Turbine airfoil cooling flow particle separator

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/052 (2006.01) F01D 5/18 (2006.01) F01D 25/32 (2006.01)

Patent

CA 2476470

A vane assembly for a turbine engine comprising a plurality of vanes each comprising a pressure side wherein the pressure side of at least one of the plurality of vanes comprises at least one opening extending through the pressure side into an interior portion of the at least one of the plurality of vanes.

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