Airfoil and method for protecting airfoil leading edge

Details Airfoil and method for protecting airfoil leading edge Airfoil and method for protecting airfoil leading edge

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/14 (2006.01) F01D 5/28 (2006.01)

Patent

CA 2630951

An airfoil is disclosed having a concave pressure side (70) and a convex suction side (72) defining a chord length, and a leading edge (74) and a trailing edge (76). A leading edge protective strip (80) is adhered by a bond layer (82) to and protectively covers the leading edge (74) and respective predetermined portions of the pressure side (70) and suction side (72) of the airfoil body from the leading edge (74) downstream towards the trailing edge (76). The predetermined portion of the suction side (72) covered by the leading edge protective strip (80) is less than the predetermined portion of the pressure side (70) covered by the leading edge protective strip (80).

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