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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Main Authors | , , , |
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Format | Patent |
Language | English French German |
Published |
21.03.2007
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Subjects | |
Online Access | Get full text |
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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. |
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Bibliography: | Application Number: EP20050381045 |