• 제목/요약/키워드: Gas Turbine Combustion

검색결과 413건 처리시간 0.022초

Process Evaluation for Current Ceramic Filters and Granular Bed Filters for High Temperature High Pressure Applications

  • Chung, Jin-Do
    • 에너지공학
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    • 제5권2호
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    • pp.138-145
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    • 1996
  • The particulate collection at high temperature and high pressure (HTHP) is important on the advanced coal power generation system not only to improve the thermal efficiency of the system, but also to prevent the gas turbine from erosion and to meet the emission limits of the effluent gas. The specifications for particulate collection in those systems such as Integrated Coal Gasification Combined Cycle (IGCC) and Pressurized Fluidized Bed Combustion (PFBC) require the absolutely high collection efficiency and reliability. Advanced cyclone, granular bed filter, electrostatic precipitator, and ceramic filter have been developed for particulate collection on the advanced coal power generation system. However, rigid ceramic filters and granular bed filter among them show the best potential. The current technology of these collectors was evaluated in this paper. The experienced problems of these systems on performance, materials, and mechanical design were investigated. Ceramic candle filters has the best potential for IGCC at this moment because it has nearly the highest efficiency comparing with other filtering systems and has accumulated many reliable design data resulted from many field experiences.

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고온고압용기에서 충돌분무 특성에 관한 실험적 연구 (An Experimental Studies on Impingement Spray Characteristic in High Temperature and Pressure Chamber)

  • 안병규;류호성;오은탁;송규근;정재연
    • 한국자동차공학회논문집
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    • 제10권3호
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    • pp.36-43
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    • 2002
  • The characteristics of spray has much effect on performance and emissions for automobile, diesel engine, gas turbine and combustion engines. So spray behavior after impinging the wall is very important for prediction the engine performance. This studies examined about impingement spray considering ambient density(18,24,30kg/ms), temperature(293,473K), impingement angle(0,30,45°). The images of impingement spray were obtained by the high speed video camera. After that we analyzed impingement spray characteristics to use this images. In this experiment, we found that 1) The spray width is reduced by increasing the ambient gas density and temperature,2) The growth of downstream is increased by increasing the impingement angle.

도심지 복합화력 배가스 통로에서의 이상 소음 현상과 영향 (Abnormal Resonance Noise Phenomenon and Effect through Exhaust Gas Passageway in Urban Combined Power Plant)

  • 김연환;이영신;배용채;이현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.866-869
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    • 2004
  • Power transformers, air-intakes and stacks in the urban combined power plant are main noisy sources. Because of Inhabitant complaint by abnormal noise transferred from the power plant. the noise was investigated at power plant and uptown area. The result of diagnosis made the acoustic resonance phenomenon by 580Hz's combustion dynamic pressure with the standing wave mode of sound fields in exhaust passageway of gas turbine into main noise source of public complain. The abnormal noise is caused by the resonance exhaust noise transferred through stacks of power plant.

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열분포를 고려한 열음향 모델의 개선 (Improved Thermoacoustic Model Considering Heat Release Distribution)

  • 김대식;김규태
    • 대한기계학회논문집B
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    • 제38권6호
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    • pp.443-449
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    • 2014
  • 가스터빈 희박 예혼합 연소기에서 발생하는 연소 불안정 현상을 예측하기 위하여 열음향 해석 기법이 폭넓게 사용되고 있다. 그러나 이러한 모델들은 전체 연소기 시스템과 화염의 형상을 과도하게 단순화함으로써, 모델 정확도에 한계를 드러내왔다. 본 연구에서는 두 가지 측면에서 열음향 모델의 정확도를 개선하고자 하는 노력을 시도하였다. 우선 화염의 위치를 연소기 입구가 아닌 실제 계측 결과를 반영할 수 있도록 열음향 모델을 수정하였으며, 두 번째로는 열 발생 위치가 얇은 화염의 형태가 아닌, 실제 화염의 형상과 같이 열 분포 현상을 반영할 수 있도록 하였다. 모델 수정 결과 기존의 열음향 모델 대비, 불안정 현상의 성장률을 예측하는데 있어서 오차가 줄어드는 것으로 나타났다.

모형연소기에서 연료-공기의 혼합정도 및 당량비가 NOx 배출과 열 방출량에 미치는 영향에 대한 연구 (Effect of the Degree of Fuel-Air Mixing and Equivalence Ratio on the NOx Emission and Heat Release in a Dump Combustor)

  • 조봉국;최도욱;김규보;장영준;송주헌;전충환
    • 대한기계학회논문집B
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    • 제33권9호
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    • pp.658-665
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    • 2009
  • Lean premixed combustors are used for significant NOx reduction which one of issues in current gas turbine combustor. This study was investigated to estimate the effects of the unmixedness of fuel-air, equivalence ratio on the instability mechanism, NOx emission and combustion oscillation in a lean premixed combustor. The experiments were conducted in a dump combustor at atmospheric pressure conditions using methane as fuel. The swirler angle was $45^{\circ}$, the degrees of fuel-air mixing were 0, 50 and 100 and inlet temperature was 650K. The equivalence ratio was ranging from 0.5 to 0.8. This paper shows that NOx emission was increased when the degree of fuel-air mixing is increased in same equivalence ratio and when equivalence ratio is increased. And the range of the combustion instability was enlarged as a function of increasing of the degree of fuel-air mixing.

