Combustion and emission performance of swirling-flow single trapped vortex combustor
The swirling-flow single trapped vortex combustor (SSTVC) provides a new design approach for aviation engine combustors, showing promising potential for achieving high-temperature rises or low emissions. However, current research on it is limited to demonstrating its feasibility and lacks further in...
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sg-ntu-dr.10356-1732712024-01-23T00:58:34Z Combustion and emission performance of swirling-flow single trapped vortex combustor Guo, Yuxi Gong, Cheng Huang, Yakun Duan, Fei He, Xiaomin School of Mechanical and Aerospace Engineering Engineering::Mechanical engineering Trapped Vortex Combustor Swirling Flow The swirling-flow single trapped vortex combustor (SSTVC) provides a new design approach for aviation engine combustors, showing promising potential for achieving high-temperature rises or low emissions. However, current research on it is limited to demonstrating its feasibility and lacks further investigation into its combustion organization, combustion, and emission characteristics. In this study, experiments are conducted to investigate the flow field, combustion, and emission characteristics of the SSTVC under 5 inlet reference velocities and 3 inlet temperatures. As the inlet reference velocities increase from 9.96 m/s to 14.95 m/s, noticeable changes are observed in the backflow velocity of the cavity, increasing from 33.8 m/s to 48.3 m/s. By combining the flow field structure and flame features, the combustion organization of the SSTVC is summarized. With an increase in the inlet reference velocities, the combustion efficiency remains almost unchanged initially at 95.75% and then increases to 96.55%. The outlet temperature distribution improves, with the pattern factor value decreasing from 0.23 to 0.14. The carbon monoxide emissions initially increased from 94.91 to 99.89 and then decreased to 88.80, the total unburned hydrocarbons decreased from 23.22 to 16.03, and the nitrogen oxide emissions showed no significant change. With an increase in the inlet temperature, all parameters improved, with the combustion efficiency increasing from 93.71% to 96.61%, the pattern factor decreasing from 0.26 to 0.12, and all emission parameters decreasing as well. This work was supported by the National Science and Technology Major Project. Yuxi gratefully acknowledges the financial support from the China Scholarship Council, NO.202206830122. 2024-01-23T00:58:34Z 2024-01-23T00:58:34Z 2024 Journal Article Guo, Y., Gong, C., Huang, Y., Duan, F. & He, X. (2024). Combustion and emission performance of swirling-flow single trapped vortex combustor. Applied Thermal Engineering, 236, 121678-. https://dx.doi.org/10.1016/j.applthermaleng.2023.121678 1359-4311 https://hdl.handle.net/10356/173271 10.1016/j.applthermaleng.2023.121678 2-s2.0-85173839945 236 121678 en Applied Thermal Engineering © 2023 Published by Elsevier Ltd. All rights reserved. |
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Engineering::Mechanical engineering Trapped Vortex Combustor Swirling Flow Guo, Yuxi Gong, Cheng Huang, Yakun Duan, Fei He, Xiaomin Combustion and emission performance of swirling-flow single trapped vortex combustor |
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The swirling-flow single trapped vortex combustor (SSTVC) provides a new design approach for aviation engine combustors, showing promising potential for achieving high-temperature rises or low emissions. However, current research on it is limited to demonstrating its feasibility and lacks further investigation into its combustion organization, combustion, and emission characteristics. In this study, experiments are conducted to investigate the flow field, combustion, and emission characteristics of the SSTVC under 5 inlet reference velocities and 3 inlet temperatures. As the inlet reference velocities increase from 9.96 m/s to 14.95 m/s, noticeable changes are observed in the backflow velocity of the cavity, increasing from 33.8 m/s to 48.3 m/s. By combining the flow field structure and flame features, the combustion organization of the SSTVC is summarized. With an increase in the inlet reference velocities, the combustion efficiency remains almost unchanged initially at 95.75% and then increases to 96.55%. The outlet temperature distribution improves, with the pattern factor value decreasing from 0.23 to 0.14. The carbon monoxide emissions initially increased from 94.91 to 99.89 and then decreased to 88.80, the total unburned hydrocarbons decreased from 23.22 to 16.03, and the nitrogen oxide emissions showed no significant change. With an increase in the inlet temperature, all parameters improved, with the combustion efficiency increasing from 93.71% to 96.61%, the pattern factor decreasing from 0.26 to 0.12, and all emission parameters decreasing as well. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Guo, Yuxi Gong, Cheng Huang, Yakun Duan, Fei He, Xiaomin |
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Article |
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Guo, Yuxi Gong, Cheng Huang, Yakun Duan, Fei He, Xiaomin |
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Guo, Yuxi |
title |
Combustion and emission performance of swirling-flow single trapped vortex combustor |
title_short |
Combustion and emission performance of swirling-flow single trapped vortex combustor |
title_full |
Combustion and emission performance of swirling-flow single trapped vortex combustor |
title_fullStr |
Combustion and emission performance of swirling-flow single trapped vortex combustor |
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Combustion and emission performance of swirling-flow single trapped vortex combustor |
title_sort |
combustion and emission performance of swirling-flow single trapped vortex combustor |
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2024 |
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https://hdl.handle.net/10356/173271 |
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