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
19.02.2025
Patent
Elektronische Ressource
Englisch
LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL
Europäisches Patentamt | 2015
|LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL
Europäisches Patentamt | 2018
|