METHOD AND SYSTEM FOR AUTOMATED REPAIRMENT DESIGN OF DAMAGED BLADES OF COMPRESSOR OR TURBINE

摘要

PROBLEM TO BE SOLVED: To provide a method 50 for evaluating a damaged blade in a compressor or turbine using a computer system accessing a database 52 of blade repair information.

SOLUTION: The method comprises the steps of: selecting a blade damage geometry category (58) corresponding to the damage of the blade from a plurality of blade damage geometry categories; measuring the blade damage (60, 62); and generating a repair geometry (72) for the blade based on the blade damage measurements and the selected blade damage geometry category.

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