| 摘要 |
<p>The present invention relates to a device for attaching an aircraft engine comprising a rigid structure forming a box, and a device for taking up the thrust forces having a main brace (34) mounted fixedly on one of the longerons (17) forming the box, by fixing means (40). According to the invention, the means (40) comprise a fixing pin (50) mounted on the longeron (17) and having a main portion (54) situated externally with respect to the box, this brace (34) having the portion (54) of the pin (50) passing through it and being pressed against the longeron (17) by a bell-shaped support washer (68) surrounding the main portion (54) and stressed by a screw (72) passing through it, the latter being screwed into a barrel nut (78) housed in a bore (74) formed within the main portion (54).</p> |
