公开(公告)号：US20220281097A1

公开(公告)日：2022-09-08

申请号：US17684646

申请日：2022-03-02

Applicant: Airbus Operations SAS

Inventor： Brice ALBERT ,  Benjamin TRARIEUX ,  Stéphane DAURE ,  Julien BIGOT ,  Damien BATTISTELLA

IPC: B25G3/02 ,  B25G1/04 ,  B25B23/00 ,  B25B11/00

Abstract: A method for installing a screw in at least one through-orifice of a box-type structure, including inserting a body of a first tool into the through-orifice from an external region of the box-type structure, moving the body in an internal region of the box-type structure, towards an end of the box-type structure, securing the screw to the body, the first tool comprising a link connected to the body which remains accessible from the external region during the inserting, moving and securing steps, pulling on the link from the external region until the shank of the screw is positioned in the through-orifice, and separating the body from the screw.

公开(公告)号：US20230062638A1

公开(公告)日：2023-03-02

申请号：US17799954

申请日：2021-02-16

Applicant: Airbus Operations SAS

Inventor： Brice ALBERT ,  Benjamin TRARIEUX ,  Harleen KAUR ,  Stéphane DAURE

IPC: B64C9/32 ,  B64F5/10

Abstract: A method for manufacturing an aerodynamic structure including a first panel having an aerodynamic face, as well as a second reinforced panel. The method includes a step of stamping the second panel to obtain at least one raised shape which is recessed on the second face, and a step of joining the first and second panels by pressing them against each other outside the at least one raised shape. An aerodynamic shape is obtained using this method.