-
公开(公告)号:US11325715B2
公开(公告)日:2022-05-10
申请号:US16807351
申请日:2020-03-03
Applicant: Airbus Operations SAS
Inventor: Thomas Deforet , Rémi Lansiaux , Olivier Dubois , Anthony Mertes , David Alric , Stéphane Nogues
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, extending between first and second ends that has a central part connected to the support by a principal link comprising a principal rotation axis, at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops, secured to a fitting secured to the support, between which the extension is positioned.