Vane assembly with improved vane roots

Details Vane assembly with improved vane roots Vane assembly with improved vane roots

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/30 (2006.01) F01D 5/02 (2006.01) F01D 5/14 (2006.01)

Patent

CA 2597443

A vane for a vane assembly of a gas turbine engine includes a vane root connected to the airfoil portion opposite a tip thereof. The vane root includes a platform and a button portion interconnecting the platform and the airfoil position. The button portion has relatively blunt leading and trailing ends which respectively protrude beyond leading and trailing edges of the airfoil portion.

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