Method for manufacturing a base structure (8) of an aeronautical torsion box (1) for an aircraft (11) characterized in that it comprises the steps of: a.- providing at least a fresh skin (3), at least one fresh stringer (4), at least a fresh front spar (5) and fresh rear spar (6), b.- positioning the fresh skin (3), the at least one fresh stringer, the fresh spars (5, 6) in a curing tool in a configuration corresponding to that of a base structure (8), c.- subjecting the structure (8) to a single curing cycle, obtaining a cured base structure (8).
METHOD FOR MANUFACTURING AN AERONAUTICAL TORSION BOX, TORSION BOX AND TOOL FOR MANUFACTURING AN AERONAUTICAL TORSION BOX
VERFAHREN ZUR HERSTELLUNG EINES AERONAUTISCHEN TORSIONSKASTENS, TORSIONSKASTEN UND WERKZEUG ZUR HERSTELLUNG EINES AERONAUTISCHEN TORSIONSKASTENS
PROCÉDÉ DE FABRICATION D'UN CAISSON DE TORSION AÉRONAUTIQUE, CAISSON DE TORSION ET OUTIL DE FABRICATION D'UNE CAISSE DE TORSION AÉRONAUTIQUE
2018-03-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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