Experimental investigations on flow field and combustion characteristics of a model trapped vortex combustor

被引:39
|
作者
Jin, Yi [1 ,3 ,4 ]
Li, Yefang [1 ,3 ]
He, Xiaomin [1 ,3 ,4 ]
Zhang, Jingyu [1 ]
Jiang, Bo [1 ,2 ]
Wu, Zejun [1 ]
Song, Yaoyu [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing 210016, Jiangsu, Peoples R China
[2] Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA
[3] Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Jiangsu, Peoples R China
[4] Coinnovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
关键词
Trapped vortex combustor; Experimental investigation; PIV; Flow field; Combustion characteristics; DYNAMICS; PERFORMANCE; FLAME;
D O I
10.1016/j.apenergy.2014.08.029
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Experimental studies are carried out to investigate cold flow field and combustion performance of a workable liquid-fueled trapped vortex combustor (TVC). A remarkable design of the model is that all the air flows through the combustor is supplied from a single source, which makes it distinct from most of the models mentioned in open literatures. Planar particle image velocimetry (PIV) is used to measure the cold flow field, with particular emphasis placed on vortical flow pattern within cavities, turbulence intensity distribution and interaction between cavity stream and mainstream. The aim of the PIV measurement is to better understand the underlying flow physics in a TVC, as well as to provide a benchmark for validation and improvement of computational models. Combustion experiments are carried out with preheated air (473 K) at atmospheric pressure using liquid kerosene. Flame images at different operating conditions are obtained and the effects of fuel to air ratio (FAR) and inlet Mach number on the physical appearance of flames are clearly revealed. The fuel to air ratio at lean blow out (LBO) is in the range from 0.0043 to 0.0056 as the inlet Mach number varies from 0.15 to 030, which indicates good flame stability. The combustion efficiency falls reasonably in the range of 92-100%. The improvement of the radial profile of outlet temperatures indicates the effectiveness of dilution holes. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:257 / 269
页数:13
相关论文
共 50 条
  • [31] Impact of interaction between cavity flow and mainstream on the performance of a model trapped vortex combustor
    Wu, Zejun
    He, Xiaomin
    Jin, Yi
    Song, Yaoyu
    Zhu, Yixiao
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 230 (07) : 1181 - 1200
  • [32] Numerical investigation on flow structures of a laboratory-scale trapped vortex combustor
    Jin, Yi
    He, Xiaomin
    Zhang, Jingyu
    Jiang, Bo
    Wu, Zejun
    APPLIED THERMAL ENGINEERING, 2014, 66 (1-2) : 318 - 327
  • [33] EXPERIMENTAL AND NUMERICAL STUDIES IN A COMPACT TRAPPED VORTEX COMBUSTOR: STABILITY ASSESSMENT AND AUGMENTATION
    Agarwal, Krishna Kant
    Ravikrishna, R. V.
    COMBUSTION SCIENCE AND TECHNOLOGY, 2011, 183 (12) : 1308 - 1327
  • [34] Experimental study on flow field characteristics of TBCC multibypass combustor
    Zhao, Wensheng
    Fan, Weijun
    Zhang, Rongchun
    AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 133
  • [35] Numerical investigation on the influence of injection angle from afterbody in cold flow field of the trapped vortex combustor
    Liu S.-Q.
    Zhong J.-J.
    Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2010, 31 (08): : 1065 - 1072
  • [36] Experimental and numerical studies on a trapped vortex combustor with different struts width
    Wu, Zejun
    Jin, Yi
    He, Xiaomin
    Xue, Chong
    Hong, Liang
    APPLIED THERMAL ENGINEERING, 2015, 91 : 91 - 104
  • [37] Performance of a novel swirling-flow single trapped vortex combustor
    Guo, Yuxi
    He, Xiaomin
    Gong, Cheng
    Zhang, Qiufeng
    Ma, Yichao
    Gui, Tao
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 127
  • [38] Experimental study on flow field and combustion characteristics of V-gutter and integrated flameholders
    Li, Jie
    Xia, Tao
    Sun, Bolun
    Song, Wenyan
    He, Chen
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2025, 42 (01) : 87 - 98
  • [39] Study on the effect of fuel injection on combustion performance and NOx emission of RQL trapped-vortex combustor
    Zhao Wensheng
    Fan Weijun
    Zhang Rongchun
    ENERGY REPORTS, 2023, 9 : 54 - 63
  • [40] Influence of improved structure of bluff-body on combustion flow characteristics in advanced vortex combustor
    Sun, Hai-Jun
    Zeng, Zhuo-Xiong
    Xu, Yi-Hua
    Hu, Chun-Bo
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2014, 29 (07): : 1639 - 1646