EXPERIMENTAL INVESTIGATION OF DUAL-SWIRL SPRAY FLAME IN A FUEL STAGED OPTICAL MODEL COMBUSTOR WITH LASER DIAGNOSTICS

被引:0
作者
Yang, Siheng [1 ]
Wang, Jianchen [1 ]
Wang, Zhichao [1 ]
Han, Meng [1 ]
Lin, Yuzhen [1 ]
Wang, Yexin [2 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 102206, Peoples R China
[2] COMAC Shanghai Aircraft Design & Res Inst, Liaison Engn, Shanghai 201210, Peoples R China
来源
PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 3A | 2021年
基金
中国国家自然科学基金;
关键词
Spray flame; Fuel-staged; Laser diagnostics; PREMIXED COMBUSTION; STRATIFICATION; SIMULATIONS; EMISSIONS; FLOW; OH;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
Lean premixed prevaporized combustors often feature staged combustion with a premixed main flame anchored by the nonpremixed pilot flame to obtain a wide operating range. Interaction between pilot flame and main flame is complex. The present article investigates the flame topologies and flame-fuel interactions in separated stratified swirl flames under various operating conditions (fuel to air ratio FAR and fuel stage ratio a) and injector designs (main stage swirl number S-m and fuel injection angle JA). Experiments are carried out in the centrally staged optical model combustor at inlet pressure P-3 = 0.49-0.7 MPa and inlet temperature T-3 = 539 K. At first, the flame structures obtained from OH-PLIF are investigated and discussed for the baseline injector (S-m = 0.9, JA = 50 degrees). The V-shaped flame is stabilized in the inner shear layer (ISL) with the flame attachment point located at the lip for the pilot flame mode (alpha = 1). Dual flame is observed in the combustor for the fuel staged combustion (alpha < 1): the main flame stabilized in the outer shear layer (OSL) and the pilot flame stabilized in the inner shear layer (ISL). For increasing a from 0.15 to 0.25, gaps between the main flame and pilot flame are decreased, indicating a stronger interaction between the two flames. The flame structure for different injector geometries is then investigated. It is found that the higher main stage swirl number induces a larger flame opening angle, decreasing the interaction between two flames. Fuel injected into crossflow (JA = 50 degrees) is found to generated a more separated flame, decreasing the flame interactions. Finally, fuel distribution measured by kerosene-PLIF is analyzed with the correlation to flame structure. Results show that the existence of a good mixing of fuel and fresh air in ISL and OSL provide favorable conditions for chemical reaction with high heat release. The OH distribution is highly correlated to fuel distribution. The fuel zone is located at the inner side of high OH region, indicating the reaction and heat release take place after the mixing of preheating of fuel-air mixture.
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页数:11
相关论文
共 29 条
[1]   Application of Raman/Rayleigh/LIF diagnostics in turbulent stratified flames [J].
Barlow, R. S. ;
Wang, G. -H. ;
Anselmo-Filho, P. ;
Sweeney, M. S. ;
Hochgreb, S. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2009, 32 :945-953
[2]   Effect of mixture flow stratification on premixed flame structure and emissions under counter-rotating swirl burner configuration [J].
Chong, Cheng Tung ;
Lam, Su Shiung ;
Hochgreb, Simone .
APPLIED THERMAL ENGINEERING, 2016, 105 :905-912
[3]   FLAME AND FLOW TOPOLOGIES IN AN ANNULAR SWIRLING FLOW [J].
Chterev, I. ;
Foley, C. W. ;
Foti, D. ;
Kostka, S. ;
Caswell, A. W. ;
Jiang, N. ;
Lynch, A. ;
Noble, D. R. ;
Menon, S. ;
Seitzman, J. M. ;
Lieuwen, T. C. .
COMBUSTION SCIENCE AND TECHNOLOGY, 2014, 186 (08) :1041-1074
[4]   Simultaneous imaging of fuel, OH, and three component velocity fields in high pressure, liquid fueled, swirl stabilized flames at 5 kHz [J].
Chterev, Ianko ;
Rock, Nicholas ;
Ek, Hanna ;
Emerson, Benjamin ;
Seitzman, Jerry ;
Jiang, Naibo ;
Roy, Sukesh ;
Lee, Tonghun ;
Gord, James ;
Lieuwen, Tim .
COMBUSTION AND FLAME, 2017, 186 :150-165
[5]   Unsteady Aspects of Lean Premixed Prevaporized Gas Turbine Combustors: Flame-Flame Interactions [J].
Dhanuka, Sulabh K. ;
Temme, Jacob E. ;
Driscoll, James E. .
JOURNAL OF PROPULSION AND POWER, 2011, 27 (03) :631-641
[6]   Experimental and numerical studies of a lean-burn internally-staged combustor [J].
Fu Zhenbo ;
Lin Yuzhen ;
Li Lin ;
Zhang Chi .
CHINESE JOURNAL OF AERONAUTICS, 2014, 27 (03) :488-496
[7]   The response of stratified swirling flames to acoustic forcing: Experiments and comparison to model [J].
Han, Zhiyi ;
Hochgreb, Simone .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2015, 35 :3309-3315
[8]   Bifurcation of flame structure in a lean-premixed swirl-stabilized combustor: transition from stable to unstable flame [J].
Huang, Y ;
Yang, V .
COMBUSTION AND FLAME, 2004, 136 (03) :383-389
[9]   The nonlinear heat release response of stratified lean-premixed flames to acoustic velocity oscillations [J].
Kim, K. T. ;
Hochgreb, S. .
COMBUSTION AND FLAME, 2011, 158 (12) :2482-2499
[10]  
Lefebvre A.H., 1998, GAS TURBINE COMBUSTI