• Title/Summary/Keyword: Combustion Field

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An Experimental Study on the Characteristics of Temperature field according to the Combustor Diameters in the Dual Swirl Burner (이중 선회버너에서 연소실 직경에 따른 온도장 특성에 관한 실험적 연구)

  • Choi, Inchan;Lee, Keeman
    • 한국연소학회:학술대회논문집
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    • 2013.06a
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    • pp.107-108
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    • 2013
  • An experimental study in the dual swirl burner was conducted to analyze the temperature characteristics in the combustion field. The dual swirl burner consists of a main swirling pre-mixed flame with tangential swirler surrounding a pilot which can stabilize a diffusion flame or a partially premixed flame with vane swirler depending on whether fuel is supplied at the exit plane or further upstream. The purpose of this study is to analyse experimentally the characterization of flame temperature in the reacting zone, specially, according to the various combustor diameters like 80mm, 100mm, 130mm and 150mm(O.D). As a result, the temperatures of combustion field were decreased as the diameter of combustor increased. Therefore, these results can be expected that the larger diameter of combustor tend to emit less NOx emission than the small combustor.

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Visualization of the Combustion-field in Ultrasonically-atomized Slit-jet Flame Using a Thermo-graphic Camera (열화상카메라를 이용한 초음파 무화 슬릿제트화염의 연소장 가시화)

  • Kim, Min Sung;Koo, Jaye;Kim, Heuy Dong;Kim, Jeong Soo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.4
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    • pp.1-8
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    • 2016
  • An experimental study was performed for the combustion-field visualization of the burner which burns the liquid hydrocarbon fuel atomized by an ultrasonic oscillator. Configurations of the flame and combustion-field were caught by both high-speed camera and thermo-graphic camera, and those images were analyzed in detail through a post-processing. As a result, the combustion-field grew and reaction-temperature rose due to the strengthening of combustion reaction with the increasing flow-rate of carrier-gas. In addition, a phenomenon of flame flickering was discussed through the comparative analysis of the variational behaviors between the visible flame and IR (Infrared) flame-field.

Combustion Emission Characteristics on the Effect of Secondary Air Injection in Model Gas Turbine Combustor (모형 가스터빈 연소기의 2차공기 주입에 따른 연소배출특성)

  • 김규성;임경달;이도형
    • Journal of Ocean Engineering and Technology
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    • v.14 no.3
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    • pp.84-89
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    • 2000
  • The purpose of this study is to investigate the combustion emission characteristics by the effect of secondary air injection and variation of the excess air ratio in combustion field of model gas turbine combustor. For this purpose, mean temperature, CO, $CO_2$, $O_2$ and HC concentrations were measured by changing excess air ratio and secondary air injection. As a result of this study, mean temperature was decreased and CO, HC emission increased by increasing the excess air ratio of secondary air. Therefore, this results showed the secondary air injection effected strongly on the flame structure and combustion emission characteristics.

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Experimental Study on Combustion Noise Characteristics in Turbulent Jet Diffusion Flames (난류 제트확산화염의 연소소음 특성에 관한 실험연구)

  • 김호석;오상헌
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.5
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    • pp.1253-1263
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    • 1994
  • The experimental study is carried out to identify the combustion generated noise mechanism in free turbulent jet diffusion flames. Axial mean fluctuating velocities in cold and reacting flow fields were measured using hot-wire anemometer and LDv.The overall sound pressure level and their spectral distribution in far field with and without combustion were also measured in an anechoic chamber. The axial mean velocity is 10-25% faster and turbulent intensities are about 10 to 15% smaller near active reacting zone than those in nonreacting flow fields. And sound pressure level is about 10-20% higher in reacting flow fields. It is also shown that the spectra of the combustion noise has lower frequency characteristics over a broadband spectrum. These results indicate that the combustion noise characteristics in jet diffusion flames are dominated by energy containing large scale eddies and the combusting flow field itself. Scaling laws correlating the gas velocity and heat of combustion show that the acoustic power of the combustion noise is linearly proportional to the 3.8th power of the mean axial velocity rather than 8th power in nonreacting flow fields, and the SPL increases linearly with logarithmic 1/2th power of the heat of combustion.

