• Title/Summary/Keyword: Equivalence air ratio

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A study of Overall Combustion Characteristics according to the Air Preheated Temperature in a Hybrid/Dual Swirl Jet Combustor (하이브리드/이중 선회제트 연소기에서 공기 예열온도에 의한 배출 특성 연구)

  • Choi, Inchan;Jo, Junik;Lee, Keeman
    • 한국연소학회:학술대회논문집
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    • 2012.11a
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    • pp.149-152
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    • 2012
  • The laboratory experiments have been conducted to investigate the effects of air preheated temperature on the emission characteristics by a model gas turbine burner with a hybrid/dual swirl jet flames configuration. The concentration of NOx and CO emissions, and flue gas temperature at combustor exit were measured with varying the equivalence ratio for different air preheated temperatures of 300, 400, 500K at atmospheric pressure. It was overall shown that the NOx and CO emissions, and flue gas temperature were decreased according to the decreasing of equivalence ratio due to the effects of lean premixed combustion regardless of the air preheated temperature. Experimental results of a lean premixed flames configuration indicated that the NOx emission was increased with higher inlet air temperature and air flow rate, which is attributed to the increasing of flue gas temperature and heat release related to the thermal NOx mechanism. But the CO emission was shown the opposite tendency, that is, the CO emission was decreased with increasing of inlet air temperature and flow rate.

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Numerical Investigation on Cavity-Enhanced-Supersonic Combustion Engine of Upstream Fuel Injection in Cavity (공동내부 연료분사방식 초음속 연소기의 수치해석 연구)

  • Jeong, Eun-Ju;Jeung, In-Seuck
    • 한국연소학회:학술대회논문집
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    • 2003.05a
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    • pp.35-39
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    • 2003
  • A numerical study is carried out to investigate combustion phenomena in a model SCRamjet engine, which has been experimentally studied at the Australian National University using a T3 free-piston shock tunnel. The Mach number is 3.8, the static pressure 110kPa and the static temperature 1100K in the main air flow. The fuel is hydrogen, which is injected in the cavity. Equivalence ratio is set to either 0.25 or 0.5 to access its effect on the fuel-air mixing combustion phenomena. The results show that the cavity generates several recirculation zones, which increase the fuel-air mixing. Self ignition occurs near the point of fuel injection. The flame is anchored by the cavity and generates the precombustion shock on the step. For a high equivalence ratio, the recirculation zones are bigger and the flame is present throughout the combustor.

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An Experimental Study on NOx Characteristics in Air-Staging Burner (공기-다단 연소기에서의 NOx 발생특성)

  • Sung, Yong-Jin;Cho, Eun-Seong;Chung, Suk-Ho
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.167-171
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    • 2001
  • Air-staging combustion is a relatively well-known technique to reduce NOx emission and used in combination with other techniques nowadays. However, the design variables are still selected depending upon operating circumstances. Though the fuel-rich condition of the primary combustion zone is very helpful to NOx reduction, its range is known to be restricted by the increase of carbon monoxide. However, in many cases carbon monoxide level is so low not to be the restriction at all. So we tried to expand the equivalence ratio range to the richer condition in the primary combustion zone and make the function of each burner component and its contribution to the overall NOx production clear.

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A Experimental Study on the Instability of Combustion in a Dump Combustor with Respect to Fuel and Air Mixing and Flow Conditions (혼합기 공급방식에 따른 덤프연소기의 연소 불안정성에 관한 실험적 연구)

  • Hong, Jung-Goo;Lee, Min-Chul;Lee, Uen-Do;Oh, Kwang-Chul;Shin, Hyun-Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.29 no.8 s.239
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    • pp.963-970
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    • 2005
  • The combustion instability of turbulent flames is the most important problem of the gas turbine combustor. Thus improved understanding of mechanisms of combustion instability is necessary for the design and operation of gas turbine combustors. In this study, the cause of the combustion instability in a rearward-step dump combustor was investigated with respect to the fuel flow modulation; choked fuel flow, unchoked fuel flow and fully premixed mixture flow. We observed various types of combustion instabilities with respect to the change of equivalence ratio, fuel flow conditions and fuel injection location. Particularly in the unchoked fuel flow condition, it was found that the oscillation time of combustion instability is strongly related to the convection time of the fuel and that the pressure fluctuation in a lab-scale combustor is highly related to the vortex and the equivalence ratio fluctuations due to fuel flow modulation and unmixedness of the fuel and air.

Flame Structure and NOx Emission Characteristics in Laminar Partially Premixed $CH_4$/Air Flames;Effect of Premixing Degree (메탄/공기 층류 부분 예혼합화염의 화염구조와 NOx 배출특성;예혼합 인자의 영향)

  • Oh, Jeong-Seog;Jeong, Yong-Ki;Jeon, Chung-Hwan;Chang, Young-June
    • 한국연소학회:학술대회논문집
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    • 2003.12a
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    • pp.75-81
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    • 2003
  • In this paper, the study of effects of flow variables on flame structure and NOx emission concentration was performed in co-axial laminar partially premixed methane/air flames. the objectives are to reveal its effect as parameters were varied and to understand the correlation between flame structure and NOx emission characteristics in the reaction zone. equivalence ratio(${\Phi}$), fuel split degree(${\sigma}$), and mixing distance(x/D) were defined as a premixing degree and varied within $1.36{\sim}3.17$(equivalence ratio), $50{\sim}100$(fuel split degree), and $5{\sim}20$(mixing distance). the image of $OH{\ast}$ and $CH{\ast}$, and NOx concentration were obtained with an ICCD camera and a NOx analyzer. additionally the maximum intensity location of $OH{\ast}$ chemiluminescence and $CH{\ast}$ chemiluminescence were measured to compare each flame structures. In conclusion flame structure and NOx emission characteristics were changed from diffused to premixed flame when mixing degree was on the increase. the main effect on flame structure and NOx production was at first equivalence ratio(${\Phi}$), and next fuel split degree(${\sigma}$), and finally mixing distance(x/D).

