B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 45/02 (2006.01)
Patent
CA 2501503
An aircraft panel assembly (10) is provided, including a panel core (28), a plurality of pre-preg layers (30) surrounding the panel core (28) forming an internal layer of plies, at least one metal foil layer (38) positioned on an outer layer of the internal layer of plies. The at least one metal foil layer (38) providing an electrical conduit between the outer surface (24) of the aircraft panel assembly (10) and sub-structure (26) for grounding.
L'invention concerne un ensemble de panneaux (10) pour aéronef comprenant une âme (28) entourée d'une pluralité de couches préimprégnées (30) formant une couche interne de plusieurs épaisseurs, ainsi qu'au moins une feuille métallique (38) placée sur une couche externe de la couche interne des épaisseurs. Cette feuille métallique (38) forme un conduit électrique entre la surface externe (24) de l'ensemble de panneaux (10) de l'aéronef et l'infrastructure (26) pour la mise à la terre.
Gleason Gregory R.
Pham Doan D.
Tollan Mark W.
Smart & Biggar
The Boeing Company
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