Experimental and numerical study of the micromix combustion principle applied for hydrogen and hydrogen-rich syngas as fuel with increased energy density for industrial gas turbine applications
- The Dry Low NOx (DLN) Micromix combustion principle with increased energy density is adapted for the industrial gas turbine APU GTCP 36-300 using hydrogen and hydrogen-rich syngas with a composition of 90%-Vol. hydrogen (H₂) and 10%-Vol. carbon-monoxide (CO). Experimental and numerical studies of several combustor geometries for hydrogen and syngas show the successful advance of the DLN Micromix combustion from pure hydrogen to hydrogen-rich syngas. The impact of the different fuel properties on the combustion principle and aerodynamic flame stabilization design laws, flow field, flame structure and emission characteristics is investigated by numerical analysis using a hybrid Eddy Break Up combustion model and validated against experimental results.
Author: | Harald FunkeORCiD, J. Dickhoff, Jan Keinz, H. A. Anis, A. Parente, P. Hendrick |
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DOI: | https://doi.org/10.1016/j.egypro.2014.12.201 |
ISSN: | 1876-6102 (E-Journal) |
Parent Title (English): | Energy procedia |
Publisher: | Elsevier |
Place of publication: | Amsterdam |
Document Type: | Article |
Language: | English |
Year of Completion: | 2014 |
Issue: | 61 |
First Page: | 1736 |
Last Page: | 1739 |
Link: | https://doi.org/10.1016/j.egypro.2014.12.201 |
Zugriffsart: | weltweit |
Institutes: | FH Aachen / Fachbereich Luft- und Raumfahrttechnik |
open_access (DINI-Set): | open_access |
collections: | Verlag / Elsevier |
Open Access / Gold | |
Licence (German): | Creative Commons - Namensnennung-Nicht kommerziell-Keine Bearbeitung |