An experimental study was conducted in the lean-premixed swirl-stabilized combustor at atmospheric pressure and temperature in order to analyze the pressure oscillation in occurrence of the combustion instability. The fluctuating pressure signals exhibited as non-stationary signals. A new method using Hilbert-Huang transform(HHT) based on empirical mode decomposition(EMD) and intrinsic mode function(IMF) reconstruction was investigated. This method was applied to demonstrate the characteristics of pressure oscillations in the lean-premixed combustor when the equivalent ratio was at 0.71 and 0.80. The pulsating signals were decomposed with EMD
and IMF containing specific frequencies was obtained. Through the HHT and statistical analysis
the instantaneous frequency of the IMF was analyzed. The results show that the pressure oscillations display the characteristics of intermittent pulsating
and present the beat at the equivalent ratio of 0.71; whereas at the equivalent of ratio 0.80
the pressure oscillations feature the limit cycle. The validity of this method proves that the IMF reflects the inherent mode when the combustion instability occurs
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Related Author
Pei HE
Xiaoxing FENG
Xiangyang DENG
Jingjing JIANG
Xianzhi GAO
ZHUANG Fengchen
TAN Yonghua
WANG Guangxu
Related Institution
Commercial Aircraft Engine Company Limited,Aero Engine Corporation of China
中国航天科技集团有限公司 航天推进技术研究院 西安航天动力研究所 液体火箭发动机技术重点实验室
中国航天科技集团有限公司 航天推进技术研究院
浙江工业大学 机械工程学院 能源与动力工程研究所
Science and Technology on Liquid Rocket Engine Laboratory, Xi'an Aerospace Propulsion Institute, Academy of Aerospace Propulsion Technology, China Aerospace Science and Technology Corporation