• 제목/요약/키워드: Lean combustion

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메탄-공기/합성가스-공기 예혼합화염의 후류 상호 작용에 대한 연구 (A Study on Downstream Interaction between Methane-air and Syngas-air Premixed Flames)

  • 박정;권오붕;길상인;윤진한
    • 한국연소학회지
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    • 제21권1호
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    • pp.8-17
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    • 2016
  • Downstream interactions between lean premixed flames with mutually different fuels of syngas and $CH_4$ have been numerically investigated particularly on and near lean extinction limits. The interaction characteristics between lean premixed (50% $H_2$ + 50% CO)-air and $CH_4$-air flames were shown to be quite different from those between the same hydrocarbon flames. The lean extinction boundaries were of slanted shape, thereby implying strong interactions. The weaker flames had negative flame speeds on the upper extinction boundaries, whereas the weaker flame speeds on the lower extinction boundaries were both negative and positive. The results also showed that the flame interaction characteristics did not follow the general tendency with the dependency of Lewis number in downstream interactions between the same hydrocarbon flames. Importance of chemical interaction in flame characteristics is discussed in the downstream interactions between lean premixed (50% $H_2$ + 50% CO)-air and $CH_4$-air flames.

직접분사식 가솔린엔진의 분사 비율에 따른 연소특성에 관한 연구 (A Study on the Characteristics of Combustion according to Injection Strategy in DISI Engine)

  • 인병덕;박상기;이기형
    • 한국자동차공학회논문집
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    • 제20권1호
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    • pp.68-76
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    • 2012
  • Recently, the important issues of gasoline engine are to reduce the fuel consumption and emission. Thus, many researchers are studying the technology to solve these problems. One approach of these issues is to achieve homogeneous charge combustion and stratified change combustion with various injection strategy. In this study, the combustion characteristics of DISI engine accrding to injection strategy were examined. The effect of injection timing on lean limit A/F were investigated using dual DISI single cylinder. The results show that the engine operation region of dual DISI type engine is larger than that of PFI and DISI type engine cases. Especially, late injection is very effective to extend the operation region more than any other injection timings. In addition, the results show that when the DISI injection ratio is increase, leam limit A/F is improved. It means that the dual injection system car meet with emission regulations and reduce the fuel consumption. Also, combustion pressure of dual injection system is much higher than PFI and DISI injection.

메탄-수소-공기 예혼합기의 연소특성( I ) (Combustion Characteristics of Methane-Hydrogen-Air Premixture( I ))

  • 김봉석;권철홍
    • 한국자동차공학회논문집
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    • 제3권3호
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    • pp.129-139
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    • 1995
  • This study investigates the combustion characteristics of methane-hydrogen-air premixture in a constant volume combustion chamber. Primary factors of the combustion characteristics of methane- hydrogen-air premixture are the equivalence ratio and hydrogen supplement rate. In the case of $\phi$= 1.1, maximum combustion pressure and heat release rate have peaks, and they increase as the initial pressure and hydrogen supplement rate increase. The total burning time is also the shortest at the $\phi$= 1.1, it shorten by lowering the initial pressure and by increasing the hydrogen supplement rate. The maximum flame temperature is shown at the $\phi$= 1.0, and increasing the initial pressure and hydrogen supplement rate, it increases. The concentration of NO reveals the highest value at the $\phi$= 0.9, and it increases by increasing the initial pressure and hydrogen supplement rate. It is also found that the limit of lean inflammability of methane-hydrogen-air premixture is greatly widened by increasing the hydrogen supplement rate.

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화염거동을 통한 이중선회 가스터빈 모델 연소기에서 연소실 길이에 따른 연소 불안정성 이해 (Combustion Instability Comprehension with Combustion Chamber Length in Dual Swirl Gas Turbine Model Combustor from Flame Behaviors)

  • 장문석;이기만
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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    • pp.233-235
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    • 2015
  • This study is to investigate the combustion instability of the variation of combustion chamber length in dual swirl gas turbine model combustor. When equivalence ratio was fixed at 1.1, as the length of the combustion chamber increases the value of the frequency decreased in 7kW while the value of the frequency was constant in 4kW. The analysis of flame behaviors by high speed camera was conducted to identify such trend.

