An aircraft wing cover (10) comprising an integrally stiffened sandwich panel including first and second skins (11, 12) sandwiching a core layer (13), wherein at least one of the skins has a plurality of spanwise extending integral regions of increased thickness (18) accommodated by corresponding regions (19) of decreased thickness in the core. Also, a method of fabricating an aircraft wing cover, and a method of designing an aircraft wing.
AIRCRAFT WING COVER COMPRISING A SANDWICH PANEL AND METHODS TO MANUFACTURE AND DESIGN THE SAID WING COVER
FLUGZEUGFLÜGELABDECKUNG MIT EINER SANDWICHPLATTE SOWIE VERFAHREN ZUR KONZEPTION UND HERSTELLUNG DIESER FLÜGELABDECKUNG
PANNEAU DE VOILURE D'AÉRONEF COMPRENANT UN PANNEAU SANDWICH ET MÉTHODES POUR LA FABRICATION ET LA CONCEPTION DUDIT PANNEAU DE VOILURE
2016-01-13
Patent
Electronic Resource
English
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