| 发明名称 |
DUAL FUEL COMBUSTOR FOR A GAS TURBINE ENGINE |
| 摘要 |
The present application and the resultant patent provide a dual fuel combustor for a gas turbine engine. The combustor may include a primary premixer positioned within a head end plenum of the combustor, and a dual fuel, injection system positioned within the head end plenum and upstream of the premixer. The injection system may be configured to inject a gas fuel about an inlet end of the premixer when the combustor operates on the gas fuel. The injection system also may be configured to vaporize and inject a liquid fuel about the inlet end of the premixer when the combustor operates on the liquid fuel. The present application and the resultant patent also provide a related method of operating a dual fuel combustor. |
| 申请公布号 |
US2015059352(A1) |
申请公布日期 |
2015.03.05 |
| 申请号 |
US201314017509 |
申请日期 |
2013.09.04 |
| 申请人 |
General Electric Company |
发明人 |
Myers Geoffrey D. |
| 分类号 |
F23R3/36;F02C7/22 |
主分类号 |
F23R3/36 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A dual fuel combustor for a gas turbine engine, the combustor comprising;
a primary premixer positioned within a head end plenum of the combustor; and a dual fuel injection system positioned within the head end plenum and upstream of the premixer; wherein the injection system is configured to inject a gas feel about an inlet end of the premixer when the combustor operates on the gas fuel; and wherein the injection system is configured to vaporize and inject a liquid fuel about the inlet end of the premixer when the combustor operates on the liquid fuel, |
| 地址 |
Schenectady NY US |
