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

掺氢比对阵列微管火焰燃烧噪声的影响研究

罗守博 张弛 昌运鑫 高安雯 甘志超 韩啸 梁勇

罗守博, 张弛, 昌运鑫, 等. 掺氢比对阵列微管火焰燃烧噪声的影响研究[J]. 航空动力学报, 2025, 40(5):20230606 doi: 10.13224/j.cnki.jasp.20230606
引用本文: 罗守博, 张弛, 昌运鑫, 等. 掺氢比对阵列微管火焰燃烧噪声的影响研究[J]. 航空动力学报, 2025, 40(5):20230606 doi: 10.13224/j.cnki.jasp.20230606
LUO Shoubo, ZHANG Chi, CHANG Yunxin, et al. Study on influence of hydrogen doping ratio on combustion noise of array microtube flame[J]. Journal of Aerospace Power, 2025, 40(5):20230606 doi: 10.13224/j.cnki.jasp.20230606
Citation: LUO Shoubo, ZHANG Chi, CHANG Yunxin, et al. Study on influence of hydrogen doping ratio on combustion noise of array microtube flame[J]. Journal of Aerospace Power, 2025, 40(5):20230606 doi: 10.13224/j.cnki.jasp.20230606

掺氢比对阵列微管火焰燃烧噪声的影响研究

doi: 10.13224/j.cnki.jasp.20230606
基金项目: 航空发动机及燃气轮机基础科学中心项目(P2022-A-Ⅱ-006-001); 国家自然科学基金(52106128);中央高校基本科研业务费专项资金(501XTCX2023146001)
详细信息
    作者简介:

    罗守博(2001-),男,博士生,研究领域为燃气轮机燃烧。E-mail:Luoshoubo@buaa.edu.cn

    通讯作者:

    韩啸(1993-),男,副研究员,博士,研究领域为燃烧振荡机理及控制、燃烧噪声。E-mail:han_xiao@buaa.edu.cn

  • 中图分类号: V231.2

Study on influence of hydrogen doping ratio on combustion noise of array microtube flame

  • 摘要:

    针对不同掺混比例下甲烷/氢气的直接燃烧噪声声压级和频谱特征开展实验研究,采用阵列微管燃烧器在常温常压条件下组织甲烷掺氢燃烧,微管内采用螺旋叶片强化燃料与空气混合。实验采用传声器记录了燃烧噪声的压力脉动,对数据进行频谱分析,研究发现随着掺氢功率比(HPR)的增加,燃烧噪声频谱峰值逐渐由低频向高频转变,高频部分的功率谱密度有明显升高;在掺氢功率比一定时,直接燃烧噪声的声功率谱形状受当量比影响不显著。实验中使用分贝仪测量了A计权下的燃烧噪声分贝值。基准氢气当量比在0.5~0.8时,掺氢功率比从0变化至100%,燃烧噪声变化趋势一致,噪声分贝值约提高11 dB。本研究对直接燃烧噪声进行了拟合,得到了以甲烷燃烧噪声为归一化基准的甲烷掺氢燃烧噪声预测关系式。

     

  • 图 1  阵列微管模型燃烧室实验系统示意图

    Figure 1.  Schematic diagram of the AMT experimental system

    图 2  微管内部结构示意图

    Figure 2.  Schematic diagram of the internal structure of microtubules

    图 3  P=16.55 kW,φ=0.6,时RHPR=0~100%的火焰图像

    Figure 3.  Flame images of RHPR=0—100% whenP=16.55 kW, φ=0.6

    图 4  不同当量比下火焰可见光长度随掺氢比的变化

    Figure 4.  Changes in flame visible light length with HPR under different reference equivalence ratios

    图 5  不同基准当量比下燃烧噪声随火焰可见光长度的变化

    Figure 5.  Changes in combustion noise with flame visible light length under different reference equivalence ratios

    图 6  φ=0.6时不同掺氢比下的频谱特征

    Figure 6.  Spectrum features under different hydrogen doping power ratios when φ=0.6

    图 7  不同基准当量比下的功率谱密度特征

    Figure 7.  PSD characteristics under different reference equivalence ratios

    图 8  φ=0.6时不同掺氢比下的功率谱密度特征

    Figure 8.  PSD characteristics under different hydrogen power ratios when φ=0.6

    图 9  不同掺氢比下的燃烧噪声随基准当量比的变化

    Figure 9.  Combustion noise changes with φ under different hydrogen power ratios

    图 10  不同基准当量比下的燃烧噪声随掺氢比的变化

    Figure 10.  Combustion noise changes with RHPR under different reference equivalence ratios

