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난류 예혼합 연소기에서의 흡입 유동 섭동에 대한 화염의 동적 거동

Flame Dynamic Response to Inlet Flow Perturbation in a Turbulent Premixed Combustor

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This paper describes the forced flame response in a turbulent premixed gas turbine combustor. The fuel was premixed with the air upstream of a choked inlet to avoid equivalence ratio fluctuations. To impose the inlet flow velocity, a siren type modulation device was developed using an AC motor, rotating and static plates. Measurements were made of the velocity fluctuation in the nozzle using hot wire anemometry and of the heat release fluctuation in the combustor using chemiluminescence emission. The test results showed that flame length as well as geometry was strongly dependent upon modulation frequency in addition to operating conditions such as inlet velocity. Convection delay time between the velocity perturbation and heat release fluctuations was calculated using phase information of the transfer function, which agreed well with the results of flame length measurements. Also, basic characteristics of the flame nonlinear response shown in the current test conditions were introduced

Abstract

This paper describes the forced flame response in a turbulent premixed gas turbine combustor. The fuel was premixed with the air upstream of a choked inlet to avoid equivalence ratio fluctuations. To impose the inlet flow velocity, a siren type modulation device was developed using an AC motor, rotating and static plates. Measurements were made of the velocity fluctuation in the nozzle using hot wire anemometry and of the heat release fluctuation in the combustor using chemiluminescence emission. The test results showed that flame length as well as geometry was strongly dependent upon modulation frequency in addition to operating conditions such as inlet velocity. Convection delay time between the velocity perturbation and heat release fluctuations was calculated using phase information of the transfer function, which agreed well with the results of flame length measurements. Also, basic characteristics of the flame nonlinear response shown in the current test conditions were introduced

참고문헌 (7)

  1. Ducruix, S., "Combustion dynamics and instabilities: elementary coupling and driving mechanisms", Journal of Propulsion and Power, 19(5), pp.722~734 (2003)
  2. Lieuwen, T., "Modeling premixed combustionacoustic wave interactions: a review", Journal of Propulsion and Power, 19(5), pp.765~781 (2003)
  3. Balachandran, R., "Experimental investigation of the nonlinear response of turbulent premixed flames to imposed inlet velocity oscillations", Combustion and Flame, 143, pp.37~55 (2005)
  4. Kim, D., "Effect of flame structure on the flame transfer function in a premixed gas turbine combustor", Journal of Engineering for Gas Turbine and Power, 132 (2010)
  5. Dasch, C. J., "One-dimensional tomography: a comparison of Abel, onion-peeling, and filtered backprojection methods", Applied Optics, 31(8), pp.1146~1152 (1992)
  6. A study of combustion instabilities driven by flame-vortex interactions, "Gonzalez, E.", ~, pp.AIAA paper 2005-4330
  7. Bellows, B. D., "Nonlinear flame transfer function characteristics in a swirl-stabilized combustor", Journal of Engineering for Gas Turbines and Power, 129(4), pp.954~961 (2007)

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