EFFECTS OF COMBUSTOR GEOMETRY ON THE FLOWFIELDS AND FLAME PROPERTIES OF A LOW-SWIRL INJECTOR

被引:0
|
作者
Cheng, R. K. [1 ]
Littlejohn, D. [1 ]
机构
[1] Univ Calif Berkeley, Lawrence Berkeley Lab, Environm Energy Technol Div, Berkeley, CA 94720 USA
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Low-swirl injector (LSI) is a novel dry-low NOx combustion method that is being developed for gas turbines to burn a variety of gaseous fuels including natural gas, low-Btu fuels, syngases and hydrogen. Its basic principle is described by a top level analytical model that relates the flame position to the flowfield similarity parameters and the turbulent flame speed correlation. The model was based on experimental measurements in open laboratory flames. It has been useful for guiding hardware development. As the LSI is being adapted to different engine configurations, one open question is how the combustor geometry and size affect its basic operating principle. The objective of this paper is to investigate these effects by conducting Particle Image Velocimetry (PIV) measurements in open and enclosed flames produced by a 6.35 cm diameter LSI using two quartz cylinders of 15.5 and 20 cm diameter to simulate the combustor casing. Results from 18 methane-air flames show that the enclosures do not alter the flame properties or the nearfield flow structures. The differences occur mostly in the farfield where the tighter enclosure deters the formation of a weak recirculation zone. The enclosure effects on hydrogen and hydrogen-methane flames were studies using the 20 cm cylinder. The results show that the outer recirculation zone generated at the corner of the dump plane promotes the formation of attached flames. However, the properties and nearfield flow features of the attached flames are similar to those of the lifted flames. At higher stoichiometries, the attached flame collapses to form a compact disc shaped flame that has very different flowfield structures. These results show that the enclosure effects on the LSI are strongly coupled to the fuel type and dump plane geometry but are less dependent on the enclosure size. These observations will provide the basis for developing computational methods that can be used as design tools for LSI adaptation.
引用
收藏
页码:393 / 407
页数:15
相关论文
共 50 条
  • [1] PARAMETRIC STUDY OF LOW-SWIRL INJECTOR GEOMETRY ON ITS OPERABILITY
    Therkelsen, Peter L.
    Littlejohn, David
    Cheng, Robert K.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 2, PTS A AND B, 2012, : 309 - 318
  • [2] Combustion dynamics of a low-swirl combustor
    Kang, D. M.
    Culick, F. E. C.
    Ratner, A.
    [J]. COMBUSTION AND FLAME, 2007, 151 (03) : 412 - 425
  • [3] Fuel effects on a low-swirl injector for lean premixed gas turbines
    Littlejohn, D.
    Cheng, R. K.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2007, 31 : 3155 - 3162
  • [4] Effect of fuel reactivity on flame properties of a low-swirl burner
    Akhtar, Muhammad Saqib
    Shahsavari, Mohammad
    Ghosh, Anupam
    Wang, Bing
    Hussain, Zahid
    Rao, Zhuming
    [J]. EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2023, 142
  • [5] Effects of hydrogen on the thermo-acoustics coupling mechanisms of low-swirl injector flames in a model gas turbine combustor
    Davis, D. W.
    Therkelsen, P. L.
    Littlejohn, D.
    Cheng, R. K.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2013, 34 : 3135 - 3143
  • [6] Reacting Flow Prediction of the Low-Swirl Lifted Flame in an Aeronautical Combustor With Angular Air Supply
    Hoffmann, Sven
    Koch, Rainer
    Bauer, Hans-Joerg
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2024, 146 (03):
  • [7] REACTING FLOW PREDICTION OF THE LOW-SWIRL LIFTED FLAME IN AN AERONAUTICAL COMBUSTOR WITH ANGULAR AIR SUPPLY
    Hoffmann, Sven
    Koch, Rainer
    Bauer, Hans-Jorg
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 3B, 2023,
  • [8] Hysteretic Dynamics of Flashback in a Low-Swirl Stabilized Combustor
    Szasz, R.
    Subash, A. A.
    Lantz, A.
    Collin, R.
    Fuchs, L.
    Gutmark, E.
    [J]. COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 189 (02) : 266 - 289
  • [9] Flame stability limits of premixed low-swirl combustion
    Xiao, Yinli
    Cao, Zhibo
    Wang, Changwu
    [J]. ADVANCES IN MECHANICAL ENGINEERING, 2018, 10 (09):
  • [10] Setup for microwave stimulation of a turbulent low-swirl flame
    Ehn, Andreas
    Hurtig, Tomas
    Petersson, Per
    Zhu, Jiajian
    Larsson, Anders
    Fureby, Christer
    Larfeldt, Jenny
    Li, Zhongshan
    Alden, Marcus
    [J]. JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2016, 49 (18)