Airfoil locator rib and method of positioning an insert in...

Details Airfoil locator rib and method of positioning an insert in... Airfoil locator rib and method of positioning an insert in...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/14 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2535140

An airfoil for a gas turbine engine, the airfoil comprising a locator rib provided at a bottom of a cavity in the airfoil core, the locator rib having an inclined surface to be engaged by a leading end of the insert during installation thereof in the cavity.

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