Volume 40 Issue 7
Jul.  2025
Turn off MathJax
Article Contents
ZHAO Chang, LIU Yuying, LIU Guanghai, et al. Combustion efficiency prediction model of upstream-injection flame stabilizer in afterburner[J]. Journal of Aerospace Power, 2025, 40(7):20240588 doi: 10.13224/j.cnki.jasp.20240588
Citation: ZHAO Chang, LIU Yuying, LIU Guanghai, et al. Combustion efficiency prediction model of upstream-injection flame stabilizer in afterburner[J]. Journal of Aerospace Power, 2025, 40(7):20240588 doi: 10.13224/j.cnki.jasp.20240588

Combustion efficiency prediction model of upstream-injection flame stabilizer in afterburner

doi: 10.13224/j.cnki.jasp.20240588
  • Received Date: 2024-08-22
    Available Online: 2025-04-03
  • The prediction of combustion efficiency at different downstream locations of the flame stabilizer is an important problem in the length design of afterburner. Taking the upstream-injection U-shaped bluff-body flame stabilizer as the research object, a prediction model of the combustion efficiency downstream the flame holder in the afterburner based on reaction rate controlling was proposed and verified by the combination of numerical simulation and theoretical analysis, under the conditions of incoming flow temperature of 600—900 K, incoming flow velocity of 75—170 m/s and equivalent ratio of 0.22—1.20. At the same time, the prediction model of turbulent flame velocity and the semi-empirical prediction formula of turbulent intensity for afterburner were determined. The results showed that compared with the numerical simulation results, the prediction errors of the model for the combustion efficiency at different downstream locations of the flame stabilizer were less than 2.5% at different incoming temperatures and velocities, and less than 20% at different equivalent ratios.

     

  • loading
  • [1]
    黄勇,林宇震,樊未军,等. 燃烧与燃烧室[M]. 北京: 北京航空航天大学出版社,2009. HUANG Yong,LIN Yuzhen,FAN Weijun,et al. Combustion and combustion chamber[M]. Beijing: Beihang University Press,2009. (in Chinese

    HUANG Yong, LIN Yuzhen, FAN Weijun, et al. Combustion and combustion chamber[M]. Beijing: Beihang University Press, 2009. (in Chinese)
    [2]
    季鹤鸣,刘玉英. 涡扇加力与多功能排气装置[M]. 上海: 上海交通大学出版社,2021. JI Heming,LIU Yuying. Afterburner and multi-function exhaust system of turbofan engine[M]. Shanghai: Shanghai Jiao Tong University Press,2021. (in Chinese

    JI Heming, LIU Yuying. Afterburner and multi-function exhaust system of turbofan engine[M]. Shanghai: Shanghai Jiao Tong University Press, 2021. (in Chinese)
    [3]
    张孝春,孙雨超,刘涛. 先进加力燃烧室设计技术综述[J]. 航空发动机,2014,40(2): 24-30,60. ZHANG Xiaochun,SUN Yuchao,LIU Tao. Summary of advanced afterburner design technology[J]. Aeroengine,2014,40(2): 24-30,60. (in Chinese

    ZHANG Xiaochun, SUN Yuchao, LIU Tao. Summary of advanced afterburner design technology[J]. Aeroengine, 2014, 40(2): 24-30, 60. (in Chinese)
    [4]
    CROSS C,LUBARSKY E,SHCHERBIK D,et al. Determination of equivalence ratio and oscillatory heat release distributions in non-premixed bluff body-stabilized flames using chemiluminescence imaging[R]. ASME Paper GT2011-45,2011.
    [5]
    KING C R. A semiempirical correlation of afterburner combustion efficiency and lean-blowout fuel-air-ratio data with several afterburner-inlet variables and afterburner lengths[R]. NACA-RM-E57F26,1957.
    [6]
    MA Zhuang,JI Tingwei,CUI Tao,et al. Access to empirical formulations of combustion efficiency for gas turbine combustors with improved generalization ability[J]. Journal of Thermal Science and Engineering Applications,2021,13(2): 021001.
    [7]
    LEFEBVRE A H. Theoretical aspects of gas turbine combustion performance[R]. Cranfield,US:College of Aeronautics Note Aero R33088,1966.
    [8]
    LEFEBVRE A H. Fuel effects on gas turbine combustion: ignition,stability,and combustion efficiency[J]. Journal of Engineering for Gas Turbines and Power,1985,107(1): 24-37. doi: 10.1115/1.3239693
    [9]
    冯玉桦. 射流预冷对蒸发式火焰稳定器燃烧性能的影响[D]. 北京: 北京航空航天大学,2019. FENG Yuhua. Effect of MIPCC on the combustion performance of piloted evaporation flameholder[D]. Beijing: Beihang University,2019. (in Chinese

