公开(公告)号：US20200307815A1

公开(公告)日：2020-10-01

申请号：US16826993

申请日：2020-03-23

Applicant: Airbus Operations SAS

Inventor： Isabelle PETRISSANS ,  Rémi LANSIAUX ,  Pascal FORICHON ,  Patrice PEREZ ,  Wan HU

IPC: B64D27/26

Abstract: An assembly for an aircraft, which includes a pylon with a bearing face and a contact face, an engine mount with a bearing face and a contact face bearing against the contact face of the pylon, at least two bolts comprising a threaded stem with a head and a nut bearing against the bearing face of the engine mount, for each head, a bearing washer with a first bearing face and a second bearing face, where the second bearing face of the bearing washer bears against the bearing face of the pylon, and where the head bears against the first bearing face of the bearing washer, a shoe, and, for each bearing washer, a clamp that is secured to the shoe and comprises a first branch and a second branch between which the bearing washer is clamped and is free to rotate.

公开(公告)号：US20200262571A1

公开(公告)日：2020-08-20

申请号：US16791094

申请日：2020-02-14

Applicant: Airbus Operations SAS

Inventor： Michael BERJOT ,  Isabelle PETRISSANS

IPC: B64D27/26

Abstract: An assembly comprising a wing with lower spars, a mounting pylon having an upper spar and two lateral panels, a front fixing system and a rear fixing system, each comprising a beam pierced with a principal bore and, for each beam, an upper bore traversing the upper spar and a shear pin positioned in the upper bore and in the principal bore. The assembly also comprises, for each fixing system, bolts, the nut of which is accommodated in a secondary hole of the beam and the screw of which traverses the upper spar and the beam in order to be screwed into the nut.