Cooled airfoil and method for making an airfoil having...

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 5/18 (2006.01) B22D 19/00 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2614031

An airfoil component (100) having a body having a leading edge (105) and a trailing edge (107), a ceramic casting insert for making the component (100) and the method for making the component (100). The component (100) includes an internal cooling passageway (201) and an elongated opening (211) in communication with the internal cooling passageway (201). The opening (211) is configured with a geometry that provides structural stability during casting and has a cross-section that sufficiently restricts airflow through the opening (211) to provide efficient component operation. The casting insert includes outer edge projections (601) and a web portion (603) corresponding to the geometry of the openings when cast around the insert. The method includes casting the airfoil component (100) around the casting insert and removing the insert to provide the component (100) having the openings (211).

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