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자발광 계측 결과와 EDMD 기법을 적용한 가스터빈 연소기의 연소불안정성 분석

Chemi-luminescence Measurement and Exact Dynamic Mode Decomposition for Combustion-Instability Analysis in a Gas Turbine Combustor

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초록

To analyze combustion instability in the combustor of a gas turbine, the results of chemi-luminescence measurement are applied for the exact dynamic mode decomposition (EDMD) as hydrogen blending ratio, pilot split ratio, and operating pressure. The resonant frequencies obtained using fast Fourier transform (FFT) and EDMD are compared to confirm the growth rate and mode shape. The effect of hydrogen blending ratio, pilot split ratio, and pressure on the combustion instability was confirmed by comparing these results and used for analysis of combustion instability.

Abstract

To analyze combustion instability in the combustor of a gas turbine, the results of chemi-luminescence measurement are applied for the exact dynamic mode decomposition (EDMD) as hydrogen blending ratio, pilot split ratio, and operating pressure. The resonant frequencies obtained using fast Fourier transform (FFT) and EDMD are compared to confirm the growth rate and mode shape. The effect of hydrogen blending ratio, pilot split ratio, and pressure on the combustion instability was confirmed by comparing these results and used for analysis of combustion instability.

참고문헌 (8)

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