| 发明名称 |
SYSTEM AND METHOD FOR CONTROL OF COMBUSTION DYNAMICS IN COMBUSTION SYSTEM |
| 摘要 |
A system includes a gas turbine engine that includes a first combustor and a second combustor. The first combustor includes a first oxidant flow path and a first perforated structure comprising a first plurality of oxidant ports, wherein the first perforated structure is disposed in the first oxidant flow path. The second combustor includes a second oxidant flow path and a second perforated structure comprising a second plurality of oxidant ports. The second perforated structure is disposed in the second oxidant flow path and the first perforated structure has at least one difference relative to the second perforated structure. |
| 申请公布号 |
US2015241066(A1) |
申请公布日期 |
2015.08.27 |
| 申请号 |
US201414192687 |
申请日期 |
2014.02.27 |
| 申请人 |
General Electric Company |
发明人 |
Crothers Sarah Lori;Stoia Lucas John;Carnell, JR. William Francis |
| 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 comprising:
a first oxidant flow path; anda first perforated structure comprising a first plurality of oxidant ports, wherein the first perforated structure is disposed in the first oxidant flow path; anda second combustor comprising:
a second oxidant flow path; anda second perforated structure comprising a second plurality of oxidant ports, wherein the second perforated structure is disposed in the second oxidant flow path, and the first perforated structure has at least one difference relative to the second perforated structure. |
| 地址 |
Schenectady NY US |
