Hydrogen injection as additional fuel in gas turbine combustor. Evaluation of effects

被引:69
|
作者
Juste, G. L. [1 ]
机构
[1] Univ Politecn Madrid, Lab Prop, Escuela Tecn Super Ingn Aeronaut, E-28040 Madrid, Spain
关键词
gas turbine; hydrogen combustion emissions;
D O I
10.1016/j.ijhydene.2006.02.006
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Industrial gas turbines fuelled by fossil fuels have been used widely in power generation and combined heat and power for many years. However they have to meet severe NOx CO and CO2 (greenhouse effect) emissions legislation in many countries. This paper reports a study on injection of small quantities of hydrogen in a hydrocarbon fuelled burner like additionally fuel to reduce the pollutants emissions. Hydrogen is injected in the primary zone, premixed with the air. Using this injection together lean primary zone, it is possible to reduce the NOx level while CO an HC levels remains approximately constant. The influence of hydrogen injection on CO, HC and CO2 emissions is mainly due to factors such as hydrocarbon fuel substitution and chemical kinetics. (c) 2006 International Association for Hydrogen Energy. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:2112 / 2121
页数:10
相关论文
共 50 条
  • [41] COMBUSTION CHARACTERISTICS AND HYDROGEN ADDITION EFFECTS ON THE PERFORMANCE OF A CAN COMBUSTOR FOR A MICRO GAS TURBINE
    Shih, Hsin-Yi
    Liu, Chi-Rong
    PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 5, 2010, : 271 - 280
  • [42] The effects and characteristics of hydrogen in SNG on gas turbine combustion using a diffusion type combustor
    Park, Seik
    Kim, Uisik
    Lee, Minchul
    Kim, Sungchul
    Cha, Dongjin
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2013, 38 (29) : 12847 - 12855
  • [43] Design and development test of a gas turbine combustor for high hydrogen medium heating value syngas fuel
    Xu, Gang
    Cui, Yufeng
    Yu, Bin
    Lei, Yu
    Nie, Chaoqun
    Xiao, Yunhan
    Huang, Weiguang
    Proceedings of the ASME Turbo Expo 2005, Vol 2, 2005, : 415 - 425
  • [44] 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
  • [45] LAMINAR BURNING VELOCITY AND BLOW-OFF LIMITS OF A HIGH PRESSURE (55 ATM) GAS TURBINE COMBUSTOR.
    Tamaru, Taku
    Shimodaira, Kazuo
    Kurosawa, Yoji
    Kuyama, Toshiyuki
    Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 1986, 52 (474): : 981 - 984
  • [46] Numerical simulation of angular injection of hydrogen fuel in scramjet combustor
    Murty, M. S. R. Chandra
    Chakraborty, D.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2012, 226 (G7) : 861 - 872
  • [47] Fifty years of gas turbine fuel injection
    Lefebvre, A
    ATOMIZATION AND SPRAYS, 2000, 10 (3-5) : 251 - 276
  • [48] INFLUENCE OF FUEL INJECTION LOCATION IN A SMALL RADIAL SWIRLER LOW NOX COMBUSTOR FOR MICRO GAS TURBINE APPLICATIONS
    Andrews, Gordon E.
    Kim, Su
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 4A, 2019,
  • [49] Fifty years of gas turbine fuel injection
    Lefebvre, Arthur
    Atomization and Sprays: Journal of the International Institutions for Liquid Atomization and Spray Systems, 2000, 10 (3-5): : 251 - 276
  • [50] COMBUSTION PERFORMANCE OF HYDROGEN IN A SMALL GAS-TURBINE COMBUSTOR
    SAMPATH, P
    SHUM, F
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 1985, 10 (12) : 829 - 837