• 제목/요약/키워드: 희박혼합연소

검색결과 132건 처리시간 0.026초

저 NOx 희박연소기의 주연소영역에서의 연소특성 연구 (The Combustion Characteristics at Primary Zone of Lean Premixed low NOx Combustor)

  • 임암호;안국영;김한석;김용모
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.314-319
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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 enviromental standards on NOx emissions. The combustion characteristics of 75 kW class lean premixed combustor were investigated at the conditions of high temperature and ambient pressure. The exit temperature and emissions of CO and NOx were measured at the center of exit plane. The high temperature air of $550K{\sim}650K$ was supplied through air preheater. As expected, experimental results indicate that NOx emission was increased and CO emission was decreased by increasing inlet air temperature. But CO emission measured at the center of exit plane was increased because of the non-uniform radial direction profiles. The Semi-Empirical Correlation method was applied to obtain the design point emissions of NOx and CO. Also the flame temperature, CO and NOx emissions were measured along the centerline of liner at 650K inlet air temperature to determine the position of dilution holes.

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연소 불안정 예측을 위한 열음향 해석 모델 - Part 2 : 비선형 안정성 해석 (Thermoacoustic Analysis Model for Combustion Instability Prediction - Part 2 : Nonlinear Instability Analysis)

  • 김대식;김규태
    • 한국추진공학회지
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    • 제16권6호
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    • pp.41-47
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    • 2012
  • 연소 불안정 현상을 완전하게 이해하기 위해서는 천이 과정과 한계 진폭과 같은 비선형 거동에 대한 예측이 매우 중요하다. 가스터빈 희박 예혼합 연소기에서 이러한 비선형 거동은 화염의 비선형 동특성에 크게 의존하게 된다. 본 연구에서는 기존에 선형 해석으로부터 비선형 열음향 해석으로 확장하기 위해서 화염 묘사 함수를 통한 시스템 안정성 해석 기법이 소개되었다. 이를 위하여, 주파수 뿐만 아니라 속도 진폭에 따른 열발생율의 변동 특성이 실험 결과로부터 모델링되었다. 현재 해석 조건에서 비선형 모델링 결과, 주어진 연소기 길이에서 속도 진폭이 불안정 주파수에 미치는 영향은 미비하였으나, 성장률에는 크게 영향을 미치는 것으로 나타났다. 향후 다양한 조건에서 비선형 모델의 검증과 한계 진폭의 예측 결과에 대한 실험 결과와의 비교가 요구된다.

Heavy-duty HCNG엔진의 연소 및 배기성능 최적화에 관한 연구 (A Study on the Optimization of Combustion and Emission Performance in a Heavy-duty HCNG Engine)

  • 최영;박철웅;원상연;김창기
    • 한국가스학회지
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    • 제15권2호
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    • pp.15-20
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    • 2011
  • 도심 대기오염을 줄이고자 도입된 CNG 버스는 현재의 배기규제 기준을 만족시켜 도시 대기환경 개선에 많은 기여를 했지만 추가적인 후처리 장치의 도움 없이는 차기 배기기준인 유로6 배기규제를 만족시키기 매우 어렵다. 수소는 매우 활발하고 빠른 반응성을 가지고 있으며 희박가연한계 또한 매우 넓어 기존 연료와 함께 사용 시 개선된 연소 및 배기성능을 기대할 수 있다. 따라서 본 연구에서는 시내버스용 대형 CNG 엔진에 수소를 일정 부분 CNG와 혼합한 HCNG 연료를 공급하여 희박연소를 시킴으로서 연소 및 배기성능을 개선하는 실험을 수행하였다. 수소혼합비율, 공연비, 점화시기 변화에 따른 연소 및 배기성능을 살펴보고 최적운전조건을 찾아내었으며 산화촉매 성능평가를 통해 11리터 버스용 HCNG 엔진의 상용화 가능성을 검토하였다.

