Aircraft component panels stiffened with stringers with two types of local widenings.

摘要

Aircraft component comprising at least one panel (11) of composite material, comprising a coating (13) and a plurality of stiffeners stringers (15) configured with a web (17) and a foot (19) of width (A) , said stiffeners stringers (15) a first local enlargements (21) of its feet (19) designed to enable joining areas with other elements located on flat areas of the coating (13) and a local second widenings (23) feet comprising (19) intended to enable joining areas with other elements located in areas of the coating (13) including ramps (33) thickness change, which are formed on two end sections (41, 45) located on flat areas of the coating ( 13) and a central portion (43) located on one of said ramps (33) of the liner (13), being enabled one of said end sections (41, 45) and bond area with other elements.