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 |