본문 바로가기
KERD
논문KCI 등재

LNG 연료를 이용한 가스 터빈 연소기의 연소유동 해석

Analysis of Combustion Flow of LNG-Fueled Gas Turbine Swirl Burner

1

조회

0

다운로드

1

인용

0

참고문헌

키워드

초록

Two- and Three- dimensional numerical simulations are carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation using imported and domestic natural gases. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the numerical results with the flow conditions selected from the gas turbine operation data. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well. The flow structures of the recirculation and combustion region was understood from the comparison of the two- and three-dimensional results. The complexity of the three-dimensional swirl flows inside the gas turbine combustor with multiple swirlers was understood those resulting from the interactions of the stage and pilot burners.

Abstract

Two- and Three- dimensional numerical simulations are carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation using imported and domestic natural gases. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the numerical results with the flow conditions selected from the gas turbine operation data. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well. The flow structures of the recirculation and combustion region was understood from the comparison of the two- and three-dimensional results. The complexity of the three-dimensional swirl flows inside the gas turbine combustor with multiple swirlers was understood those resulting from the interactions of the stage and pilot burners.

참고문헌 (10)

  1. Broda, J. C., "An Experimental Study of Combustion Dynamics of a Premixed Swirl Injector", Proceedings of the Combustion Institute, 27(2), pp.1849~1856 (1998)
  2. Ikeda, Y., ""Flow Structure in a Can-type Model Gas Turbine Combustor", JSME, 535, pp.1175~1182 (1991)
  3. Terasaki, T., "The Effects of Fuel-Air mixing on NOx Formulation in Non-Premixed Swirl Burner", Proceedings of the Combustion Institute, 26(2), pp.2733~2739 (1996)
  4. 이강엽, "2중스월류에 의한 난류분무화염의 연소특성 연구", 한국연소학회지, 5(1) (2000)
  5. Chang, Y. J., "A Study on the Effects of Swirling and Recirculation on the Combustion in a Non-Premixed Flate Flame", Proceedings of the PNU-LGE Tianjin Joint Workshop, pp.1~17 (2005)
  6. Computer Program for Calculation of Complex Chemical Equilibrium Composition and Applications, "Gordon, S.", NASA, ~ (1994)
  7. 신재렬, "화학 평형과 열복사를 고려한 로켓 플룸 유동 해석", 한국추진공학회지, 9(1), pp.35~46 (2005)
  8. Chemkin-II: A Fortran Chemical Kinetics Package for the Analysis of Gas Phase Chemical Kinetics, "Kee, R. J.", Gov. Pub., ~ (1989)
  9. "Fluent 6.1 User’s Guide, Vol. I, II, III.", ~

관련 논문AI추천

이 간행물의 다른 논문 (4건)