TURBOMACHINE ELEMENT COMPRISING AT LEAST ONE BLADE OBTAINED BY ADDITIVE MANUFACTURING

The present invention relates to a turbomachine element (1), comprising at least one blade (2) obtained by additive manufacturing, the blade (2) having a skin (4) and an internal lattice (6) allowing air circulation in the blade (2) and having an additive manufacturing support function for the skin...

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Bibliographische Detailangaben
Hauptverfasser: BOISSELEAU, Denis, Daniel, Jean, BETBEDER-LAÜQUE, Xavier, Roger, VOTIE, Sylvain Pierre
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:The present invention relates to a turbomachine element (1), comprising at least one blade (2) obtained by additive manufacturing, the blade (2) having a skin (4) and an internal lattice (6) allowing air circulation in the blade (2) and having an additive manufacturing support function for the skin (4).