| 发明名称 |
SYSTEM AND METHOD FOR CONTROL OF COMBUSTION DYNAMICS IN COMBUSTION SYSTEM |
| 摘要 |
The present disclosure generally relates to a system with a gas turbine engine including a first combustor and a second combustor. The first combustor includes a first end cover with a first geometry and the second combustor includes a second end cover with a second geometry. The first geometry has one or more geometric differences relative to the second geometry. |
| 申请公布号 |
US2015292744(A1) |
申请公布日期 |
2015.10.15 |
| 申请号 |
US201414249158 |
申请日期 |
2014.04.09 |
| 申请人 |
General Electric Company |
发明人 |
Ziminsky Willy Steve;Crothers Sarah Lori |
| 分类号 |
F23R3/42 |
主分类号 |
F23R3/42 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system, comprising:
a gas turbine engine comprising:
a first combustor having a first end cover with a first geometry; anda second combustor having a second end cover with a second geometry, wherein the first geometry has at least one geometrical difference relative to the second geometry. |
| 地址 |
Schenectady NY US |