    FENG Yuhua. Effect of MIPCC on the combustion performance of piloted evaporation flameholder[D]. Beijing: Beihang University, 2019. (in Chinese)
    [10]
    MA Hongan,XIE Maozhao,ZENG Wen,et al. Experimental study on combustion characteristics of Chinese RP-3 kerosene[J]. Chinese Journal of Aeronautics,2016,29(2): 375-385.
    [11]
    FUGGER C A,FORLINES R A,PAXTON B T,et al. Freestream and shear layer effects in bluff-body-stabilized turbulent premixed flames[J]. Combustion and Flame,2024,263: 113378. doi: 10.1016/j.combustflame.2024.113378
    [12]
    OATES G C. Aerothermodynamics of aircraft engine components[M]. New York: AIAA,1985.
    [13]
    YOU Jiaping,YANG Yue. Modelling of the turbulent burning velocity based on Lagrangian statistics of propagating surfaces[J]. Journal of Fluid Mechanics,2020,887: A11.
    [14]
    杨茂林,黄勇,顾善建,等. 燃油分布对V形稳定器后燃烧的影响[J]. 航空动力学报,1996,11(1): 48-52. YANG Maolin,HUANG Yong,GU Shanjian,et al. Influence of fuel distribution on combustion behined a V-gutter flameholder[J]. Journal of Aerospace Power,1996,11(1): 48-52. (in Chinese

    YANG Maolin, HUANG Yong, GU Shanjian, et al. Influence of fuel distribution on combustion behined a V-gutter flameholder[J]. Journal of Aerospace Power, 1996, 11(1): 48-52. (in Chinese)
    [15]
    LU Zhen,YANG Yue. Modeling of the turbulent burning velocity for planar and Bunsen flames over a wide range of conditions[J]. Acta Mechanica Sinica,2022,38(3): 121504. doi: 10.1007/s10409-021-09027-3
    [16]
    GÜLDER Ö L. Turbulent premixed flame propagation models for different combustion regimes[J]. Symposium (International) on Combustion,1991,23(1): 743-750.
    [17]
    ZIMONT V L. Theory of turbulent combustion of a homogeneous fuel mixture at high Reynolds numbers[J]. Combustion,Explosion and Shock Waves,1979,15(3): 305-311.
    [18]
    CLAVIN P,WILLIAMS F A. Effects of molecular diffusion and of thermal expansion on the structure and dynamics of premixed flames in turbulent flows of large scale and low intensity[J]. Journal of Fluid Mechanics,1982,116: 251-282.
    [19]
    PETERS N. The turbulent burning velocity for large-scale and small-scale turbulence[J]. Journal of Fluid Mechanics,1999,384(1): 107-132.
    [20]
    Fluent Incorporation. ANSYS Fluent user’s guide[EB/OL]. (2020-12-01)[2024-12-18]. https://ansyshelp.ansys.com/public/account/secured?returnurl=/Views/Secured/corp/v242/en/flu_ug/flu_ug.html.
    [21]
    刘广海,刘玉英,谢奕. 凹腔对一体化支板火焰稳定器燃烧性能的影响[J]. 航空动力学报,2018,33(8): 1838-1844. LIU Guanghai,LIU Yuying,XIE Yi. Effect of cavity on combustion characteristics of integrated strut flame stabilizer[J]. Journal of Aerospace Power,2018,33(8): 1838-1844. (in Chinese

    LIU Guanghai, LIU Yuying, XIE Yi. Effect of cavity on combustion characteristics of integrated strut flame stabilizer[J]. Journal of Aerospace Power, 2018, 33(8): 1838-1844. (in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (491) PDF downloads(49) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return