| 摘要 |
<p>The invention concerns an assembly for aircraft comprising a wing system element (2) as well as an attachment mast, the assembly further comprising means for attaching (8) the mast on the element (2), said means (8) including two front half-attachments (29a) each provided with a shackle (38) and designed to absorb stresses exerted along a vertical direction, said shackle being mounted articulated on a first fitting (50) integral with a front spar (34) of the element (2) extending along a wingspan direction (32) and mounted articulated on a second fitting (42) integral with a rigid structure (6) of the mast. The invention is characterized in that the two shackles (38) are arranged in a common plane (P) parallel to the direction (32).</p> |