    图 11  归一化噪声的拟合曲线

    Figure 11.  Fitting curve of normalized noise

  • [1] Advisory Council for Aeronautics Research in Europe. Flightpath 2050 Europe’s vision for aviation [M]. Luxembourg: Publications Office of the European Union,2011: 26-28.
    [2] 余筱,赵晓尧,马康,等. 声场扰动下预混旋流管状火焰动态响应特性[J]. 航空动力学报,2020,35(8): 1655-1663. YU Xiao,ZHAO Xiaoyao,MA Kang,et al. Characteristics of premixed swirling tubular flame under acoustics perturbation[J]. Journal of Aerospace Power,2020,35(8): 1655-1663. (in Chinese

    YU Xiao, ZHAO Xiaoyao, MA Kang, et al. Characteristics of premixed swirling tubular flame under acoustics perturbation[J]. Journal of Aerospace Power, 2020, 35(8): 1655-1663. (in Chinese)
    [3] 莫妲,林宇震,韩啸,等. 氢气微混燃烧技术进展现状和未来展望[J]. 航空学报,2024,45(7):028994. MO Da,LIN Yuzhen,HAN Xiao,et al. Research progress and future prospect of hydrogen micromix combustion technology[J]. Acta Aeronautica et Astronautica Sinica,2024,45(7):028994. (in Chinese

    MO Da, LIN Yuzhen, HAN Xiao, et al. Research progress and future prospect of hydrogen micromix combustion technology[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 028994. (in Chinese)
    [4] 邱朋华,卢成,张林瑶,等. 氢燃料微混燃烧技术研究进展[J]. 热能动力工程,2023,38(5): 14-23. QIU Penghua,LU Cheng,ZHANG Linyao,et al. Research progress of hydrogen micromix combustion technology[J]. Journal of Engineering for Thermal Energy and Power,2023,38(5): 14-23. (in Chinese

    QIU Penghua, LU Cheng, ZHANG Linyao, et al. Research progress of hydrogen micromix combustion technology[J]. Journal of Engineering for Thermal Energy and Power, 2023, 38(5): 14-23. (in Chinese)
    [5] DONG Chen,ZHOU Qulan,ZHANG Xiaoguang,et al. Experimental study on the laminar flame speed of hydrogen/natural gas/air mixtures[J]. Frontiers of Chemical Engineering in China,2010,4(4): 417-422. doi: 10.1007/s11705-010-0515-8
    [6] HU Erjiang,HUANG Zuohua,ZHENG Jianjun,et al. Numerical study on laminar burning velocity and NO formation of premixed methane-hydrogen-air flames[J]. International Journal of Hydrogen Energy,2009,34(15): 6545-6557. doi: 10.1016/j.ijhydene.2009.05.080
    [7] UEDA A,NISIDA K,MATSUMURA Y,et al. Effects of hydrogen and carbon dioxide on the laminar burning velocities of methane-air mixtures[J]. Journal of the Energy Institute,2021,99: 178-185. doi: 10.1016/j.joei.2021.09.007
    [8] CHOI J,RAJASEGAR R,LEE W,et al. Hydrogen enhancement on a mesoscale swirl stabilized burner array[J]. International Journal of Hydrogen Energy,2021,46(46): 23906-23915. doi: 10.1016/j.ijhydene.2021.04.157
    [9] 陈伊宇,龙礼文,黄泰明,等. 天然气掺氢燃烧技术研究进展[J]. 油气储运,2023,42(8): 872-881. CHEN Yiyu,LONG Liwen,HUANG Taiming,et al. Research progress in hydrogen-doped natural gas combustion technology[J]. Oil & Gas Storage and Transportation,2023,42(8): 872-881. (in Chinese

    CHEN Yiyu, LONG Liwen, HUANG Taiming, et al. Research progress in hydrogen-doped natural gas combustion technology[J]. Oil & Gas Storage and Transportation, 2023, 42(8): 872-881. (in Chinese)
    [10] 王明晓,邓凯,管清强,等. 不同当量比下氢气体积分数对甲烷-氢混合气预混火焰燃烧不稳定性的影响[J]. 航空动力学报,2018,33(12): 2851-2858. WANG Mingxiao,DENG Kai,GUAN Qingqiang,et al. Effect of hydrogen volume fraction on combustion instability of hydrogen/methane premixed flame under different equivalence rates[J]. Journal of Aerospace Power,2018,33(12): 2851-2858. (in Chinese

