公开(公告)号：US10563422B2

公开(公告)日：2020-02-18

申请号：US16012241

申请日：2018-06-19

Applicant: Airbus SAS ,  Airbus Operations SAS

Inventor： Jean-Claude Marty ,  Julien Charles ,  Olivier Lebahar ,  Franck Dobigeon ,  Guillaume Ferrer ,  Thierry Borja ,  Sebastien Hanser

IPC: E04H15/20 ,  B29C73/02 ,  B05D3/02 ,  B05D3/04 ,  B29C73/34 ,  B05D5/00 ,  B29L31/30 ,  B64C1/06

Abstract: A method for repairing a structure comprising at least one zone to be heated and which comprises the steps of inflating a frame to form a framework, attaching panels removably to the frame to form an enclosure referred to as a heating enclosure, positioning the enclosure over the zone, heating the interior space of the enclosure using a heating device.

公开(公告)号：US10183451B2

公开(公告)日：2019-01-22

申请号：US15216914

申请日：2016-07-22

Applicant: Airbus SAS ,  Airbus Operations SAS

Inventor： Guillaume Ferrer ,  Thierry Borja ,  Julien Charles

IPC: B29C73/08 ,  B29C73/06 ,  B29C73/12 ,  B29C73/30 ,  B29L31/30

Abstract: A method and a tool for repairing a composite-material panel of an aircraft with at least one repair part made of composite material without using an autoclave. The repair method includes the steps of preparing the panel, placing at least one repair part made of composite material on the second face to cover a damaged zone, positioning a vacuum bag configured to sealingly cover the repair part, polymerizing or consolidating the repair part, compressing the vacuum bag against the repair part using a compression plate concomitantly with the step in which the repair part is polymerized or consolidated.

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。

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.