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相对旋向对纯氢双旋流燃烧动态特性的影响

谷午,  薛然然,  郑洪涛,  刘潇

谷午, 薛然然, 郑洪涛, 等. 相对旋向对纯氢双旋流燃烧动态特性的影响[J]. 航空动力学报, 2026, 42(X):20260295 doi: 10.13224/j.cnki.jasp.20260295
引用本文: 谷午, 薛然然, 郑洪涛, 等. 相对旋向对纯氢双旋流燃烧动态特性的影响[J]. 航空动力学报, 2026, 42(X):20260295 doi: 10.13224/j.cnki.jasp.20260295
Gu Wu, Xue Ranran, Zheng Hongtao, et al. Effects of relative swirl direction on combustion dynamics of a pure-hydrogen dual-swirl combustor[J]. Journal of Aerospace Power, 2026, 42(X):20260295 doi: 10.13224/j.cnki.jasp.20260295
Citation: Gu Wu, Xue Ranran, Zheng Hongtao, et al. Effects of relative swirl direction on combustion dynamics of a pure-hydrogen dual-swirl combustor[J]. Journal of Aerospace Power, 2026, 42(X):20260295 doi: 10.13224/j.cnki.jasp.20260295

相对旋向对纯氢双旋流燃烧动态特性的影响

doi: 10.13224/j.cnki.jasp.20260295
基金项目: 国家自然科学基金(52576109); 哈尔滨市制造业科技创新人才项目(2023CXRCCG005)
详细信息
    作者简介:

    谷午(1996-),男,博士生,主要从事氢气湍流燃烧及燃烧不稳定性研究。E-mail:13889330948@163.com

    通讯作者:

    刘潇(1988-),男,副教授,博士,主要从事燃气轮机低排放燃烧与燃烧不稳定性研究。E-mail:liuxiao_heu@163.com

  • 中图分类号: V231.2

Effects of relative swirl direction on combustion dynamics of a pure-hydrogen dual-swirl combustor

  • 摘要:

    为明确相对旋向对纯氢双旋流燃烧动态特性的影响,在喷孔、流道尺寸和名义旋流数幅值相同条件下,对反向旋流(CR)与同向旋流(CO)开展常压试验。空气体积流量为2.20、3.30、4.40×10−3 m3/s,当量比为0.05~1.00,共120个工况。采用动态压力与高速OH*化学发光测量,分析压力幅频特征和火焰投影。结果表明:两构型的压力脉动随当量比非单调变化。CR高响应窗口较窄,最大压力均方根为0.28 kPa;CO在中高流量下形成较宽高响应区,最大值为0.55 kPa。在最大空气流量且当量比0.80~1.00时,CO为CR的2.6~3.0倍。主频为0.70~1.14 kHz;CO在中高流量及较高当量比下呈连续窄带谱脊,CR低流量强响应的宽带与多频特征更明显。投影面积在当量比0.20~0.50时快速增至(2.5~2.8)×103 mm2后趋于饱和。CR较早形成高窄包络,CO在较宽范围保持低宽杯形结构。相对旋向改变了压力响应窗口、频谱组织与火焰投影形态。

     

  • 图 1  常压受限纯氢燃烧试验系统示意图(单位:mm)

    Figure 1.  Schematic of the atmospheric confined pure-hydrogen combustion facility (unit:mm)

    图 2  纯氢同轴双旋流燃烧器结构及CR、CO构型

    Figure 2.  Pure-hydrogen coaxial dual-swirl combustor and CR/CO configurations

    图 4  CR与CO构型主导压力频率随当量比的变化

    Figure 4.  Dominant pressure frequency versus equivalence ratio for the CR and CO configurations

    图 6  CR与CO构型时间平均OH*化学发光投影(每组上行为CR、下行为CO;当量比由0.10增至1.00,间隔0.10;色标为各工况图像独立归一化的OH*发光强度IOH*/Imax)

    Figure 6.  Time-averaged OH* chemiluminescence projections for the CR and CO configurations (CR in the upper row and CO in the lower row of each group; equivalence ratio from 0.10 to 1.00 at an interval of 0.10; the color bar denotes OH* intensity independently normalized within each condition, IOH*/Imax)

    图 3  不同空气体积流量下CR与CO构型压力脉动方均根值随当量比的变化

    Figure 3.  Pressure-fluctuation RMS versus equivalence ratio for the CR and CO configurations

    图 5  CR与CO构型压力功率谱密度随当量比的演化

    Figure 5.  Evolution of pressure power spectral density with equivalence ratio

    图 7  CR与CO构型OH*发光投影面积随当量比的变化

    Figure 7.  Projected OH*-emitting area versus equivalence ratio for the CR and CO configurations

    表  1  CR与CO双旋流燃烧器主要对比参数

    Table  1.   Main comparative parameters of the CR and CO dual-swirl combustors

    参数 反向旋流(CR) 同向旋流(CO)
    燃料喷孔 28×ϕ0.6 mm:1个轴向孔、12个倾斜孔、15个径向孔 与CR相同
    内旋流器 8个叶片,名义几何旋流数0.47 与CR相同
    外旋流器 24个叶片,名义几何旋流数幅值0.90 标量尺寸与CR相同,叶片手性镜像
    相对旋向 内、外旋流方向相反 内、外旋流方向相同
    出口 直径为22.6397 mm,面积为402.56 mm2 与CR相同
    下载: 导出CSV

    表  2  试验工况与采集参数

    Table  2.   Experimental conditions and acquisition parameters

    参数/单位 数值
    环境压力pa/kPa 102~103
    环境与入口温度T/K 300
    空气体积流量qV,a/10−3 (m3/s) 2.20,3.30,4.40
    全局当量比φ 0.05~1.00,增量0.05
    压力采样频率fs/kHz 20
    压力采集时长t/s 10
    高速相机采样频率fcam/kHz 10
    曝光时间texp/μs 89
    每个工况图像数Nimg 5000
    下载: 导出CSV
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  • 收稿日期:  2026-08-14
  • 网络出版日期:  2026-10-19

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