The improvement of the durability properties of metal parts is a major issue for many industrial sectors, such as aeronautics, aerospace, military, etc. The choice of the manufacturing process directly influences the microstructure and, therefore, the properties of the metallic alloys. The elaboration of metallic parts by pressure-assisted sintering processes, such as spark plasma sintering (SPS), represents a relevant way to explore as an alternative to conventional manufacturing processes (casting, forging, or machining) 1. During SPS, the powder inserted in a mold is densified by the simultaneous application of heating (via an electric current) and pressure (via a uniaxial charge). This fast sintering limits grain growth 2. SPS makes possible, in a single stage, the elaboration of high-performance materials and structural elements, with improved mechanical properties 3, even if in the case of parts having large sizes and/or complex shapes 4. The SPS process requires the use of graphite tooling (punches and die). As a consequence, one of the major issues is the carbon contamination of the metallic powder. In addition, graphite foils are inserted between the powder and the surfaces in contact with the tooling 5 to ensure a good electric, physical, and thermal contact of the tooling-powder assembly 6, but also to facilitate the sample demolding and to preserve the tooling. Whatever the used grade and the intended application, carbon contamination of the metallic powder during SPS must be considered and given special attention. One of the aims of the ANR OEDIPUS project (ANR-23-CE08-0028) is to develop physical vapor deposition (PVD) barriers against carbon diffusion during SPS process. In the
present project, a PVD coating of a pure element or an alloy will be deposited on the graphite foils to limit carbon diffusion.

The objective of the internship, which is part of the ANR OEDIPUS project, will be to study the diffusion phenomena occurring during the SPS process at the interface between the PVD-coated graphite foil and the metallic powders of different titanium and aluminum alloys, which are of great interest for aeronautics applications.

The internship will take place at the ICB laboratory (Dijon).

Sintering experiences will be performed within the CALHIPSO/EQUIPEX+ platform (ANR-21-ESRE-0039).

Microstructural, chemical, and mechanical characterizations (optical microscopy, SEM-EDS, XRD, microhardness, etc.) will be carried out within the
ARCEN-CARNOT platform.

Regular day trips to the company (Sintermat) are to be expected for certain sintering and characterization tests.

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2 P. Angerer et al., Mater. Sci. Eng. A 381 (2004) 16-19.
3 A. Bolsonella et al., J. Alloys Compd. 856 (2021) 157869.
4 S. Akhtar et al., Mater. Today Proc. 5 (2018) 18649-18655.
5 M. Moser at al. Metals 10 (2020) 948-965.
6 K. Vanmeensel et al., Acta Mater. 53 (2005) 4379-4388