发明名称 Turbine exhaust section structures with internal flow passages
摘要 A system is provided including a turbine exhaust section. The turbine exhaust section includes an exhaust flow path. The turbine exhaust section also includes an outer structure having an outer casing, an outer exhaust wall disposed along the exhaust flow path, and an outer cavity disposed between the outer exhaust wall and the outer casing. The turbine exhaust section further includes an inner structure having an inner exhaust wall disposed along the exhaust flow path, an inner cavity disposed between the inner exhaust wall and an inner casing, and a bearing cavity disposed between the inner casing and a bearing housing. In addition, the turbine exhaust section includes a strut extending between the outer structure and the inner structure. The strut includes a first flow passage configured to flow a fluid from the inner cavity to the outer cavity.
申请公布号 US9546567(B2) 申请公布日期 2017.01.17
申请号 US201213633625 申请日期 2012.10.02
申请人 General Electric Company 发明人 Kasibhotla Ravi Shankar Venkata;Kobek Piotr Edward;Pakkala Srinivasarao;Danescu Radu Ioan;Johnson David Martin
分类号 F01D25/12;F01D25/14;F02C7/12 主分类号 F01D25/12
代理机构 Fletcher Yoder, P.C. 代理人 Fletcher Yoder, P.C.
主权项 1. A system, comprising: a turbine exhaust section, comprising: an exhaust flow path;an outer structure comprising an outer casing, an outer exhaust wall disposed along the exhaust flow path, and an outer cavity disposed between the outer exhaust wall and the outer casing;an inner structure comprising an inner exhaust wall disposed along the exhaust flow path, an inner cavity disposed between the inner exhaust wall and an inner casing, and a bearing cavity disposed between the inner casing and a bearing housing;a strut extending between the outer structure and the inner structure, wherein the strut at least partially defines a first flow passage configured to flow a fluid from the inner cavity to the outer cavity;a second flow passage disposed at a downstream end portion of the turbine exhaust section downstream of the strut, wherein the second flow passage is configured to flow the fluid into the bearing cavity; andone or more tunable areas through the inner casing, wherein the one or more tunable areas are configured to control a flow of the fluid from the bearing cavity to the inner cavity.
地址 Schenectady NY US