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성층희박연소 운전조건에서 분사시기에 따른 분무유도식 직접분사 가솔린엔진의 분무 및 화염특성 (Effect of Injection Pressure and Injection Timing on Spray and Flame Characteristics of Spray-Guided Direct-Injection Spark-Ignition Engine under Lean Stratified Combustion Operation)

  • 오희창;이민석;박정서;배충식
    • 대한기계학회논문집B
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    • 제37권3호
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    • pp.221-228
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    • 2013
  • 분무유도식 DISI엔진의 성층연소운전조건에서 분무 및 화염특성에 대한 실험적 연구가 수행되었다. 연소가시화를 통하여 성층연소 DISI의 연소는 희박 예혼합 연소와 확산연소의 성격을 모두 가지고 있는 것으로 확인되었다. 분사시기에 따른 혼합기 형성특성이 연소의 특성을 결정하는 중요한 인자임을 관찰하였다. 분무와 혼합기 가시화를 통해 낮은 분위기압에서의 over-mixing, 높은 분위기압에서의 under-mixing이 발생하는 것을 확인하였으며 이러한 혼합기 형성과정의 결과에 따라 화염특성, 연소효율 등의 연소특성이 결정되는 것을 살펴볼 수 있었다. 또한, NOx, IMEP도 분사시기에 따른 경향성을 보였으며, 분사시기에 따른 연소상의 변화에 의한 영향임을 확인하였다.

제트 혼합 반응기 내 희박 예혼합 메탄-공기 연소의 NO 생성 예측을 위한 화학 반응기 모델링 (A Chemical Reactor Modeling for Prediction of NO Formation of Methane-Air Lean Premixed Combustion in Jet Stirred Reactor)

  • 이보람;박정규;이도용;이민철;박원식
    • 대한기계학회논문집B
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    • 제34권4호
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    • pp.365-373
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    • 2010
  • 제트 혼합 반응기(JSR) 내의 NOx와 같은 배출물질을 예측하기 위해서 화학반응기 모델을 개발했다. 본 연구에서는 JSR에 대한 화학반응기 모델로서 two-PSR 모델이 채택되었다. CHEMKIN 코드와 4가지 NO 생성 메커니즘을 포함한 GRI 3.0 메탄-공기 연소 메커니즘을 이용해서 JSR내의 희박 예혼합 메탄-공기 연소의 NO 생성예측을 실시하였다. 모델의 검증을 위해서 계산된 결과를 Rutar의 실험 데이터와 비교하였다. NO 생성의 중요 파라미터와 4 가지 NO 경로의 기여도를 조사하였다. 화염 영역에서는 prompt 메커니즘이 주된 경로이고, 화염후영역에서는 Zeldovich 메커니즘이 주된 경로이다. 희박 예혼합 조건에서는 N2O 메카니즘이가 화염 및 화염후 영역 모두에서 중요한 경로이다.

바이오에탄올 SI 엔진에서 에탄올-가솔린 연료 혼합비율에 따른 희박연소 및 배기 특성 (Effect of Ethanol-gasoline Blending Ratio on Lean Combustion and Exhaust Emissions Characteristics in a SI Engine Fueled with Bioethanol)

  • 윤승현;김대성;이창식
    • 한국자동차공학회논문집
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    • 제19권1호
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    • pp.82-88
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    • 2011
  • Lean combustion and exhaust emission characteristics in a ethanol fueled spark-ignited engine according to ethanol-gasoline fuel blending ratio were investigated. The test engine was $1591cm^3$ and 10.5 of compression ratio SI engine with 4 cylinders. In addition, lambda sensor system was connected with universal ECU to control the lambda value which is varied from 1.0 to 1.5. The engine performance and lean combustion characteristics such as brake torque, cylinder pressure and rate of heat release were investigated according to ethanol-gasoline fuel blending ratio. Furthermore, the exhaust emissions such as carbon monoxide (CO), unburned hydrocarbon (HC), nitrogen oxides ($NO_x$) and carbon dioxide ($CO_2$) were measured by emission analyzers. The results showed that the brake torque, cylinder pressure and the stability of engine operation were increased as ethanol blending ratio is increased. Brake specific fuel consumption (BSFC) was increased in higher ethanol blending ratio while brake specific energy consumption (BSEC) was decreased in higher ethanol blending ratio. The exhaust emissions were decreased as ethanol blending ratio is increased under overall experimental conditions, however, some specific exhaust emission characteristics were mainly influenced by lambda value and ethanol-gasoline fuel blending ratio.

