Method and system to facilitate enhanced local cooling of...

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

Patent

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F01D 25/12 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2602311

An engine assembly (108) is provided. The engine assembly includes a nozzle assembly (520) including an inner band, an outer band (183) including an aft flange (504) and a radial inner surface (522), the aft flange including a first group of cooling openings (194) having a larger aggregate cross-sectional area and a second group of cooling openings having a smaller aggregate cross-sectional area, the cooling openings configured to direct cooling fluid therefrom at an oblique discharge angle, and at least one airfoil vane (510) extending between the inner band and the outer band.

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