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