Blade cooling for gas turbine engine

Details Blade cooling for gas turbine engine Blade cooling for gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

170/68

F02C 7/18 (2006.01) F01D 5/18 (2006.01)

Patent

CA 1138345

Abstract of the Disclosure A hollow blade for a turbine in a gas turbine engine comprising passageways in the hollow blade for passing a coolant therethrough and pairs of ridges having a chevron shape and being segmented form a channel therebetween with corresponding pairs on opposed side walls of the passageway such that each corresponding opposed pair has the chevron angle open in opposite directions relative to the longitudinal direction of the passageway.

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