METHOD FOR MANUFACTURING A COMPOSITE BLADE FOR AN AIRCRAFT ENGINE

ABSTRACT Method for manufacturing a blade (10) made of a composite material for a turbomachine, in particular of an aircraft, comprising steps consisting in: a) arranging a preform (24) produced by three-dimensional weaving of fibres within a mould (30), a polymerisable adhesive (26) being inserted...

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Bibliographische Detailangaben
Hauptverfasser:	RAVEY, Christophe, BOSSAN, Pierre-Antoine, DROZ, Nicolas, QUAGLIA, Nicolas, BLAISE, Maxime Marie Désiré
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING BLASTING COMBINED OPERATIONS ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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