Method and device for mending damaged areas in fiber composite components
AssigneeAirbus Operations GmbH
InventorsBenedikt Schulte, Tobias Barth, Jan Bremer
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Abstract
A method for mending damaged areas in fiber composite components formed from a plurality of unidirectional fiber layers includes the steps of automatically lifting at least one fiber layer of the fiber composite component at a cutting edge of the at least one fiber layer using a delaminating device, removing the at least one fiber layer in the extension direction of the fiber orientation of the at least one fiber layer, and separating off the removed at least one fiber layer in a defined manner at a separating edge defined by a separating device placed on the fiber composite component.
Claims10
A method for mending damaged areas in a fiber composite component formed from a plurality of unidirectional fiber layers, the method comprising:
- automatically lifting at least one fiber layer of the fiber composite component at a cutting edge of the at least one fiber layer using a delaminating device, which comprises a gripping device that acts adhesively on a surface of the at least one fiber layer, wherein the gripping device is placed on the at least one fiber layer to remove the at least one fiber layer and is moved diagonally upwards away from a surface of the fiber composite component;
- removing the at least one fiber layer in an extension direction of a fiber orientation of the at least one fiber layer;
- and
- separating off the removed at least one fiber layer in a defined manner at a separating edge defined by a separating device placed on the fiber composite component.
Dependencies are inferred from the claim text.