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基于静态混合器的预混阵列微管纯氢燃烧研究

昌运鑫 林宇震 谢法 李炳涛 高安雯 任浩祺 刘鑫 徐维 韩啸

昌运鑫, 林宇震, 谢法, 等. 基于静态混合器的预混阵列微管纯氢燃烧研究[J]. 航空动力学报, 2025, 40(10):20240053 doi: 10.13224/j.cnki.jasp.20240053
引用本文: 昌运鑫, 林宇震, 谢法, 等. 基于静态混合器的预混阵列微管纯氢燃烧研究[J]. 航空动力学报, 2025, 40(10):20240053 doi: 10.13224/j.cnki.jasp.20240053
CHANG Yunxin, LIN Yuzhen, XIE Fa, et al. Research on pure hydrogen combustion in premixed array micro-tubes based on static mixer[J]. Journal of Aerospace Power, 2025, 40(10):20240053 doi: 10.13224/j.cnki.jasp.20240053
Citation: CHANG Yunxin, LIN Yuzhen, XIE Fa, et al. Research on pure hydrogen combustion in premixed array micro-tubes based on static mixer[J]. Journal of Aerospace Power, 2025, 40(10):20240053 doi: 10.13224/j.cnki.jasp.20240053

基于静态混合器的预混阵列微管纯氢燃烧研究

doi: 10.13224/j.cnki.jasp.20240053
基金项目: 国家自然科学基金(52106128); 航空发动机及燃气轮机基础科学中心项目(P2022-A-Ⅱ-006-001); 中央高校基本科研业务费专项资金
详细信息
    作者简介:

    昌运鑫(2000-),男,博士生,主要从事氢燃烧与燃烧振荡研究。E-mail:changyunxin@buaa.edu.cn

    通讯作者:

    韩啸(1993-),男,副研究员,博士,主要从事燃烧振荡机理及控制方法、氢燃料低排放燃烧室设计研究。E-mail:han_xiao@buaa.edu.cn

  • 中图分类号: V231.2

Research on pure hydrogen combustion in premixed array micro-tubes based on static mixer

  • 摘要:

    为助力完成“双碳”目标,实现燃气轮机纯氢燃烧达到零碳排放,设计了一种基于静态混合器的预混微管燃烧器,可满足纯氢低排放燃烧需求。在常温常压,23.7、47.3、71.1 m3/h这3种空气体积流量下,对4×4阵列排布的预混微管燃烧器进行了纯氢燃烧实验,当量比为0.25~0.85。获取了时均宏观火焰图像,测量了燃烧排放的NOx,用压力脉动传感器测量腔室内的燃烧振荡特性,探究不同空气体积流量、不同当量比下纯氢燃烧的燃烧特性,并结合Fluent软件对阵列微管中的氢气-空气掺混情况进行分析。结果发现在当量比在0.7以内时,燃烧器各工况NOx排放的体积分数均在20×10−6以内。微混火焰近似纯预混火焰,空气体积流量增大,微管喷孔速度增大,整体长度拉伸,火焰锥角变小。空气体积流量为23.7 m3/h,当量比小于0.55时,可实现氢气稳定燃烧;其他工况,空气体积流量增大,起振点前移;当量比增大,燃烧振荡的振幅先增大后呈现波动下降的趋势。振荡频率普遍在700 Hz以上,且随着当量比增大稳步增大。

     

  • 图 1  氢气微混单管模型示意图(单位:mm)

    Figure 1.  Schematic diagram of hydrogen micro-mixing single tube model (unit:mm)

    图 2  阵列微混燃烧器模型示意图

    Figure 2.  Schematic diagram of the array micro-mixing burner model

    图 3  实验系统示意图

    Figure 3.  Schematic diagram of experimental system

    图 4  流体域网格划分

    Figure 4.  Grid of the fluid domain

    图 5  维管出口的径向速度分布

    Figure 5.  Radial velocity distribution at the micro-tube outlet

    图 6  微管截面均匀性变化

    Figure 6.  Uniformity variation of micro-tube cross-section

    图 7  SK 1方案的纯氢火焰图像

    Figure 7.  Pure hydrogen flame image of SK 1 scheme

    图 8  标尺对比

    Figure 8.  Ruler comparison

    图 9  不同空气体积流量下氢气火焰长度随当量比变化

    Figure 9.  Hydrogen flame length varies with equivalent ratio at different air flow rates

    图 10  不同空气体积流量下NOx排放随当量比的变化

    Figure 10.  Variation of NOx emission with equivalent ratio at different air flow rates

    图 11  不同体积流量下NOx随绝热火焰温度变化

    Figure 11.  Variation of NOx emission with adiabatic flame temperature at different air flow rates

    图 12  NOx排放随绝热火焰温度变化曲线(空气体积流量为23.7 m3/h)

    Figure 12.  NOx emission changes with adiabatic flame temperature (air flow rate is 23.7 m3/h)

    图 13  当量比为0.4~0.55的压力脉动频谱图(空气体积流量为23.7 m3/h)

    Figure 13.  Pressure pulsation spectrum for equivalent ratio of 0.4—0.55 (air flow rate is 23.7 m3/h)

    图 14  当量比为0.4~0.55的极限环(空气体积流量为23.7 m3/h)

    Figure 14.  Limit cycle for equivalent ratio of 0.4—0.55 (air flow rate is 23.7 m3/h)

    图 15  压力脉动振幅随当量比变化

    Figure 15.  Variation of pressure pulsation amplitude with equivalence ratio

    图 16  压力脉动频率随当量比变化

    Figure 16.  Variation of pressure pulsation frequency with equivalent ratio

    图 17  压力脉动频率随绝热火焰温度变化

    Figure 17.  Pressure pulsation frequency changes with adiabatic flame temperature

    表  1  实验工况

    Table  1.   Test conditions

    工况 空气体积流量/(m3/h) 当量比
    1 23.7 0.25~0.85
    2 47.3 0.25~0.85
    3 71.1 0.3~0.85
    下载: 导出CSV

    表  2  预混微管模型结构参数

    Table  2.   Structural parameters of premixed micro-tube model mm

    方案编号 SK叶片螺距 通道长度 通道外径 收口外径 收口内径 氢喷孔直径
    SK 1 27 63.5 11 10 6 1.2
    SK 2 54 123 22 20 12 2.4
    SK 3 27 123 11 10 6 1.2
    下载: 导出CSV

    表  3  微管出口SMD以及NOx排放

    Table  3.   SMD and NOx emissions of micro-tube outlet

    方案 不均匀度/% 当量比为0.45的
    NOx体积分数/10−6
    SK 1 3.50 2.417
    SK 2 4.56 4.922
    SK 3 3.46 2.416
    下载: 导出CSV

    表  4  NOx排放实验值与仿真计算对比(空气体积流量为23.7 m3/h)

    Table  4.   NOx emission test value compared with the simulation calculation (the air flow rate is 23.7 m3/h)

    当量比NOx排放的体积分数/10−6
    实验Chemkin计算
    0.515.4
    0.5539.5
    0.6417.4
    0.65833.6
    0.71665.8
    0.7531126.0
    0.861228.2
    下载: 导出CSV
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  • 收稿日期:  2024-01-23
  • 网络出版日期:  2025-07-18

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