Preliminary study on lean premixed combustion of ammonia-hydrogen for swirling gas turbine combustors

被引:193
|
作者
Valera-Medina, A. [1 ]
Pugh, D. G. [1 ]
Marsh, P. [1 ]
Bulat, G. [2 ]
Bowen, P. [1 ]
机构
[1] Cardiff Univ, Gas Turbine Res Ctr, Cardiff, S Glam, Wales
[2] Siemens Ind Turbomachinery Ltd, Lincoln, England
关键词
Ammonia combustion; Premixing; Swirling flows; EMISSION CHARACTERISTICS;
D O I
10.1016/j.ijhydene.2017.08.028
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
Hydrogen has been considered one of the most promising materials for energy storage during the last decade with considerable research having been undertaken to demonstrate the use of the molecule in power production systems. However, hydrogen presents drawbacks in terms of global commercialisation and deployment since its distribution is only feasible with significant dedicated infrastructure investment including liquefaction or if it is combined with other gases such as methane. The latter will still produce carbon emissions, whilst the former is not economically viable with current technologies. Therefore, an alternative is to use ammonia as a hydrogen storage vector. Ammonia, a molecule that has been used for more than a century, is a well-known material distributed across the world. Moreover, its properties allow its liquefaction at a relatively low pressure under atmospheric temperature compared to hydrogen, serving as a compound that can be used from fertilising to industrial processes. For power generation, ammonia has demonstrated to have a very slow reaction hence flame speeds, thus one option is to dope the fuel with a more reactive molecule such as hydrogen, which conveniently can be obtained from cracking ammonia. Hence, this paper presents the results of a numerical and experimental campaign where a 50:50 (vol%) ammonia-hydrogen blend was used for lean premixed combustion in a generic swirl combustor used in gas turbine studies. The results show that whilst the mixture can produce a good flame velocity similar to methane with the mixture having near equivalent laminar flame speed characteristics, the high diffusivity of hydrogen under these conditions leads to a narrow operational envelope with the potential for boundary layer flashback. High NO. emissions are produced due to the excess production of OH and O radicals. Recommendations for further studies and future developments are also discussed. (C) 2017 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:24495 / 24503
页数:9
相关论文
共 50 条
  • [21] Flow structure in lean premixed swirling combustion
    Jun, J
    Gore, JR
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2002, 29 : 861 - 867
  • [22] Experimental study of lean premixed prevaporized combustion fluctuations in a gas turbine burner
    Allouis, C.
    Beretta, F.
    Amoresano, A.
    [J]. COMBUSTION SCIENCE AND TECHNOLOGY, 2008, 180 (05) : 900 - 909
  • [23] Flow structure in lean premixed swirling combustion
    Ji, Jun
    Gore, Jay P.
    [J]. Proceedings of the Combustion Institute, 2002, 29 (01) : 861 - 867
  • [24] MODEL BASED ACTIVE COMBUSTION CONTROL CONCEPT FOR REDUCTION OF PULSATIONS AND NOX EMISSIONS IN LEAN PREMIXED GAS TURBINE COMBUSTORS
    Schneider, Ernst
    Staudacher, Stephan
    Schuermans, Bruno
    Ye, Haiwen
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 2, 2008, : 67 - 76
  • [25] Combustion instability mechanism of a lean premixed gas turbine combustor
    Se, S
    [J]. KSME INTERNATIONAL JOURNAL, 2003, 17 (06): : 906 - 913
  • [26] FUEL INTERCHANGEABILITY FOR LEAN PREMIXED COMBUSTION IN GAS TURBINE ENGINES
    Ferguson, Don
    Richard, Geo. A.
    Straub, Doug
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 3, PTS A AND B, 2008, : 973 - 981
  • [27] Combustion instability mechanism of a lean premixed gas turbine combustor
    Seonghyeon Seo
    [J]. KSME International Journal, 2003, 17 (6): : 906 - 913
  • [28] Passive control of combustion instability in lean premixed combustors
    Steele, RC
    Cowell, LH
    Cannon, SM
    Smith, CE
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 412 - 419
  • [29] AN EXPERIMENTAL STUDY ON THE COUPLING OF COMBUSTION INSTABILITY MECHANISMS IN A LEAN PREMIXED GAS TURBINE COMBUSTOR
    Lee, Hyung Ju
    Kim, Kyu Tae
    Lee, Jong Guen
    Quay, Bryan D.
    Santavicca, Domenic A.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 2, 2009, : 749 - 758
  • [30] Lean-limit combustion instabilities of a lean premixed prevaporized gas turbine combustor
    Dhanuka, Sulabh K.
    Temme, Jacob E.
    Driscoll, James F.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2011, 33 : 2961 - 2966