| 摘要 |
<p>The assembly i.e. double flow turbojet assembly (6), has a rigid structure (30) with a set of fasteners (38, 78, 94). A set of aerofoil fasteners (40, 98) is fixed at the rigid structure for fixing of an aerofoil (2) of an aircraft i.e. commercial plane. A set of force recovery units is arranged at the rigid structure for recovery of forces along longitudinal direction (X), transversal direction (Y), and vertical direction (Z) of the turbojet. One recovery unit is arranged behind another recovery unit according to the longitudinal direction and is integrated into side beams (34, 36). An independent claim is also included for an aircraft wing and propelling unit assembly.</p> |
