| 发明名称 |
COMBUSTOR NOZZLES IN GAS TURBINE ENGINES |
| 摘要 |
A micro-mixer nozzle for use in a combustor of a combustion turbine engine, the micro-mixer nozzle including: a fuel plenum defined by a shroud wall connecting a periphery of a forward tube sheet to a periphery of an aft tubesheet; a plurality of mixing tubes extending across the fuel plenum for mixing a supply of compressed air and fuel, each of the mixing tubes forming a passageway between an inlet formed through the forward tubesheet and an outlet formed through the aft tubesheet; and a wall mixing tube formed in the shroud wall. |
| 申请公布号 |
US2016033133(A1) |
申请公布日期 |
2016.02.04 |
| 申请号 |
US201414448321 |
申请日期 |
2014.07.31 |
| 申请人 |
General Electric Company |
发明人 |
Johnson Thomas Edward;Keener Christopher Paul;Stewart Jason Thurman;Ostebee Heath Michael |
| 分类号 |
F23R3/28 |
主分类号 |
F23R3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A micro-mixer nozzle for use in a combustor of a combustion turbine engine, the micro-mixer nozzle comprising:
a fuel plenum defined by a shroud wall connecting a periphery of a forward tube sheet to a periphery of an aft tubesheet; a plurality of mixing tubes extending across the fuel plenum for mixing a supply of compressed air and fuel, each of the mixing tubes forming a passageway between an inlet formed through the forward tubesheet and an outlet formed through the aft tubesheet; and a wall mixing tube formed in the shroud wall. |
| 地址 |
Schenectady NY US |
