Demonstration of Natural Gas and Hydrogen Cocombustion in an Industrial Gas Turbine

被引:5
|
作者
Laget, Hannes [1 ]
Griebel, Peter [2 ]
Gooren, Luc [3 ]
Hampp, Fabian [2 ]
Jouret, Nicolas [4 ]
Lammel, Oliver [2 ]
机构
[1] ENGIE Laborelec Brussels, B-1630 Linkebeek, Belgium
[2] DLR Stuttgart, D-70569 Stuttgart, Germany
[3] ENGIE Laborelec Brussels, B-1630 Linkebeek, Belgium
[4] Katholieke Univ Leuven, Dept Appl Mech & Energy Convers, B-3001 Leuven, Belgium
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2023年 / 145卷 / 04期
关键词
hydrogen; natural gas; cocombustion; single burner tests; industrial gas turbine; METHANE; ENRICHMENT;
D O I
10.1115/1.4056046
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Hydrogen cofiring in a gas turbine is believed to cover an energy transition pathway with green hydrogen as a driver to lower the carbon footprint of existing thermal power generation or cogeneration plants through the gradual increase of hydrogen injection in the existing natural gas grid. Today there is limited operational experience on cocombustion of hydrogen and natural gas in an existing gas turbine in an industrial environment. The ENGIE owned Siemens SGT-600 (Alstom legacy GT10B) 24MW industrial gas turbine in the port of Antwerp (Belgium) was selected as a demonstrator for cofiring natural gas with hydrogen as it enables ENGIE to perform tests at higher H-2 contents (up to 25vol.%) on a representative turbine with limited hydrogen volume flow (one truck load at a time). Several challenges like increasing risk of flame flashback due to the enhanced turbulent flame speed, avoiding higher NOx emissions due to an increase of local flame temperature, supply and homogeneous mixing of hydrogen with natural gas as well as safety aspects have to be addressed when dealing with hydrogen fuel blends. In order to limit the risks of the industrial gas turbine testing a dual step approach was taken. ENGIE teamed up with the German Aerospace Center (DLR), Institute of Combustion Technology in Stuttgart to perform in a first step scaled-burner tests at gas turbine relevant operating conditions in their high-pressure combustor rig. In these tests the onset of flashback as well as the combustor characteristics with respect to burner wall temperatures, emissions and combustion dynamics were investigated for base load and part load conditions, both for pure natural gas and various natural gas and hydrogen blends. For H-2<30vol.% only minor effects on flame position and flame shape (analyzed based on OH* chemiluminescence images) and NOx emission were found. For higher hydrogen contents the flame position moved upstream and a more compact shape was observed. For the investigated H-2 contents no flashback event was observed. However, thermo acoustics are strongly affected by hydrogen addition. In general, the scaled-burner tests were encouraging and enabled the second step, the exploration of hydrogen limits of the second generation dry low emissions burner installed in the engine in Antwerp. To inject the hydrogen into the industrial gas turbine, a hydrogen supply line was developed and installed next to the gas turbine. All tests were performed on the existing gas turbine hardware without any modification. A test campaign of several operational tests at base and part load with hydrogen variation up to 25vol.% has been successfully performed where the gas composition, emissions, combustion dynamics and operational parameters are actively monitored in order to assess the impact of hydrogen on performance. Moreover, the impact of the hydrogen addition on the flame stability has been further assessed through the combustion tuning. The whole test campaign has been executed while the gas turbine stayed online, with no impact to the industrial steam customer. It has been proved that cofiring of up to 10% could be achieved with no adverse effects on the performance of the machine. Stable operation has been observed up to 25vol.% hydrogen cocombustion, but with trespassing the local emission limits.
引用
收藏
页数:9
相关论文
共 50 条
  • [21] Degradation of gas turbine performance in natural gas service
    Kurz, Rainer
    Brun, Klaus
    JOURNAL OF NATURAL GAS SCIENCE AND ENGINEERING, 2009, 1 (03) : 95 - 102
  • [22] The practice of natural gas fuel booster for gas turbine
    Xin, Qifeng
    CHALLENGES OF POWER ENGINEERING AND ENVIRONMENT, VOLS 1 AND 2, 2007, : 377 - 380
  • [23] Generation of synthesis gas by Partial Oxidation of natural gas in a Gas Turbine
    Cornelissen, R
    Tober, E
    Kok, J
    de Meer, TV
    Energy-Efficient, Cost-Effective and Environmentally-Sustainable Systems and Processes, Vols 1-3, 2004, : 443 - 451
  • [24] Generation of synthesis gas by partial oxidation of natural gas in a gas turbine
    Cornelissen, R.
    Tober, E.
    Kok, J.
    van de Meer, T.
    ENERGY, 2006, 31 (15) : 3199 - 3207
  • [25] Numerical study on effects of hydrogen doping of natural gas on the combustion characteristics in micro gas turbine combustor
    Pan, Weiguo
    Kang, Lianwei
    Chi, Zhiwei
    Wang, Wenhuan
    Tang, Congwei
    APPLIED THERMAL ENGINEERING, 2024, 255
  • [26] INDUSTRIAL GAS TURBINE FUEL CONTROLS
    ANDREONI, L
    SAE TRANSACTIONS, 1966, 74 : 126 - &
  • [27] AERODYNAMIC REDESIGNING OF AN INDUSTRIAL GAS TURBINE
    Rubechini, Filippo
    Schneider, Andrea
    Arnone, Andrea
    Dacca, Federico
    Canelli, Claudio
    Garibaldi, Pietro
    PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 7, PTS A-C, 2012, : 1387 - +
  • [28] INDUSTRIAL GAS TURBINE FUEL CONTROLS
    ANDREONI, L
    NEWBURGH, FW
    INGOLD, B
    SAE PROGRESS IN TECHNOLOGY, 1965, 9 : 70 - &
  • [29] THE LIGHTWEIGHT INDUSTRIAL GAS-TURBINE
    ROBERTS, JA
    ENERGIA ES ATOMTECHNIKA, 1985, 38 (01): : 42 - 47
  • [30] Forced Oscillation Characteristics of Natural Gas Mixed with Hydrogen Combustion in Gas Turbine Central Staged Burner
    Shi T.
    Jin M.
    Ge B.
    Zang S.
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2024, 58 (03): : 304 - 311