SMALL RADIAL SWIRLER LOW NOx COMBUSTORS FOR MICRO GAS TURBINE APPLICATIONS

被引:0
|
作者
Andrews, Gordon E. [1 ]
Kim, Myeong [1 ]
机构
[1] Univ Leeds, Sch Chem & Proc Engn, Clean Combust Res, Leeds LS2 9JT, W Yorkshire, England
关键词
BURNING VELOCITY;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
There is a growing interest in micro-gas turbines for distributed electric power production. This work examines the scale down of a successful low NOX radial swirler from a combustor of 140mm diameter to one of 76mm diameter, suitable for micro gas turbines in the 30 -100kW electric size range. A 40mm outlet eight bladed radial swirler was investigated for four radial swirld vane depths from 30.5mm to 12.2mm and a constant pressure loss of 2.7% at different reference Mach numbers or residence times: For a 740K inlet temperature and 0.6 equivalence ratio,empty set, these gave combustor thermal loadings at atmospheric pressure from 33 to 62 kW and heat release of 7 14 MW/m(2)bar. The small radial swirlers had lean stable flames with near lean flammability weak extinction. The vane passage single hole fuel injection achieved NOX emissions of 1 - 5ppm at 15% oxygen, 740K air inlet temperature and 1700K primary zone temperature, with <10ppm CO. The 1ppm NOX was for the smallest vane depth and lowest thermal power. The higher NOX for the larger heat release swirler designs were due to the longer flame development and a greater formation of prompt NOX, due to the high UHC for most of the flame development.
引用
收藏
页数:15
相关论文
共 50 条
  • [11] Control of NOx and other emissions in micro gas turbine combustors fuelled with mixtures of methane and ammonia
    Okafor, Ekenechukwu C.
    Somarathne, K. D. Kunkuma A.
    Ratthanan, Rattanasupapornsak
    Hayakawa, Akihiro
    Kudo, Taku
    Kurata, Osamu
    Iki, Norihiko
    Tsujimura, Taku
    Furutani, Hirohide
    Kobayashi, Hideaki
    COMBUSTION AND FLAME, 2020, 211 : 406 - 416
  • [12] CFD Prediction and Design of Low NOx Radial Swirler Systems
    King, Phil T.
    Andrews, Gordon E.
    Kim, Myeong N.
    Pourkashanian, Mohamed
    McIntosh, Andy C.
    PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 2, 2009, : 867 - 876
  • [13] TURBULENT MIXING AND NOX FORMATION IN GAS-TURBINE COMBUSTORS
    VRANOS, A
    COMBUSTION AND FLAME, 1974, 22 (02) : 253 - 258
  • [14] LAMINAR FLAMELET BASED NOX PREDICTIONS FOR GAS TURBINE COMBUSTORS
    Sripathi, Mohan
    Krishnaswami, Sundar
    Danis, Allen M.
    Hsieh, Shih-Yang
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 4B, 2014,
  • [15] CRITICAL REVIEW OF NOX CORRELATIONS FOR GAS-TURBINE COMBUSTORS
    SULLIVAN, DA
    MAS, PA
    MECHANICAL ENGINEERING, 1976, 98 (02) : 80 - 80
  • [16] Multidisciplinary optimization of a radial compressor for micro gas turbine applications
    Verstraete, T.
    Alsalihi, Z.
    Van den Braembussche, R. A.
    Proceedings of the ASME Turbo Expo 2007, Vol 6, Pts A and B, 2007, : 1291 - 1299
  • [17] Numerical simulations on the effect of swirler installation angle on outlet temperature distribution in gas turbine combustors
    Wang, Kefu
    Li, Feng
    Zhou, Tao
    Wang, Dichang
    APPLIED THERMAL ENGINEERING, 2024, 240
  • [18] DEVELOPMENT OF LOW EMISSION GAS TURBINE COMBUSTORS
    Jung, Seung-chai
    Yang, Siwon
    Kim, Shaun
    Kim, Ik Soo
    Ahn, Chul-ju
    Cho, Ju Hyeong
    Yoon, Jisu
    Yoon, Youngbin
    Yoon, Samson
    Ryu, Shiyang
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 4A, 2015,
  • [19] MODELING OF CATALYTIC COMBUSTORS FOR GAS-TURBINE APPLICATIONS
    GROPPI, G
    TRONCONI, E
    FORZATTI, P
    CATALYSIS TODAY, 1993, 17 (1-2) : 237 - 249
  • [20] Large eddy simulation and preliminary modeling of the flow downstream a variable geometry swirler for gas turbine combustors
    Eldrainy, Yehia A.
    Saqr, Khalid M.
    Aly, Hossam S.
    Lazim, Tholudin Mat
    Jaafar, Mohammad Nazri Mohd
    INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2011, 38 (08) : 1104 - 1109