희박 예혼합 연소를 이용한 마이크로터빈의 저공해 연소기 개발에 관한 연구 (The Study on Development of Low NOx Combustor with Lean Burn Characteristics for Microturbine)

  • 윤정중;이헌석
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.63-72
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    • 2003
  • In order to reduce NOx emissions in the 20kW class microturbine under development, the low NOx characteristics, as being an application to the lean premixed combustion technology, have been investigated. The study has been conducted at the conditions of high temperature and high pressure. Theair from a compressor with the pressure of 2.5bar, 3.0bar, 3.5bar was supplied to the combustor with the temperature 560K through the air preheat-treatment. The sampling exhaust gas was measured at the immediate exit of the combustor. For the effect of temperature on NO and CO emissions, though NOx were increased, CO was decreased with increasing inlet air temperature. With increasing inlet air pressure, NOx were increased and CO was decreased also. NOx were decreased, but CO was increased with increasing inlet air mass flow rate. The test has been performed on the equivalent ratio of 0.10 to 0.16 in the lean region. NOx were increased with increasing equivalent ratio, but CO was decreased as an influence of flame temperature. CFD work with an appropriate combustion model predicated a complicated swirling flow pattern in the combustor, and also produced a numerical value of NOx and CO emissions which was to be compared with the experimental one. As the results of this study, NOx are expected to be reduced to less than 42ppm at 15% O2 when operated at the design condition of the 20kW class microturbine.

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희박 예혼합 모형 가스터빈 연소기의 화염구조와 배기특성에 관한 실험적 연구 (Experimental Investigation on Flame Structure and Emission Characteristics in a Lean Premixed Model Gas Turbine Combustor)

  • 이종호;김대현;전충환;장영준
    • 대한기계학회논문집B
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    • 제28권4호
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    • pp.425-432
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    • 2004
  • The objective of this study is a qualitative comparison between line-integrated OH chemiluminescence(OH$\^$*/) image and its Abel inverted image to investigate the flame structure at different phase of the oscillating pressure field. PIV(Particle Image Velocimetry) measurements were conducted under non-reacting conditions to see the global flow structure and NOx emission was measured to investigate the effect of fuel-air premixing on combustion instability and emission characteristics. Experiments were carried out in an atmospheric pressure, laboratory-scale dump combustor operating on natural gas. Combustion instabilities in present study exhibited a longitudinal mode with a dominant frequency of ∼341.8㎐, which corresponded to a quarter wave mode of combustor. Heat release and pressure waves were in-phase when instability occurred. Results gave an insight about the location where the strong coherence of pressure and heat release existed. Also an additional information on active control to suppress the combustion instabilities was obtained. For lean premixed combustion, strong correlation between OH$\^$*/ and NOx emissions was expected largely due to the exponential dependence of thermal NOx mechanism on flame temperature.

희박 예혼합 덤프 연소기에서 OH 자발광을 이용한 열 방출에 관한 실험적 연구 (Experimental Study on Heat Release in a Lean Premixed Dump Combustor using OH Chemiluminescence Images)

  • 문건필;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1146-1151
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    • 2004
  • Measurements of OH chemiluminescence in an atmospheric pressure, laboratory-scale dump combustor at equivalence ratios ranging from 0.63 to 0.89 were reported. The signal from the first electronically excited state of OH to ground state was detected through a band-pass filter with an ICCD. The objectives of this study are two: One is to see the effects of equivalence ratio on global heat release rate and local Rayleigh index distribution. To get the local Rayleigh index distribution, the line-of-sight images were inverted by tomographic method, such as Abel de-convolution. Another aim is to investigate the validity of using OH chemiluminescence acquired with an ICCD as a qualitative measure of local heat release. For constant inlet velocity and temperature, the overall intensities of OH emission acquired at different equivalence ratio showed periodic and higher value at high equivalence ratio. OH intensity averaged over one period of pressure increased exponentially with equivalence ratio. Local Rayleigh index distribution clearly showed the region of amplifying or damping the combustion instability as equivalence ratio increased. It could provide an information/insights on active control such as secondary fuel injection. Finally, local heat release rate derived from reconstructed OH images were presented for typical locations.

