发明名称 Cast turbine casing and nozzle diaphragm preforms
摘要 Various turbine component preforms are disclosed having near-net shape features. In one embodiment, a turbine casing preform is disclosed. The turbine casing preform includes an as-cast body comprising a partially cylindrical wall section of a turbine casing, the wall section having an inner surface and an outer surface. The turbine casing preform also includes a circumferentially-extending vane slot formed in the wall section on the inner surface. In another embodiment, a turbine nozzle diaphragm preform is disclosed. The turbine nozzle diaphragm preform includes an as-cast body comprising a partially-cylindrical wall section of a turbine nozzle diaphragm having an inner surface and an outer surface. The turbine nozzle diaphragm preform also includes an as-cast, circumferentially-extending seal member projecting from one of the outer surface or inner surface.
申请公布号 US8979488(B2) 申请公布日期 2015.03.17
申请号 US201113069471 申请日期 2011.03.23
申请人 General Electric Company 发明人 Park Junyoung;Goller George Albert;Moore Brian Victor;Parolini Jason Robert
分类号 F04D29/02;F01D25/24;F01D9/02 主分类号 F04D29/02
代理机构 Cantor Colburn LLP 代理人 Cantor Colburn LLP
主权项 1. A turbine casing preform, comprising: an as-cast body comprising a partially cylindrical wall section of a turbine casing, the wall section having an inner surface and an outer surface, the as-cast body comprising a nodular cast iron; and an as-cast vane slot formed in the wall section on the inner surface, the inner surface proximate the as-cast vane slot comprising a fine grain size as-cast microstructure having an average graphite nodule count of 100/mm2 or less, the as-cast vane slot having an as-cast slot profile that is configured for removal of the nodular cast iron to a depth sufficient to form a final vane slot having a final slot profile and a microstructure proximate the final vane slot that is substantially the same as the as-cast microstructure.
地址 Schenectady NY US
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