Torsion box of an aircraft stabilizing surface comprising a front spar (15), a rear spar (17), ribs (21) and upper and lower stiffened skins, in which at least one of said skins (31) is stiffened with a plurality of stringers (33, 43), preferably omega-shaped stringers, extending all of them along the full skin span, preferably in a "conical" distribution, and having a decreasing cross section towards the skin outer edge.
TORSION BOX FOR AN AIRCRAFT STIFFENED WITH NON-PARALLEL STRINGERS
MIT NICHT PARALLELEN BÄNDERN VERSTEIFTE HÜLLE EINER TORSIONSBOX FÜR FLUGZEUGE
REVÊTEMENT DE CAISSON DE TORSION POUR AVION RIGIDIFIÉ PAR DES LISSES NON PARALLÈLES
2018-03-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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