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

中心分级旋流燃烧室不稳定燃烧动态压力信号特征分析

王旭怀 刘勇 张祥 杨晨 李昊

王旭怀, 刘勇, 张祥, 等. 中心分级旋流燃烧室不稳定燃烧动态压力信号特征分析[J]. 航空动力学报, 2023, 38(12):2883-2894 doi: 10.13224/j.cnki.jasp.20220045
引用本文: 王旭怀, 刘勇, 张祥, 等. 中心分级旋流燃烧室不稳定燃烧动态压力信号特征分析[J]. 航空动力学报, 2023, 38(12):2883-2894 doi: 10.13224/j.cnki.jasp.20220045
WANG Xuhuai, LIU Yong, ZHANG Xiang, et al. Characteristic analysis of dynamic pressure signal of unstable combustion in central staged swirl combustor[J]. Journal of Aerospace Power, 2023, 38(12):2883-2894 doi: 10.13224/j.cnki.jasp.20220045
Citation: WANG Xuhuai, LIU Yong, ZHANG Xiang, et al. Characteristic analysis of dynamic pressure signal of unstable combustion in central staged swirl combustor[J]. Journal of Aerospace Power, 2023, 38(12):2883-2894 doi: 10.13224/j.cnki.jasp.20220045

中心分级旋流燃烧室不稳定燃烧动态压力信号特征分析

doi: 10.13224/j.cnki.jasp.20220045
基金项目: 中国航发自主创新专项资金项目(ZZCX-2019-009)
详细信息
    作者简介:

    王旭怀(1998-),男,硕士生,主要研究方向为燃烧室不稳定燃烧

  • 中图分类号: V231;TK16

Characteristic analysis of dynamic pressure signal of unstable combustion in central staged swirl combustor

  • 摘要:

    针对中心分级旋流模型燃烧室中出现的不稳定燃烧特征进行试验研究,在常压试验中同步采集了不同工况下燃烧室动态压力脉动信号、释热率脉动信号和高速火焰图像信号。通过经验模态分解(EMD)对压力脉动信号进行分析,发现脉动特征主要集中在前3阶本征模态(IMF)中。这些IMF通过快速傅里叶变换(FFT)进行主频分析后发现分别与释热率脉动、气流旋流脉动和火焰不稳定脉动特征频谱吻合。进而可以判断通过EMD可以从单一燃烧室压力脉动信号中分解出3个主要物理过程的脉动特征,为进一步分析工程级燃烧室试验中振荡燃烧的诱发机制和燃烧诊断提供了数据处理方法。

     

  • 图 1  试验系统布局示意图

    Figure 1.  Layout diagram of test system

    图 2  旋流器头部结构示意图

    Figure 2.  Structural diagram of swirler head

    图 3  燃烧室压力脉动随油气比调节的变化

    Figure 3.  Variation of combustor pressure pulsation with oil-gas ratio regulation

    图 4  FI状态和CI状态压力信号频谱结果

    Figure 4.  Pressure signal spectrum results of FI state and CI state

    图 5  A组各工况的0~2 s内DP信号

    Figure 5.  DP signal within 0—2 s under each working condition of group A

    图 6  DP信号频谱

    Figure 6.  Spectrum of DP signal

    图 7  油压信号频谱

    Figure 7.  Spectrum of fuel pressure signal

    图 8  不同进口空气质量流量下压力脉动峰值变化

    Figure 8.  Variation of pressure fluctuation peak value under different inlet air mass flows

    图 9  A02 压力脉动各个分量的时频域

    Figure 9.  Time frequency spectrum of each component of A02 pressure pulsation

    图 10  DP各阶分量脉动主频变化

    Figure 10.  Variation of pulsation dominant frequency of DP components

    图 11  DP各阶分量脉动峰值能量占比变化

    Figure 11.  Variation of the proportion of pulsation peak energy of DP components

    图 12  无进气时燃烧室内DP频谱

    Figure 12.  DP spectrum in combustor without inlet air

    图 13  不同进气量下冷态DP频谱

    Figure 13.  Cold state DP spectrum under different air intakes

    图 14  冷态DP次主频随进口空气质量流量变化

    Figure 14.  Variation of secondary dominant frequency of cold DP with inlet mass flow of air

