发明名称 SYSTEM AND METHOD FOR REHEAT IN GAS TURBINE WITH EXHAUST GAS RECIRCULATION
摘要 <p>A system includes a turbine having an exhaust flow path through a plurality of turbine stages, wherein the plurality of turbine stages is driven by combustion products flowing through the exhaust flow path, at least one main combustor disposed upstream from the turbine, wherein the at least one main combustor is configured to combust a fuel with a first oxidant and an exhaust gas to generate the combustion products, at least one reheat combustor disposed in or between turbine stages of the turbine, wherein the at least one reheat combustor is configured to reheat the combustion products by adding a second oxidant to react with unburnt fuel in the combustion products, and an exhaust gas compressor, wherein the exhaust gas compressor is configured to compress and route the exhaust gas from the turbine to the at least one main combustor along an exhaust recirculation path.</p>
申请公布号 WO2014071118(A1) 申请公布日期 2014.05.08
申请号 WO2013US67946 申请日期 2013.11.01
申请人 GENERAL ELECTRIC COMPANY;EXXONMOBIL UPSTREAM RESEARCH COMPANY 发明人 WOODALL, JOHN FARRIOR;EVULET, ANDREI TRISTAN;DRAPER, SAMUEL DAVID
分类号 F02C3/34;F02C6/00;F02C7/18 主分类号 F02C3/34
代理机构 代理人
主权项
地址