Airbus Operations (s.a.s.)

Olivier Gleize

Thomas Deforet

Benoit Orteu

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.

Mounting pylon for a jet engine of an aircraft comprising a particular structure

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.

Primary structure of an aircraft pylon having at least one transverse reinforcer equipped with two diagonally disposed link rods, and aircraft comprising such a primary structure

Growing community of inventors

Toulouse, France

Olivier Gleize