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Combustion and emissions characteristics of dual-channel double-vortex combustion for gas turbine engines

Author

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  • Zhang, R.C.
  • Fan, W.J.
  • Shi, Q.
  • Tan, W.L.

Abstract

A vortex combustor is a novel gas turbine combustor that uses staged combustion technology. Research examining the combustion organization method of the pilot combustion zone and the mainstream combustion zone is an important component of the design of the structure of a vortex combustor. In this paper, a new type of single-cavity vortex combustor fueled with aviation kerosene is presented. A double-vortex flow field structure and an evaporation tube for the fuel supply are used in the pilot zone. The flow-field structure of a double recirculation zone and a pneumatic atomization injector for the fuel supply are used in the mainstream combustion zone. The combustion experiment was performed under atmospheric pressure. The influence of the air-flow parameters, fuel parameters and staged method on the combustion performance and the characteristics of the pollutant emissions were studied in detail. Research indicates that the inlet temperature and the staged method primarily influence the ignition limit, lean blowout, combustion efficiency, temperature distribution of the outlet and pollutant emissions. The equivalence ratio primarily influences the temperature distribution of the wall and pollutant emissions. The inlet velocity influences the total pressure loss of the combustor.

Suggested Citation

  • Zhang, R.C. & Fan, W.J. & Shi, Q. & Tan, W.L., 2014. "Combustion and emissions characteristics of dual-channel double-vortex combustion for gas turbine engines," Applied Energy, Elsevier, vol. 130(C), pages 314-325.
    • Handle: RePEc:eee:appene:v:130:y:2014:i:c:p:314-325
    DOI: 10.1016/j.apenergy.2014.05.059
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    References listed on IDEAS

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    Cited by:

    1. Zhang, Rongchun & Xu, Quanyong & Fan, Weijun, 2018. "Effect of swirl field on the fuel concentration distribution and combustion characteristics in gas turbine combustor with cavity," Energy, Elsevier, vol. 162(C), pages 83-98.
    2. Jin, Yi & Li, Yefang & He, Xiaomin & Zhang, Jingyu & Jiang, Bo & Wu, Zejun & Song, Yaoyu, 2014. "Experimental investigations on flow field and combustion characteristics of a model trapped vortex combustor," Applied Energy, Elsevier, vol. 134(C), pages 257-269.
    3. Fu, Zaiguo & Sui, Lichao & Lu, Jin & Liu, Jiang & Weng, Peifen & Zeng, Zhuoxiong & Pan, Weiguo, 2023. "Investigation on effects of hydrogen addition to the thermal performance of a traditional counter-flow combustor," Energy, Elsevier, vol. 262(PA).
    4. Chen, Longfei & Zhang, Zhichao & Lu, Yiji & Zhang, Chi & Zhang, Xin & Zhang, Cuiqi & Roskilly, Anthony Paul, 2017. "Experimental study of the gaseous and particulate matter emissions from a gas turbine combustor burning butyl butyrate and ethanol blends," Applied Energy, Elsevier, vol. 195(C), pages 693-701.
    5. Li, Mingyu & Wang, Qian & He, Xiaomin & Xiao, Jiankun & Ma, Heng, 2022. "Effects of fuel injection on the combustion and emission performance of a trapped vortex combustor," Energy, Elsevier, vol. 252(C).
    6. Zhang, R.C. & Bai, N.J. & Fan, W.J. & Huang, X.Y. & Fan, X.Q., 2019. "Influence of flame stabilization and fuel injection modes on the flow and combustion characteristics of gas turbine combustor with cavity," Energy, Elsevier, vol. 189(C).
    7. Zhang, R.C. & Bai, N.J. & Fan, W.J. & Yan, W.H. & Hao, F. & Yin, C.M., 2018. "Flow field and combustion characteristics of integrated combustion mode using cavity with low flow resistance for gas turbine engines," Energy, Elsevier, vol. 165(PA), pages 979-996.
    8. Zhang, R.C. & Fan, W.J. & Xing, F. & Song, S.W. & Shi, Q. & Tian, G.H. & Tan, W.L., 2015. "Experimental study of slight temperature rise combustion in trapped vortex combustors for gas turbines," Energy, Elsevier, vol. 93(P2), pages 1535-1547.
    9. Zhang, R.C. & Huang, X.Y. & Fan, W.J. & Bai, N.J., 2019. "Influence of injection mode on the combustion characteristics of slight temperature rise combustion in gas turbine combustor with cavity," Energy, Elsevier, vol. 179(C), pages 603-617.
    10. Zhao, Yuling & He, Xiaomin & Li, Mingyu, 2020. "Effect of mainstream forced entrainment on the combustion performance of a gas turbine combustor," Applied Energy, Elsevier, vol. 279(C).
    11. Shen, Wenkai & Liu, Li & Hu, Qiming & Liu, Guichuang & Wang, Jiwei & Zhang, Ning & Wu, Shaohua & Qiu, Penghua & Song, Shaowei, 2021. "Combustion characteristics of ignition processes for lean premixed swirling combustor under visual conditions," Energy, Elsevier, vol. 218(C).
    12. Zhang, R.C. & Hao, F. & Fan, W.J., 2018. "Combustion and stability characteristics of ultra-compact combustor using cavity for gas turbines," Applied Energy, Elsevier, vol. 225(C), pages 940-954.
    13. Li, Mingyu & He, Xiaomin & Zhao, Yuling & Jin, Yi & Yao, Kanghong & Ge, Zhenghao, 2018. "Performance enhancement of a trapped-vortex combustor for gas turbine engines using a novel hybrid-atomizer," Applied Energy, Elsevier, vol. 216(C), pages 286-295.
    14. Miao, Junjie & Fan, Yuxin & Wu, Weiqiu & Zhao, Shilong, 2021. "Effect of air-assistant on ignition and flame-holding characteristics in a cavity-strut based combustor," Applied Energy, Elsevier, vol. 283(C).

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