Method and system for automated repair design of damaged blades of a compressor or turbine
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United States of America Patent
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Jul 5, 2005
Grant Date -
Feb 10, 2005
app pub date -
Nov 22, 2002
filing date -
Nov 22, 2002
priority date (Note) -
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Abstract
A method is disclosed for evaluating a damaged blade in a compressor or turbine using a computer system accessing a database of blade repair information, where the method includes: selecting a blade damage geometry category corresponding to the damage of the blade from a plurality of blade damage geometry categories; measuring the blade damage, and generating a repair geometry for the blade based on the blade damage measurements and the selected blade damage geometry category.
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