Active control of fuel splits in gas turbine DLE combustion systems

被引:0
|
作者
Bulat, Ghenadie [1 ]
Skipper, Dorian [1 ]
McMillan, Robin [1 ]
Syed, Khawar [1 ]
机构
[1] Siemens Ind Turbomachinery Ltd, Lincoln LN5 7FD, England
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents a system for the active control of the fuel split within a two-stream Dry Low Emissions (DLE) gas turbine. The system adjusts the fuel split based upon the amplitude of combustor pressure fluctuations and burner metal temperature. The active control system, its implementation and its performance during engine tests on Siemens SGT-200 is described. The paper describes the active fuel split control algorithm. Engine test results are then presented for steady and transient loads with different rates of change of the engine operation temperature, including rapid load acceptance and load shedding. Additionally, cycling operating conditions were tested to evaluate the performance of the algorithm in typical island mode and mechanical drive applications. The active control algorithm was successful in providing stable and reliable control of the turbine allowing very low emissions levels to be attained without manual intervention. In fact it allows areas to be reached that until now were excluded. The impact of operational parameter changes (e.g. load change, ambient temperature, fuel composition etc.) on the engine operability proved the active control software's ability to respond seamlessly. In addition, it prevented flameout and/or high pressure fluctuation while keeping burner temperatures within limits. Recorded emissions showed a reduction in NOx was achieved when the fuel split was controlled by the algorithm compared to standard operation. This was a direct result of the algorithm successfully identifying the lean stability limit and operating close to it.
引用
收藏
页码:135 / 144
页数:10
相关论文
共 50 条
  • [31] Measurement of fuel mixing and transport processes in gas turbine combustion
    McDonell, VG
    Samuelsen, GS
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2000, 11 (07) : 870 - 886
  • [32] FUEL INTERCHANGEABILITY FOR LEAN PREMIXED COMBUSTION IN GAS TURBINE ENGINES
    Ferguson, Don
    Richard, Geo. A.
    Straub, Doug
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 3, PTS A AND B, 2008, : 973 - 981
  • [33] Adding hydrogen fuel to the synthesis gas for the possibility of combustion in a turbine
    Marin, G. E.
    Mingaleeva, G. R.
    Novoselova, M. S.
    Akhmetshin, A. R.
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2024, 96 : 378 - 384
  • [34] FUEL SYSTEMS FOR THE AERO-GAS TURBINE
    不详
    NATURE, 1948, 161 (4084) : 196 - 196
  • [35] Gas turbine fuel systems and Data Analytics
    Arshad, Waleed
    Khalid, Usman
    2017 FIFTH INTERNATIONAL CONFERENCE ON AEROSPACE SCIENCE & ENGINEERING (ICASE), 2017,
  • [36] GAS-TURBINE FUELS AND FUEL SYSTEMS
    KIERNAN, JG
    FOSTER, AD
    HARDEN, DT
    POWER ENGINEERING, 1978, 82 (10) : 64 - 67
  • [37] COMBUSTION OSCILLATION IN GAS TURBINE COMBUSTOR FOR FUEL MIXTURE OF HYDROGEN AND NATURAL GAS
    Uemichi, Akane
    Kanetsuki, Ippei
    Kaneko, Shigehiko
    PROCEEDINGS OF THE ASME PRESSURE VESSELS AND PIPING CONFERENCE, 2017, VOL 4, 2017,
  • [38] Influence of Hydrogen in Fuel Gas on the Processes in Gas Turbine Combustion Chambers (Review)
    Bulysova L.A.
    Vasiliev V.D.
    Pugach K.S.
    Power Technology and Engineering, 2023, 57 (04) : 599 - 604
  • [39] Sub-scale demonstration of the active feedback control of gas-turbine combustion instabilities
    Sattinger, SS
    Neumeier, Y
    Nabi, A
    Zinn, BT
    Amos, DJ
    Darling, DD
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2000, 122 (02): : 262 - 268
  • [40] Active and passive control of combustion oscillations in a 260 MW heavy-duty gas turbine
    Hermann, J
    Orthmann, A
    Hoffmann, S
    Berenbrink, P
    OCOS 2000: FROM THERMO-ECONOMICS TO SUSTAINABILITY, PTS 1-4, 2000, : 2089 - 2102