| 发明名称 |
METHOD OF REDUCING COMBUSTION INDUCED OSCILLATIONS IN A TURBINE ENGINE |
| 摘要 |
<p>A method for operating a turbine engine (100) having a plurality of fuel injectors (30) arranged circumferentially in a combustor (50), with each fuel injector having a main fuel supply and a pilot fuel supply, includes supplying fuel to the plurality of fuel injectors through the main fuel supply to create a circumferential thermal gradient in the combustor.</p> |
| 申请公布号 |
WO2013191954(A1) |
申请公布日期 |
2013.12.27 |
| 申请号 |
WO2013US45055 |
申请日期 |
2013.06.11 |
| 申请人 |
SOLAR TURBINES INCORPORATED |
发明人 |
ABREU, MARIO E. |
| 分类号 |
F02C7/00;F02C3/14;F02C7/22 |
主分类号 |
F02C7/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
