Shrouded single crystal dual alloy turbine disk

Details Shrouded single crystal dual alloy turbine disk Shrouded single crystal dual alloy turbine disk

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/30 (2006.01) B23K 20/00 (2006.01) B23P 15/04 (2006.01)

Patent

CA 2629460

A turbine engine component for a gas turbine engine includes an inner disk, an outer shroud, and a plurality of blades. Each blade comprises a blade root and an airfoil body. The blade root is plated at least in part with a noble metal, and is coupled to the inner disk. The airfoil body extends at least partially between the blade root and the outer shroud.

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