Effect of Swirl Angles in Low-Swirl Combustor

저선회 연소기의 선회각도에 따른 영향

  • 정황희 (순천대학교 우주항공공학과) ;
  • 최인찬 (두산중공업(주) 가스터빈개발팀) ;
  • 이기만 (순천대학교 기계.우주항공공학부)
  • Published : 2015.12.10

Abstract

A study has been conducted to investigate the effect of swirl angle in low swirl combustor. In this study, the employed swirl angles were $28^{\circ}$, $32^{\circ}$ and $37^{\circ}$. Direct flame photos show that the width of the flame is expanded and the length of the flame is shortened when swirl angle is increased. Also, as the swirl angle was increased, the flame stability region could be widened due to the expansion of lower flammable limit. Between 3 and 7kW, CO emissions was below 10 ppm and NOx emissions was also below 27 ppm at $O_2$ 15% basis over the lean burning range of 0.6 < ${\Phi}$ < 0.9. From this investigation of stability expansion effect and emission performance, it was identified that the swirl angle $37^{\circ}$ is most suitable swirling condition in the low swirl model combustor.

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