Core for high-temperature shaping of a metal part and manufacturing, regeneration and shaping process
AssigneeSafran Aircraft Engines
InventorsGilles Charles Casimir Klein, Dominique Michel Serge Magnaudeix
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Abstract
A metal core for hot-forming a titanium-based alloy metal component is disclosed. The metal core has on an outer surface, intended to come into contact with the metal component, a layer of metal carbonitride-enriched material. The metal core comprises a nickel- or cobalt-based alloy. The metal core comprising a steel coating having an outer surface intended to come into contact with the metal component, the steel coating having a layer of metal carbonitride-enriched material. Processes for manufacturing and regenerating the metal core and a process for hot-forming a metal component using the metal core are also disclosed.
Claims10
Metal core for hot-forming a titanium-based alloy metal component, the metal core comprising a nickel- or cobalt-based alloy core and the metal core comprising a steel coating having an outer surface intended to come into contact with the metal component, the steel coating having a layer of metal carbonitride-enriched material.
Dependencies are inferred from the claim text.