Monolithic and bi-metallic turbine blade dampers and method...

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 5/28 (2006.01) F01D 5/26 (2006.01)

Patent

CA 2645380

A method for manufacturing a turbine damper (36) by a metal injection molding process is disclosed. The damper (36) includes a base section (46) and a wire section (38), and is formed of a nickel-base or cobalt base superalloy.

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