留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

数值研究低热值燃料环管燃烧室燃烧流场

何敏 蔡文祥 赵坚行 吉洪湖

何敏, 蔡文祥, 赵坚行, 吉洪湖. 数值研究低热值燃料环管燃烧室燃烧流场[J]. 航空动力学报, 2013, 28(2): 324-330.
引用本文: 何敏, 蔡文祥, 赵坚行, 吉洪湖. 数值研究低热值燃料环管燃烧室燃烧流场[J]. 航空动力学报, 2013, 28(2): 324-330.
HE Min, CAI Wen-xiang, ZHAO Jian-xing, JI Hong-hu. Numerical investigation of combustion flow fields in low heating value fuel cannular combustor[J]. Journal of Aerospace Power, 2013, 28(2): 324-330.
Citation: HE Min, CAI Wen-xiang, ZHAO Jian-xing, JI Hong-hu. Numerical investigation of combustion flow fields in low heating value fuel cannular combustor[J]. Journal of Aerospace Power, 2013, 28(2): 324-330.

数值研究低热值燃料环管燃烧室燃烧流场

基金项目: 南京理工大学自主科研专项计划(2011YBXM48,2011YBXM44)

Numerical investigation of combustion flow fields in low heating value fuel cannular combustor

  • 摘要: 在任意曲线坐标系下对采用两种不同组分(天然气掺混氮气、一氧化碳)的低热值燃料环管燃烧室燃烧流场进行计算,结果表明低热值燃料的化学反应速率与其组分直接有关,燃料一氧化碳的燃烧效率高于天然气与氮气掺混物燃料,燃料组分变化对燃烧室燃烧效率与出口温度影响很大,因此选用合适的燃料十分重要.计算所得的燃烧室的燃烧效率和出口温度分布与试验数据符合较好,表明所用的数学模型与计算方法合理,计算程序可靠,可为低热值气体燃料燃烧室研制和优化设计提供有用的数据.

     

  • [1] Hung W S Y,Meier J G.Gaseous fuels capability of industrial gas turbines[R].ASME Paper 85-IGT-129,1985.
    [2] Meier J G,Hung W S Y,Sood V M.Development and application of industrial gas turbines for medium-Btu gaseous fuels[R].ASME Paper 85-GT-28,1985.
    [3] Larson E D,Marrison C I.Economic scales for first-generation biomass-gasifier/gas turbine combined cycles fueled from energy plantations[J].Journal of Engineering for Gas Turbines and Power,1997,119(2):285-290.
    [4] 王艳杰.超低热值燃料催化燃烧燃气轮机系统特性研究[D].上海:上海交通大学,2007. WANG Yanjie.Characteristics study on super-low value fuel catalytic combustion gas turbine system[D].Shanghai:Shanghai Jiaotong University,2007.(in Chinese)
    [5] 朱世澜.国外中、低热值气体燃料开发及应用于燃气轮机的概况[J].燃气轮机技术,1991,4(2):16-22. ZHU Shilan.Overview of abroad low calorific value gas fuel developed and applied to the gas turbine[J].Gas Turbine Technology,1991,4(2):16-22.(in Chinese)
    [6] 刘文和,杨若仪.低热值煤气燃气轮机联合循环发电在钢铁厂的应用[J].冶金动力,2004(1):21-25. LIU Wenhe,YANG Ruoyi.Application of the combined cycle power plant technology of gas turbine using low caloric value gas in iron and steel plants[J].Metallurgic Power,2004(1):21-25.(in Chinese)
    [7] 王乃井,李茉莉.三菱重工业公司M701F型燃气轮机资料[R].深圳:2004年燃气轮机发电技术会议,2004. WANG Naijing,LI Moli.Information of Mitsubishi Heavy Industries M701F type gas turbine information[R].Shenzhen:2004 Conference of Gas Turbine Power Generation Technology,2004.(in Chinese)
    [8] 徐强,张楹,崔耀欣.西门子V94.3A燃气轮机的技术特点[J].上海电力,2006,19(1):3-8. XU Qiang,ZHANG Ying,CUI Yaoxin.Technical features of Siemens V94.3A gas turbine[J].Shanghai Electric Power,2006,19(1):3-8.(in Chinese)
    [9] 林公舒.ALSTOM公司GT26型燃气轮机资料[R].深圳:燃气轮机发电技术会议,2004. LIN Gongshu.Information of ALSTOM GT26 type gas turbine information[R].Shenzhen:2004 Conference of Gas Turbine Power Generation Technology,2004.(in Chinese)
    [10] 赵坚行,伍艳玲.先进燃烧室涡流杯流场计算[J].工程热物理学报,2000,21(1):110-115. ZHAO Jianxing,WU Yanling.Numerical computation of turbulent flow-field characteristics inside an advanced combustor swirl cup[J].Journal of Engineering Thermophysics,2000,21(1):110-115.(in Chinese)
    [11] Yakhot V,Orszag S A.Renormalization group analysis of turbulence:basic theory[J].J Scientific Computing,1986,1(3):39-51.
    [12] 郭尚群,赵坚行.RNG k-ε 模型数值模拟油雾燃烧流场[J].航空动力学报,2005,20(5):807-811. GUO Shangqun,ZHAO Jianxing.Numerical simulation of three-dimensional spray combustion flow field by RNG k-ε turbulent model[J].Journal of Aerospace Power,2005,20(5):807-811.(in Chinese)
    [13] Magnussen B F.On mathematical modeling of turbulent combustion with special emphasis on soot formation and combustion[R].Pittsburgh:16th Symposium(Interational) on Combustion,1977.
    [14] 胡好生,蔡文祥,赵坚行,等.回流燃烧室燃烧过程的三维数值模拟[J].航空动力学报,2008,23(3):444-449. HU Haosheng,CAI Wenxiang,ZHAO Jianxing,et al.Numerical simulation of three-dimensional combustion flows in annular reversed combustor[J].Journal of Aerospace Power,2008,23(3):444-449.(in Chinese)
    [15] 蔡文祥.环形燃烧室两相燃烧流场与燃烧性能数值研究[D].南京:南京航空航天大学,2007. CAI Wenxiang.Research on numerical simulation of two-phase reacting flow field and combustion performance of annular combustors[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2007.(in Chinese)
  • 加载中
计量
  • 文章访问数:  2242
  • HTML浏览量:  197
  • PDF量:  1465
  • 被引次数: 0
出版历程
  • 收稿日期:  2012-01-16
  • 刊出日期:  2013-02-28

目录

    /

    返回文章
    返回