发明名称 AIRCRAFT PANEL FOR AN INTERIOR OF AN AIRCRAFT AND METHOD FOR MAKING THE AIRCRAFT PANEL
摘要 Aircraft panel 1 for an interior of an aircraft, wherein the aircraft panel 1 has a sandwich structure 2, wherein the sandwich structure 2 comprises a core section 4 and a covering section 3 as sandwich layers, wherein the covering section 3 comprises a prepreg layer 6 and wherein the aircraft panel 1 comprises at least one switching element 8 for activating at least one electrical device of the aircraft, wherein at least one switching element 8 is fixed in the covering section 3 by the prepreg layer 6.
申请公布号 US2015232165(A1) 申请公布日期 2015.08.20
申请号 US201514613598 申请日期 2015.02.04
申请人 DIEHL AIRCABIN GMBH 发明人 STAUDIGEL Norbert
分类号 B64C1/06;B32B3/08;B32B3/12;B32B37/18 主分类号 B64C1/06
代理机构 代理人
主权项 1. An aircraft panel for an interior of an aircraft, wherein the aircraft panel has a sandwich structure, which comprises a core section and a covering section as sandwich layers, wherein the covering section comprises a prepreg layer, and the aircraft panel comprises at least one switching element for activating at least one electrical device of the aircraft, wherein the at least one switching element is fixed in the covering section by the prepreg layer, and wherein the aircraft panel comprises at least one supporting element for the supportive holding of the switching element in the aircraft panel, wherein the supporting element is configured as a platelet with a central depression and with a circumferential edge region.
地址 Laupheim DE