发明名称 Aircraft galley monument structure
摘要 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.
申请公布号 US9359078(B2) 申请公布日期 2016.06.07
申请号 US201313850781 申请日期 2013.03.26
申请人 B/E Aerospace, Inc. 发明人 Burd Peter John Leslie
分类号 B64D11/04 主分类号 B64D11/04
代理机构 Fulwider Patton LLP 代理人 Fulwider Patton LLP
主权项 1. A monument for an aircraft, comprising an above work deck subassembly, a below work deck subassembly, and a rear service wall subassembly, wherein the above work deck subassembly and below work deck subassembly are each manufactured and cured as a complete integrated structural subassembly of carbon fiber reinforced composites (CFRC) pre-impregnated panel skins, and wherein localized reinforcement at mating surfaces is established by application of unidirectional carbon fiber plies at a juncture of the mating surfaces over the CFRC pre-impregnated panel skins.
地址 Wellington FL US