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A Study on Combustion Characteristics and Flow Analysis of a Lean Premixed Flame in Lab-Scale Gas Turbine Combustor (모형 가스터빈 연소기에서 희박 예혼합 화염의 연소 특성 및 유동 해석에 관한 연구)

  • Ryu, Hye-Yeon;Kim, Gyu-Bo;Jeon, Chung-Hwan;Chang, Young-June
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.32 no.8
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    • pp.574-581
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    • 2008
  • The characteristics of combustion and flow for a lean premixed flame in lab-scale gas turbine combustor was studied through experiment and numerical analysis. From the experiment, flame structure and heat release rate were obtained from OH emission spectroscopy. Qualitative comparisons were made line-integrated OH chemiluminescence image and abel-transformed one. NOx analyzer was implemented to get the characteristic of NOx exhaust from the combustor. From the numerical analysis, the thermal distribution and characteristic of recirculation zone with the change of fuel-air mixing degree, the characteristic of methane distribution with equivalence ratio in the combustor respectively. Total heat release rate is increased with increasing equivalence ratio. Thermal Nox is reduced with increasing fuel-air mixing degree. Increasing equivalence ratio results in the decrease of the size of reaction zone and alteration of the position of the reaction zone into the entrance of the combustor.

Development of LIBS Plug for Combustor Diagnosis (연소실 진단을 위한 LIBS 소형화 장비 개발)

  • Jun, Hyung Min;Kim, Hyunwoo;Yoh, Jai-ick
    • Journal of the Korean Society of Propulsion Engineers
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    • v.23 no.2
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    • pp.53-59
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    • 2019
  • LIBS plug, a simplified laser-induced breakdown spectroscopy(LIBS) device with the purpose of measuring the fuel distribution inside the combustion chamber, was developed and manufactured. The LIBS plug receives only two wavelengths (H:656.3 nm, O: 777 nm) that are closely related to the equivalence ratio in the overall spectrum. The calibration curve between the signal of the LIBS plug and the equivalence ratio was constructed, and the fuel distribution of gasoline-air and LPG-air mixtures was measured using the LIBS plug.

A Study on the NOx Emission Characteristics in Parametrically Varied Laminar Hydrogen-Air Coflow flames (수소 연료의 연소조건 변화에 따른 NOx 배출 특성에 관한 연구)

  • 김종현;이근오;이창언
    • Journal of the Korean Society of Safety
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    • v.16 no.4
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    • pp.82-87
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    • 2001
  • The NOx emission characteristics of jet flames fueled with It was studied. Experimental and numerical investigations were carried out for various flames with varying equivalence ratio, fuel flow rate and nozzle diameter. The Emission indices of NOx(EINOx) were measured by chemiluminescent method and calculated by simulation using detailed chemistry. The results show that the numerical results represent well the trends of EINOx experimentally observed. EINOx of H$_2$ flame steeply increase at small equivalence ratio, gently increase and steady at more than equivalence ratio is 4.0. EINOx trends of H$_2$ flame can be describe in function of residence time in the high-temperature region weighted by the maximum flame temperature.

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A Study on the Effects of Recirculated Exhaust Gas on Soot Emissions in Diesel Engines (디젤기관 매연 배출물에 미치는 재순환 배기의 영향에 관한 연구)

  • Bae, M.W.;Lim, J.K.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.6
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    • pp.142-154
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    • 1998
  • The effects of recirculated exhaust gas on the characteristic of soot emissions have been investigated by using an eight-cylinder, four-stroke, direct injection and water-cooled diesel engine operating at several loads and speeds. The experiments in this study are carried out at the fixed fuel injection timing of $38^{\circ}$ BTDC regardless of experimental conditions. The intake oxygen concentration and the mean equivalence ratio calculated by the intake air flow and fuel consumption rate are used to analyze and discuss the influences of EGR rate on soot emissions. Results of this study indicate that soot emissions increase owing to the drop of intake oxygen concentration and the rise of equivalence ratio as the EGR rate increases at a given engine load and speed, especially the high load.

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Combustion Characteristics According to the Equivalence Ratio of Hydrocarbon Fuel/Air Premixture Excited by Ultrasonic Standing Wave (정상초음파가 인가된 탄화수소계 연료/공기 혼합물의 당량비에 따른 연소특성)

  • Kim, Min Cheol;Bae, Seong Hun;Hong, Joon Yeol;Kim, Jeong Soo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.628-631
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    • 2017
  • An experimental study of the combustion characteristics according to the equivalence ratio of hydrocarbon fuel/air premixture excited by ultrasonic standing wave are presented. The image of the propagating flame was acquired using a high-speed camera, and the combustion characteristics of each fuel were closely observed through image processing. it was conformed that ultrasonic standing wave has been found to stimulate the combustion reaction in the stoichiometric ratio.

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