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US08434543B2 Method of making turbine stator airfoils with individual orientations 失效
制造具有各个方位的涡轮机定子翼型的方法

Method of making turbine stator airfoils with individual orientations
Abstract:
In accordance with an exemplary embodiment, a turbine stator component includes a first endwall; a second endwall; a first stator airfoil coupled between the first and second endwalls; and a second stator airfoil adjacent to the first airfoil and coupled between the first and second endwalls. The first stator airfoil has first crystallographic primary and secondary orientations. The second stator airfoil has second crystallographic primary and secondary orientations, the first crystallographic primary and secondary orientations being different from the second crystallographic primary and secondary orientations.
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