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清华大学学报(自然科学版)  2023, Vol. 63 Issue (4): 572-584    DOI: 10.16511/j.cnki.qhdxxb.2023.25.027
  论文 本期目录 | 过刊浏览 | 高级检索 |
氢燃料微预混火焰燃烧不稳定性实验研究
扈学超1,2, 毕笑天1,2, 刘策1,2, 邵卫卫1,2,3
1. 中国科学院 工程热物理研究所, 先进能源动力重点实验室, 北京 100190;
2. 中国科学院大学, 北京 100049;
3. 江苏中科能源动力研究中心, 连云港 222069
Study of combustion characteristics and flame stabilization mechanism of hydrogen-containing micromix jet flames
HU Xuechao1,2, BI Xiaotian1,2, LIU Ce1,2, SHAO Weiwei1,2,3
1. Key Laboratory of Advances Energy and Power, Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100190, China;
2. University of Chinese Academy of Science, Beijing 100049, China;
3. Jiangsu Zhongke Research Center for Clean Energy and Power, Lianyungang 222069, China
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摘要 该文针对一种自主设计的氢燃料微预混燃烧器,开展了常压下掺氢甲烷燃料微预混火焰燃烧不稳定性实验研究。从纯甲烷到纯氢气,研究了不同氢含量下NOx排放、动态压力、火焰结构等燃烧特性,结果表明:该预混燃烧器具有较优异的低排放燃烧性能,可适应较宽氢含量燃料并实现稳定燃烧,其中纯氢燃料在绝热火焰温度1 850 K时NOx不高于5 μmol/mol (干基,15% O2摩尔浓度);在氢含量为10%和20%时,氢燃料微预混火焰出现振荡燃烧现象,且激发更高阶的谐波;在更高氢含量下微混火焰出现高频脉动,但幅值较低。利用本征正交分解(proper orthogonal decomposition,POD)方法对振荡工况进行分析,提取其模态的时间系数和空间分布特征,发现一阶模态都表现为与整体脉动主频相同的体积振荡,二阶模态都表现为轴向脉动,脉动频率是主频的2倍。随着氢含量进一步升高,轴向模态渐渐转变为火焰间相互作用。
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扈学超
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刘策
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关键词 燃气轮机氢燃烧微预混燃烧燃烧不稳定性本征正交分解    
Abstract:[Objective] Micromix combustion is an excellent low-pollution combustion technology. However, the instability of micromix combustion based on multiple small flames, especially high-frequency oscillation under high hydrogen content, is still unclear. [Methods] Herein, the emission performance and oscillation characteristics of micromix combustion under different hydrogen enrichments were studied. Furthermore, an experimental study on the combustion instability of hydrogen-rich fuel was conducted using a novel micromix burner under atmospheric pressure and preheated air at 673 K, which provided a reference for practical engineering applications. Power spectral density was used for spectral analysis. Phase-space reconstruction was applied to analyze the developmental changes in the dynamical system and determine the limit cycle oscillations. Proper orthogonal decomposition (POD) was used to analyze flame dynamics under oscillating conditions, and the time coefficients and spatial distribution characteristics of the modes were extracted. Dynamic pressure sensors were arranged in the air inlet and exhaust outlet contraction sections to measure pressure fluctuations. A high-speed camera system was used to realize the fast acquisition of chemiluminescence signals. The NOx emission, dynamic pressure, flame structure, and other combustion characteristics were studied under different hydrogen contents, from pure methane to pure hydrogen. [Results] The results showed that: 1) The micromix burner had an excellent low-emission performance for pure hydrogen with< 5 μmol/mol NOx at 15% O2 and could adapt to a wide hydrogen content to achieve stable combustion. These characteristics indicated that this micromix burner could be directly applied to designing hydrogen turbine combustion chambers. 2) The oscillatory combustion phenomenon occurred when the hydrogen content was between 10% and 20%. Under those conditions, the phase-space reconstruction trajectory manifested as limit cycle oscillation, and the root mean square values of pressure fluctuation were >1%, representing strong correlation structures. High-order harmonics were also found. Heat release was shown as a periodic overall increase and decrease, and the periodic formation and axial propagation of flame vortices could be observed. The flames with high hydrogen contents fluctuated at a high frequency of >900 Hz, but the amplitude of these flames was low. 3) Time-average images were used to characterize the flame structure under different conditions. The decreasing flame height with increasing hydrogen content contributed to the changes in the heat release concentration position. On the one hand, it affected the coupling relationship between the heat release fluctuation and pressure fluctuation, on the other hand, it shortened the period of pressure fluctuation, corresponding to the increase in main frequency. 4) Between 10% and 20% hydrogen content, the first-order mode was a volume oscillation, which was identical to the main frequency of the whole oscillation, and the second-order mode was an axial oscillation, which was twice the main frequency of the oscillation. With the increase of hydrogen content, the main POD modes switched from the axial mode to flame interaction. [Conclusions] The oscillation conditions and the instability characteristics of the hydrogen-containing fuel were obtained via data analysis. The experimental results could be used to master the mechanism of combustion instability and provide a reference for developing control technology for combustion instability.
Key wordsgas turbine    hydrogen combustion    micromixing combustion    combustion instability    proper orthogonal decomposition
收稿日期: 2023-02-18      出版日期: 2023-04-22
基金资助:航空发动机及燃气轮机基础科学中心重大项目(P2022-A-II-006-003);中国科学院青年创新促进会项目(Y2021054)
通讯作者: 邵卫卫,研究员,E-mail:shaoww@iet.cn     E-mail: shaoww@iet.cn
作者简介: 扈学超(1998-),男,硕士研究生。
引用本文:   
扈学超, 毕笑天, 刘策, 邵卫卫. 氢燃料微预混火焰燃烧不稳定性实验研究[J]. 清华大学学报(自然科学版), 2023, 63(4): 572-584.
HU Xuechao, BI Xiaotian, LIU Ce, SHAO Weiwei. Study of combustion characteristics and flame stabilization mechanism of hydrogen-containing micromix jet flames. Journal of Tsinghua University(Science and Technology), 2023, 63(4): 572-584.
链接本文:  
http://jst.tsinghuajournals.com/CN/10.16511/j.cnki.qhdxxb.2023.25.027  或          http://jst.tsinghuajournals.com/CN/Y2023/V63/I4/572
  
  
  
  
  
  
  
  
  
  
  
  
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