发明名称 Reducing Oxygen in a Gas Turbine Exhaust
摘要 The present techniques are directed to a system and methods for operating a gas turbine system. An exemplary gas turbine system includes an oxidant system, a fuel system, and a control system. A combustor is adapted to receive and combust an oxidant from the oxidant system and a fuel from the fuel system to produce an exhaust gas. A catalyst unit including an oxidation catalyst that includes an oxygen storage component is configured to reduce the concentration of oxygen in the exhaust gas to form a low oxygen content product gas.
申请公布号 US2014230446(A1) 申请公布日期 2014.08.21
申请号 US201414182058 申请日期 2014.02.17
申请人 Beutel Tilman W.;Dhanuka Sulabh K. 发明人 Beutel Tilman W.;Dhanuka Sulabh K.
分类号 F01N3/28;F02C3/34;F02C7/10 主分类号 F01N3/28
代理机构 代理人
主权项 1. A gas turbine system, comprising: an oxidant system; a fuel system; a control system; a combustor adapted to receive and combust an oxidant from the oxidant system and a fuel from the fuel system to produce an exhaust gas; and a catalyst unit comprising an oxidation catalyst that comprises an oxygen storage component configured to reduce the concentration of oxygen in the exhaust gas to form a low oxygen content product gas.
地址 Neshanic Station NJ US