Numerical Simulations for Combustion and NOx Emission Characteristics in Oscillating Combustion Burner (수치해석을 이용한 맥동연소과정 및 NOx 배출특성 해석)

  • Kim, Hoo-Joong;Cho, Han-Chang
    • Journal of the Korean Society of Combustion
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    • v.14 no.3
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    • pp.37-44
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    • 2009
  • An experimental study was conducted to reduce NOx emission in RT(radiant tube)burner by using oscillating combustion processes in RIST. A solenoid valve gives the various oscillating conditions, such as oscillation frequency, duty ratio of fuel flow. In this study, we used commercial software, CFD-ACE+ to predict combustion and NOx emission characteristics for various experimental oscillation conditions. The effect of oscillation frequency and duty ratio on NOx emission will be discussed in terms of flow field, temperature and equivalence ratio distributions in detail.

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Investigation of Turbulent Combustion Characteristics for Different Injector Port Diameter in Hybrid Rocket (하이브리드 로켓 인젝터 포트직경 변화에 따른 난류연소 유동장 해석)

  • Moon, Hee-Jang;Koo, Ja-Ye;Yoon, Chang-Jin;Min, Moon-Ki;Jang, Won-Jae
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.14 no.1
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    • pp.2-8
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    • 2006
  • Numerical analysis of the flow field in the reactive medium of End-Burring combustor is studied in order to investigate the combustion characteristics of hybrid combustion. The main part of this study is focused on the port diameter effects of oxidizer injector on the temperature distribution within the reactive field. It is found that the case having the largest port diameter(25 mm) delivers the optimum conditions for the design of End-Burring combustor where the predicted temperature field showed the most acceptable distribution.

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Simultaneous Synthesis and Densification of Ti5Si3 and Ti5Si3-20 vol%Nb Composite by Field-Activated and Pressure-Assisted Combustion

  • Shon, In Jin;Kim, Hwan Chal;Rho, Dae Ho
    • The Korean Journal of Ceramics
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    • v.5 no.2
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    • pp.148-154
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    • 1999
  • A method to simultaneously synthesize and consolidate $Ti_5Si_4 \;and\; Ti_5Si_3$-20 vol%Nb composite from powders of Ti, Si and Nb was investigated. Combustion synthesis was carried out under the combined effect of an electric field and mechanical pressure. Highly dense $Ti_5Si_4 \;and\; Ti_5Si_3$-20 vol% Nb with relative densities up to 98% was produced from powders of Ti, Si and Nb under the application of 60 MPa pressure and 3000A current on the reactant.

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Combustion Modeling of Vacuum Residue Fuel Sprays (잔사유 분무 연소 해석에 관한 연구)

  • Choi, Chan-Ho;Huh, Kang-Y.
    • 한국연소학회:학술대회논문집
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    • 2004.06a
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    • pp.207-214
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    • 2004
  • Extra heavy vacuum residue oil has advantage as the fuel of a power plant in reducing the cost of power generation. Numerical study is conducted by the KIVA code to understand combustion, heat transfer and flow field characteristics in the test reactor. The combustion model of pulverized coal particles is adopted as the combustion process of extra heavy oil is similar to that of coal. As an initial phase of investigation parametric study is performed with respect to SMD and spray angle of injected spray droplets.

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The evaluation of error due to flame in the measurement using phase doppler anemometry (위상도플러 유속계를 이용한 계측에 있어서의 화염에 기인한 오차의 평가)

  • Yang, Young-Joon
    • Journal of Sensor Science and Technology
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    • v.14 no.5
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    • pp.313-321
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    • 2005
  • Spray combustion has been used in many industrial fields, for instance, such as diesel engines, gas turbines and industrial furnaces, and furthermore various measurement techniques have been applied to elucidate the phenomenon of spray combustion. In order to measure simultaneously the droplet velocity and the droplet size of spray, phase doppler anemometry (PDA) was frequently used in spray combustion. However, the measurement error is occurred due to existence of flame, which is considered as influencing the precision of measurement. Therefore, the purpose of this study is experimentally to conduct the systematic evaluation on the measurement error when PDA measurement is applied to combustion field.