대형 천연가스엔진에서의 수소 첨가에 의한 희박연소특성 연구 (A Study on Lean Combustion Characteristics with Hydrogen Addition in a Heavy Duty Natural Gas Engine)

  • 박철웅;김창기;최영;원상연
    • 한국가스학회지
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    • 제14권4호
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    • pp.12-17
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    • 2010
  • 자동차 연료로서의 천연가스는 고옥탄가, 넓은 연소 한계, 낮은 미연탄화수소 배출 특성, 지구 온난화 물질인 $CO_2$배출 저감 등 디젤과 가솔린을 대신할 수 있는 현실성 있는 대체연료이다. 그러나 희박운전 영역에서는 느린 연소속도 등으로 연소가 불안정해지고 유해 배기가스가 증가하는 단점이 있다. 수소의 첨가는 연소속도를 빠르게 하고 가연한계를 확장시켜 초희박 영역에서도 안정된 운전을 가능하게 하며, NOx의 저감에 유리하다. 본 연구에서는 대형 수소-천연가스 혼합연료 엔진에서 수소 첨가에 따른 기본 연소특성과 희박영역 확장, 배기성능 및 효율 특성에 대해 검토하였다.

희박연소를 이용한 가스터빈 연소기의 저 $NO_{x}$ 특성 (The Low $NO_{x}$ Characteristics of a Lean Premixed Gas Turbine Combustor)

  • 손민규;안국영;김한석;김용모
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.66-70
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    • 2001
  • The combustion characteristics have been investigated to develop the low $NO_{x}$ gas turbine combustor. The lean premixed combustion technology was applied to reduce the $NO_{x}$ emission. Also, the conventional combustor was designed and tested for the baseline of low $NO_{x}$ combustor performance. The test was conducted at the condition of high temperature and ambient pressure. The combustion air which has the temperature of 500K were supplied to the combustor through the air preheater. The temperature and emissions of $NO_{x}$ and CO were measured at the exit of combustor. The premixing chamber can be operated very lean condition of equivalence ratio around 0.35. The $NO_{x}$ was decreased with decreasing the equivalence ration. The CO was decreased with decreasing the equivalence ratio, but the CO was increased with decreasing the equivalence ratio below 0.45. But, at the very lean condition of equivalence ratio below 0.35 both NOx and CO were increased because of the flame unstability. The $NO_{x}$ was decreased slightly and CO was increased with increasing inlet air flowrate. This results can be used to determine the size of combustor. The low $NO_{x}$ combustor has lower values of $NO_{x}$ and CO compared with conventional one. Consequently the performance of combustor shows the possibility of the application to the gas turbine system.

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메탄 과농-희박 예혼합화염의 안정화 메커니즘 (Stabilizing Mechanism for Methane Rich-Lean Flame)

  • 이원남;서동규
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2002년도 제25회 KOSCI SYMPOSIUM 논문집
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    • pp.19-24
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    • 2002
  • Recent studies of a triple flame suggested that the presence of triple point (triple line in this planar configuration) could explain the mechanisms of stable fuel-lean premixed flames with equivalence ratio lower than the flammability limit. In the present study, for better understanding of the stability mechanisms of fuel rich-lean premixed flames, the fuel-rich flames were replaced with hot coils that will provide heat flux into the fuel-lean flames. It is found that the fuel-lean premixed flames could be stabilized without any triple point (triple line): however, the equivalence ratio limit for stable fuel-lean flame in this case is higher than that of the present work with the presence of fuel-rich flames. These results demonstrate that heat flux coming from fuel-rich flames should be considered in order to properly understand the roll of a triple flame for stable fuel rich-lean flames.

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