| 发明名称 |
SYSTEM AND METHOD FOR A TURBINE COMBUSTOR |
| 摘要 |
A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber and the combustion chamber, a mixing region configured to mix an exhaust flow with an oxidant flow to provide an oxidant-exhaust mixture, and a flow distributor configured to distribute the oxidant-exhaust mixture circumferentially around the head end chamber. The flow distributor includes at least one oxidant-exhaust mixture path. |
| 申请公布号 |
US2014182305(A1) |
申请公布日期 |
2014.07.03 |
| 申请号 |
US201314067739 |
申请日期 |
2013.10.30 |
| 申请人 |
ExxonMobil Upstream Research Company ;General Electric Company |
发明人 |
Antoniono Carolyn Ashley;Byrne William Lawrence;Fadde Elizabeth Angelyn |
| 分类号 |
F02C6/18;F02C7/00;F23R3/26;F02C3/34 |
主分类号 |
F02C6/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system, comprising:
a turbine combustor, comprising:
a head end portion having a head end chamber;a combustion portion having a combustion chamber disposed downstream from the head end chamber;a cap disposed between the head end chamber and the combustion chamber;a mixing region configured to mix an exhaust flow with an oxidant flow to provide an oxidant-exhaust mixture; anda flow distributor configured to distribute the oxidant-exhaust mixture circumferentially around the head end chamber, wherein the flow distributor comprises at least one oxidant-exhaust mixture path. |
| 地址 |
Houston TX US |
