公开(公告)号：US11242157B2

公开(公告)日：2022-02-08

申请号：US16782271

申请日：2020-02-05

Applicant: Airbus Operations SAS

Inventor： Olivier Gleize

IPC: B64D27/26 ,  B64D29/02

Abstract: A primary structure of an aircraft pylon, which comprises upper and lower spars, right-hand and left-hand lateral panels, transverse reinforcers that are disposed in transverse planes and, each have a square or rectangular contour and at least one sole to which the upper and lower spars and the right-hand and left-hand lateral panels are fastened. At least one of the transverse reinforcers of the primary structure has first and second link rods that are oriented along diagonals of the transverse reinforcer, and connecting systems that each connect first and second ends of the first and second link rods to the sole or to one of the soles.

公开(公告)号：US11319081B2

公开(公告)日：2022-05-03

申请号：US16437260

申请日：2019-06-11

Applicant: Airbus Operations SAS

Inventor： Thomas Deforet ,  Benoit Orteu ,  Olivier Gleize

IPC: B64D27/26 ,  B64D27/18

Abstract: A mounting pylon comprising a structure that comprises two C-shaped semi-structures and comprising an upper spar, a lower spar and a lateral flank, an upper panel, a lower panel, a reacting attachment point, two bars attached between the reacting attachment point and a jet engine, and a front wing attachment point attached to a wing box. The lateral flank comprises joists that are aligned between the front wing attachment point and the reacting attachment point, and where the angles between two successive joists are equal.