Repair of airfoil edges

Metal working – Method of mechanical manufacture – Impeller making

Patent

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Details

2940219, B21D 100, B21D 316, B23P 600

Patent

active

051971917

ABSTRACT:
The present invention provides a method and apparatus to repair gouged out and damaged leading and trailing edges of gas turbine engine blades, particularly fan blades, by cutting away a curved section including the damaged area and forming a blend radius along the repaired edge. The apparatus includes a unique machine tool guide having an adjustable cutting depth guide and mountable to a hand held machine tool driver, such as 90 degree angle head air motor, that drives a rotary cutter.

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patent: 5023987 (1991-06-01), Wuepper et al.
patent: 5031313 (1991-07-01), Blair et al.

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