| 发明名称 |
Variable Volume Combustor with an Air Bypass System |
| 摘要 |
The present application provides a combustor for use with flow of fuel and a flow of air in a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles positioned within a liner and an air bypass system position about the liner. The air bypass system variably allows a bypass portion of the flow of air to bypass the micro-mixer fuel nozzles. |
| 申请公布号 |
US2014216051(A1) |
申请公布日期 |
2014.08.07 |
| 申请号 |
US201313760101 |
申请日期 |
2013.02.06 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Johnson Thomas Edward;Ziminsky Willy Steve;Ostebee Heath Michael;Keener Christopher Paul |
| 分类号 |
F02C7/22 |
主分类号 |
F02C7/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustor for use with a flow of fuel and a flow of air in a gas turbine engine, comprising:
a plurality of micro-mixer fuel nozzles; the plurality of micro-mixer fuel nozzles positioned within a liner; and an air bypass system positioned about the liner; the air bypass system variably allowing a bypass portion of the flow of air to bypass the plurality of micro-mixer fuel nozzles. |
| 地址 |
Schenectady NY US |
