Methods and apparatus for fabricating turbine engine airfoils

Metal founding – Process – Shaping a forming surface

Reexamination Certificate

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C164S340000, C164S369000, C164S397000, C164S137000

Reexamination Certificate

active

06915840

ABSTRACT:
A method for casting an airfoil for a turbine engine is provided. The method includes forming a casting core to define a hollow portion in the airfoil and forming a print out region at one end of the casting core. The method also includes coupling the casting core to the print out region with at least one frusto-conical member to facilitate structurally supporting the casting core.

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