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旋流数对贫预混燃烧特性影响

徐丽 刘凯 曾文

徐丽, 刘凯, 曾文. 旋流数对贫预混燃烧特性影响[J]. 航空动力学报, 2023, 38(6):1292-1298 doi: 10.13224/j.cnki.jasp.20210675
引用本文: 徐丽, 刘凯, 曾文. 旋流数对贫预混燃烧特性影响[J]. 航空动力学报, 2023, 38(6):1292-1298 doi: 10.13224/j.cnki.jasp.20210675
XU Li, LIU Kai, ZENG Wen. Effect of swirl number on lean premixed combustion characteristics[J]. Journal of Aerospace Power, 2023, 38(6):1292-1298 doi: 10.13224/j.cnki.jasp.20210675
Citation: XU Li, LIU Kai, ZENG Wen. Effect of swirl number on lean premixed combustion characteristics[J]. Journal of Aerospace Power, 2023, 38(6):1292-1298 doi: 10.13224/j.cnki.jasp.20210675

旋流数对贫预混燃烧特性影响

doi: 10.13224/j.cnki.jasp.20210675
基金项目: 国家自然科学基金(51376133); 航空科学基金(2015ZB54003)
详细信息
    作者简介:

    徐丽(1971-),女,副教授,硕士,研究方向为燃烧设计、试验与分析

  • 中图分类号: V231.2

Effect of swirl number on lean premixed combustion characteristics

  • 摘要:

    采用数值模拟与试验的手段,研究了旋流数对贫预混燃烧室燃烧性能的影响。数值模拟结果表明:旋流数在0.56~0.73之间,火焰筒头部均能产生明显的回流区,随旋流数的增加,回流区增大,但燃料掺混均匀性变差,主燃区燃料不均匀度由0.00853增加到0.01047,不利于温度场均匀性的提升和氮氧化物(NOx)排放的降低。试验结果表明:随旋流数增加,贫油熄火燃空比减小,且随进口马赫数越小这种趋势越明显;随旋流数增加,燃烧室出口温度均匀性变差,温度分布系数由0.1640增加到0.1915,一氧化碳(CO)排放指数由26.23 g/kg减少到18.07 g/kg,未燃碳氢化合物(UHC)排放指数由12.55 g/kg减少到9.21 g/kg,而NOx排放指数由0.609 g/kg增大到0.850 g/kg。

     

  • 图 1  燃烧室几何模型

    Figure 1.  Combustor geometric model

    图 2  不同网格数的轴向速度

    Figure 2.  Axis velocity with different grid numbers

    图 3  燃烧室流场

    Figure 3.  Flow field of combustor

    图 4  燃烧室中心截面燃料分布

    Figure 4.  Fuel distribution in central section of combustor

    图 5  燃烧室横截面燃料分布

    Figure 5.  Fuel distribution in cross sections of combustor

    图 6  燃烧室中心截面温度场

    Figure 6.  Temperature field in central section of combustor

    图 7  NOx的质量分数

    Figure 7.  Mass fraction of NOx

    图 8  试验系统图片

    Figure 8.  Picture of test system

    图 9  火焰筒

    Figure 9.  Flame tube

    图 10  贫油熄火燃空比

    Figure 10.  Fuel-air ratio of lean blowout

    图 11  热电偶耙及布置方式

    Figure 11.  Thermocouple and distribution

    图 12  燃气采样耙及布置方式

    Figure 12.  Gas sampling device and distribution

    表  1  天然气成分及体积分数

    Table  1.   Composition and volume fraction of natural gas

    成分CH4C2H6CO2N2
    体积分数/%94.661.251.272.82
    下载: 导出CSV

    表  2  数值模拟工况

    Table  2.   Numerical simulation condition

    天然气流量/
    (kg/s)
    空气总温/
    K
    空气总压/
    MPa
    空气流量/(kg/s)
    头部冷却
    0.009786500.2020.3100.136
    下载: 导出CSV

    表  3  燃料不均匀度统计结果

    Table  3.   Statistical results of fuel nonuniformity

    截面旋流数CH4质量分数
    最大值最小值不均匀度
    Z=210 mm0.560.031750.021820.02521
    0.650.037050.017960.02661
    0.730.046300.010550.02718
    Z=320 mm0.560.030940.027640.00853
    0.650.031950.026770.00897
    0.730.033820.026130.01047
    下载: 导出CSV

    表  4  出口温度场统计结果

    Table  4.   Statistical results of outlet temperature field

    旋流数平均温度/K热点温度/K出口温度分布系数
    0.561638.41789.20.1526
    0.651644.11802.30.1591
    0.731645.61822.60.1778
    下载: 导出CSV

    表  5  NOx排放指数

    Table  5.   Emission index of NOx

    旋流数排放指数/(g/kg)
    0.560.632
    0.650.824
    0.730.901
    下载: 导出CSV

    表  6  贫油熄火试验工况

    Table  6.   Lean blowout test conditions

    工况进口总温/K进口总压/MPa进口马赫数
    16500.2020.15
    20.18
    30.21
    下载: 导出CSV

    表  7  出口温度场试验结果

    Table  7.   Test results of outlet temperature field

    旋流数平均温度/K热点温度/K出口温度分布系数
    0.561623.51783.20.1640
    0.651625.51792.60.1713
    0.731626.61813.60.1915
    下载: 导出CSV

    表  8  污染物排放指数

    Table  8.   Emission index of pollution

    旋流数排放指数/(g/kg)
    COUHCNOx
    0.5626.2312.550.609
    0.6519.7310.930.783
    0.7318.079.210.850
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-11-28
  • 网络出版日期:  2023-04-29

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