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30 years of dry low NOx micromix combustor research for hydrogen-rich fuels: an overview of past and present activities

  • The paper presents an overview of the past and present of low-emission combustor research with hydrogen-rich fuels at Aachen University of Applied Sciences. In 1990, AcUAS started developing the Dry-Low-NOx Micromix combustion technology. Micromix reduces NOx emissions using jet-in-crossflow mixing of multiple miniaturized fuel jets and combustor air with an inherent safety against flashback. At first, pure hydrogen as fuel was investigated with lab-scale applications. Later, Micromix prototypes were developed for the use in an industrial gas turbine Honeywell/Garrett GTCP-36-300, proving low NOx characteristics during real gas turbine operation, accompanied by the successful definition of safety laws and control system modifications. Further, the Micromix was optimized for the use in annular and can combustors as well as for fuel-flexibility with hydrogen-methane-mixtures and hydrogen-rich syngas qualities by means of extensive experimental and numerical simulations. In 2020, the latest Micromix application will be demonstrated in a commercial 2 MW-class gas turbine can-combustor with full-scale engine operation. The paper discusses the advances in Micromix research over the last three decades.

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Metadaten
Author:Harald FunkeORCiD, Nils Beckmann, Jan Keinz, Atsushi Horikawa
DOI:https://doi.org/10.1115/GT2020-16328
ISBN:978-0-7918-8413-3
Parent Title (English):Conference Proceedings Turbo Expo: Power for Land, Sea and Air, Volume 4B: Combustion, Fuels, and Emissions
Publisher:ASME
Place of publication:New York, NY
Document Type:Conference Proceeding
Language:English
Year of Completion:2021
Date of first Publication:2021/01/11
Date of the Publication (Server):2021/02/15
Tag:Emissions; Fuel-flexibility; Hydrogen; Micromix; NOx
Length:14 Seiten
Note:
ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition
September 21–25, 2020, Virtual, Online
Note:
Paper No. GT2020-16328, V04BT04A069
Link:https://doi.org/10.1115/GT2020-16328
Zugriffsart:bezahl
Institutes:FH Aachen / Fachbereich Luft- und Raumfahrttechnik