Numerical simulation of influence of equivalence ratio on turbine inter-vane burner

被引:0
|
作者
Li, Ming [1 ]
Tang, Hao [1 ]
Mo, Da [1 ]
Zhang, Chao [1 ]
机构
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
关键词
Combustion efficiencies - Equivalence ratios - Gas-liquid two phase combustion - K-epsilon turbulent model - PDF combustion model - Radial temperature profile - Turbine inter-vane burners - Ultra-compact combustions;
D O I
暂无
中图分类号
学科分类号
摘要
To investigate the performance of turbine inter-vane burner(TIB), 4 loading conditions with different equivalence ratios were designed. The realizable k-Ε turbulent model, PDF combustion model, DO radiation model and DPM model of FLUENT were used to simulate the turbulent flow and combustion in the burner. The TIB can increase the gas temperature by about 650, K under a wide range of equivalence ratio(2.59-0.81). The combustion efficiency remains above 96% with the total pressure loss less than 2.4%. As the equivalence ratio gets lower, the combustion efficiency is increased and the pollutant emissions of CO, UHC and NOx are decreased, thus improving the temperature distribution, but meanwhile increasing the total pressure loss. The optimal equivalence ratio equals 1.00, and in such a case, the combustion efficiency is above 99.95% and the total pressure loss is relatively low(1.5%). Meanwhile, a parabolic shape radial temperature profile emerges, which is appropriate for gas turbine engine design. The comparison with literature data shows that the loading conditions are reasonable and the numerical results provide an important reference to the design of TIB.
引用
收藏
页码:161 / 168
相关论文
共 50 条
  • [1] Numerical investigation of influence of radial vane cavity on turbine inter-vane burner performance
    Tang, Hao, 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
  • [2] Study of design methods and heat transfer characteristics of combined cooling structure for turbine blades with turbine inter-vane burner
    Cheng, Zeyuan
    Zhang, Heng
    Qing, Liming
    Zhu, Jianqin
    APPLIED THERMAL ENGINEERING, 2024, 254
  • [3] Investigation on turbine inter-vane combustion performance based on fuel cooled vane
    Qing L.
    Zhu J.
    Cheng Z.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2024, 39 (06):
  • [4] Research of Flame Stabilization and Mixing Mechanisms for Turbine Inter-vane Burner Based on Jet-vortex Flow
    Zheng, Haifei
    Tang, Hao
    Xu, Xingya
    Li, Ming
    Liu, Yinli
    12TH INTERNATIONAL CONFERENCE ON COMBUSTION & ENERGY UTILISATION, 2015, 66 : 113 - 116
  • [5] Overall performance and combustion organization based on turbine inter-vane burning technology
    Tang, H. (hao.tang@nuaa.edu.cn), 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
  • [6] PREDICTION OF INTER-TURBINE BURNER (ITB) PERFORMANCE WITH CURVED RADIAL VANE CAVITY AT VARIOUS EQUIVALENCE RATIOS
    Thornburg, Hugh J.
    Sekar, Balu
    Zelina, Joseph
    Lin, Charlie
    Holder, Richard
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 2131 - 2139
  • [7] Numerical Simulation Of Burner For Micro Gas Turbine
    Jia Lei
    Liu Shi
    Huang Yaosong
    Wang Neng
    Wang Fuzhen
    Li Zhihong
    ADVANCED MATERIALS DESIGN AND MECHANICS, 2012, 569 : 51 - 55
  • [8] Numerical Simulation of Inter-Turbine Burner (ITB) Flows with the Inclusion of V-Gutter Flame Holders
    Lin, Cheng-Xian
    Sekar, Balu
    Zelina, Joseph
    Holder, Richard Jack
    Thornburg, Hugh
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 2243 - 2255
  • [9] Effect of curved radial vane cavity arrangements on predicted inter-turbine burner (ITB) performance
    Thornburg, Hugh
    Sekar, Balu
    Zelina, Joseph
    Greenwood, Roger
    PROCEEDINGS OF THE HPCMP USERS GROUP CONFERENCE 2007, 2007, : 110 - +
  • [10] Numerical simulation study on influence of blockage ratio on wake characteristics of tidal turbine
    Li Y.
    Zhang Y.
    Zheng Y.
    Zhang Z.
    Guo H.
    Zhan Y.
    Taiyangneng Xuebao/Acta Energiae Solaris Sinica, 2022, 43 (06): : 256 - 263