发明名称 Turbine airfoil component and method for making
摘要 A component such as a turbine bucket or blade, and method for making the component, are presented. One embodiment is an article that comprises an airfoil casting portion comprising a plurality of integral regions, wherein the plurality of integral regions comprises a single-crystalline region and a columnar-grained region. Another embodiment is a method for fabricating an article. The method comprises providing a quantity of molten metal; providing a mold defining an airfoil portion having an axial direction and a transverse direction, wherein the airfoil portion of the mold comprises a single-crystal growth region and a columnar growth region disposed along the transverse direction from the single crystal growth region; introducing the molten metal into the mold; and solidifying the metal such that a solidification front progresses in the axial direction to produce an airfoil casting portion comprising a single-crystalline region and a columnar-grained region.
申请公布号 US8770944(B2) 申请公布日期 2014.07.08
申请号 US201113077475 申请日期 2011.03.31
申请人 General Electric Company 发明人 Suzuki Akane;Rutkowski Stephen Francis;Gigliotti, Jr. Michale Francis Xavier
分类号 F01D5/14;B22D25/00;B22D27/04 主分类号 F01D5/14
代理机构 代理人 DiConza Paul J.
主权项 1. An article, comprising: an airfoil casting portion comprising: a plurality of integral regions comprising a single-crystalline region and a columnar-grained region;a leading edge section comprising a leading edge of the airfoil casting portion; anda trailing edge section comprising a trailing edge of the airfoil casting portion, wherein the single-crystalline region comprises a single-crystalline material; andthe single-crystalline material is disposed at least at the leading edge of the airfoil casting portion or at the trailing edge of the airfoil casting portion.
地址 Niskayuna NY US
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