公开(公告)号：US20210130001A1

公开(公告)日：2021-05-06

申请号：US17081193

申请日：2020-10-27

Applicant: Airbus Operations SAS

Inventor： Julien Allain ,  Stéphane Dida ,  Jérome Colmagro ,  Olivier Dubois ,  Julien Moulis ,  Jacky Puech ,  Laurent Lafont

IPC: B64D27/26 ,  B64F5/10 ,  F16B5/08

Abstract: The pylon, intended to support a flying vehicle engine, includes a primary structure formed by at least one longeron and one panel, the panel including at least one end part provided with a notch, the longeron being provided with an end adapted to be positioned in the notch, the panel and the longeron being assembled by welding a part of the end to a part of the notch. A welded primary structure enables minimization of the blanks of parts associated with the longerons and with the panels by avoiding having recourse to the production of edges.

公开(公告)号：US11807373B2

公开(公告)日：2023-11-07

申请号：US17081193

申请日：2020-10-27

Applicant: Airbus Operations SAS

Inventor： Julien Allain ,  Stéphane Dida ,  Jérome Colmagro ,  Olivier Dubois ,  Julien Moulis ,  Jacky Puech ,  Laurent Lafont

IPC: B64D27/26 ,  B64F5/10 ,  F16B5/08

CPC classification number: B64D27/26 ,  B64F5/10 ,  F16B5/08 ,  B64D2027/266

Abstract: The pylon, intended to support a flying vehicle engine, includes a primary structure formed by at least one longeron and one panel, the panel including at least one end part provided with a notch, the longeron being provided with an end adapted to be positioned in the notch, the panel and the longeron being assembled by welding a part of the end to a part of the notch. A welded primary structure enables minimization of the blanks of parts associated with the longerons and with the panels by avoiding having recourse to the production of edges.