Process for making a metal part such as a turbine engine blade reinforcement

1. A process for manufacturing a metal part, the process comprising:

manufacturing a three-dimensional metal structure made up of an insert which has properties which allow superplastic forming and diffusion welding to be carried out, and of multiple separate metal wires each encircling a periphery of said insert, wherein a space separates at least two adjacent separate metal wires of the multiple separate metal wires, and wherein said three-dimensional metal structure forms a preform of said metal part;

positioning said three-dimensional metal structure in a forming tool, and

hot-pressing said three-dimensional metal structure which causes agglomeration of said three-dimensional metal structure, so as to obtain said metal part.

2. The process for manufacturing a metal part according to claim 1 , wherein said manufacturing includes:

a first sub-step for manufacturing said insert;

a second sub-step for winding said multiple separate metal wires around said insert.

3. The process for manufacturing a metal part according to claim 2 , wherein said sub-step for manufacturing said insert is performed by forging or machining or casting or by a three-dimensional weaving process.

4. The process for manufacturing a metal part according to claim 1 , wherein the manufacturing comprises separately bending each of the multiple separate metal wires so that, after bending, each of the multiple separate metal wires forms one or more loops to encircle the periphery of said insert.

5. The process for manufacturing a metal part according to claim 4 , wherein, after bending each of the multiple separate metal wires, the insert is inserted into the one or more loops of each of the multiple separate metal wires.

6. The process for manufacturing a metal part according to claim 1 , wherein said process is a process for manufacturing a metal reinforcement for a leading edge or trailing edge of a blade of a turbine engine, or of a metal reinforcement of a propeller such that said metal part obtained during said hot pressing is a metal reinforcement.

7. The process for manufacturing a metal part according to claim 1 , wherein said hot-pressing is an isostatic pressing step or an isothermal forging step.

8. The process for manufacturing a metal part according to claim 1 , wherein said manufacturing includes:

a first sub-step for manufacturing said insert;

a second sub-step of bending said multiple separate metal wires such that each metal wire of said multiple separate metal wires exhibits at least one loop; and

a third sub-step of inserting said insert in each loop of said multiple separate metal wires.

9. The process for manufacturing a metal part according to claim 1 , wherein said insert is a metal insert.

10. The process for manufacturing a metal part according to claim 1 , wherein said multiple separate metal wires are bent into an A-shape.

11. The process for manufacturing a metal part according to claim 1 , wherein said multiple separate metal wires are titanium-based wires and/or SiC-Titanium wires.

12. The process for manufacturing a metal part according to claim 1 , wherein said process includes:

manufacturing multiple three-dimensional metal structures made up of an insert and of multiple metal wires surrounding said insert, where said multiple three-dimensional metal structures form a pre-form of said metal part;

positioning said multiple three-dimensional metal structures in a forming tool:

hot-pressing said multiple three-dimensional metal structures which causes agglomeration of said multiple three-dimensional metal structures, so as to obtain said metal part.

13. The process for manufacturing a metal part according to claim 1 , wherein the metal part is a turbine engine blade metal reinforcement.

14. The process for manufacturing a metal part according to claim 1 , wherein the space depends on a thickness of said multiple separate metal wires encircling the periphery of said insert.