An aircraft skin part having a leading edge (1) made of composite material, said part having an inner face which part comprises on its inner face a metallic type reinforcement (2) directly and firmly adhered to the said inner face of the leading edge by having been sprayed thereon, said reinforcement being arranged such that the cost of implementing this material and of reinforcing it is much less than that of Glare, while at the same time it has a better capacity to adapt to deformability and a greater absorption of energy due to impacts, typically due to bird impacts.
LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL
BORD D'ATTAQUE POUR AVION FAIT DE MATERIAU COMPOSITE RENFORCE
2015-05-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL
European Patent Office | 2018
|European Patent Office | 2023
|Composite airfoil with rolled fiberglass reinforced leading edge
European Patent Office | 2020
|