发明名称 REAGENT INJECTION SYSTEM FOR EXHAUST OF TURBINE SYSTEM
摘要 A reagent injection system for a catalytic emissions reduction assembly of a combustion turbine that includes an exhaust duct and at least one injector. The exhaust duct includes a first section including an entrance end and an exit end, wherein the entrance end is configured to be fluidly coupled to the combustion turbine to receive exhaust gases therefrom. The exhaust duct also includes and a second section having an entrance end that is fluidly coupled to the exit end of the first section. The at least one injector is operatively coupled to one of the first and second sections, and each injector is configured to inject a reagent into the exhaust gases flowing through the exhaust duct.
申请公布号 US2015361850(A1) 申请公布日期 2015.12.17
申请号 US201514741345 申请日期 2015.06.16
申请人 LP Amina LLC 发明人 Forwerck Mark A.;Muzio Lawrence J.;Zedler Matthew
分类号 F01N3/20;F23R3/40 主分类号 F01N3/20
代理机构 代理人
主权项 1. A reagent injection system for a catalytic emissions reduction assembly of a combustion turbine, the reagent injection system comprising: an exhaust duct comprising: a first section including an entrance end and an exit end, wherein the entrance end is configured to be fluidly coupled to the combustion turbine to receive exhaust gases therefrom; anda second section having an entrance end that is fluidly coupled to the exit end of the first section; and at least one injector operatively coupled to one of the first and second sections, the at least one injector extending radially inward toward a longitudinal axis of the exhaust duct; wherein each injector is configured to inject a reagent into the exhaust gases flowing through the exhaust duct.
地址 Charlotte NC US