| 摘要 |
<p>The present invention relates to a connecting device two curved ribs (1, 2) of an aircraft or spacecraft, with: a coupling element (5) which can be connected by means of predetermined coupling sections (6, 7) to respective connecting sections (Vl, V2) of the two ribs (1, 2); wherein at least the predetermined coupling sections (6, 7) of the coupling element (5) are rectilinear Iy designed; and in that at least the respective connecting sections (Vi, V2) of the two ribs (1, 2) each have rectilinearly running inner belt regions (15) for a respective rectilinear connection of the predetermined coupling sections {6, 7) of the coupling element (5).</p> |
