Large Eddy simulation of dilution and preheating impacts on chemical aspects of flame stabilization in a gas turbine model combustor

IF 7.5 1区 工程技术 Q2 ENERGY & FUELS Fuel Pub Date : 2025-06-15 Epub Date: 2025-02-19 DOI:10.1016/j.fuel.2025.134719
Amir A. Beige, Amir Mardani
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Abstract

Reducing fuel consumption and chemical pollutions is considered as a crucial issue, as many applications still depend on fossil fuels. In this paper, large eddy simulations of a gas turbine model combustor (GTMC) are performed in both normal and diluted/preheated conditions to have a better understanding of MILD combustion in these combustors. For this purpose, the flame structures are studied using the graphical and statistical tools, and the accuracy of the simulations is assessed by comparing the time-averaged results to the available experimental data. To model the turbulent combustion, Eddy Dissipation Concept (EDC) method is used with DRM-22 reduced mechanism in addition to the Wall-Adapting Local Eddy-Viscosity (WALE) turbulence model. To simulate the MILD combustion conditions, about 36 % reduction in fuel flow rate, 32 % dilution of the oxidizer (by EGR), in addition to preheating air to 730 K are used in the investigated diluted/preheated case. It is shown that the dilution/preheating of the incoming air creates stronger vortices (due to higher inlet velocities), faster mixings, and lower rates of H-atom abstraction (also due to lower fuel flow rates) in the upstream parts of the reactant jet, which is shown effective in expanding the radicals of the diluted/preheated flame. Moreover, it is observed that dilution/preheating reduces HO2 formation rates (and consequently weakens H2O2 routes) in upstream parts of the reactant jet, and also increases the rate of both chain branching and recombination reactions. Investigation of negative heat release spots reveals that their strength shows an almost linear relation with Q-criterion in the regions dominated by vorticity and they also appear closer to the positive heat release spots in the diluted/preheated mode. Furthermore, a generalized autoignition index is proposed based on the HO2 kinetics and it is used to illustrate the flame propagation and autoigntion regions for the investigated flames, which shows the spatial expansion of reaction spots in the diluted/preheated combustion mode and small role of auto-ignition spots in overall heat release for both flames. The CH2O dynamics also shows more distributed ignition for the diluted/preheated case in addition to the appearance of intermittent strong CH2O spots for both flames. Furthermore, the statistical analysis reveals less dependence of the ignition process on velocity gradients in the diluted/preheated mode. It is shown that while the rate of kinetically slower elementary reactions drops sharply in high strain regions of the normal combustion case, the rate of these reactions are less affected in the diluted/preheated mode. Consequently, some of the OH producing reactions are inhibited in high strain regions of the conventional combustion case, which causes the flame of this case to be stabilized outside of the high strain zones. Remarkably, while the positive heat release spots of the diluted/preheated flame are observed to be active inside the reactant jet, they are shown to be located mostly near the boundaries of the reactant jet in the normal flame case.

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稀释和预热对燃气轮机模型燃烧室稳焰化学影响的大涡模拟
减少燃料消耗和化学污染被认为是一个关键问题,因为许多应用仍然依赖于化石燃料。为了更好地理解燃气轮机模型燃烧室(GTMC)在正常和稀释/预热条件下的轻度燃烧,本文对燃气轮机模型燃烧室进行了大涡模拟。为此,使用图形和统计工具对火焰结构进行了研究,并通过将时间平均结果与现有实验数据进行比较来评估模拟的准确性。为了模拟紊流燃烧,在采用自适应壁面局部涡流黏度紊流模型的基础上,采用DRM-22还原机理的涡流耗散概念(EDC)方法。为了模拟轻度燃烧条件,在稀释/预热的情况下,除了将空气预热到730 K外,还使用了约36%的燃油流量减少,32%的氧化剂稀释(通过EGR)。研究表明,进入空气的稀释/预热在反应物射流的上游部分产生了更强的涡流(由于更高的入口速度),更快的混合和更低的h原子萃取速率(也由于更低的燃料流速),这对稀释/预热火焰的自由基扩展是有效的。此外,我们观察到稀释/预热降低了反应物射流上游部分的HO2形成速率(从而减弱H2O2路线),并增加了链支反应和重组反应的速率。对负放热斑的研究表明,在涡度占主导地位的区域,负放热斑的强度与q准则几乎呈线性关系,在稀释/预热模式下,负放热斑也更接近正放热斑。在此基础上,提出了基于HO2动力学的广义自燃指数,并用该指数描述了所研究火焰的火焰传播和自燃区域,表明在稀释/预热燃烧模式下,反应点的空间扩展和自燃点在两种火焰的总放热中的作用较小。CH2O动力学还显示,除了两种火焰出现间歇性强CH2O点外,稀释/预热情况下的点火分布更分散。此外,统计分析表明,在稀释/预热模式下,点火过程对速度梯度的依赖性较小。结果表明,在正常燃烧情况下,在高应变区,动力学较慢的元素反应速率急剧下降,而在稀释/预热模式下,这些反应速率受到的影响较小。因此,在常规燃烧情况下,一些生成OH的反应在高应变区被抑制,这使得这种情况下的火焰在高应变区之外稳定。值得注意的是,虽然观察到稀释/预热火焰的正放热点在反应物射流内活跃,但在正常火焰情况下,它们大多位于反应物射流的边界附近。
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来源期刊
Fuel
Fuel 工程技术-工程:化工
CiteScore
12.80
自引率
20.30%
发文量
3506
审稿时长
64 days
期刊介绍: The exploration of energy sources remains a critical matter of study. For the past nine decades, fuel has consistently held the forefront in primary research efforts within the field of energy science. This area of investigation encompasses a wide range of subjects, with a particular emphasis on emerging concerns like environmental factors and pollution.
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