The invention relates to a method for repairing a turbomachine air intake lip comprising a damaged region of which the shape differs from the initial shape of the lip, characterized in that it comprises: - a step (41) of identifying the damage; a step (44) of depositing a filler material on the damaged region so as to give it an identical shape to the initial shape; a step (45) of checking the shape of the lip; a step (47) of checking the repair carried out.
PROCÉDÉ DE RÉPARATION D'UNE LÈVRE D'ENTRÉE D'AIR
METHOD FOR REPAIRING AN AIR INTAKE LIP
VERFAHREN ZUR REPARATUR EINER LUFTEINLASSLIPPE
2022-08-24
Patent
Electronic Resource
French
IPC: | B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
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