• Title/Summary/Keyword: 예혼합실

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The Study for Designs of Lean-Premixed low NOx Combustor (희박-예혼합 저 NOx 연소기 설계에 대한 연구)

  • Lim, Am-Ho;Kim, Han-Suck;Ann, Kuk-Young;Lee, Sang-Min;Kim, Yong-Mo
    • 한국연소학회:학술대회논문집
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    • 2003.12a
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    • pp.83-88
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    • 2003
  • The concept of lean-premixed combustion in gas turbine combustor operation has become a standard in recent years as an effective means to meet stringent environmental standards on NOx emissions. Various types of air-fuel premixer, which affect greatly NOx emission and stability of lean-premixed low NOx combustor, were investigated experimentally to reduce the NOx emission. One type of the premixers is selected by experiments and applied it to 70kW class lean-premixed gas turbine combustor. The exit temperature and emissions of CO and NOx were measured with equivalence ratios at ambient pressure. From the results, the emissions of CO and NOx were influenced by the type of air-fuel premixer. As the mixing length of air and fuel is longer, the NOx and CO emission were decreased in the primary reaction zone. Compared with of conventional combustor, the lean-premixed low NOx combustor has low NOx emission characteristics.

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Study on the Combustion Characteristics of a Lean-Premixed Combustor (예혼합 희박 연소기의 연소특성에 관한 연구)

  • Kim, Han-Seok;Lim, Am-Ho;Ann, Kuk-Young;Lee, Sang-Min
    • Journal of the Korean Society of Combustion
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    • v.9 no.1
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    • pp.25-31
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    • 2004
  • Various types of the air/fuel pre-mixer have been designed and tested to investigate the combustion characteristics of the lean-premixed gas turbine combustor, such as NO emission and flame stability. One type of the pre-mixers has been selected and installed to a 70 kW lean-premixed gas turbine combustor. The concentrations of CO and NO were measured with varying equivalence ratios in the combustion chamber at ambient pressure. The result shows that the emissions of CO and NO are heavily affected by the shape of the pre-mixer. The NO and CO emissions decreased, as the mixing ratio of air and fuel increased. In addition, the NO emission of the lean-premixed low NOx combustor is more dependent on the equivalence ratio than that of the conventional combustor.

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The Low-NOx Characteristics of Premixed Lean-Burn Gas Turbine Combustor (예혼합 희박연소 가스터빈 연소기의 저 NOx 특성)

  • Pae, H.S.;Ahn, K.Y.;Park, J.I.;Ahn, J.H.;Kim, Y.M.
    • 한국연소학회:학술대회논문집
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    • 1999.10a
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    • pp.201-207
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    • 1999
  • The combustion characteristics for the low NOx 50 kW-class gas turbine combustor have been experimentally investigated. In order to achieve the premixing and the lean burn combustion, the geometries of the primary zone including premixed chamber were modified from conventional combustor. The centerline profiles of CO and NO concentration, and temperature were measured for the premixed combustors with or without dilution holes in the liner. The effects of the pilot fuel injection rate and air dilution on flame stabilization and pollutant (CO, NO) emission are discussed in detail.

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Study on the Effect of Thermal Stratification on DME/n-Butane HCCI Combustion (열적성층화가 DME/n-Butane 예혼합압축자기착화연소에 미치는 영향에 관한 연구)

  • Lim, Ock-Taeck
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.12
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    • pp.1035-1042
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    • 2010
  • The thermal stratification effect has been thought as one of the way to avoid dramatically generating the heat from HCCI combustion. We investigate the effect of thermal stratification on HCCI combustion fueled by DME and n-Butane. The thermal stratification occurs in a combustion chamber of a rapid compression machine with premixture by buoyancy effect that is made of fuel and air. The premixture is then adiabatically compressed, and during the process, the in-cylinder gas pressure is measured and two-dimensional chemiluminescence images are prepared and analyzed. Under the thermal stratification, the LTR starting time and the HTR starting time are advanced than that of homogeneous case. Further, the LTR period and the luminosity duration under homogeneous conditions are shorter than the corresponding quantities under stratified conditions. Additionally, under stratified conditions, the brightest luminosity intensity is delayed longer than that of homogeneous condition.

Concept Design on Heating System for Supersonic Air-Breathing Engine Test Facility (초음속 유도무기 지상 시험용 가열기 개념 설계)

  • Han Poong-Gyoo;NamKoung Hyuck-Joon;Lee Kyoung-Hoon;Kim Young-Soo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.321-326
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    • 2006
  • Vitiated air heater which could supply air of 700K and 6 bar was designed conceptually for the firing test on the ground of the air breathing propulsion engines. This vitiated air heater consists of premixer with air and excessive gas oxygen, mixing head, combustor with gas passage, convergent-divergent nozzle and diffuser. the fuel was natural gas and/or liquefied natural gas. Through computational fluid dynamics, each component of the air heater was analyzed and flame-holding after ignition was investigated.

