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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Gas turbine load control system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/22    F02C-001/00    F02C-003/34    F02C-009/48    F02C-009/52    F02C-009/54    F01D-015/10    F02C-001/08   
출원번호 US-0144511 (2013-12-30)
등록번호 US-10208677 (2019-02-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fletcher Yoder P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 538
초록
▼

A gas turbine system includes a combustor configured to combust an oxidant and a fuel in the presence of an exhaust gas diluent to produce combustion products, an oxidant supply path fluidly coupled to the combustor and configured to flow the oxidant to the combustor at an oxidant flow rate, and a turbine configured to extract work from the combustion products to produce an exhaust gas used to generate the exhaust gas diluent. The turbine causes a shaft of the gas turbine system to rotate when the work is extracted from the combustion products. The syste...

대표
청구항
▼

1. A gas turbine system comprising: a turbine combustor configured to combust a compressed oxidant and a fuel in the presence of an exhaust gas diluent generated from an exhaust gas to produce combustion products;an oxidant supply path fluidly coupled to the turbine combustor and configured to flow the compressed oxidant from a main oxidant compression system to the turbine combustor at an oxidant flow rate;a turbine configured to extract work from the combustion products to produce the exhaust gas, wherein the turbine causes a shaft of the gas turbine s...

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