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多孔径穿孔板控制液雾燃烧不稳定的研究

刘子华 周昊 方浩

刘子华, 周昊, 方浩. 多孔径穿孔板控制液雾燃烧不稳定的研究[J]. 航空动力学报, 2021, 36(8): 1646-1656. doi: 10.13224/j.cnki.jasp.20200478
引用本文: 刘子华, 周昊, 方浩. 多孔径穿孔板控制液雾燃烧不稳定的研究[J]. 航空动力学报, 2021, 36(8): 1646-1656. doi: 10.13224/j.cnki.jasp.20200478
LIU Zihua, ZHOU Hao, FANG Hao. Study on controlling liquid fuel spray combustion instability by multi-aperture perforated plate[J]. Journal of Aerospace Power, 2021, 36(8): 1646-1656. doi: 10.13224/j.cnki.jasp.20200478
Citation: LIU Zihua, ZHOU Hao, FANG Hao. Study on controlling liquid fuel spray combustion instability by multi-aperture perforated plate[J]. Journal of Aerospace Power, 2021, 36(8): 1646-1656. doi: 10.13224/j.cnki.jasp.20200478

多孔径穿孔板控制液雾燃烧不稳定的研究

doi: 10.13224/j.cnki.jasp.20200478
基金项目: 

国家杰出青年科学基金(51825605)

详细信息
    作者简介:

    刘子华(1994-),男,博士生,主要研究液体喷雾学、燃烧不稳定被动控制。

    通讯作者:

    周昊(1973-),男,教授、博士生导师,博士,主要研究节能和低污染利用、燃烧振动控制、太阳能发电、先进储能和微流控制。E-mail:zhouhao@zju.edu.cn

  • 中图分类号: V232;TK47

Study on controlling liquid fuel spray combustion instability by multi-aperture perforated plate

  • 摘要: 研究了一种带可调背腔的多孔径穿孔板声阻尼器的吸声特性,并通过声学模型预测了穿孔板的吸声特性。实验研究了偏流穿孔板对液雾燃烧器的燃烧室、气室内波动的动态压力及热释放率的控制效果。多孔径穿孔板存在两种孔径:小孔半径均为1.0 mm,大孔半径分别为1.5、2.0、2.5、3.0 mm。发现孔径差异过大的穿孔板消声性能不佳。但是大小孔径相近的穿孔板对腔室内的热声振荡有明显衰减效果。安装穿孔板后,燃烧室脉动压力下降59%~84%,放热波动下降47%~87%,同时火焰形态变得稳定。

     

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出版历程
  • 收稿日期:  2020-11-08
  • 刊出日期:  2021-08-28

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