B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 3/26 (2006.01) B64C 3/00 (2006.01) B64C 3/20 (2006.01)
Patent
CA 2682289
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.
La présente invention concerne un bord d'attaque (1) pour avion fait de matériau composite, caractérisé en ce que sa face interne comporte un renforcement de type métallique (2) qui adhère solidement à ladite face interne du bord d'attaque (1) ; et qui est agencé pour permettre au bord d'attaque (1) de mieux s'adapter à la déformabilité et de mieux absorber l'énergie causée par les impacts. L'invention concerne également un procédé de fabrication d'un bord d'attaque (1) à renforcement métallique (2) pour avion fait de matériau composite.
Airbus Operations S.l.
Bereskin & Parr Llp/s.e.n.c.r.l.,s.r.l.
LandOfFree
Leading edge for aircraft made of reinforced composite material does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Leading edge for aircraft made of reinforced composite material, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Leading edge for aircraft made of reinforced composite material will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-2050070