According to an embodiment, 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. The method involves: 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, 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
2018-05-17
Patent
Electronic Resource
English
Method for reconditioning of a damaged portion of a component and insert therefor
European Patent Office | 2019
|METHOD FOR RECONDITIONING OF A DAMAGED PORTION OF A COMPONENT AND INSERT THEREFOR
European Patent Office | 2021
|