A study of Overall Combustion Characteristics according to the Air Preheated Temperature in a Hybrid/Dual Swirl Jet Combustor

하이브리드/이중 선회제트 연소기에서 공기 예열온도에 의한 배출 특성 연구

  • 최인찬 (순천대학교 우주항공공학전공) ;
  • 조준익 (순천대학교 우주항공공학전공) ;
  • 이기만 (순천대학교 기계우주항공공학부)
  • Published : 2012.11.30

Abstract

The laboratory experiments have been conducted to investigate the effects of air preheated temperature on the emission characteristics by a model gas turbine burner with a hybrid/dual swirl jet flames configuration. The concentration of NOx and CO emissions, and flue gas temperature at combustor exit were measured with varying the equivalence ratio for different air preheated temperatures of 300, 400, 500K at atmospheric pressure. It was overall shown that the NOx and CO emissions, and flue gas temperature were decreased according to the decreasing of equivalence ratio due to the effects of lean premixed combustion regardless of the air preheated temperature. Experimental results of a lean premixed flames configuration indicated that the NOx emission was increased with higher inlet air temperature and air flow rate, which is attributed to the increasing of flue gas temperature and heat release related to the thermal NOx mechanism. But the CO emission was shown the opposite tendency, that is, the CO emission was decreased with increasing of inlet air temperature and flow rate.

Keywords