Method for producing a blade for a turbomachine

Disclosed is a method for producing a blade for a turbomachine, in particular for an aero engine. The method comprises providing at least one blade airfoil with a first platform region and at least one blade root with a second platform region and joining the blade airfoil and the blade root at the r...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Smarsly, Wilfried, Schloffer, Martin
Format: Patent
Sprache:eng
Schlagworte:
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