| 发明名称 |
SYSTEM AND METHOD FOR PROTECTING COMPONENTS IN A GAS TURBINE ENGINE WITH EXHAUST GAS RECIRCULATION |
| 摘要 |
A system includes a gas turbine engine that includes a turbine section having one or more turbine stages between an upstream end and a downstream end, an exhaust section disposed downstream from the downstream end of the turbine section, and a fluid supply system coupled to the exhaust section. The fluid supply system is configured to route an inert gas to the exhaust section. |
| 申请公布号 |
US2014196464(A1) |
申请公布日期 |
2014.07.17 |
| 申请号 |
US201314135055 |
申请日期 |
2013.12.19 |
| 申请人 |
EXXONMOBIL UPSTREAM RESEARCH COMPANY ;GENERAL ELECTRIC COMPANY |
发明人 |
Biyani Pramod K.;Saha Rajarshi;Dasoji Anil Kumar;Huntington Richard A.;Mittricker Franklin F. |
| 分类号 |
F02C3/04 |
主分类号 |
F02C3/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system, comprising:
a gas turbine engine, comprising:
a turbine section having one or more turbine stages between an upstream end and a downstream end;an exhaust section disposed downstream from the downstream end of the turbine section; anda fluid supply system coupled to the exhaust section, wherein the fluid supply system is configured to route an inert gas to the exhaust section. |
| 地址 |
Houston TX US |
