According to the invention, a method is provided for preparing a reconditioning of a damaged portion of a component, particularly of an aircraft, by adding an insert, which fills and/or bridges the damaged portion, comprising the steps of: producing a 3D CAD repair model of the damaged portion by scanning; analysing the repair model and thus evaluating complexity of the damage and/or its reconditioning; as a function of the complexity, deciding between at least two alternative means to perform at least a following step, which is analysing the repair model and thus dimensioning the reconditioning including the insert. Further, according to the invention, an insert is provided for filling and/or bridging a damaged portion for reconditioning of the damaged portion of a component, particularly of an aircraft, produced according to the method.
METHOD FOR RECONDITIONING OF A DAMAGED PORTION OF A COMPONENT AND INSERT THEREFOR
VERFAHREN ZUR NEUKONDITIONIERUNG EINES BESCHÄDIGTEN TEILS EINER KOMPONENTE UND EINSATZ DAFÜR
PROCÉDÉ DE RECONDITIONNEMENT D'UNE PARTIE ENDOMMAGÉE D'UN COMPOSANT ET ÉLÉMENT INSÉRÉ
2021-03-03
Patent
Electronic Resource
English
IPC: | G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / 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 |
METHOD FOR RECONDITIONING OF A DAMAGED PORTION OF A COMPONENT AND INSERT THEREFOR
European Patent Office | 2018
|Method for reconditioning of a damaged portion of a component and insert therefor
European Patent Office | 2019
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