公开(公告)号：US20180009543A1

公开(公告)日：2018-01-11

申请号：US15641771

申请日：2017-07-05

Applicant: Airbus Operations SAS

Inventor： Frederic JOURNADE ,  Eric BOUCHET ,  Nicolas GROSSEAU ,  Antoine MUTIN

IPC: B64D27/26

CPC classification number: B64D27/26 ,  B64D2027/266 ,  F16B37/047

Abstract: An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.