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A Study on the Combustion Characteristics of Flat-Plate Premixed Burner for Various Flame Surface Media and Heat Exchangers (평판형 예혼합 버너의 다양한 화염면 매질 및 열교환기에 따른 연소 특성)

  • Cho, Eun-Seong;Park, Chang-Kwon;Choi, Kyung-Suhk
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.10
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    • pp.1033-1040
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    • 2011
  • The premixed burner is a very strong candidate for using household boiler burner system because it has high efficiency, low emission and can be used in compact boiler system. Usually, household boiler burner systems use a Bunsen burner, which consists of an inner rich premixed flame and fuel burned completely by a secondary air supply. It has a relatively long flame length and operates in a high excess of air, so it is difficult to fit such a burner into a high efficiency compact boiler. In this paper, the characteristics of a premixed combustion burner for surface media such as metal fiber, ceramic, and SUS fin were evaluated. In particular, the flow velocity over the burner surface for the cold flow characteristics of the surface material were measured and adjusted. The combustion tests were carried out by taking pictures of the flame and measuring the flame temperature. The amounts of CO and NO were measured and the characteristics of the surface burner materials, combustion chamber, and heat exchangers were evaluated for various excess air ratios and heating values.

Using Two-Dimensional Chemiluminescence Images to Study Inhomogeneity in Mixture Gas in the Combustion Chamber for HCCI Combustion (이차원발광화상계측에 의한 예혼합압축자기착화연소의 연소실내 혼합기의 불균질성에 관한 연구)

  • Lim, Ock-Taeck;Iida, Norimasa
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.12
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    • pp.1043-1050
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    • 2010
  • Fuel stratification and thermal stratification occur in the HCCI combustion chamber on a microscopic scale. They affect the ignition and combustion processes. In this study, the effect of the inhomogeneity in the mixture gas on the HCCI combustion process was investigated. Two-dimensional chemiluminescence images were captured using a framing camera to evaluate the flame structure. DME was used as the test fuel. First, the effect of inhomogeneity in the fuel distribution in the premixture was investigated for the four-stroke optically accessible engine. Then, by comparing the combustion of the homogeneous mixture in the rapid compression machine, which does not contain any residual gas, with the combustion in the four-stroke engine, the effect of inhomogeneity in temperature due to the residual gas was analyzed. The results showed that a time lag appears spatially in combustion under inhomogeneous conditions in the four-stroke engine. The spatial variation in the combustion without the residual gas in the rapid compression machine is less than that in the combustion in the four-stroke engine.

A study on the combustion characteristics according to evaporation rate of gasoline (가솔린 연료의 기화율 변화에 따른 연소 특성에 관한 기초 연구)

  • Lee, K.H.;Lee, C.S.;Shin, K.S.;Cho, H.M.
    • Journal of ILASS-Korea
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    • v.1 no.3
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    • pp.29-36
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    • 1996
  • The present study systematically investigates the effect of evaporation rate on the combustion characteristics and the flame stabilization in a gasoline engine. A constant volume combustion chamber was used to elucidate a basic combustion characteristics and the premixer was installed to control temperature and equivalence ratio. And the maximum pressure, combustion duration and flame propagation according to the evaporation rate were measured to determine the optimal temperature range for evaparating a gasoline fuel. These experimental results indicate that the combustion characteristics such as combustion chamber pressure and combustion duration were deteriorated by decreasing surrounding temperature of fuel injected. It was also found that the overall gasification process for gasoline fuel was strongly influenced by a combustion chamber temperature rather than a premixer temperature.

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Dual-Fuel Combustion Phenomena of Pilot Distillate Injected to Pre-mixed Natural Gas in a Constant Volume Combustion Bomb (천연가스가 예혼합된 정적연소실에 파일럿오일을 분사한 복합연소현상)

  • Choi, I.S.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.3 no.6
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    • pp.112-122
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    • 1995
  • As an alternative fuel producing less exhaust emissions, natural gas is of interest for use both in SI and CI engines. The potential of natural gas fuelled dual-fuel engine is considered high enough. However, much effort has to be made so that gaseous fuel is used efficiently with simultaneous minimum use of pilot oil. Hence, a simplified three-dimensional model, using a finite volume method in cylindrical coordinates, has been developed to facilitate an understanding of the dual-fuel combustion phenomena and to predict the complex interactions between the pilot distillate and natural gas. The computer model was calibrated by comparing it with the experimental results obtained from diesel engine like combustion bomb tests. In the pre-mixed natural gas combustion, the fuel burning was highly reliant on the injection condition and subsequent burning nature of the pilot distillate.

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