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Method and apparatus for refurbishing a gas turbine airfoil

  • US 6,302,625 B1
  • Filed: 10/15/1999
  • Issued: 10/16/2001
  • Est. Priority Date: 10/15/1999
  • Status: Expired due to Term
First Claim
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1. A method for refurbishing a spanwise extending edge of a fan blade mounted within a gas turbine engine, comprising the steps of:

  • (a) providing a portable refurbishing device having a channel, a plurality of locator sets disposed in said channel, and a rotary edge shaper;

    (b) securing said fan blade to prevent said fan blade from moving within said engine;

    (c) placing a portion of said edge into said refurbishing device channel, wherein said edge portion is located adjacent a tip or a base of said fan blade;

    (d) locating said edge within said channel using said locator sets;

    (e) engaging said edge with said edge shaper, and (f) moving said device along said edge, wherein said edge shaper refurbishes said edge while moving along said edge.

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