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
03.03.2021
Patent
Elektronische Ressource
Englisch
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
Europäisches Patentamt | 2018
|Method for reconditioning of a damaged portion of a component and insert therefor
Europäisches Patentamt | 2019
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