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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Model Analysis of Syngas Combustion and Emissions for a Micro Gas Turbine
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Model Analysis of Syngas Combustion and Emissions for a Micro Gas Turbine

机译:微型燃气轮机的合成气燃烧与排放模型分析

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The purpose of this study is to investigate the combustion and emission characteristics of syngas fuels applied in a micro gas turbine, which is originally designed for a natural gas fired engine. The computation results were conducted by a numerical model, which consists of the three-dimension compressible k-ε model for turbulent flow and PPDF (presumed probability density function) model for combustion process. As the syngas is substituted for methane, the fuel flow rate and the total heat input to the combustor from the methane/syngas blended fuels are varied with syngas compositions and syngas substitution percentages. The computed results presented the syngas substitution effects on the combustion and emission characteristics at different syngas percentages (up to 90%) for three typical syngas compositions and the conditions where syngas applied at fixed fuel flow rate and at fixed heat input were examined. Results showed the flame structures varied with different syngas substitution percentages. The high temperature regions were dense and concentrated on the core of the primary zone for H_2-rich syngas, and then shifted to the sides of the combustor when syngas percentages were high. The NO_x emissions decreased with increasing syngas percentages, but NO_x emissions are higher at higher hydrogen content at the same syngas percentage. The CO_2 emissions decreased for 10% syngas substitution, but then increased as syngas percentage increased. Only using H_2-rich syngas could produce less carbon dioxide. The detailed flame structures, temperature distributions, and gas emissions of the combustor were presented and compared. The exit temperature distributions and pattern factor (PF) were also discussed. Before syngas fuels are utilized as an alternative fuel for the micro gas turbine, further experimental testing is needed as the modeling results provide a guidance for the improved designs of the combustor.
机译:这项研究的目的是研究微型燃气轮机中使用的合成气燃料的燃烧和排放特性,该燃气轮机最初是为天然气发动机设计的。计算结果由一个数值模型进行,该模型由用于湍流的三维可压缩k-ε模型和用于燃烧过程的PPDF(假定概率密度函数)模型组成。当合成气代替甲烷时,燃料流量和从甲烷/合成气混合燃料输入燃烧室的总热量随合成气组成和合成气替代百分比而变化。计算结果显示了三种典型合成气成分在不同合成气百分比(最高90%)下合成气替代对燃烧和排放特性的影响,并研究了以固定燃料流量和固定热量输入施加合成气的条件。结果表明,火焰结构随合成气替代百分比的不同而变化。高温区域密集且集中在富含H_2的合成气的主要区域的核心,然后在合成气百分比高时转移到燃烧器的侧面。 NO_x排放随着合成气百分比的增加而降低,但是在相同的合成气百分比下,氢气含量越高,NO_x排放就越高。合成气替代量为10%时,CO_2排放量减少,但随着合成气百分比增加,CO_2排放量增加。仅使用富含H_2的合成气可以产生较少的二氧化碳。介绍并比较了燃烧器的详细火焰结构,温度分布和气体排放。还讨论了出口温度分布和模式因子(PF)。在将合成气燃料用作微型燃气轮机的替代燃料之前,需要进行进一步的实验测试,因为建模结果为燃烧器的改进设计提供了指导。

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