METHOD FOR MANUFACTURING A MEMBER FOR REINFORCING AN AIRCRAFT BLADE

This invention relates to a process for manufacturing a reinforcement member for an aircraft blade. According to the invention, the manufacturing process comprises at least: .cndot. a plurality of positioning steps to position networks of reinforcement wires (10, 20) on supports (11, 21), each posit...

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Bibliographische Detailangaben
1. Verfasser:	GAFFIERO, Jacques
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	This invention relates to a process for manufacturing a reinforcement member for an aircraft blade. According to the invention, the manufacturing process comprises at least: .cndot. a plurality of positioning steps to position networks of reinforcement wires (10, 20) on supports (11, 21), each positioning step comprising a positioning of at least one network of reinforcement wires (10) on a support (11), .cndot. a plurality of securing steps to secure said networks of reinforcement wires (10, 20) with said supports (11, 21), each securing step comprising a securing of said at least one network of reinforcement wires (10, 20) with said support (11, 21) to form a monolithic subassembly (12, 22) following a same direction of superposition in a mould (13) and .cndot. a resin polymerization step (14) in said mould (13).