Advanced Search
Volume 41 Issue 6
Jun.  2015
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(6): 1117-1121.
LIU Guigui, LIN Yuzhen, HU Haosheng, et al. Effect of swirl cup's primary swirl number on ignition performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(6): 1117-1121. doi: 10.13700/j.bh.1001-5965.2014.0408(in Chinese)
Citation: LIU Guigui, LIN Yuzhen, HU Haosheng, et al. Effect of swirl cup's primary swirl number on ignition performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(6): 1117-1121. doi: 10.13700/j.bh.1001-5965.2014.0408(in Chinese)
shu

Effect of swirl cup's primary swirl number on ignition performance

doi: 10.13700/j.bh.1001-5965.2014.0408
  • 1.

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. AVIC China Aviation Powerplant Research Institute, Zhuzhou 412002, China

  • Received Date: 09 Jul 2014
  • Publish Date: 20 Jun 2015
    Abstract
  • All swirl cups have the same primary inclined multi hole and secondary radial straight blade and a simplex pressure atomizer. The effects of primary swirl number of airblast atomizer on small combustion ignition performance were examined. The ignition experiments for swirl cups with three different primary swirl numbers were conducted under atmospheric pressure and temperature in a rectangular reflux combustion chamber, and the pressure drop across the flame tube was between 0.5% and 5% of inlet total pressure. The experimental results show that the primary swirl number significantly influence the ignition performance. Under the same pressure drop, within a certain range, the increase of primary swirl number affects the downstream flow field distribution, which is beneficial for fire nuclear spreading along the upstream of recirculation region and forming a steady flame in the swirl cup exit. So the swirl cup with strong primary vortex has better ignition performance.

     

    • FullText(HTML)
  • loading
    • References(15)
  • [1]
    方昌德.世界航空发动机手册[M].北京:航空工业出版社, 1996. Fang C D.World aviation engine mannual[M].Beijing:Aviation Industry Press, 1996(in Chinese).
    [2]
    彭云晖, 林宇震, 许全宏, 等.双旋流空气雾化喷嘴喷雾、流动和燃烧性能[J].航空学报, 2008, 29(1):1-14. Peng Y H, Lin Y Z, Xu Q H, et al.Atomization, aerodynamics and combustion performance of swirl cup[J].Acta Aeronautica et Astronautica Sinica, 2008, 29(1):1-14(in Chinese).
    [3]
    林宇震, 许全宏, 刘高恩.燃气轮机燃烧室[M].北京:国防工业出版社, 2008:107. Lin Y Z, Xu Q H, Liu G E.Gas turbine combustor[M].Beijing:National Defence Industry Press, 2008:107(in Chinese).
    [4]
    徐华胜, 黄义勇, 王秀兰.喷嘴供油特性对双旋流器头部气动雾化效果的影响研究[J].燃气涡轮试验与研究, 2004, 17(2):14-17. Xu H S, Huang Y Y, Wang X L.Study on the effect of fuel jet characteristics on airblast atomization performance for device with two-stage swirler[J].Gas Turbine Experiment and Research, 2004, 17(2):14-17(in Chinese).
    [5]
    Hsiao G, Mongia H C, Vij A.Swirl cup modeling part Ⅱ:inlet boundary conditions, AIAA-2003-1350[R].Reston:AIAA, 2003.
    [6]
    Hsiao G, Mongia H C.Swirl cup modeling part Ⅲ:grid independent solution with different turbulence models, AIAA-2003-1349[R].Reston:AIAA, 2003.
    [7]
    Cai J, Fu Y, Elkadi A, et al.Swirl cup modeling part Ⅳ:effect of confinement on flow characteristics, AIAA-2003-0486[R].Reston:AIAA, 2003.
    [8]
    Wang S, Yang V, Mongia H C, et al, Modeling of gas turbine swirl cup dynamics, part Ⅴ:Large eddy simulation of cold flow, AIAA-2003-0485[R].Reston:AIAA, 2003.
    [9]
    Stevens E J, Held T J, Mongia H C.Swirl cup modeling part Ⅷ:spray combustion in CFM-56 single cup flame tube, AIAA-2003-0319[R].Reston:AIAA, 2003.
    [10]
    Wang H Y, McDonell V G, Samuelsen G S.Influence of hardware design on the flow field structures and the patterns of droplet dispersion, Part I:mean quantities[J].Journal of Engineering for Gas Turbines and Power, 1995, 117(2):282-289.
    [11]
    Ateshkadi A, McDonell V G, Samuelsen G S.Effect of hardware geometry on gas and drop behavior in a radial mixer spray[J].Proceedings of the 1998 27th International Symposium on Combustion, 1998, 2:1985-1992.
    [12]
    罗国良, 宋双文, 胡好生, 等.旋流杯空气雾化喷嘴套筒出口形状对小型燃烧室点火性能的影响[J].航空动力学报, 2001, 22(8):1708-1712. Luo G L, Song S W, Hu H S, et al.Influences of the swirl cup flares design on the small combustor ignition performance[J].Journal of Aerospace Power, 2011, 22(8):1708-1712(in Chinese).
    [13]
    康尧, 林宇震, 霍伟业, 等.双级旋流杯结构变化对点火特性的影响研究[J].推进技术, 2014, 35(5):675-679. Kang Y, Lin Y Z, Huo W Y, et al.Effect of hardware geometry of dual-stage swirl cup on ignition performance[J].Journal of Propulsion Technology, 2014, 35(5):675-679(in Chinese).
    [14]
    林宇震, 林培华, 许全宏, 等.复合式收扩套筒空气雾化喷嘴燃烧室点火研究[J].航空动力学报, 2007, 28(3):342-346. Lin Y Z, Lin P H, Xu Q H, et al.Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent sleeve[J].Journal of Aerospace Power, 2007, 28(3):342-346(in Chinese).
    [15]
    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, 2006:264. Huang Y, Lin Y Z, Fan W J, et al.Combustion and Combustors[M].Beijing:Beihang University Press, 2006:264(in Chinese).
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1106) PDF downloads(555) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return