An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.
BEADED COMPOSITE STRUCTURAL WEB
2024-09-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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