Volume 40 Issue 5
May  2025
Turn off MathJax
Article Contents
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

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

doi: 10.13224/j.cnki.jasp.20230606
  • Received Date: 2023-09-20
    Available Online: 2024-08-20
  • Experimental research was conducted on the direct combustion noise sound pressure level and spectral characteristics of methane/hydrogen at different mixing ratios. An array microtube burner was utilized to organize methane-hydrogen combustion under ambient temperature and pressure conditions. Within the micro-tube, spiral blades were employed to enhance the mixing of fuel and air. Pressure pulsations of combustion noise were recorded using microphones, and the data were subjected to spectral analysis. The study revealed that with an increase in the hydrogen power ratio (HPR), the peak frequency of the combustion noise spectrum gradually shifted from low frequency to high frequency, and there was a noticeable increase in the power spectral density in the high-frequency portion. When the HPR was constant, the shape of the direct combustion noise power spectrum was not significantly affected by the equivalence ratio. Sound levels in decibels were measured using an A-weighted sound level meter. When the baseline hydrogen equivalence ratio was within the range of 0.5 to 0.8, the trend of combustion noise variation remained consistent as HPR increased from 0 to 100%, resulting in an approximate 11 dB increase in noise levels. This study fitted the direct combustion noise and obtained the prediction relationship of methane hydrogen-doped combustion noise using methane combustion noise as the normalized benchmark.

     

  • loading
  • [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

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (427) PDF downloads(41) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return