Gas turbine engine components and methods of fabricating same

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Welded – cemented or fused

Reexamination Certificate

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C416S234000, C029S889210

Reexamination Certificate

active

11234437

ABSTRACT:
A method for fabricating a component for a gas turbine engine includes providing a blisk forging fabricated from a first material, inertia welding a second material to the blisk forging to create a bi-alloy blisk forging, and machining the bi-alloy blisk forging to pre-determined dimensions.

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