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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Analysis of N0_x Formation in an Axially Staged Combustion System at Elevated Pressure Conditions
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Analysis of N0_x Formation in an Axially Staged Combustion System at Elevated Pressure Conditions

机译:轴流分级燃烧系统中高压条件下N0_x形成的分析

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摘要

The objective of this investigation was to study the effect of axially staged injection of methane in the vitiated air cross flow in a two stage combustion chamber on the formation of NO_x for different momentum flux ratios. The primary cylindrical combustor equipped with a low swirl air blast nozzle operating with Jet-A liquid fuel generates vitiated air in the temperature range of 1473-1673 K at pressures of 5-8 bars. A methane injector was flush mounted to the inner surface of the secondary combustor at an angle of 30 deg. Oil cooled movable and static gas probes were used to collect the gas samples. The mole fractions of NO, NO_2, CO, CO_2, and O_2 in the collected exhaust gas samples were measured using gas analyzers. For all the investigated operating conditions, the change in the mole fraction of NO_x due to the injection of methane (ANOx) corrected to 15% O_2 and measured in dry mode was less than 15 ppm. The mole fraction of ANOx increased with an increase in mass flow rate of methane and it was not affected by a change in the momentum flux ratio. The penetration depth of the methane jet was estimated from the profiles of mole fraction of O_2 obtained from the samples collected using the movable gas probe. For the investigated momentum flux ratios, the penetration depth observed was 15 mm at 5 bars and 5 mm at 6.5 and 8 bars. The results obtained from the simulations of the secondary combustor using a RANS turbulence model were also presented. Reaction modeling of the jet flame present in a vitiated air cross flow posed a significant challenge as it was embedded in a high turbulent flow and burns in partial premixed mode. The applicability of two different reaction models has been investigated. The first approach employed a combination of the eddy dissipation and the finite rate chemistry models to determine the reaction rate, while the presumed JPDF model was used in the further investigations. Predictions were in closer agreement to the measurements while employing the presumed JPDF model. This model was also able to predict some key features of the flow such as the change of penetration depth with the pressure.
机译:这项研究的目的是研究在不同的动量通量比下,在两级燃烧室中,在有级分的空气横流中轴向分阶段注入甲烷对NO_x形成的影响。配有低涡流喷气喷嘴的主圆柱型燃烧器与Jet-A液体燃料一起工作,在5-8 bar的压力下,可产生温度范围为1473-1673 K的排气。将甲烷注入器以30度的角度齐平安装到辅助燃烧器的内表面。使用油冷的可移动和静态气体探针收集气体样本。使用气体分析仪测量收集的废气样品中NO,NO_2,CO,CO_2和O_2的摩尔分数。对于所有研究的运行条件,由于校正为15%O_2并以干燥模式测量的甲烷(ANOx)注入,NO_x的摩尔分数变化小于15 ppm。 ANOx的摩尔​​分数随甲烷质量流量的增加而增加,并且不受动量通量比变化的影响。甲烷射流的穿透深度是根据使用活动式气体探针收集的样品中O_2的摩尔分数的分布估算的。对于研究的动量通量比,观察到的穿透深度在5巴下为15 mm,在6.5巴和8巴下为5 mm。还介绍了使用RANS湍流模型对辅助燃烧器进行仿真得到的结果。由于存在于湍流中并且在部分预混合模式下燃烧,因此存在于通风的交叉流中的喷射火焰的反应模型提出了一个重大挑战。已经研究了两种不同反应模型的适用性。第一种方法采用涡流消散和有限速率化学模型的组合来确定反应速率,而假定的JPDF模型则用于进一步的研究。在采用假定的JPDF模型时,预测与测量结果更加吻合。该模型还能够预测流体的一些关键特征,例如渗透深度随压力的变化。

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