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AssigneesAirbus Operations S.L.U., Airbus Operations GmbH
InventorsInes NIETO LEON, Nizar KHEMIRI, Jorge GARCIA LOPEZ-VARELA
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A method and device for repairing an element (100) of composite material, the method comprising infusing a resin (300) into the internal damaged area (101) of the element (100) of composite material, wherein the method further comprises: drilling on the element (100) of composite material at least one first non-through hole (200a) and at least one second non-through hole (200b), each of the non-through holes (200) running from one face of the element (100) of composite material up to the internal damaged area (101), and infusing the resin (300) from the at least one first non-through hole (200a) until the resin (300) fills at least the internal damaged area (101) of the element (100) of composite material. The method comprises applying vibrations at a given frequency to the element (100) of composite material.
A method for repairing an element of composite material, the method comprising:
A device configured to repair an element of composite material, wherein the element of the composite material includes an internal damaged area and the internal damaged area is accessible from outside of the element of composite material through a first non-through hole and a second non-through hole, wherein the device comprises:
A method to repair a panel formed of layers of a composite material, the method comprising:
Dependencies are inferred from the claim text.