Experimental Investigation of Pure Hydrogen Flame in a Matrix Micro-Mixing Combustor

Pure hydrogen combustion is a critical pathway to achieving zero-carbon emissions for the gas turbine industry. Micro-mixing combustion is one of the most widely attractive hydrogen combustion methods in gas turbines. This study investigates pure hydrogen flame in a 3 × 3 matrix micro-mix combustor. The setup includes nine micro-mix injectors, each equipped with a bluff body and a hydrogen injection tube. The OH* chemiluminescence imaging and PIV (Particle Image Velocimetry) techniques were employed to visualize the single- and triple-flame morphology and flow field under various operating conditions. The results show that equivalence ratio, flow rate, and air injector exit angle can influence the flame structure and combustion characteristics, providing an insightful understanding of micro-mix pure hydrogen combustion.

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Publication Details

Journal
Aerospace
Published
2025-05-23
DOI
https://doi.org/10.3390/aerospace12060464
Citations
2
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
9.99

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article

Experimental Investigation of Pure Hydrogen Flame in a Matrix Micro-Mixing Combustor

Xi Xia, Xiaojing Tian, Zhenzhen Feng, Fei Qi et al.
2 citations
Aerospace
Rocket and propulsion systems research
9.99
article

Experimental Investigation of Pure Hydrogen Flame in a Matrix Micro-Mixing Combustor

Xi Xia, Xiaojing Tian, Zhenzhen Feng, Fei Qi, Liangliang Xu
article en
2 citations

Abstract

Pure hydrogen combustion is a critical pathway to achieving zero-carbon emissions for the gas turbine industry. Micro-mixing combustion is one of the most widely attractive hydrogen combustion methods in gas turbines. This study investigates pure hydrogen flame in a 3 × 3 matrix micro-mix combustor. The setup includes nine micro-mix injectors, each equipped with a bluff body and a hydrogen injection tube. The OH* chemiluminescence imaging and PIV (Particle Image Velocimetry) techniques were employed to visualize the single- and triple-flame morphology and flow field under various operating conditions. The results show that equivalence ratio, flow rate, and air injector exit angle can influence the flame structure and combustion characteristics, providing an insightful understanding of micro-mix pure hydrogen combustion.

AerospaceVol. 12(6)
Shanghai Jiao Tong University (CN), Dongfang Electric Corporation (China) (CN)
National Natural Science Foundation of China
Openalex Percentile: Top 3%
Rocket and propulsion systems research
9.99
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