Chevron film cooled wall

Details Chevron film cooled wall Chevron film cooled wall

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/14 (2006.01)

Patent

CA 2504165

A wall (32) in a gas turbine engine includes inner and outer surfaces (34,36) having a row of compound chevron film cooling holes (38) extending therethrough. The chevron holes (38) diverge both longitudinally and laterally between an inlet (40) at the wall inner surface (34) and a chevron outlet (42) at the wall outer surface (36).

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