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특허 상세정보

System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/18    F02C-003/34    F02C-007/141   
출원번호 US-0456575 (2012-04-26)
등록번호 US-9784185 (2017-10-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fletcher Yoder P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 526
초록

A system for cooling a gas turbine with an exhaust gas provided by the gas turbine generally includes an exhaust gas recirculation system including an exhaust gas scrubber. The exhaust gas recirculation system is disposed downstream from the gas turbine and may receive at least a portion of the exhaust gas provided by the gas turbine. The system may also include a moisture separator located downstream from the exhaust gas recirculation system, and a cooling circuit configured to connect to one or more cooling circuit inlets. The one or more cooling circu...

대표
청구항

1. A system, comprising: an exhaust gas path configured to receive at least a portion of an exhaust gas provided by a gas turbine;an exhaust gas scrubber fluidly coupled to the exhaust gas path;a moisture separator fluidly coupled to the exhaust gas path; anda cooling circuit fluidly coupled to the exhaust gas path downstream from the exhaust gas scrubber and the moisture separator, wherein the cooling circuit is configured to fluidly couple to a plurality of cooling paths through the gas turbine, wherein the plurality of cooling paths is separate from a...

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