An example aircraft wing (100) includes a skin (106, 202), a composite shear tie (206, 306), a stringer base charge (308) overlaying the skin, and a stringer (110, 210, 310) overlaying the stringer base charge. The composite shear tie includes a shear-tie web (216), a first shear-tie flange (218) extending from a first side of the shear-tie web, a second shear-tie flange (220) extending from a second side of the shear-tie web, and a first shear-tie tab (222) extending from an end of the first side of the shear-tie web. The stringer includes a stringer web (228), a first stringer flange (230) extending from a first side of the stringer web, and a second stringer flange (232) extending from a second side of the stringer web. The first stringer flange is stitched to and integrated with the stringer base charge and the skin. Further, the first shear-tie flange is stitched to and integrated with the first stringer flange.
SHEAR TIES FOR AIRCRAFT WING
SCHERBÄNDER FÜR FLUGZEUGFLÜGEL
ATTACHES DE CISAILLEMENT POUR AILE D'AÉRONEF
2022-05-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |