发明名称 Interior covering device for an aircraft cabin incorporating at least one system
摘要 A device for interior covering of an aircraft cabin, intended to be fastened to a structure of an aircraft and to extend along a skin of the aircraft, the device comprising a covering panel. The covering panel bears at least one system, possibly through a system support. It advantageously comprises at least one air circulation pipe fastened to an exterior face of the covering panel, each air pipe having an upstream end equipped with a connection device.
申请公布号 US8915468(B2) 申请公布日期 2014.12.23
申请号 US201113181074 申请日期 2011.07.12
申请人 AIRBUS Operations S.A.S. 发明人 Sabadie Lionel;Bertandeau Laurent;Bernabe Thomas;Banis Christian;Tomasi Marc
分类号 B64C1/00;B64C1/06;H02G3/32;B64C1/40;B64D11/00 主分类号 B64C1/00
代理机构 Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P. 代理人 Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
主权项 1. A device for interior covering of an aircraft, the aircraft including a skin fastened onto frames by clips, said device comprising: a covering panel bearing at least one air circulation pipe fastened to an exterior face of the covering panel, the covering panel being fastened to fastening supports on the frames, wherein the at least one air circulation pipe has an upstream end, equipped with a connection device, and wherein the at least one air circulation pipe has a downstream end, opening onto at least one air outlet, said at least one air outlet traversing the covering panel.
地址 Toulouse FR