Wing panels composed of metallic and composite materials.

摘要

A set (100) of wing for use on an aircraft (300), comprising: a structure (110) support having a first end portion adapted to be coupled to the aircraft (300); a set (102) of the top panel and a pair of top chords (104) of the beam, which extend in the direction of the crossbar, each said upper panel assembly and each of said upper spar chords being connected, and formed from metallic material, the assembly (102) exceeding the structure (110) being coupled support panel; a set (112) of the bottom panel and a pair of lower cords (114) of the beam, which extend in the direction of the crossbar, each said lower panel and each of said lower spar chords being connected, and formed from composite material, the assembly (112) of the bottom panel to the structure (110) support, and a pair of parts (120) interface, located at opposite ends of the cords of the structure (110) support being coupled coupling each part (120) interface of the top chords (104) of the beam with the corresponding lower chord (114) of the beam.