스월변화에 따른 모형 가스터빈 연소기의 열유동장의 실험적 연구 (Experimental Study of Thermo-Flow Field in a Model Gas Turbine Combustor with Various Swirl Conditions)

  • 류송열;구자예
    • 한국항공우주학회지
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    • 제30권4호
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    • pp.70-76
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    • 2002
  • 가스터빈 연소기의 스월러와 노즐을 제작하여 스월러 형상 변화에 따른 비연소시 케로신 분무 특성과 연소시에 열유동장의 특성을 조사하였다. 액적의 크기(SMD)와 속도를 파악하기 위해서 위상도플러입자분석기(PDPA)를 이용하였고, 연소 온도를 조사하기 위해서 R-type 열전대(Platinum vs. Platinum-13%rhodium)를 이용하였다. 분무와 화염의 가시화는 스틸 카메라를 이용하였다. 스월러각이 커서 스월수가 큰 경우에 분무 및 화염이 반경방향으로 빠르게 발전하였다. 화염은 스월수가 작을 때는 원추형의 화염이 형성되지만 스월수가 커지면서 스월 모멘텀이 중심축으로 이송되고 혼합이 촉진되어 원통형으로 바뀌었다.

압력변동이 연료 분사구에서의 당량비 변동에 미치는 영향에 관한 수치 해석 (Numerical Simulation of the Effect of Pressure Fluctuation on the Modulation of Equivalence Ratio at the Fuel Injection Hole)

  • 김현준;홍정구;신현동
    • 대한기계학회논문집B
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    • 제31권3호
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    • pp.292-299
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    • 2007
  • In gas turbine technology, the flame stability is inherently greater in conventional diffusion type combustion over a wider range fuel to oxidizer ratio. However, premixed type combustion which has narrow flame stability region, is widely used due to environmental reason. It has been observed in experiments that combustion instability of low frequency (${\sim}10Hz$) results from the modulation of equivalence ratio at fuel injection hole when a pressure fluctuation propagates upwards along the channel of the burner under an unchoked fuel flow condition. In this study, a commercial program was used to determine how the fuel flow rate changed with respect to the pressure, velocity of the fuel flow and the mass fraction in a choked and an unchoked condition. The calculation focuses on the upstream of the dump plane to know how the forced pressure with the fuel injection conditions affects the modulation of the equivalence ratio. Therefore, it is found that pressure fluctuation leads to oscillation of mass flow rate and then results in equivalence ratio modulation under the unchoked fuel flow condition.

이중선회 가스터빈 모델연소기에서 맥놀이 현상으로 인한 연소불안정 특성 (Combustion Instability Characteristics due to the Beating Phenomenon in the Dual Swirl Gas Turbine Model Combustor)

  • 장문석;이기만
    • 한국추진공학회지
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    • 제20권6호
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    • pp.61-69
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    • 2016
  • 본 연구는 이중 선회 가스터빈 연소기에서 연소실 길이와 열용량을 변수로 연소불안정 현상과 관련된 결과이다. 특히 열용량이 상대적으로 작은 구간에서 연소실 길이가 길어지면 공진 주파수의 값이 일정하게 유지되는 맥놀이 현상이 발생하는 것이 확인되었다. 이러한 맥놀이 현상은 메인 화염과 파일럿 화염이 각각 다른 주기로 거동하기 때문에 발생되었으며, 연소실 길이가 증가하여도 주파수의 값이 변하지 않는 현상은 메인 화염과 파일럿 화염의 서로 다른 상호작용 결과라고 판단된다.

유동 섭동에 의한 난류예혼합화염의 열발생 모델에 관한 연구 (A Heat Release Model of Turbulent Premixed Flame Response to Acoustic Perturbations)

  • 조주형;백승욱
    • 대한기계학회논문집B
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    • 제32권6호
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    • pp.413-420
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    • 2008
  • The unsteady heat release characteristics play a significant role in combustion instabilities observed in low emissions gas turbine combustors. Such combustion instabilities are often caused by coupling mechanisms between unsteady heat release rates and acoustic perturbations. A generalized model of the turbulent flame response to acoustic perturbations is analytically formulated by considering a distributed heat release along a curved mean flame front and using the flame's kinematic model that incorporates the turbulent flame development. The effects of the development of flame speed on the flame transfer functions are examined by calculating the transfer functions with a constant or developing flame speed. The flame transfer function due to velocity fluctuation shows that, when a developing flame speed is used, the transfer function magnitude decreases faster with Strouhal number than the results with a constant flame speed at low Strouhal numbers. The flame transfer function due to mixture ratio fluctuation, however, exhibits the opposite results: the transfer function magnitude with a developing flame speed increases faster than that with a constant flame speed at low Strouhal numbers. Oscillatory behaviors of both transfer function magnitudes are shown to be damped when a developing flame speed is used. Both transfer functions also show similar behaviors in the phase characteristics: The phases of both transfer functions with a developing flame speed increase more rapidly than those with a constant flame speed.

DMD 기법을 적용한 모형 가스터빈의 연소불안정성 평가에 관한 실험적 연구 (An Experimental Study on the Combustion Instability Evaluation by Using DMD)

  • 손진우;손채훈;윤지수;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.59-60
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    • 2017
  • 가스터빈 연소기의 연소불안정성을 평가하기 위해 동적모드분해(dynamic mode decomposition, DMD) 기법을 적용하였다. DMD 기법으로 도출된 감쇠계수(damping coefficient)와 FFT 결과를 비교 분석 하였다. 또한 화염전달함수 (flame transfer function, FTF)를 도출하는 실험적 방법에 DMD 기법을 적용하여 분석을 시도하였다. 기존에 제시된 열방출 섭동을 추출하는 방법에서 개선된, OH PLIF 이미지를 이용하여 열방출 섭동을 추출하는 방법을 사용하였다. 분석 결과, 열방출 섭동의 추출 위치에 따라 화염전달함수의 이득(gain)이 변하는 것을 확인하였다.

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