화염거동을 통한 이중선회 가스터빈 모델 연소기에서 연소실 길이에 따른 연소 불안정성 이해

Combustion Instability Comprehension with Combustion Chamber Length in Dual Swirl Gas Turbine Model Combustor from Flame Behaviors

  • 장문석 (순천대학교 대학원 우주항공공학과) ;
  • 이기만 (순천대학교 기계우주항공공학부)
  • 발행 : 2015.12.10

초록

This study is to investigate the combustion instability of the variation of combustion chamber length in dual swirl gas turbine model combustor. When equivalence ratio was fixed at 1.1, as the length of the combustion chamber increases the value of the frequency decreased in 7kW while the value of the frequency was constant in 4kW. The analysis of flame behaviors by high speed camera was conducted to identify such trend.

키워드