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 |