Airfoil cooling passage trailing edge flow restriction

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

Patent

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Details

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

Patent

CA 2513036

An internal metering structure permits the exit apertures of a cooled airfoil to be sized to provide for easy manufacturability.

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