    图 15  不同燃烧状态下CH*信号及频谱

    Figure 15.  CH* signal and spectrum under different combustion conditions

    图 16  IMF1与CH*信号变化

    Figure 16.  Variation of IMF1 and CH* signals

    图 17  CH*脉动频率变化

    Figure 17.  Variation of CH* pulsation frequency

    图 18  火焰变化图像

    Figure 18.  Flame change images

    图 19  火焰长度分析

    Figure 19.  Analysis of flame length

    图 20  A组火焰脱落频率

    Figure 20.  The frequency of flame shedding in group A

    表  1  旋流器结构参数

    Table  1.   Structural parameters of swirler (°)

    位置值班级主级
    一级轴向二级轴向径向
    数值3035−60
    下载: 导出CSV

    表  2  中心分级燃烧室不稳定燃烧试验工况

    Table  2.   Unstable combustion test conditions of central staged combustor

    试验
    编号
    进口空气质量
    流量/(g/s)
    进气
    温度/K
    进口Re油气比
    A01100.2426404000.063
    A02100.2426404000.057
    A03100.2426404000.050
    A04100.2426404000.046
    A05100.2426404000.038
    A06100.2426404000.033
    B01130.1423.4520000.054
    B02130.1423.4520000.052
    B03130.1423.4520000.048
    B04130.1423.4520000.046
    B05130.1423.4520000.044
    B06130.1423.4520000.038
    C01140.0434568000.050
    C02140.0434568000.048
    C03140.0434568000.045
    C04140.0434568000.044
    C05140.0434568000.040
    C06140.0434568000.038
    下载: 导出CSV
  • [1] TIMOTHY C L, VIUOR Y. Combustion instabilities in gas turbine engines[M]. Fort Collins, US: American Institute of Aeronautics and Astronautics. 2005.
    [2] COHEN J, ANDERSON T. Experimental investigation of near-blowout instabilities in a lean, premixed step combustor[R]. AIAA 1996-819, 1996.
    [3] KELLER J J. Thermoacoustic oscillations in combustion chambers of gas turbines[J]. AIAA Journal,1995,33(12): 2280-2287. doi: 10.2514/3.12980
    [4] 张均勇,张宝诚. 航空发动机燃烧室工作稳定性研究[J]. 航空发动机,2001,27(1): 31-39. doi: 10.3969/j.issn.1672-3147.2001.01.007

    ZHANG Junyong,ZHANG Baocheng. Study on working stability of aero-engine combustion chamber[J]. Aeroengine,2001,27(1): 31-39. (in Chinese) doi: 10.3969/j.issn.1672-3147.2001.01.007
    [5] HOBSON D E,FACKRELL J E,HEWITT G. Combustion instabilities in industrial gas turbines: measurements on operating plant and thermoacoustic modeling[J]. Journal of Engineering for Gas Turbines and Power,2000,122(3): 420-428. doi: 10.1115/1.1287238
    [6] HUANG N E,SHEN Zheng,LONG S R,et al. The empirical mode decomposition and the Hilbert spectrum for nonlinear and non-stationary time series analysis[J]. Proceedings of the Royal Society of London Series A: Mathematical, Physical and Engineering Sciences,1998,454(1971): 903-995. doi: 10.1098/rspa.1998.0193
    [7] BI Fengrong,MA Teng,WANG Xu. Development of a novel knock characteristic detection method for gasoline engines based on wavelet-denoising and EMD decomposition[J]. Mechanical Systems and Signal Processing,2019,117: 517-536. doi: 10.1016/j.ymssp.2018.08.008
    [8] BODA S,MAHADEVAPPA M,DUTTA P K. A hybrid method for removal of power line interference and baseline wander in ECG signals using EMD and EWT[J]. Biomedical Signal Processing and Control,2021,67: 102466. doi: 10.1016/j.bspc.2021.102466
    [9] AMOURA S,GACI S,BARBOSA S,et al. Investigation of lithological heterogeneities from velocity logs using EMD-Hölder technique combined with multifractal analysis and unsupervised statistical methods[J]. Journal of Petroleum Science and Engineering,2022,208: 109588. doi: 10.1016/j.petrol.2021.109588
    [10] YAN Shisen,LIANG Qinfeng,GUO Qinghua,et al. Analysis on acoustic characteristics of opposed multi-burner gasifier[J]. Applied Acoustics,2011,72(1): 43-47. doi: 10.1016/j.apacoust.2010.09.008
    [11] 李珊, 闫勇, 吴佳丽, 等. 基于EMD降噪的燃烧器火焰静电信号能量熵分析[J]. 中南大学学报(自然科学版), 2021, 52(1): 285-293.

