A method and apparatus for an aircraft structure. In one advantageous embodiment, the aircraft structure (400,526) may have a rib (506-510), a plurality of stringers (512-522), and a set of shear ties (600,602). The plurality of stringers may have skin flanges (608-612) at ends of the plurality of stringers capable of being fastened to skin (524) for the aircraft structure. The set of shear ties may extend from the rib and have a set of elongate members (624-635) in which the set of elongate members are attached to the plurality of stringers.
Rib support for wing panels
Stützrippen für Flügelpaneele
Support nervuré pour panneaux ailés
02.11.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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