Cooled airfoil component

Details Cooled airfoil component Cooled airfoil component

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) B23P 15/02 (2006.01)

Patent

CA 2610670

A gas turbine engine airfoil component having an airfoil body with a core cavity, an end opening in communication with the core cavity, and a wall having a plurality of cooling holes defined therein, each cooling hole being oriented such that the respective hole axis extends out of the core cavity through the end opening.

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