发明申请
US20090324415A1 AIRFOIL CORE SHAPE FOR A TURBINE NOZZLE 有权
用于涡轮喷嘴的气翼芯形

AIRFOIL CORE SHAPE FOR A TURBINE NOZZLE
摘要:
An article of manufacture includes an object having an airfoil core shape. The airfoil core shape has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in TABLE 1 where X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances are joined smoothly with one another to form a complete airfoil core shape.
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