| 摘要 |
<p>The present invention regards an aeronautical structural section (3) provided for assembly with a mating section (3", 4), the section (3) comprises end portions (17a, 17b) adapted for join-up with said mating section (3", 4). The (3) comprises an elongated shaft-like element (7) exhibiting a first shaft entry (19a) and a second shaft entry (19b), each of which are provided in the respective end portion (17a, 17b). It also regards an aeronautical structure join-up comprising a plurality of sections (3) having shafts, wherein the sections (3) are arranged to each other for forming a common shaft. The present invention also regards a method for join-up of sections (3, 4) having channels together forming a common shaft (10) of the assembled join-up. It has steps of providing the sections (3, 4) comprising the elongated shaft-like elements (7); positioning the sections (3, 4) for join-up; and joining the sections (3, 4) to each other in such way that an entry (19a) of an element (7) of a first section (3) faces an entry (19b) of an element (7) of a joined second section (4) so that the elements (7) form a common shaft-like element (10).</p> |
