公开(公告)号：US20240383598A1

公开(公告)日：2024-11-21

申请号：US18666960

申请日：2024-05-17

Applicant: Airbus Operations SAS

Inventor： Jean-Guillaume QUARANTA ,  William BRAS ,  Emy VINCON ,  Mathieu SENTENAC

IPC: B64C7/02 ,  B64D29/06

Abstract: An aircraft fairing having at least one structure, at least one fairing panel, at least one fastening element connecting the fairing panel and the structure, and at least one compressible seal interposed between first and second bearing zones that are as one, respectively, with the fairing panel and with the structure. The fairing panel comprises at least one rigid stop positioned in the first bearing zone, the stop and the compressible seal being configured such that the compression ratio of the compressible seal is less than or equal to 90%.

公开(公告)号：US20220340293A1

公开(公告)日：2022-10-27

申请号：US17725641

申请日：2022-04-21

Applicant: Airbus Operations SAS

Inventor： Michael BERJOT ,  Rémi LANSIAUX ,  William BRAS ,  Germain GUENEAU ,  Sébastien VAN ARENDONK ,  Jacques DEMANGE ,  Sébastien COMMENGE

IPC: B64D27/26

Abstract: A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader having a central part connected to the support and a first and a second end that are connected to thrust rods, at least one limiting system for limiting the travel of the spreader having an upper and a lower stop between which is positioned the first or second end of the spreader, the upper and the lower stop being connected to one another so as to form a single part connected to a fitting secured to the support.