An improved monument structure combining an integrated construction system with carbon fiber reinforced composites to form an exoskeleton chassis. The chassis includes an above work deck subassembly, a below work deck subassembly, and a rear service wall subassembly, each respective subassembly is formed using carbon fiber reinforced composites (CFRC) pre-impregnated panel skins. The subassemblies are reinforced with a unidirectional carbon fiber.
Aircraft galley monument structure
07.06.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |