• 제목/요약/키워드: DLN 연소기

검색결과 13건 처리시간 0.02초

M501J 가스터빈 연소기 단별 연료비율이 연소상태에 미치는 영향 고찰 (Effects of Combustor Stages on M501J Gas Turbine Combustion)

  • 유원주;정진도
    • 대한안전경영과학회지
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    • 제21권2호
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    • pp.1-8
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    • 2019
  • Most of gas turbine combined cycle power plants are located in urban areas to provide peak load and district heating. However, NOx(nitrogen oxides) of exhaust gas emission from the power plants cause additional fine dust and thus it has negative impact on the urban environment. Although DLN(dry low NOx) and multi-stage combustors have been widely applied to solve this problem, they have another critical problem of damages to combustors and turbine components due to combustion dynamic pressure. In this study, the effect of different fuel ratio on NOx emission and pressure fluctuation was investigated regarding two variable conditions; combustor stages and power output on M501J gas turbine.

발전용 희박예혼합 가스터빈에서 연소모드변환 시기의 연소특성 해석 (Numerical Analysis of Combustion Characteristics during Mode Transfer Period in a Lean Premixed Gas Turbine for Power Generation)

  • 정재화;서석빈;김종진;차동진;안달홍
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.279-282
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    • 2002
  • Recently, gas turbines for power generation adopt multistage DLN(Dry Low NOx) type combustion, where diffusion combustion is applied at low load and, with increase in load, the combustion mode is changed to lean premixed combustion to reduce NOx emissive concentration. However, during the mode changeover from diffusion to premixed flame, unfavorable phenomena, such as flashback, high amplitude combustion oscillations, or thermal damage of combustor parts could frequently occur. In the present study, to apply for the analysis of such unfavorable phenomena, three-dimensional CFD investigations are carried out to compare the detailed flow characteristics and temperature distribution inside the gas turbine combustor before and after combustion mode changeover. The fuel considered here is pure methane gas. A standard $k-{\varepsilon}$ turbulence model with wall function and a P-N type radiation heat transfer model, have been utilized. To analyze the complex geometric effects of combustor parts on combustion characteristics, fuel nozzles, a swirl vane f3r fuel-air mixing, and cooling air holes on the combustor liner wall, are included in this simulation.

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GE 7F 가스터빈의 성능개선 결과 분석 (GE 7F Gas Turbine Performance Improvement Results and Analysis)

  • 정재모;심재용;박정규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.2111-2116
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    • 2004
  • This paper shows how to improve the efficiency and output and to reduce NOx emission of Seoinchon GE 7F gas turbine, Korea Western Power Co. by replacing the existing 7F gas turbine with new 7FA+e gas turbine because the performance of 7F gas turbine was degraded due to long term operation. In this paper, we will study gas turbine development trend and O&M technology. Finally, we will review for uprate of Seoinchon 7F gas turbine to help someone to improve their units in the future.

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