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RISS 인기검색어
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- 저자 : Alexander Bograd (검색결과 2 건)
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DaiKi Min,Alexander M. Bograd 한국유체기계학회 1998 유체기계 연구개발 발표회 논문집 Vol.- No.-
The recent results of the engine development performed in this year on Turbogreen 1200, the first industrial gas turbine engine developed in Korea, are presented. In order to improve the engine performance and structural stability from the first prototype engine, several variants of the engine and major components such as combustor and rotor assembly have been developed and tested. This paper shows these results especially focused on the engine test and performance analysis, in which test system, instrumentation and data processing are discussed as well. The engine performance and its trend give relatively good coincidence with the design ones. At design power of 1.2㎿, the thermal efficiency of the engine is estimated over 25% which is below the design target of 27.2%. This gap of efficiency is caused mainly by large tip clearance between turbine blades and casing. Considering high design efficiency superior to those of other competitive engines in this power class, Turbogreen 1200 would have a strong competition in its performance if the design efficiency is achieved by further developments such as tip clearance control, which are very possible and natural in final mass production of the developed gas turbine engine.
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박준철(Juncheol Park),홍성진(Sungjin Hong),Alexander Bograd,류제욱(Jewook Ryu) 한국추진공학회 2010 한국추진공학회 학술대회논문집 Vol.2010 No.11
두산중공업(주)에서 개발 중인 발전용 가스터빈 DGT-5 엔진의 작동 특성을 평가하였다. 다양한 연료 스케쥴과 여러 가지 조합의 bleed valve 개폐 제어에 대한 영향을 분석하기 위한 시험을 통해 시동 특성을 개선하였고, 시동부터 부하운전 전체 작동 영역에서 압축기에서의 불안정 현상 없이 엔진이 안정적으로 작동됨을 확인하였다. 순간적인 부하 변동과 load rejection에 대한 엔진의 동적 거동 분석을 통해 실제 계통 병입 조건에서 급격한 부하변동 시 엔진이 안정적으로 제어될 수 있음을 확인하였다. Operating characteristics of DGT-5 being developed by Doosan Heavy Industries & Construction Co., Ltd. for power generation service was evaluated. Starting behavior was improved by a series of tests to investigate the effect of various fuel schedule and several combination of bleed valve control. The engine showed stable operation without any instability of compressor in the full operating regime covering from start-up to load conditions. If there is a rapid change of load in the condition of synchronization to Grid, the engine can be controlled stably based on the analysis of dynamic responses of the engine to an rapid load change and a sudden load rejection.
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