Numerical Study of Ignition and Combustion of Hydrogen-Enriched Methane in a Sequential Combustor
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Date
2024-04Type
- Journal Article
ETH Bibliography
yes
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Abstract
gnition and combustion behavior in the second stage of a sequential combustor are investigated numerically at atmospheric pressure for pure CH₄ fueling and for two CH₄-H₂ fuel blends in 24:1 and 49:1 mass ratios , respectively, using Large Eddy Simulation (LES). Pure CH₄ fueling results in a turbulent propagating flame anchored by the hot gas recirculation zones developed near the inlet of the sequential combustion chamber. As the H₂ content increases, the combustion process changes drastically, with multiple auto-ignition kernels produced upstream of the main flame brush. Analysis of the explosive modes indicates that, for the highest H₂ amount investigated, flame stabilization in the combustion chamber is strongly supported by auto-ignition chemistry. The analysis of fuel decomposition pathways highlights that radicals advected from the first stage flame, in particular OH, induce a rapid fuel decomposition and cause the reactivity enhancement that leads to auto-ignition upstream of the sequential flame. This behavior is promoted by the relatively large mass fraction of OH radicals found in the flow reaching the second stage, which is approximately one order of magnitude greater than it would be at chemical equilibrium. The importance of the out-of-equilibrium vitiated air on the ignition behavior is proven via an additional LES that features weak auto-ignition kernel formation when equilibrium is artificially imposed. It is therefore concluded that parameters affecting the relaxation towards chemical equilibrium of the vitiated flow can have an important influence on the operability of sequential combustors fueled with varying fractions of H₂ blending. Show more
Permanent link
https://doi.org/10.3929/ethz-b-000668697Publication status
publishedExternal links
Journal / series
Flow, Turbulence and CombustionVolume
Pages / Article No.
Publisher
SpringerSubject
Sequential combustor; Hydrogen blending; Turbulent combustion; Gas turbine for power generation; Combustion regimeFunding
820091 - ThermoacOustic instabilities contRol in sequential Combustion cHambers (EC)
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ETH Bibliography
yes
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