Turbine engine blade having a zone of fine grains of a high stre

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Coating – specific composition or characteristic

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415200, F01D 528

Patent

active

054511429

ABSTRACT:
Blades for use in modern gas turbine engines are described and are characterized by a thin zone of fine grains of a high strength composition on the surface of the blade root.

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