-
1.发明授权公开(公告)号：US11820089B2
公开(公告)日：2023-11-21
申请号：US17092696
申请日：2020-11-09
Applicant: AIRBUS SAS , Airbus Operations S.A.S.
Inventor： Julien Charles , Franck Dobigeon , Guillaume Ferrer , Anthony Rince
CPC classification number: B29C73/10 , B29C35/08 , B29C2795/002 , B29K2995/002 , B29L2031/3076
Abstract: An assembly includes a bag and of a composite panel exhibiting a damaged region to be repaired by polymerization of a repair piece using the bag. The bag includes a sheet intended to be laid over the panel. When the panel and the sheet are laid one atop of the other, the sheet exhibits regions capable of absorbing heat emitted by radiation onto it in a proportion that is dependent on the polymerization temperature needed for that region of the panel that corresponds to it, the radiation being partially absorbed by suitable colouration of the sheet in the region concerned. Determining those regions of the panel in which radiation is less well absorbed than in others means that the heating can be adapted to suit the needs of polymerization in terms of repair and that even polymerization can thus be obtained over the entire damaged region, thereby consolidating the repair.
-
公开(公告)号：US11619645B2
公开(公告)日：2023-04-04
申请号：US16400417
申请日：2019-05-01
Applicant: Airbus SAS
Inventor： Julien Charles , Guillaume Ferrer
Abstract: A bumper for a vehicle, comprising at least one part made of resilient material, having a curved front portion forming an inner cavity. The front portion has apertures enabling the cavity to be put into communication with the exterior of the resilient part. At least one marking fluid cell is provided inside the cavity. A fastener is provided to fasten the one part to the vehicle.
-
Patent Agency Ranking
3.发明申请公开(公告)号：US20210146642A1
公开(公告)日：2021-05-20
申请号：US17092696
申请日：2020-11-09
Applicant: AIRBUS SAS , Airbus Operations S.A.S.
Inventor： Julien Charles , Franck Dobigeon , Guillaume Ferrer , Anthony Rince
Abstract: An assembly includes a bag and of a composite panel exhibiting a damaged region to be repaired by polymerization of a repair piece using the bag. The bag includes a sheet intended to be laid over the panel. When the panel and the sheet are laid one atop of the other, the sheet exhibits regions capable of absorbing heat emitted by radiation onto it in a proportion that is dependent on the polymerization temperature needed for that region of the panel that corresponds to it, the radiation being partially absorbed by suitable colouration of the sheet in the region concerned. Determining those regions of the panel in which radiation is less well absorbed than in others means that the heating can be adapted to suit the needs of polymerization in terms of repair and that even polymerization can thus be obtained over the entire damaged region, thereby consolidating the repair.
-
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
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.
-
5.发明授权公开(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
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：US11577795B2
公开(公告)日：2023-02-14
申请号：US16400438
申请日：2019-05-01
Applicant: Airbus SAS
Inventor： Julien Charles , Guillaume Ferrer
Abstract: A vehicle bumper comprising at least one part made of resilient material, in the interior of which there is provided at least one marking fluid cell with an opening to the exterior. The opening is closed by a closure device which, under the effect of a pressure applied with a determined intensity, can open up the opening, allowing the marking fluid to access the exterior of the cell through which the marking fluid can flow, and also comprising a securing element configured to secure the at least one part on the vehicle.
-
7.发明授权公开(公告)号：US10414097B2
公开(公告)日：2019-09-17
申请号：US15622820
申请日：2017-06-14
Applicant: Airbus Operations SAS , Airbus SAS
Inventor： Julien Vidal , Bruno Marechal , Guillaume Ferrer , Jean-Claude Marty
Abstract: A method and tool for repairing a damaged zone of an aircraft radome, using the actual radome itself as a heating chamber to avoid resorting to an autoclave and the removal of certain parts of the radome which cannot withstand the curing temperature needed for the repair. The method for repairing a radome, wherein the radome comprises a composite panel exhibiting a double curvature forming a dome, the panel comprising at least one damaged zone, comprises the steps of closing an interior space of the panel using a cap to form a repair chamber. The surface of the panel forms the repair chamber containing the damaged zone. Another step is heating the space inside the repair chamber to form a heating chamber allowing the curing expected for repairing the damaged zone.
-
-
-
-
-
-
Search Results
7
records
(took 0.019 seconds)
