发明名称 |
Method and apparatus for operating gas turbine engine combustors |
摘要 |
<p>A method facilitates assembling a gas turbine engine (10). The method comprises coupling a combustor (16) including a dome assembly (113) and a combustor liner (110, 112) that extends downstream from the dome assembly to a combustor casing (114) that is positioned radially outwardly from the combustor, coupling a fuel injector (30) including a fuel inlet and an air inlet to the combustor casing such that the fuel injector extends axially through the dome assembly such that fuel may be discharged from the primer nozzle into the combustor, and coupling the air inlet to an air source such that cooling air received therethrough is circulated through the fuel injector to facilitate cooling the fuel injector.
</p> |
申请公布号 |
EP1493971(A3) |
申请公布日期 |
2012.08.29 |
申请号 |
EP20040252522 |
申请日期 |
2004.04.30 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MCCAFFREY, TIMOTHY P.;TINGLE, WALTER J.;JACOBSON, JOHN CARL;HOWELL, STEPHEN JOHN;BARNES, BARRY FRANCIS |
分类号 |
F23R3/28;F23R3/60 |
主分类号 |
F23R3/28 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|