A wing assembly includes a center wing structure (150) and a pair of outer wing structures (210). The center wing structure (150) includes a center wing front spar (152), a center wing rear spar (154), and an engine mounting location on each side of a wing centerline (124). Each outer wing structure (210) includes an outer wing front and rear spar (212,214) configured to be coupled respectively to the center wing front and rear spar (152,154) to define a wing joint (172) coupling the outer wing structure (210) to the center wing structure (150). The center wing structure (150) is configured such that the spar terminal ends (156) of the center wing front and rear spars (152,154) at each wing joint (172) are located no further inboard than an engine centerline (108) associated with the engine mounting location, and no further outboard of the engine centerline (108) than ten percent of a distance between the engine centerline (108) and the wing centerline (124).
WING ASSEMBLY HAVING WING JOINTS JOINING OUTER WING STRUCTURES TO CENTER WING STRUCTURE
FLÜGELANORDNUNG MIT FLÜGELVERBINDUNGEN ZUM VERBINDEN ÄUSSERER FLÜGELSTRUKTUREN MIT MITTLEREN FLÜGELSTRUKTUR
ENSEMBLE D'AILE DOTÉ DE JOINTS D'AILE RELIANT LES STRUCTURES D'AILE EXTÉRIEURES À LA STRUCTURE D'AILE CENTRALE
2022-05-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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