| 发明名称 |
COMBUSTOR CAN TEMPERATURE CONTROL SYSTEM |
| 摘要 |
The present application provides a fuel delivery system for a combustor with reduced coherence and/or reduced combustion dynamics. The combustor can assembly may include a first manifold for delivering a first flow of fuel to a first set of fuel injectors and a second manifold for delivering a second flow of fuel to a second set of fuel injectors. The first flow of fuel may have a first temperature and the second flow of fuel may have a second temperature. The first temperature may be higher than the second temperature. |
| 申请公布号 |
US2014238041(A1) |
申请公布日期 |
2014.08.28 |
| 申请号 |
US201313778164 |
申请日期 |
2013.02.27 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
CROTHERS SARAH LORI;STEVENSON CHRISTAN XAVIER;LEACH DAVID |
| 分类号 |
F02C7/24;F02C7/224;F02C7/228 |
主分类号 |
F02C7/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuel delivery system for a combustor with reduced coherence and/or reduced combustion dynamics, comprising:
a first manifold for delivering a first flow of fuel to a first set of fuel injectors; and a second manifold for delivering a second flow of fuel to a second set of fuel injectors; the first flow of fuel comprising a first temperature; the second flow of fuel comprising a second temperature; and wherein the first temperature is higher than the second temperature. |
| 地址 |
Schenectady NY US |
