Study on the Effects of Dome Fuel Distribution Ratio on Lean Blowout of a Model Combustor

被引:4
|
作者
Shen, Xiaoming [1 ,2 ]
Yuan, Yixiang [1 ,2 ]
Zeng, Detang [1 ]
Xie, Pengfu [1 ]
Tan, Chunqing [1 ,2 ]
机构
[1] Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
[2] Univ Chinese Acad Sci, Beijing 100190, Peoples R China
基金
中国国家自然科学基金;
关键词
combustor; dome fuel distribution ratio; lean blowout; pressure fluctuation; FLAME;
D O I
10.1007/s11630-019-1146-0
中图分类号
O414.1 [热力学];
学科分类号
摘要
The experimental studies and numerical simulation were conducted on the effects of the dome fuel distribution ratio on the lean blowout of a model combustor. The experimental results indicate that as the key parameter, the dome fuel distribution ratio, increases from 2.06% to 16.67%, the lean blowout equivalence ratio declines obviously at the beginning, and then the decrease slows down, in addition, the amplitude of the pressure fluctuation in the combustor reduces significantly while the dominant frequency keeps basically constant. In order to analyze the experimental results, the numerical simulation is adopted. The temperature and local equivalence ratio distributions are employed to explain the reason why the lean blowout performance improves with the increase of the dome fuel distribution ratio.
引用
收藏
页码:52 / 57
页数:6
相关论文
共 50 条
  • [31] EVALUATION OF SYNTHETIC FUEL CHARACTER EFFECTS ON A RICH LEAN TURBINE COMBUSTOR
    ANGELLO, LC
    ROVESTI, WC
    SEDERQUIST, RA
    ROSFJORD, TJ
    ABSTRACTS OF PAPERS OF THE AMERICAN CHEMICAL SOCIETY, 1982, 183 (MAR): : 62 - PETR
  • [32] Lean blowout characteristics of spray flame in a multi-swirl staged combustor under different fuel decreasing rates
    Qianpeng ZHAO
    Jinhu YANG
    Cunxi LIU
    Fuqiang LIU
    Shaolin WANG
    Yong MU
    Gang XU
    Junqiang ZHU
    Chinese Journal of Aeronautics, 2022, (12) : 130 - 143
  • [33] Lean blowout characteristics of spray flame in a multi-swirl staged combustor under different fuel decreasing rates
    Qianpeng ZHAO
    Jinhu YANG
    Cunxi LIU
    Fuqiang LIU
    Shaolin WANG
    Yong MU
    Gang XU
    Junqiang ZHU
    Chinese Journal of Aeronautics, 2022, 35 (12) : 130 - 143
  • [34] Lean blowout characteristics of spray flame in a multi-swirl staged combustor under different fuel decreasing rates
    Zhao, Qianpeng
    Yang, Jinhu
    Liu, Cunxi
    Liu, Fuqiang
    Wang, Shaolin
    Mu, Yong
    Xu, Gang
    Zhu, Junqiang
    CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (12) : 130 - 143
  • [35] INFLUENCE OF WATER INJECTION ON HEAT RELEASE DISTRIBUTION, LEAN BLOWOUT AND EMISSIONS OF A PREMIXED SWIRL FLAME IN A TUBULAR COMBUSTOR
    Lellek, Stephan
    Sattelmayer, Thomas
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 4A, 2015,
  • [36] Effects of wall confinement on flame topologies and lean blowout characteristics of partially premixed DME/air flames in a gas turbine model combustor
    Shi, Xiaoxiang
    Liu, Zundi
    Lian, Tianyou
    Han, Sibo
    Zhang, Yi
    Xi, Zhongya
    Li, Wei
    Li, Yuyang
    FUEL, 2024, 372
  • [37] Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor
    Yang, Jun
    Wu, Xian-yu
    Wang, Zhen-guo
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2016, 2016
  • [38] Fuel effects on lean blow-out in a realistic gas turbine combustor
    Esclapez, Lucas
    Ma, Peter C.
    Mayhew, Eric
    Xu, Rui
    Stouffer, Scott
    Lee, Tonghun
    Wang, Hai
    Ihme, Matthias
    COMBUSTION AND FLAME, 2017, 181 : 82 - 99
  • [39] The effects of fuel composition on flame structure and combustion dynamics in a lean premixed combustor
    Figura, Lorenzo
    Lee, Jong Guen
    Quay, Bryan D.
    Santavicca, Domenic A.
    PROCEEDINGS OF THE ASME TURBO EXPO, VOL 2, 2007, : 181 - 187
  • [40] Effects of airflow split and primary holes arrangement on lean blowout limits of combustor with dual-axial swirlers
    Xie, Fa
    Huang, Yong
    Miao, Hui
    Chen, Haigang
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2011, 37 (11): : 1456 - 1460