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
07.03.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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