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저공해 성능 개량을 위한 5㎿급 가스터빈용 연소기 시험
박부민(Poomin Park),김형모(Hyungmo Kim),최채홍(Chaehong Choi),이춘식(Chunsik Lee),양수석(Sooseok Yang) 한국연소학회 2009 KOSCOSYMPOSIUM논문집 Vol.- No.39
A combustor for 5MW class gasturbine engine nearly has been developed. 8 can-type combustors are installed in the engine and have radial swirlers to premix air and natural gas. the combustor performance tests was carried out at the test facility in KARI(Korea Aerospace Research Institute). its designed performance target had been achieved in previous tests but some tests to get more improvement in low emission still have been performing with small revisions on the combustor. The characteristics of combustor were measured including emission and exit temperature distribution.