发明名称 航空機胴体のフレーム要素
摘要 The elements (101-103) have a cross-piece part (1a) and a frame section (1b) i.e. upper/lower curved section, joined together into a single part, where the cross-piece part, the frame section and a rod (1c) forming three sides of the single part are arranged to form an integral triangle. A metal part, a machined part and an integral composite material part are arranged in element bodies. Junction parts are arranged at corners of a triangular general profile, where height of a profile of the junction parts is constant with respect to the cross-piece part, the frame section and the rod. An independent claim is also included for a frame assembly for a fuselage of an aircraft.
申请公布号 JP6054105(B2) 申请公布日期 2016.12.27
申请号 JP20120193366 申请日期 2012.09.03
申请人 エアバス オペラシオン(エス.ア.エス) 发明人 ドラエ.ロマン;リーベン.パトリック;ミアレ.クリストフ
分类号 B64C1/06 主分类号 B64C1/06
代理机构 代理人
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