solid wall.

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The Development of Flow-Meter System Using the Granule Flow Density And Velocity (분체 밀도와 속도를 이용한 유량검출기의 개발)

  • Gim, Jae-Hyeon;Hwang, Keon-Ho;Lee, Yong-Sik;Jeong, Sung-Won
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.23 no.5
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    • pp.9-17
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    • 2009
  • In this paper, we describe a flow meter system for pulverized coal developed for the pulverizer-burner system of a boiler or blast furnace, which uses the density and the velocity of the granule flow. The granule flow density is measured by a sensor that detects the capacitance from the electrode on the surface of the piping system. The velocity of granule flow can be calculated using the distance between two pairs of built-in sensors in the flow direction, the time obtained from the sampling cycle using the correlation method between two waveforms of the sensors. The flow rate is calculated from the density and velocity of the granule flow. The reliability and accuracy of the flow meter system has been verified by comparing the data with the weight measured from a load-cell.