基于激光诊断的燃料分级光学模型燃烧室双旋流喷射火焰实验研究

Siheng Yang, Wang Jianchen, Wang Zhichao, Han Meng, Yuzhen Lin, Wang Yexin
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引用次数: 1

摘要

精益预混预汽化燃烧器通常采用分段燃烧的方式,预混主火焰由未预混的先导火焰锚定,以获得较宽的工作范围。先导火焰和主火焰之间的相互作用是复杂的。本文研究了不同工作条件(燃料空气比FAR和燃料级比α)和喷油器设计(主级旋流数Sm和燃油喷射角JA)下分离分层旋流火焰的火焰拓扑结构和火焰-燃料相互作用。实验在中央分级光学模型燃烧室中进行,入口压力P3 = 0.49 ~ 0.7 MPa,入口温度T3 = 539 K。首先,对基线喷射器(Sm = 0.9, JA = - 50°)的火焰结构进行了研究和讨论。在先导火焰模式(α = 1)下,v形火焰稳定于内剪切层(ISL),火焰附着点位于唇部。在燃料分级燃烧模式(α < 1)下,燃烧室中观察到双火焰:主火焰稳定于外剪切层(OSL),先导火焰稳定于内剪切层(ISL)。当α从0.15增加到0.25时,主火焰和先导火焰之间的间隙减小,表明两种火焰之间的相互作用更强。然后研究了不同喷嘴几何形状下的火焰结构。结果表明,主级旋流数越高,火焰的开口角越大,两种火焰之间的相互作用越小。喷入交叉流(JA = - 50°)的燃料产生了更分离的火焰,减少了火焰的相互作用。最后,分析了煤油- plif测量的燃料分布与火焰结构的关系。结果表明,燃料与新鲜空气的良好混合为高放热的化学反应提供了有利条件。氢氧根分布与燃料分布高度相关。燃料区位于高OH区内侧,说明燃料-空气混合物经过预热混合后发生了反应和放热。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental Investigation of Dual-Swirl Spray Flame in a Fuel Staged Optical Model Combustor With Laser Diagnostics
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 α) and injector designs (main stage swirl number Sm and fuel injection angle JA). Experiments are carried out in the centrally staged optical model combustor at inlet pressure P3 = 0.49–0.7 MPa and inlet temperature T3 = 539 K. At first, the flame structures obtained from OH-PLIF are investigated and discussed for the baseline injector (Sm = 0.9, JA = −50°). 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 (α = 1). Dual flame is observed in the combustor for the fuel staged combustion (α < 1): the main flame stabilized in the outer shear layer (OSL) and the pilot flame stabilized in the inner shear layer (ISL). For increasing α 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°) 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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