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Static Stability and Combustion Characteristics of Oxy-Propane Flames in a Premixed Fuel-Flexible Swirl Combustor

机译:预混合燃料-柔性旋流燃烧器中丙烷丙烷火焰的静态稳定性和燃烧特性

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This study investigates the stability and combustion features of premixed oxy-propane flames in a dry low emission (DLE) model combustor for clean fuel/oxidizer-flexible combustion applications in gas turbines. The stability of the oxy-propane flame is characterized by its blowout and flashback limits over ranges of equivalence ratios (phi) from 0.1 to 1.0 and oxygen fractions (OF: volumetric concentration of O-2 in the O-2/CO2 oxidizer) from 15 to 70%. For better understanding of the physics behind the flame extinction mechanisms, the stability limits were plotted within the phi-OF space against the contours of adiabatic flame temperature (T-ad), inlet Reynolds number (Re), mixture mass flow rate ((m)over dot(mix)), and combustor power density (PD). The flame speed (FS) was also estimated at selected operating conditions. It was observed that the FS is contingent to T-ad only. A correlation of T-ad-FS was developed for better characterization of premixed oxy-propane flames. It was also found that the blowout curve follows a constant T-ad contour on the stability map, whereas the flashback curve does not. This implies that T-ad is a more relevant controlling parameter choice of combustor stability near the blowout limit, whereas the reaction rate is a suitable indicator of the flame stability limit near flashback. The stability map of the present oxy-propane flame was compared with that of an oxy-methane flame on the same combustor. It was found that, at the same OF, the blowout and flashback limits of the propane flame occur at leaner phi, compared to those of methane flame, which was expected for a higher hydrocarbon fuel like propane. Flame shapes at different sets of operating conditions were investigated for inferring key information on the flame behavior and macrostructure while varying phi, OF, and hence, T-ad. Similar flame shapes were obtained at the same T-ad regardless of phi and OF values. Flames of similar T-ad also demonstrated similar temperature distributions near the flame core. The findings confirm the dependence of the FS on T-ad, irrespective of the combinations of phi and OF used to achieve any particular T-ad.
机译:这项研究调查了干式低排放(DLE)模型燃烧器中预混合的氧丙烷火焰的稳定性和燃烧特性,该燃烧器适用于燃气轮机中清洁燃料/氧化剂灵活燃烧的应用。氧丙烷火焰的稳定性特征在于其当量比(phi)在0.1至1.0范围内的吹出和回火极限以及氧分率(OF:O-2 / CO2氧化剂中O-2的体积浓度) 15%至70%。为了更好地了解熄灭机制背后的物理原理,在phi-OF空间内针对绝热火焰温度(T-ad),入口雷诺数(Re),混合物质量流量((m )(点(混合))和燃烧室功率密度(PD)。在选定的运行条件下也可以估算出火焰速度(FS)。据观察,FS仅取决于T-ad。为了更好地表征预混合的氧丙烷火焰,开发了T-ad-FS的相关性。还发现,井喷曲线在稳定性图中遵循恒定的T-ad轮廓,而反吹曲线则不然。这意味着,T-ad是在爆燃极限附近的燃烧器稳定性更相关的控制参数选择,而反应速率是在回火附近的火焰稳定性极限的合适指标。在同一燃烧器上,将本发明的氧丙烷火焰的稳定性图与氧甲烷火焰的稳定性图进行了比较。发现在相同的OF下,与甲烷火焰相比,丙烷火焰的爆燃和回火极限发生在更稀薄的phi处,而甲烷火焰则是丙烷等更高碳氢燃料所期望的。研究了在不同运行条件下的火焰形状,以推断有关火焰行为和宏观结构的关键信息,同时改变phi,OF和T-ad。无论phi和OF值如何,在相同的T-ad处均获得相似的火焰形状。 T-ad相似的火焰在火焰核心附近也显示出相似的温度分布。该发现证实了FS对T-ad的依赖性,而与用于实现任何特定T-ad的phi和OF的组合无关。

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