The invention relates to an integrated multispar torsion box structure of composite material for aircraft, comprising a lower skin (12), an upper skin (11), several spars (9), each of which comprises in turn a chord (13) and a web (14), several stringers (10) in the lower skin (12) and several stringers (10) in the upper skin (11), characterized in that the mentioned integrated torsion box structure is achieved by means of joining unitary U-shaped structural elements (15), unitary U-shaped structural elements (16) with a flap and unitary C-shaped structural elements (17) with a flap. The invention also relates to a method for manufacturing an integrated multispar torsion box structure of composite material for aircraft.
MULTISPAR TORSION BOX MADE FROM COMPOSITE MATERIAL
AUS VERBUNDWERKSTOFF HERGESTELLTER TORSIONSKASTEN MIT MEHREREN HOLMEN
CAISSON DE TORSION MULTI-LONGERONS INTÉGRÉ EN MATÉRIAU COMPOSITE
2016-10-19
Patent
Elektronische Ressource
Englisch
Investigation on a multispar composite wing
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