METHOD FOR MANUFACTURING A COMPOSITE MATERIAL VANE WITH AN ATTACHED METAL LEADING EDGE

A method for manufacturing a blade in composite material with added metal leading edge for gas turbine aeroengine, the method including producing a batch of plurality of blade bodies in composite material; creating a digital model of a blade body from a blade in the batch of plurality of blade bodie...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SUCHEL, Christian, MACHERET, Christine, JOBEZ, Sophie Martine, GOUET, Sébastien
Format: Patent
Sprache:eng
Schlagworte:
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