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Prediction of ammonia ignition/quenching and emissions of NOx, NH3 and H2 in a non-premixed swirl combustor using the EDC model
被引:0
|作者:
Klimanek, Adam
[1
]
Adamczyk, Wojciech
[1
]
Sladek, Slawomir
[1
]
Fan, Yong
[2
]
Bothien, Mirko R.
[3
]
Gruber, Andrea
[4
]
Szlek, Andrzej
[1
]
机构:
[1] Silesian Tech Univ, Dept Thermal Technol, Konarskiego 22, PL-44100 Gliwice, Poland
[2] Natl Inst Adv Ind Sci & Technol, 1-1-1 Umezono, Tsukuba, Ibaraki 3058560, Japan
[3] Zurich Univ Appl Sci ZHAW, Inst Energy Syst & Fluid Engn, Technikumstr 9, CH-8401 Winterthur, Switzerland
[4] Sintef Energy Res, Div Energy Res, Sem Saelands 11, N-7034 Trondheim, Norway
关键词:
Numerical modeling;
Ammonia combustion;
Gas turbine;
CFD;
Flame quenching;
BURNING VELOCITY;
FLAMES;
OXIDATION;
LIMITS;
D O I:
10.1016/j.csite.2024.105670
中图分类号:
O414.1 [热力学];
学科分类号:
摘要:
The standard Eddy Dissipation Concept model with a modified San Diego mechanism was applied to account for nitrogen chemistry to predict ammonia flame quenching during lean non-premixed combustion in a swirl burner. This study examined the combustion of ammonia- air and ammonia-hydrogen-air flames within a two-stage swirl burner that can be used in a micro gas turbine rated at 50 kW. Various fuel energy inputs at different equivalence ratios were examined regarding flame quenching. The objective of this work was to present a series of experimental results to validate computational fluid dynamics model based on experimental data and determination of best operating conditions from the point of view of emission of pollutants. The results show that the applied San Diego mechanism, which predicts well the flame speeds in lean and stoichiometric conditions, along with the eddy decipation model can accurately predict the flame quenching at various fuel loads and is suitable for CFD simulations due to relatively small number of reactions. The results indicate that the inclusion of the radiation model and heat losses to the surroundings is necessary even for a small size combustor. Excluding the heat loss and radiation was the reason for predicting the quenching limit in much leaner conditions, especially for small fuel loads. This phenomenon was ascribed to the significantly greater impact of heat transfer (reduction in temperature) on the combustion at lower flow rates.
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页数:14
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