Use of bioethanol in a gas turbine combustor

被引:13
|
作者
Alfaro-Ayala, J. A. [1 ]
Gallegos-Munoz, A. [2 ]
Uribe-Ramirez, A. R. [1 ]
Belman-Flores, J. M. [2 ]
机构
[1] Univ Guanajuato, Dept Chem Engn, Guanajuato, Gto, Mexico
[2] Univ Guanajuato, Dept Mech Engn, Guanajuato, Mexico
关键词
Gas turbine; Combustor; Emissions; Bioethanol; LIFE-CYCLE ASSESSMENT; ETHANOL; SUGARCANE;
D O I
10.1016/j.applthermaleng.2013.08.025
中图分类号
O414.1 [热力学];
学科分类号
摘要
A study of a gas turbine combustor that considers two conventional fuels and one biofuel is presented. The kind of fuel supplied to the combustor can impact in the Turbine Inlet Temperature (TIT) provoking significant changes in the power output and efficiency. Moreover, it can cause some damage in the initial steps of the gas turbine due to the migration of the hot streak. Natural gas, Diesel and Bioethanol are considered in the combustor in order to compare the performance of the power plant. The use of biofuel in a gas turbine combustor presents some benefits; a) better behavior in the distribution of the TIT, b) slightly higher power output and c) less impact of NOx and CO2 emissions. The analysis was based in the Computational Fluid Dynamics (CFD) and thermodynamics. The results indicate that it is necessary to increase the mass flow rate of bioethanol to maintain the power output of the turbine, due to a significant reduction of the TIT was observed. On the other hand, the use of bioethanol permits an important reduction of NOx emissions when they are compared with the conventional fuels (natural gas or diesel). Also, a noble benefit is obtained due to the biofuel comes from biomass-derived material, resulting in a reduction of CO2 global warming. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:481 / 490
页数:10
相关论文
共 50 条
  • [31] Energy and exergy balance in a gas turbine combustor
    Datta, A.
    Som, S.K.
    Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 1999, 213 (01): : 23 - 32
  • [32] PERFORMANCE IMPROVEMENT OF AN AERO GAS TURBINE COMBUSTOR
    Rao, M. Srinivasa
    Sivaramakrishna, G.
    PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 2, 2009, : 689 - 694
  • [33] Experimental study of a flameless gas turbine combustor
    Li, Guoqiang
    Gutmark, Ephraim J.
    Overman, Nick
    Cornwell, Michael
    Stankovic, Dragan
    Fuchs, Laszlo
    Vladimir, Milosavljevic
    PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 1, 2006, : 793 - 804
  • [34] PARAMETRIC MODELLING SYSTEM OF GAS TURBINE COMBUSTOR
    Chen, Xi
    Zheng, Hongtao
    Pan, Gang
    Jia, Xiangyu
    TEHNICKI VJESNIK-TECHNICAL GAZETTE, 2014, 21 (06): : 1213 - 1219
  • [35] Combustion driven oscillations in a gas turbine combustor
    Abbott, DJ
    OCOS 2000: FROM THERMO-ECONOMICS TO SUSTAINABILITY, PTS 1-4, 2000, : 2033 - 2047
  • [36] A NEW GAS-TURBINE COMBUSTOR ALLOY
    KLARSTROM, DL
    TAWANCY, HM
    FLUCK, DE
    ROTHMAN, MF
    MECHANICAL ENGINEERING, 1984, 106 (06) : 86 - 86
  • [37] Mathematical modeling of an annular gas turbine combustor
    Sokolov, K.Y.
    Tumanovskiy, A.G.
    Gutnik, M.N.
    Sudarev, A.V.
    Zakharov, Y.I.
    Winogradov, E.D.
    Journal of Engineering for Gas Turbines and Power, 1995, 117 (01) : 94 - 99
  • [38] Robust Gas Turbine Combustor with Acoustic Liner
    Ikeda, Kazufumi
    Matsuyama, Keisuke
    Nishimura, Masaharu
    JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2012, 7 (01): : 199 - 210
  • [39] Parametric modelling system of gas turbine combustor
    Parametarski sustav modeliranja komore izgaranja plinske turbine
    Chen, Xi, 1600, Strojarski Facultet (21): : 1213 - 1219
  • [40] Combination of DOM with LES in a gas turbine combustor
    Jones, WP
    Paul, MC
    INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE, 2005, 43 (5-6) : 379 - 397