Process for manufacturing a monolithic leading edge

Process for manufacturing a monolithic leading edge (21) for aircraft aerodynamic surfaces formed by an outer skin (23) and a plurality of inner ribs (25) characterised by comprising the following steps: a) providing a male tool made the assembly of a plurality of blocks (31); b) cutting dry carbon...

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Bibliographic Details
Main Authors CALA ROMERO, ANTONIO, JIMENEZ GAHETE, ANTONIO, MARTIN PRIETO, FERNANDO, AMBITE IGLESIAS, JUAN CARLOS
Format Patent
LanguageEnglish
French
German
Published 21.03.2007
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Summary:Process for manufacturing a monolithic leading edge (21) for aircraft aerodynamic surfaces formed by an outer skin (23) and a plurality of inner ribs (25) characterised by comprising the following steps: a) providing a male tool made the assembly of a plurality of blocks (31); b) cutting dry carbon fibers layers for the skin (23) and the ribs (25); c) laminating dry fibers layers on the lateral sides (32) of said blocks (31) forming half ribs (37); d) assembling the male tool (33) with the ribs (25) to be formed with two half ribs (37) laminated on adjacent blocks (31) integrated on it;. e) laminating dry fibers layers (39) for the skin (23) on the male tool (33); f) placing the female tool (35) over the male tool (33) closing a mould for the next step; g) performing a resin injection / curing process under high temperature conditions.
Bibliography:Application Number: EP20050381045