The invention refers to a reinforced leading edge section (1) for an aircraft, comprising:- an outer skin (2) formed with an aerodynamic leading edge profile,- an inner reinforcement (3) arranged internally with respect to the outer skin (2) along the span of the leading edge section (1), wherein said inner reinforcement (3) comprises a base (3') with a C-shaped configuration joined to the outermost part of the outer skin (2), and a web (3") having a free end (3"a) and an opposite end (3"b) joined to the base (3'), the web (3") extended in a direction transverse to the direction of the span of the leading edge section (1).
A REINFORCED LEADING EDGE SECTION FOR AN AIRCRAFT
VERSTÄRKTER VORDERKANTENABSCHNITT FÜR EIN FLUGZEUG
SECTION DE BORD D'ATTAQUE RENFORCÉE POUR UN AÉRONEF
2025-02-19
Patent
Electronic Resource
English
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