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AssigneeSafran Aircraft Engines
InventorsMathieu Julien Charlas, Adrien Francis Paixao, Simon Talibart
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A method for repairing a part for an aircraft turbine engine, the part including a lower panel, an upper panel and a core having a honeycomb structure arranged between the lower panel and the upper panel, the part having an unimpaired portion and an at least partially impaired portion, the repair method including the following steps: (a) removing at least one portion of the lower panel or the upper panel from an area to be repaired; (b) removing at least one portion of the core from the area to be repaired; (c) reforming the core in the area to be repaired directly on the part by additive manufacturing; (d) reforming the lower panel or the upper panel in the area to be repaired, directly on the part.
A method for repairing a part for an aircraft turbine engine, the part comprising a lower panel, an upper panel, and a core having a honeycomb structure arranged between the lower panel and the upper panel, the part comprising an unimpaired portion and an at least partially impaired portion, the repair method comprising the following steps of:
Dependencies are inferred from the claim text.