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희박 예혼합 모형 가스터빈 연소기의 화염구조와 배기특성에 관한 실험적 연구 (Experimental Investigation on Flame Structure and Emission Characteristics in a Lean Premixed Model Gas Turbine Combustor)

  • 문건필;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.356-361
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    • 2003
  • The objective of this study is a qualitative comparison between line-integrated OH chemiluminescence ($OH{\ast}$) image and its Abel inversion image at different phase of the oscillating pressure field. PIV(Particle Image Velocimetry) measurements were conducted under non-reacting conditions to see the global flow structure. Also NOx emission was measured to investigate the effect of fuel-air premixing on combustion instability and emission characteristics. Experiments were carried out in an atmospheric pressure, laboratory-scale dump combustor operating on natural gas. Combustion instabilities in present study exhibited a longitudinal mode with a dominant frequency of ${\sim}341.8$ Hz, which corresponded to a quarter wave mode of combustor. Heat release and pressure waves were in-phase when instability occurred. Results gave an insight about the location where the strong coherence of pressure and heat release existed. Also an additional information on active control to suppress the combustion instabilities was obtained. For lean premixed combustion, strong correlation between $OH{\ast}$ and NOx emissions was expected largely due to the exponential dependence of thermal NOx mechanism on flame temperature.

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다공성 물질에 의한 열재순환 화염에 관한 실험적 연구 I

  • 유영돈;민대기;신현동
    • 대한기계학회논문집
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    • 제12권5호
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    • pp.1113-1120
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    • 1988
  • 본 연구에서는 4종류의 실험 모델을 채택하여 연소 반응용다공성 블럭(combu- stive reacting porous block)내의 화염대 위치와 화염의 온도 분포, 화염이 안정화 되는 범위를 고찰하여 내부 열재순환 효과를 규명하고 예열용 다공성 블럭(preheating porous block)과 복사 차폐용 다공성 블럭(radiative insulating porous block)의 효 과에 대한 연구와 초희박 혼합기나 저 발열량 연료의 연소 가능성을 제시하고 수치 계 산에 필요한 자료를 제시하는 것이다.

연료-공기 비혼합도가 희박예혼합 연소 특성에 미치는 영향 (Effects of Fuel-Air Unmixedness on Lean Premixed Combustion Characteristics)

  • 김대현;이종호;전충환;장영준
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2002년도 제24회 KOSCO SYMPOSIUM 논문집
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    • pp.133-139
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    • 2002
  • The lean premixed technique has been proven very efficient in reducing NOx emissions from gas turbine combustors. However combustion instability is susceptible to occur in lean premixed combustor. So laboratory-scale dump combustor was used to understanding the underlying mechanisms causing combustion instabilities. In this study, tests were conducted at atmospheric pressure and inlet air was up to $360^{\circ}C$ with natural gas. The observed instability was a longitudinal mode with a frequency of ${\sim}341.8Hz$. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various equivalence ratio. Combustion instability was observed to occur at higher value of equivalence ratio(>0.69). This study was performed to investigate the effects of equivalence ratio and fuel split measuring NOx and acoustic wave. The results reveal the effect of fuel-air unmixedness on lean premixed combustor.

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나노-마이크로 알루미늄 혼합 입자의 공기와의 연소 모델링 (Combustion Modeling of Nano/Micro Aluminum Particle Mixture)

  • 윤시경;신준수;성홍계
    • 한국추진공학회지
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    • 제15권6호
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    • pp.15-25
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    • 2011
  • 금속 연료 중 널리 사용되는 알루미늄의 연소 특성에 관하여 1차원 연소모델링을 제안하였다. 연소 모델링은 예열영역, 반응영역, 반응 후 영역, 세 영역으로 나누어 수행하였다. 또한 희박연소로 가정하여 단일 입자의 경우 입자크기와 당량비에 따른 화염속도, 나노와 마이크로 입자의 혼합물의 경우 혼합 비율에 따른 화염속도를 압력이 1기압 조건에서 계산하여 실험결과와 비교하였다. 단일입자의 경우, 입자의 크기가 작아질수록 화염속도가 빨라지고, 당량비가 낮아질수록 화염속도가 느려지는 현상이 관찰되었다. 나노와 마이크로 입자의 혼합물의 경우, 나노 입자의 함유량에 따라 화염속도는 빨라지며, 화염구조는 분리화염과 중첩화염이 나타남이 관찰되었다.