5MW 발전용 가스터빈 엔진 연소기 성능시험
Performance Test of 5MW Gas Turbine Engine Combustor
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다운로드
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참고문헌
키워드
초록
Performance test of 5MW class gasturbine combustor was carried out at combustor test facility of KARI(Korea Aerospace Research Institute). The combustor is dry low NOx type premixed combustor and fuel is natural gas. The characteristics of combustor were measured including emission, pressure pulsation and exit temperature distribution. Optimum operation point of combustor was found by changing parameters like fuel ratio between pilot and main burner. The test result showed that the combustor performance is sufficient to satisfy the gasturbine system requirement.
Abstract
Performance test of 5MW class gasturbine combustor was carried out at combustor test facility of KARI(Korea Aerospace Research Institute). The combustor is dry low NOx type premixed combustor and fuel is natural gas. The characteristics of combustor were measured including emission, pressure pulsation and exit temperature distribution. Optimum operation point of combustor was found by changing parameters like fuel ratio between pilot and main burner. The test result showed that the combustor performance is sufficient to satisfy the gasturbine system requirement.
참고문헌 (3)
- A.H.Lefebvre, "Gas Turbine Combustion" (1999), Taylor & Francis
- T. C. Lieuwen, "Combustion Instabilities in Gas Turbine Engine" (2005), AIAA
- 박부민, "가스터빈 연소기 성능시험", 35th KOSCO Symposium, pp.140~146 (2007)