    LI Shan, YAN Yong, WU Jiali, et al. Energy entropy analysis of flame signals obtained by an electrostatic sensor array based on EMD denoising method[J]. Journal of Central South University (Science and Technology), 2021, 52(1): 285-293. (in Chinese)
    [12] 付宇,郭志辉,杨甫江,等. 基于经验模态分解的燃烧不稳定性分析[J]. 航空动力学报,2016,31(3): 623-630. doi: 10.13224/j.cnki.jasp.2016.03.013

    FU Yu,GUO Zhihui,YANG Fujiang,et al. Analysis on combustion instability based on empirical mode decomposition[J]. Journal of Aerospace Power,2016,31(3): 623-630. (in Chinese) doi: 10.13224/j.cnki.jasp.2016.03.013
    [13] 冀树德,张晖,贾桢. EMD在柴油机燃烧不良诊断中的应用[J]. 现代车用动力,2007(4): 28-31. doi: 10.3969/j.issn.1671-5446.2007.04.007

    JI Shude,ZHANG Hui,JIA Zhen. Application of EMD method in diagnose of bad combustion in diesel engine[J]. Modern Vehicle Power,2007(4): 28-31. (in Chinese) doi: 10.3969/j.issn.1671-5446.2007.04.007
    [14] 郑丹伟,刘勇,张祥. 基于火焰图像诊断的模型燃烧室燃烧不稳定特性[J]. 航空动力学报,2021,36(7): 1481-1488.

    ZHENG Danwei,LIU Yong,ZHANG Xiang. Combustion instability characteristics of model combustor based on flame image diagnosis[J]. Journal of Aerospace Power,2021,36(7): 1481-1488. (in Chinese)
    [15] GIASSI D,CAO Su,BENNETT B A V,et al. Analysis of CH* concentration and flame heat release rate in laminar coflow diffusion flames under microgravity and normal gravity[J]. Combustion and Flame,2016,167: 198-206. doi: 10.1016/j.combustflame.2016.02.012
    [16] 赖安卿,刘云鹏,付尧明,等. 振荡燃烧火焰图像处理[J]. 燃烧科学与技术,2020,26(1): 10-17.

    LAI Anqing,LIU Yunpeng,FU Yaoming,et al. Image processing of combustion oscillating flame[J]. Journal of Combustion Science and Technology,2020,26(1): 10-17. (in Chinese)
    [17] STEINBERG A M,ARNDT C M,MEIER W. Parametric study of vortex structures and their dynamics in swirl-stabilized combustion[J]. Proceedings of the Combustion Institute,2013,34(2): 3117-3125. doi: 10.1016/j.proci.2012.05.015
    [18] DHANUKA S K,TEMME J E,DRISCOLL J F,et al. Vortex-shedding and mixing layer effects on periodic flashback in a lean premixed prevaporized gas turbine combustor[J]. Proceedings of the Combustion Institute,2009,32(2): 2901-2908. doi: 10.1016/j.proci.2008.06.155
  • 加载中
图(20) / 表(2)
计量
  • 文章访问数:  572
  • HTML浏览量:  244
  • PDF量:  79
  • 被引次数: 0
出版历程
  • 收稿日期:  2022-01-25
  • 网络出版日期:  2023-08-24

目录

    /

    返回文章
    返回