Airfoil and method for protecting airfoil leading edge

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

Reexamination Certificate

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Reexamination Certificate

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07736130

ABSTRACT:
An airfoil is disclosed having a concave pressure side and a convex suction side defining a chord length, and a leading edge and a trailing edge. A leading edge protective strip is adhered by a bond layer to and protectively covers the leading edge and respective predetermined portions of the pressure side and suction side of the airfoil body from the leading edge downstream towards the trailing edge. The predetermined portion of the suction side covered by the leading edge protective strip is less than the predetermined portion of the pressure side covered by the leading edge protective strip.

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patent: 6960065 (2005-11-01), Leach
patent: 7125222 (2006-10-01), Cormier et al.
patent: 4411679 (1994-12-01), None
patent: 1719699 (2006-11-01), None
patent: 2039526 (1980-08-01), None

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