Fuselage sections (300) having tapered wing rib interfaces (306) are disclosed. A disclosed example apparatus includes a rib (306) associated with a fuselage section (300), and a wing interface surface defined by the rib (306), where the wing interface surface is tapered relative to a longitudinal axis (330) of the fuselage section from an aft end of the fuselage section (300) to a fore end of the fuselage section (300).
FUSELAGE SECTIONS HAVING TAPERED WING RIB INTERFACES
RUMPFSEKTIONEN MIT KONISCHEN FLÜGELRIPPENSCHNITTSTELLEN
SECTIONS DE FUSELAGE AYANT DES INTERFACES DE NERVURE D'AILE CONIQUES
14.04.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |