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
  • [21] EFFECTS OF INJECTOR GEOMETRY ON SCRAMJET COMBUSTOR PERFORMANCE
    CHINZEI, N
    KOMURO, T
    KUDOU, K
    MURAKAMI, A
    TANI, K
    MASUYA, G
    WAKAMATSU, Y
    [J]. JOURNAL OF PROPULSION AND POWER, 1993, 9 (01) : 146 - 152
  • [22] Nonlinear response of a premixed low-swirl flame to acoustic excitation with large amplitude
    Liu, Weijie
    Xue, Ranran
    Zhang, Liang
    Yang, Qian
    Wang, Huiru
    [J]. COMBUSTION AND FLAME, 2022, 235
  • [23] Effects of Flame Behaviors on Combustion Noise from Lean-Premixed Hydrogen Low-Swirl Flames
    Shoji, Takeshi
    Iwasaki, Yuki
    Kodai, Kato
    Yoshida, Seiji
    Tachibana, Shigeru
    Yokomori, Takeshi
    [J]. AIAA JOURNAL, 2020, 58 (10) : 4505 - 4521
  • [24] Prediction of blowoff in a fully controllable low-swirl burner burning alternative fuels: Effects of burner geometry, swirl, and fuel composition
    Ballachey, Graham E.
    Johnson, Matthew R.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2013, 34 : 3193 - 3201
  • [25] INFLUENCE OF COMBUSTOR GEOMETRY ON SWIRL STABILIZED PREMIXED METHANE-AIR FLAME
    Tong, Yiheng
    Li, Mao
    Klingmann, Jens
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 4B, 2016,
  • [26] Experimental Investigation on Nonlinear Response of a Low-Swirl Flame to Acoustic Excitation With Large Amplitude
    Liu, Weijie
    Zhang, Liang
    Xue, Ranran
    Yang, Qian
    Wang, Huiru
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2021, 143 (12):
  • [27] LARGE EDDY SIMULATION OF COMBUSTION INSTABILITY OF LOW-SWIRL FLAMES IN A MULTI-NOZZLE COMBUSTOR
    Liu, Weijie
    Ge, Bing
    Zang, Shusheng
    Li, Mingjia
    Xu, Wenyan
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 4B, 2017,
  • [28] Experimental Study on Instability Characteristics of Low-Swirl Flames in a Multinozzle Combustor With Different Swirling Arrays
    Liu, Weijie
    Ge, Bing
    Tian, Yinshen
    Zang, Shusheng
    Weng, Shilie
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2017, 139 (06):
  • [29] EXPERIMENTAL INVESTIGATION ON NONLINEAR RESPONSE OF A LOW-SWIRL FLAME TO ACOUSTIC EXCITATION WITH LARGE AMPLITUDE
    Liu, Weijie
    Zhang, Liang
    Xue, Ranran
    Yang, Qian
    Wang, Huiru
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 3B, 2021,
  • [30] Combined effect of spatial and temporal variations of equivalence ratio on combustion instability in a low-swirl combustor
    Tachibana, Shigeru
    Kanai, Kota
    Yoshida, Seiji
    Suzuki, Kazuo
    Sato, Tetsuya
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2015, 35 : 3299 - 3308