发明名称 PREINSTALLED, ADAPTABLE ELECTRICAL GRID FOR AIRPLANES
摘要 An aircraft structure is provided that includes, but is not limited to structural elements, a first multitude of lines that are in a fixed manner connected to structural elements, a second multitude of lines that are in a fixed manner connected to structural elements and whose longitudinal direction intersects the longitudinal direction of the first multitude of lines so that the longitudinal directions of the lines form a network that covers the aircraft structure at least in some sections, and connecting elements in order to, in the state of the structural elements installed in the aircraft structure, connect selected lines of the first multitude to selected lines of the second multitude of selected points of intersection of the network in order to in this way form transmission lines, such as lines for electricity transmission and/or data transmission. Furthermore, a method is provided for manufacturing such an aircraft structure.
申请公布号 EP2359448(B1) 申请公布日期 2017.03.29
申请号 EP20090774896 申请日期 2009.12.11
申请人 Airbus Operations GmbH 发明人 BROWNJOHN, Nicholas;OSTERNACK, Stefan
分类号 H02G3/00;B64D47/00;H02G3/30;H02G3/36 主分类号 H02G3/00
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