发明名称 |
Exhaust diffuser arrangement for a turbine system and method of redirecting a flow |
摘要 |
An exhaust diffuser arrangement for a turbine system includes an inlet for receiving a flow proximate a last stage bucket of the turbine system, the flow flowing in a first flow direction. Also included is a flow redirecting component. The flow redirecting component includes a first wall having a first side of a concave surface geometry for redirecting the flow and a second side of a convex surface geometry. The flow redirecting component also includes a second wall spaced downstream of the first wall and having at least one flow exit for reducing a boundary layer along the second side of the first wall. |
申请公布号 |
US9388710(B2) |
申请公布日期 |
2016.07.12 |
申请号 |
US201213632752 |
申请日期 |
2012.10.01 |
申请人 |
General Electric Company |
发明人 |
Rai Sachin Kumar;Awasthi Richa;Kulkarni Shruti;Subramaniyan Moorthi |
分类号 |
F01D25/30 |
主分类号 |
F01D25/30 |
代理机构 |
Fletcher Yoder, P.C. |
代理人 |
Fletcher Yoder, P.C. |
主权项 |
1. An exhaust diffuser arrangement for a turbine system comprising:
an inlet for receiving a flow proximate a last stage bucket of the turbine system, the flow flowing in a first flow direction; and a flow redirecting component comprising:
a first wall having a first side of a concave surface geometry for redirecting the flow and a second side of a convex surface geometry;a second wall spaced downstream of the first wall and having at least one flow exit for reducing a boundary layer along the second side of the first wall;a cavity defined by the first wall and the second wall; andan upstream end comprising an opening, wherein the opening is configured to direct a portion of the flow into the cavity. |
地址 |
Schenectady NY US |