Reinforced aluminum fan blade

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Having wear liner – sheathing or insert

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Details

416219R, 416229A, 416248, 416220R, 416239, B63H 126

Patent

active

060041013

ABSTRACT:
A gas turbine engine fan blade includes an airfoil and dovetail having an integral aluminum core and a fatigue resistant reinforcing sheath.

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