TORSION BOX FOR AN AIRCRAFT STIFFENED WITH NON-PARALLEL STRINGERS

TORSION BOX FOR AN AIRCRAFT STIFFENED WITH NON-PARALLEL STRINGERS

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 t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: HONORATO RUIZ, Francisco Javier, CASADO ABARQUERO, Hugo, CRUZ DOMÍNGUEZ, Francisco José
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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.