METHOD FOR SUPPORTING THE PROCESSING OF DAMAGE TO A BLADING OF A TURBOMACHINE, IN PARTICULAR A JET ENGINE, COMPUTER PROGRAM PRODUCT AND SYSTEM
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United States of America Patent
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Issued Date -
Oct 10, 2024
app pub date -
Jul 15, 2022
filing date -
Jul 15, 2021
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Abstract
The invention relates to a method (100) for supporting the processing of damage on a blading of a turbomachine (10) having a plurality of blades (11), comprising the following steps/stages: determining (103) a contour for processing (202) for mechanically processing a damaged area (20) of a first blade (11.1) of the blading and capturing (104) a first image (200) of a blade area (12) of the first blade (11.1) comprising the damaged area (20). The invention also relates to a computer program product and a system (1).
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