The invention relates to an integrated structure of a composite material multispar torsion box (1) for aircraft, comprising a lower skin (12), an upper skin (11), several spars (9) defining cells (14), the first cell (19) being the closest to the input of load in the box (1), said structure comprising unit elements in the first cell, which unit elements provide the torsion box (1) with the necessary torsional rigidity to prevent the deformations occurring as a result of local loads.
STIFFENED MULTISPAR TORSION BOX
VERSTEIFTER MEHRFACHHOLMTORSIONSKASTEN
CAISSON DE TORSION MULTILONGERON RENFORCE
2016-09-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |