发明名称 PANEL STRUCTURE AND ASSOCIATED METHOD
摘要 PROBLEM TO BE SOLVED: To provide a panel structure that satisfies safety and testing standards yet also enables a lower mass construction.SOLUTION: A panel structure for a vehicle, especially for an aircraft or spacecraft, includes an area member 2, specifically a skin member, that defines an areal expanse with a first surface 3 and an opposite second surface 4 and having a thickness 5 between the first surface 3 and the second surface 4; and a plurality of elongate stiffener members 6 which are attached to the area member 2 and extend over at least one of the first and second surfaces 3, 4; where at least one of the stiffener members 6 is bifurcated at a bifurcation point into two or more branch stiffener members 6'.SELECTED DRAWING: Figure 15
申请公布号 JP2016078838(A) 申请公布日期 2016.05.16
申请号 JP20150183133 申请日期 2015.09.16
申请人 AIRBUS OPERATION GMBH 发明人 OLIVER SEACK
分类号 B64C1/12;B29C67/00;B33Y10/00;B33Y80/00;B64C1/00;B64F5/00 主分类号 B64C1/12
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