COATING FOR HOT-SHAPING CORE

The invention concerns a method for coating a core (1) for producing a turbomachine part (2) by isostatic compacting, for example a leading-edge shield of a blade, the coating method comprising the steps of:-S1: covering the core (1) by means of a first solution comprising a first refractory compone...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KLEIN, Gilles Charles Casimir, FRANCHET, Jean-Michel Patrick Maurice
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:The invention concerns a method for coating a core (1) for producing a turbomachine part (2) by isostatic compacting, for example a leading-edge shield of a blade, the coating method comprising the steps of:-S1: covering the core (1) by means of a first solution comprising a first refractory component configured to oppose the diffusion of species, the first component comprising a metal oxide,-S2: covering the core (1) by means of a second solution comprising a second component designed to bind the first component in such a way as to form a homogeneous layer, the second component comprising a mineral binder;-S3: applying a heat treatment to the covered core (1) in such a way as to dry the solution and solidify the coating.