| 发明名称 |
SYSTEM AND METHOD FOR A GAS TURBINE ENGINE SENSOR |
| 摘要 |
A system includes a gas turbine engine that includes a combustor section having a turbine combustor that generates combustion products, a turbine section having one or more turbine stages driven by the combustion products, an exhaust section disposed downstream of the turbine section, an oxygen sensor adaptor housing disposed in at least one of the combustor section, the turbine section, or the exhaust section, or any combination thereof, and an oxygen sensor disposed in the oxygen sensor adaptor housing. The oxygen sensor adaptor housing is configured to maintain a temperature of a portion of the oxygen sensor below an upper threshold. |
| 申请公布号 |
US2015033757(A1) |
申请公布日期 |
2015.02.05 |
| 申请号 |
US201414321690 |
申请日期 |
2014.07.01 |
| 申请人 |
General Electric Company ;ExxonMobil Upstream Research Company |
发明人 |
White Eugene Delano;Beadie Douglas Frank;Krull Anthony Wayne;Floyd, II Donald Earl |
| 分类号 |
F01D17/20;F02C3/34;F01D15/00;F01D25/12;F01D25/14 |
主分类号 |
F01D17/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system, comprising:
a gas turbine engine, comprising:
a combustor section having a turbine combustor that generates combustion products;a turbine section having one or more turbine stages driven by the combustion products;an exhaust section disposed downstream of the turbine section;an oxygen sensor adaptor housing disposed in at least one of the combustor section, the turbine section, or the exhaust section, or any combination thereof; andan oxygen sensor disposed in the oxygen sensor adaptor housing, wherein the oxygen sensor adaptor housing is configured to maintain a temperature of a portion of the oxygen sensor below an upper threshold. |
| 地址 |
Schenectady NY US |
