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터빈 블레이드 온도 변화를 고려한 증기분사 가스터빈 열병합발전 시스템의 성능해석
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  • 터빈 블레이드 온도 변화를 고려한 증기분사 가스터빈 열병합발전 시스템의 성능해석
저자명
강수영,김정호,김동섭,Kang. Soo Young,Kim. Jeong Ho,Kim. Tong Seop
간행물명
유체기계저널
권/호정보
2012년|15권 6호|pp.18-24 (7 pages)
발행정보
한국유체기계학회
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기타
이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

This study simulated the operation of a steam injected gas turbine combined heat and power (CHP) system. A full off-design analysis was carried out to examine the change in the turbine blade temperature caused by steam injection. The prediction of turbine blade temperature was performed for the operating modes suggested in the previous study where the limitation of compressor surge margin reduction was analyzed in the steam injected gas turbine. It was found that both the fully injected and partially injected operations suggested in the previous study would cause the blade temperature to exceed that of the pure CHP operation and the under-firing operation would provide too low blade temperature. An optimal operation was proposed where both the turbine inlet temperature and the injection amount were modulated to keep both the reference turbine blade temperature and the minimum compressor surge margin. The modulation was intended to maintain a stable compressor operation and turbine life. It was shown that the optimal operation would provide a larger power output than the under-firing operation and a higher efficiency than the original partially injected operation.