公开(公告)号：US11046414B2

公开(公告)日：2021-06-29

申请号：US16202762

申请日：2018-11-28

Applicant: Airbus Operations SAS

Inventor： Franck Batalla ,  Denis Soula ,  Javier Maqueda Lahoz

IPC: B64C1/26 ,  B64C3/18 ,  B64C1/06

Abstract: In order to be able to reduce the time and cost required for final assembly of an aircraft, a junction rib designed for the wing-central wingbox junction comprises a central web and an upper flange and a lower flange which extend from the main web, on a first side, the main web having a junction surface arranged on a second side opposite the first side, the main web including rows of orifices opening on the second side in the junction surface and on the first side, comprising a first row of orifices and a third row of orifices formed in an upper part of the main web on either side of the upper flange, and a second row of orifices formed in a lower portion of the main web, each one of the rows of orifices comprising orifices in a free state.

公开(公告)号：US20150175252A1

公开(公告)日：2015-06-25

申请号：US14566822

申请日：2014-12-11

Applicant: AIRBUS OPERATIONS SAS

Inventor： Franck Batalla ,  Denis Soula ,  Javier Maqueda Lahoz

IPC: B64C3/18 ,  B23K20/12

CPC classification number: B64C3/182 ,  B23K20/129 ,  B64C1/26 ,  B64F5/10 ,  Y10T29/49622

Abstract: A method for producing a central wing box including an upper panel, a lower panel, a front longeron, a rear longeron and four corners, wherein at least one panel and one longeron are obtained from a single flat metal wall which is bent along a bending line at approximately 90° which corresponds to a corner connecting said panel to said longeron.

Abstract translation: 一种用于制造中央翼盒的方法，包括上板，下板，前长龙，后长龙和四角，其中从弯曲的单个平板金属壁获得至少一个板和一个纵梁 线对应于将所述面板连接到所述龙门的角部的大约90°。

公开(公告)号：US09308711B2

公开(公告)日：2016-04-12

申请号：US13677557

申请日：2012-11-15

Applicant: Airbus Operations SAS

Inventor： Julien Charles ,  Guillaume Gallant ,  Denis Soula

IPC: B32B7/04 ,  B29C65/08 ,  B32B37/00 ,  B32B38/00 ,  B26D1/547 ,  B29C65/76 ,  B29C65/00 ,  B29L31/30

CPC classification number: B32B38/0004 ,  B26D1/547 ,  B29C65/08 ,  B29C65/76 ,  B29C66/0044 ,  B29C66/112 ,  B29C66/114 ,  B29C66/30223 ,  B29C66/532 ,  B29C66/721 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/8122 ,  B29C66/81427 ,  B29C66/8322 ,  B29C2793/009 ,  B29L2031/3076 ,  Y10T83/04 ,  Y10T428/24479 ,  B29K2827/18

Abstract: A method for disassembling two ultrasonically welded elements, one of the elements comprising, at a surface opposite the other element, an energy director that concentrates the heating during ultrasonic welding and forms a material junction between the two assembled elements after the ultrasonic welding. The method includes the steps of positioning a wire between the two assembled elements, so as to be secant to the energy director, said wire having suitable mechanical characteristics allowing it to cut the junction formed by the energy director and moving the wire between the two assembled elements so as to cut said junction.

公开(公告)号：US20130192433A1

公开(公告)日：2013-08-01

申请号：US13677557

申请日：2012-11-15

Applicant: AIRBUS OPERATIONS SAS

Inventor： Julien Charles ,  Guillaume Gallant ,  Denis Soula

IPC: B32B38/00 ,  B26D1/547

CPC classification number: B32B38/0004 ,  B26D1/547 ,  B29C65/08 ,  B29C65/76 ,  B29C66/0044 ,  B29C66/112 ,  B29C66/114 ,  B29C66/30223 ,  B29C66/532 ,  B29C66/721 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/8122 ,  B29C66/81427 ,  B29C66/8322 ,  B29C2793/009 ,  B29L2031/3076 ,  Y10T83/04 ,  Y10T428/24479 ,  B29K2827/18

Abstract: A method for disassembling two ultrasonically welded elements, one of the elements comprising, at a surface opposite the other element, an energy director that concentrates the heating during ultrasonic welding and forms a material junction between the two assembled elements after the ultrasonic welding. The method includes the steps of positioning a wire between the two assembled elements, so as to be secant to the energy director, said wire having suitable mechanical characteristics allowing it to cut the junction formed by the energy director and moving the wire between the two assembled elements so as to cut said junction.

Abstract translation: 一种用于拆卸两个超声波焊接元件的方法，其中一个元件在与另一元件相对的表面处包括在超声波焊接之间集中加热并在超声波焊接之后在两个组装元件之间形成材料接合的能量指向器。 该方法包括以下步骤：将线定位在两个组装元件之间，以便切割到能量指向器，所述线具有合适的机械特性，允许其切割由能量指向器形成的结，并且在两个组装的元件之间移动线 元件，以便切断所述连接处。