Cooled airfoil for gas turbine engine and method of making...

Details Cooled airfoil for gas turbine engine and method of making... Cooled airfoil for gas turbine engine and method of making...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01)

Patent

CA 2327203

An airfoil (40) for use in a gas turbine engine includes a pressure side (42) and a suction side (44) joined at a trailing edge wall (60) that defines a trailing edge (48). The airfoil (40) includes at least one cooling hole (68) extending through the trailing edge wall (60) so as to pass cooling fluid from the pressure side (42) of the airfoil (40) to the suction side (44).

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