发明名称 SEQUENTIAL COMBUSTION WITH DILUTION GAS MIXER
摘要 The invention refers to a sequential combustor arrangement including a first burner, a first combustion chamber, a dilution burner for admixing a dilution gas and a second fuel via a dilution-gas-fuel-admixer to the first combustor combustion products. The dilution-gas-fuel-admixer has at least one streamlined body which is arranged in the dilution burner for introducing the at least one second fuel into the dilution burner through at least one fuel nozzle, and which has a streamlined cross-sectional profile and which extends with a longitudinal direction perpendicularly or at an inclination to a main flow direction prevailing in the dilution burner. The streamlined body includes a dilution gas opening for admixing dilution gas into the first combustor combustion products upstream of the at least one fuel nozzle. The disclosure further refers to a method for operating a gas turbine with such a sequential combustor arrangement.
申请公布号 US2015047365(A1) 申请公布日期 2015.02.19
申请号 US201414445162 申请日期 2014.07.29
申请人 ALSTOM Technology Ltd 发明人 DUESING Michael
分类号 F23R3/34;F02C7/228 主分类号 F23R3/34
代理机构 代理人
主权项 1. A sequential combustor arrangement comprising a first burner, a first combustion chamber, a dilution burner for admixing a dilution gas and a second fuel via a dilution-gas-fuel-admixer to the first combustor combustion products leaving the first combustion chamber during operation, and a second combustion chamber arranged sequentially in a fluid flow connection, wherein dilution-gas-fuel-admixer has at least one streamlined body which is arranged in the dilution burner for introducing the at least one second fuel into the dilution burner through at least one fuel nozzle, and which has a streamlined cross-sectional profile and which extends with a longitudinal direction perpendicularly or at an inclination to a main flow direction prevailing in the dilution burner, where the streamlined body comprises a dilution gas opening for admixing dilution gas into the first combustor combustion products upstream of the at least one fuel nozzle.
地址 Baden CH