Method of repairing machined components such as turbomachine blades or blades of blisks

1. A method of using machining to repair a component workpiece, from a known and undamaged profile of the component, the method comprising:

acquiring coordinates of points on an envelope of the component workpiece, the set of points forming a cluster of points;

comparing the known and undamaged profile with the cluster of points in order to define zones on the component workpiece that have excess or insufficient thickness;

deforming the profile using a morphing method so that the deformed profile interpolates the cluster of points, the deformation of the profile using a morphing function, and

machining the component workpiece using a machine tool parameterized on the basis of the morphing function,

wherein the deforming of the profile involves

comparing each zone of the component workpiece that has excess or insufficient thickness with elementary deformation configurations (EDCs) each in the form of a mesh portion simulating the known and undamaged profile, and previously measured points simulating points of the cluster of points obtained from a damaged workpiece other than the component workpiece, the elementary deformation configurations (EDCs) being filed in a database,

identifying an EDC from the database of EDCs for the zone of the component workpiece based on the comparison of the zone of the component workpiece and the EDCs filed in the database,

using expert-defined EDC deformation parameters for the identified EDC to determine the morphing function, the parameters being stored in the database, and

defining the morphing function required to deform the known and undamaged profile portion of the identified EDC to match the previously measured points portion of the identified EDC, and

wherein the expert-defined EDC deformation parameters comprise coordinates of at least one control point to be displaced on the mesh portion simulating the known and undamaged profile, and at least one displacement vector for the at least one control point to displace to deform the mesh portion and to reduce differences between the mesh portion and previously measured points simulating points of the cluster of points obtained from a damaged workpiece other than the component workpiece.

2. The method as claimed in claim 1 , wherein the profile of the component includes a mesh of points.

3. The method as claimed in claim 2 , wherein the coordinates and displacement vectors of the points of the mesh that are to be displaced in order to interpolate the cluster of points, known as the control points, are parameters of the morphing function.

4. The method as claimed in claim 1 , wherein a three-dimensional measurement machine (3DMM), with or without physical sensing, acquires the coordinates of the points on the envelope of the component workpiece.

5. The method as claimed in claim 1 , wherein the component workpiece is a component to which material has been added.

6. The method as claimed in claim 1 , further comprising associating parameters of the morphing function with an elementary deformation configuration (EDC).

7. The method as claimed in claim 3 , wherein the morphing function parameters are entered by an expert.

8. The method as claimed in claim 1 , wherein if no match is found to any elementary deformation configuration (EDC) in the database, input will be required from an expert, and stored in the database for future use.

9. The method as claimed in claim 1 , wherein the elementary deformation configurations (EDCs) are parameterized surfaces defined by Bezier curves.

10. The method as claimed in claim 1 , wherein the database comprises EDCs for which an optimal mesh deformation has been calculated to interpolate the previously measured points simulating points of the cluster of points obtained from a damaged workpiece other than the component workpiece, for various mesh portions and previously measured points.

11. The method as claimed in claim 1 , wherein each zone of the component workpiece that has excess or insufficient thickness is compared to EDCs from the database based on differences in shape, scale ratio, and analysis as a function of a position of the mesh portion simulating the known and undamaged profile.