The present invention relates to a leading edge (1) for aircraft made of composite material, characterized in that it comprises on its inner face a metallic-type reinforcement (2) firmly adhered to the mentioned inner face of the leading edge (1) arranged such that it confers the leading edge (1) with better capacity to adapt to deformability and greater absorption of energy due to impacts. The invention also relates to a method of manufacturing a leading edge (1) with a metallic reinforcement (2) for aircraft made of composite material.
LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL
AUS EINEM VERSTÄRKTEN VERBUNDWERKSTOFF HERGESTELLTE VORDERKANTE FÜR EIN FLUGZEUG
BORD D'ATTAQUE POUR AVION FAIT DE MATÉRIAU COMPOSITE RENFORCÉ
07.03.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL
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