    WANG Mingxiao, DENG Kai, GUAN Qingqiang, et al. Effect of hydrogen volume fraction on combustion instability of hydrogen/methane premixed flame under different equivalence rates[J]. Journal of Aerospace Power, 2018, 33(12): 2851-2858. (in Chinese)
    [11] LEE T,KIM K T. Direct comparison of self-excited instabilities in mesoscale multinozzle flames and conventional large-scale swirl-stabilized flames[J]. Proceedings of the Combustion Institute,2021,38(4): 6005-6013. doi: 10.1016/j.proci.2020.05.049
    [12] JIN U,KIM K T. Experimental investigation of combustion dynamics and NOx/CO emissions from densely distributed lean-premixed multinozzle CH4/C3H8/H2/air flames[J]. Combustion and Flame,2021,229: 111410. doi: 10.1016/j.combustflame.2021.111410
    [13] DOWLING A P,MAHMOUDI Y. Combustion noise[J]. Proceedings of the Combustion Institute,2015,35(1): 65-100. doi: 10.1016/j.proci.2014.08.016
    [14] 罗守博,张耀恒,韩啸,等. 中心分级预混旋流火焰燃烧噪声的实验研究[J]. 推进技术,2023,44(5): 2207106. LUO Shoubo,ZHANG Yaoheng,HAN Xiao,et al. Experimental research on combustion noise of centrally staged premixed swirl flame[J]. Journal of Propulsion Technology,2023,44(5): 2207106. (in Chinese

    LUO Shoubo, ZHANG Yaoheng, HAN Xiao, et al. Experimental research on combustion noise of centrally staged premixed swirl flame[J]. Journal of Propulsion Technology, 2023, 44(5): 2207106. (in Chinese)
    [15] 杨尚荣,王勇,杨宝娥. 同轴离心式喷嘴噪声引发燃烧不稳定分析和预测[J]. 航空动力学报,2021,36(11): 2317-2324. YANG Shangrong,WANG Yong,YANG Baoe. Analysis and prediction of noise-induced combustion instabilities of coaxial swirl injector[J]. Journal of Aerospace Power,2021,36(11): 2317-2324. (in Chinese

    YANG Shangrong, WANG Yong, YANG Baoe. Analysis and prediction of noise-induced combustion instabilities of coaxial swirl injector[J]. Journal of Aerospace Power, 2021, 36(11): 2317-2324. (in Chinese)
    [16] 高贤智,王雄辉,冯晓星,等. 基于单扇区燃烧室试验的热声模拟方法研究及验证[J]. 航空动力学报,2022,37(2): 356-365. GAO Xianzhi,WANG Xionghui,FENG Xiaoxing,et al. Research and verification of thermo-acoustic simulation method based on single-sector combustion test[J]. Journal of Aerospace Power,2022,37(2): 356-365. (in Chinese

    GAO Xianzhi, WANG Xionghui, FENG Xiaoxing, et al. Research and verification of thermo-acoustic simulation method based on single-sector combustion test[J]. Journal of Aerospace Power, 2022, 37(2): 356-365. (in Chinese)
    [17] 高贤智,何沛,冯晓星,等. 单扇区、扇形、全环燃烧室热声不稳定性试验和模拟研究[J]. 航空动力学报,2021,36(8): 1605-1613. GAO Xianzhi,HE Pei,FENG Xiaoxing,et al. Experimental and numerical investigation of thermo-acoustic instability in single-sector,sector and full annular combustors[J]. Journal of Aerospace Power,2021,36(8): 1605-1613. (in Chinese

    GAO Xianzhi, HE Pei, FENG Xiaoxing, et al. Experimental and numerical investigation of thermo-acoustic instability in single-sector, sector and full annular combustors[J]. Journal of Aerospace Power, 2021, 36(8): 1605-1613. (in Chinese)
    [18] 曾佳进,李军伟,马宝印,等. 火箭发动机燃烧室中燃烧噪声的计算模型[J]. 航空学报,2023,44(18): 128148. ZENG Jiajin,LI Junwei,MA Baoyin,et al. Calculation model of combustion noise in rocket motor chamber[J]. Acta Aeronautica et Astronautica Sinica,2023,44(18): 128148. (in Chinese

