| 摘要 |
<p>The invention concerns an engine pylon suspension attachment (10) of an engine (16) under an aircraft center section (12) comprising a rigid structure as well as a mechanism attaching said structure under the wing section. Said mechanism includes a front attachment member (22), a rear attachment member (24) and a structure (26) for recovering thrust forces. To enable an engine (16) of larger diameter to be installed under an existing aircraft wing section (12), the rear part (20b) of the engine pylon (10) is provided with a width increasing rearwards. Moreover, the rear attachment member (24) comprises two brackets which are fixed on either side of the rigid structure and two shackles which link each of the brackets to an additional transverse rib integrated in the wing section.</p> |
