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Study on the Dynamic Combustion Characteristics of a Staged High-Temperature Rise Combustor

Author

Listed:
  • Meng Li

    (Fluid Machinery Engineering Technology Research Center, Jiangsu University, Zhenjiang 212013, China
    Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
    National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)

  • Jinhu Yang

    (Qingdao Aeronautical Technology Research Institute, Qingdao 266000, China)

  • Cunxi Liu

    (Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
    National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)

  • Fuqiang Liu

    (Qingdao Aeronautical Technology Research Institute, Qingdao 266000, China)

  • Kaixing Wang

    (Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
    National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)

  • Changlong Ruan

    (Qingdao Aeronautical Technology Research Institute, Qingdao 266000, China)

  • Yong Mu

    (Qingdao Aeronautical Technology Research Institute, Qingdao 266000, China)

  • Gang Xu

    (Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
    National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)

Abstract

Currently, steady-state analysis predominates in combustion chamber design, while dynamic combustion characteristics remain underexplored, and there is a lack of a comprehensive index system to assess dynamic combustion behavior. This study conducts a numerical simulation of the dynamic characteristics of the combustion chamber, employing a method combining large eddy simulation (LES) and Flamelet Generated Manifold (FGM). The inlet air temperature, air flow rate, and fuel flow rate were varied by 1%, 2%, and 3%, respectively, with a pulsation period of 0.008 s. The effects of nine different inlet parameter pulsations on both time-averaged and instantaneous combustion performance were analyzed and compared to benchmark conditions. The results indicate that small pulsations in the inlet parameters have minimal impact on the steady-state time-averaged performance. In the region near the cyclone outlet, which corresponds to the flame root area, pronounced unsteady flame characteristics were observed. Fluctuations in inlet parameters led to an increase in temperature fluctuations near the flame root. Analysis of the outlet temperature results for each operating condition reveals that inlet parameter fluctuations can mitigate the inherent combustion instability of the combustion chamber and reduce temperature fluctuations at the outlet hot spot.

Suggested Citation

  • Meng Li & Jinhu Yang & Cunxi Liu & Fuqiang Liu & Kaixing Wang & Changlong Ruan & Yong Mu & Gang Xu, 2025. "Study on the Dynamic Combustion Characteristics of a Staged High-Temperature Rise Combustor," Energies, MDPI, vol. 18(3), pages 1-20, January.
  • Handle: RePEc:gam:jeners:v:18:y:2025:i:3:p:662-:d:1581134
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