    ZENG Jiajin, LI Junwei, MA Baoyin, et al. Calculation model of combustion noise in rocket motor chamber[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 128148. (in Chinese)
    [19] TAM C K W,BAKE F,HULTGREN L S,et al. Combustion noise: modeling and prediction[J]. CEAS Aeronautical Journal,2019,10(1): 101-122. doi: 10.1007/s13272-019-00377-2
    [20] STRAHLE W C. Some results in combustion generated noise[J]. Journal of Sound and Vibration,1972,23(1): 113-125. doi: 10.1016/0022-460X(72)90792-4
    [21] LIGHTHILL M J. On sound generated aerodynamically: Ⅰ general theory[J]. Proceedings of the Royal Society of London Series A Mathematical and Physical Sciences,1952,211(1107): 564-587.
    [22] 国家质量监督检验检疫总局,中国国家标准化管理委员会. 电声学 声级计: 第1部分规范: GB/T 3785.1—2010[S]. 北京: 中国标准出版社,2011. General Administration of Quality Supervision,Inspection and Quarantine of the People’s Republic of China,Standardization Administration of the People’s Republic of China. Electroacoustics sound level meters: Part 1 specifications: GB/T 3785.1—2010[S]. Beijing: Standards Press of China,2011. (in Chinese

    General Administration of Quality Supervision, Inspection and Quarantine of the People’s Republic of China, Standardization Administration of the People’s Republic of China. Electroacoustics sound level meters: Part 1 specifications: GB/T 3785.1—2010[S]. Beijing: Standards Press of China, 2011. (in Chinese)
    [23] 国家质量监督检验检疫总局,中国国家标准化管理委员会. 内燃机排气消声器 测量方法: GB/T 4759—2009[S]. 北京: 中国标准出版社,2009. General Administration of Quality Supervision,Inspection and Quarantine of the People’s Republic of China,Standardization Administration of the People’s Republic of China. Exhaust silencers for internal combustion engines-Measurement procedure: GB/T 4759—2009[S]. Beijing: Standards Press of China,2009. (in Chinese

    General Administration of Quality Supervision, Inspection and Quarantine of the People’s Republic of China, Standardization Administration of the People’s Republic of China. Exhaust silencers for internal combustion engines-Measurement procedure: GB/T 4759—2009[S]. Beijing: Standards Press of China, 2009. (in Chinese)
    [24] GUPTA R B. Hydrogen fuel: production,transport,and storage[M]. Boca Raton,US: CRC Press,2008.
    [25] YU G,LAW C K,WU C K. Laminar flame speeds of hydrocarbon+air mixtures with hydrogen addition[J]. Combustion and Flame,1986,63(3): 339-347. doi: 10.1016/0010-2180(86)90003-9
    [26] 莫妲,尚守堂,林宇震,等. 一种氢燃料微尺度非预混燃烧室数值模拟[J]. 航空动力学报,2023,38(11): 2701-2710. MO Da,SHANG Shoutang,LIN Yuzhen,et al. Numerical simulation investigation on a hydrogen micromix combustor[J]. Journal of Aerospace Power,2023,38(11): 2701-2710. (in Chinese

    MO Da, SHANG Shoutang, LIN Yuzhen, et al. Numerical simulation investigation on a hydrogen micromix combustor[J]. Journal of Aerospace Power, 2023, 38(11): 2701-2710. (in Chinese)
    [27] 乔渭阳,王良锋. 航空发动机气动声学[M]. 2版. 西安: 西北工业大学出版社,2016. QIAO Weiyang,WANG Liangfeng. Aeroacoustics of aero-engine[M]. 2nd ed. Xi’an: Northwestern Polytechnical University Press,2016. (in Chinese

    QIAO Weiyang, WANG Liangfeng. Aeroacoustics of aero-engine[M]. 2nd ed. Xi’an: Northwestern Polytechnical University Press, 2016. (in Chinese)
  • 加载中
图(11)
计量
  • 文章访问数:  427
  • HTML浏览量:  211
  • PDF量:  41
  • 被引次数: 0
出版历程
  • 收稿日期:  2023-09-20
  • 网络出版日期:  2024-08-20

目录

    /

    返回文章
    返回