TY - GEN
T1 - INVESTIGATION OF PRESSURE EFFECTS ON COMBUSTION CHARACTERISTICS OF HYDROGEN ANNULAR MICRO-MIXING NOZZLES
AU - Liu, Jian
AU - Qiu, Penghua
AU - Wang, Xiyu
AU - Hu, Qiming
AU - Liu, Li
AU - Zhang, Linyao
AU - Xing, Chang
N1 - Publisher Copyright:
© 2024 by ASME.
PY - 2024
Y1 - 2024
N2 - In pursuit of achieving near-zero emissions and preventing flashback, micro-mixing combustion technology has been developed and implemented in hydrogen gas turbines. This investigation proposed an annular micro-mixing nozzles comprising seven annular nozzles arranged in a regular hexagonal pattern. Experimental investigations based on OH* Chemiluminescence with OH-PLIF synchronous measurement technique were performed. Results indicate that with increasing pressure, the flames become smaller and shorter, and the interaction between flames weakens compared to atmospheric pressure. At higher pressures, the flames predominantly rely on the bluff bodies of the annular nozzles for stability. This leads to a more concentrated flame reaction zone, increased local heat release, and an exponential increment in NO emissions. However, the experiments reveal that at combustion pressures equal to or below 0.2 MPa., NO emissions under the test conditions remain below 10ppm(@15%O2).
AB - In pursuit of achieving near-zero emissions and preventing flashback, micro-mixing combustion technology has been developed and implemented in hydrogen gas turbines. This investigation proposed an annular micro-mixing nozzles comprising seven annular nozzles arranged in a regular hexagonal pattern. Experimental investigations based on OH* Chemiluminescence with OH-PLIF synchronous measurement technique were performed. Results indicate that with increasing pressure, the flames become smaller and shorter, and the interaction between flames weakens compared to atmospheric pressure. At higher pressures, the flames predominantly rely on the bluff bodies of the annular nozzles for stability. This leads to a more concentrated flame reaction zone, increased local heat release, and an exponential increment in NO emissions. However, the experiments reveal that at combustion pressures equal to or below 0.2 MPa., NO emissions under the test conditions remain below 10ppm(@15%O2).
KW - Annular nozzles
KW - Flames interactions
KW - Hydrogen flames
KW - Micro-mixing nozzles
KW - Pressurized air
UR - https://www.scopus.com/pages/publications/85206114728
U2 - 10.1115/GT2024-123935
DO - 10.1115/GT2024-123935
M3 - 会议稿件
AN - SCOPUS:85206114728
T3 - Proceedings of the ASME Turbo Expo
BT - Combustion, Fuels, and Emissions
PB - American Society of Mechanical Engineers (ASME)
T2 - 69th ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition, GT 2024
Y2 - 24 June 2024 through 28 June 2024
ER -