| 摘要 |
<p>The invention relates to an aeroplane structure comprising structural elements (10, 12, 13); a first plurality of lines (11) fixed to structural elements (10); a second plurality of lines (14, 15) fixed to structural elements (12, 13), the longitudinal direction of the second lines crossing the longitudinal direction of the first lines such that the two longitudinal directions form a network spanning the aeroplane structure at least in sections; and connecting elements for connecting selected lines of the first plurality of lines to selected lines (14, 15) of the second plurality of lines at selected points of intersection of the network, when the structural elements (10, 12, 13) are integrated into the aeroplane structure, in order to create lines for the transmission of current and/or data. The invention also relates to a method for producing such an aeroplane structure.</p> |
