Author
Listed:
- Ziyan Li
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)
- Xiaoyan Zhang
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)
- Kaixing Wang
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)
- Fuqiang Liu
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China
Qingdao Institute of Aeronautical Technology, Qingdao 266500, China)
- Changlong Ruan
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
Qingdao Institute of Aeronautical Technology, Qingdao 266500, China)
- Jinhu Yang
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
Qingdao Institute of Aeronautical Technology, Qingdao 266500, China)
- Yong Mu
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
Qingdao Institute of Aeronautical Technology, Qingdao 266500, China)
- Cunxi Liu
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)
- Gang Xu
(Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing 100049, China
National Key Laboratory of Science and Technology on Advanced Light-Duty Gas-Turbine, Beijing 100190, China)
Abstract
This experimental study investigated the influence of different turbine guide vane parameters on the ignition limit and light-round processes in a triple-dome combustor. It was found that for the triple-dome combustor, the minimum fuel/air ratios at the ignition limit all show a trend of initial decrease followed by subsequent increase with the growth of incoming air mass flow rate. The ignition fuel/air ratio decreases with the increase in turbine blockage ratio, and the optimal scheme is achieved with a blockage ratio of 0.8. Under the condition where the incoming air mass flow rate is 0.089 kg/s, the light-round time decreases with the increase in fuel/air ratio, and the light-round time of the combustor without guide vanes is shorter than that of the other schemes. With the increase in incoming air mass flow rate, the light-round time of the schemes with guide vanes is shortened. Under the same incoming air mass flow rate and fuel/air ratio, the increase in the blockage ratio will lead to an increase in the light-round time of the triple-dome combustor.
Suggested Citation
Ziyan Li & Xiaoyan Zhang & Kaixing Wang & Fuqiang Liu & Changlong Ruan & Jinhu Yang & Yong Mu & Cunxi Liu & Gang Xu, 2024.
"The Effects of Turbine Guide Vanes on the Ignition Limit and Light-Round Process of a Triple-Dome Combustor,"
Energies, MDPI, vol. 17(18), pages 1-10, September.
Handle:
RePEc:gam:jeners:v:17:y:2024:i:18:p:4636-:d:1479643
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