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1.发明申请公开(公告)号：US20190170674A1
公开(公告)日：2019-06-06
申请号：US16204146
申请日：2018-11-29
Applicant: AIRBUS DEFENCE AND SPACE GMBH
Inventor： Christian Weimer , Christopher Buchmann , Henning Becker , Richard Hesse , Andreas Meyer-Giesow
IPC: G01N27/02
Abstract: A measurement arrangement for measuring process and structure parameters of a fiber composite material along a measuring path includes a fiber material, a matrix material which surrounds the fiber material at least in regions, and an electrical sensor element that includes at least two signal transmission lines twisted together and aligned along the measuring path in and/or at the fiber material such that the signal transmission lines are surrounded at least in portions by the matrix material, wherein the electrical sensor element is configured to measure the process and structure parameters on the basis of the behavior of electromagnetic signals that are fed into the signal transmission lines.
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公开(公告)号：US09879987B2
公开(公告)日：2018-01-30
申请号：US14945126
申请日：2015-11-18
Applicant: Airbus Defence and Space GmbH
Inventor： Franz Engel , Christian Weimer
CPC classification number: G01B11/272 , G01B11/002 , G01B11/14 , G01N21/95 , G01P3/68 , G01S17/46 , G01S17/50
Abstract: A positioning system for detecting a spatial position of a laying head of a device for automatically laying reinforcing fiber strips in relation to a base on which the reinforcing fiber strips can be laid by the laying head includes at least two laser lines which extend substantially in parallel at a spacing A from one another and substantially transversely to a laying direction can be projected on the laid reinforcing fiber strips by at least one laser source. The elevation profiles of the projected laser lines which occur on account of an irregular surface of the laid reinforcing fiber strips are able to be recorded by a camera and supplied to an evaluation unit.
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公开(公告)号：US20170297277A1
公开(公告)日：2017-10-19
申请号：US15478298
申请日：2017-04-04
Applicant: Airbus Defence and Space GmbH
Inventor： Christopher Buchmann , Christian Weimer , Christoph Meier , Jonas Gruenewald
IPC: B29C70/42 , B32B27/08 , B32B27/20 , B29K21/00 , B29L31/30 , B29K307/04 , B29K105/08 , B29L31/52 , B29K309/08
CPC classification number: B29C70/42 , B29B15/105 , B29C70/40 , B29C70/506 , B29K2021/003 , B29K2101/10 , B29K2101/12 , B29K2105/08 , B29K2307/04 , B29K2309/08 , B29L2031/3055 , B29L2031/3091 , B29L2031/52 , B32B3/263 , B32B5/14 , B32B27/08 , B32B27/20 , B32B2260/021 , B32B2605/00
Abstract: A method for producing a fiber composite laminate, including the steps of applying pressure and/or heat to a first preform, which has one or more dry fiber layers and a thermoplastic elastomer, such that the thermoplastic portion of the thermoplastic elastomer completely impregnates the dry fiber layers of the first preform in at least one first region and only partially impregnates the dry fiber layers in at least one second region and, in a thermosetting polymer matrix, impregnating and curing the fiber layers of the second region of the first preform that are still dry and have not been impregnated with the thermoplastic portion of the thermoplastic elastomer.
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公开(公告)号：US10456995B2
公开(公告)日：2019-10-29
申请号：US15359077
申请日：2016-11-22
Applicant: AIRBUS DEFENCE AND SPACE GMBH
Inventor： Franz Engel , Christian Weimer , Tilman Orth
Abstract: A laying unit for producing a fiber composite component includes a drive device which is formed for magnetic cooperation with a running face, which provides a magnetic field and/or is ferromagnetic, to advance the laying unit on the running face. A device for producing a fiber composite component comprising a laying unit of this type and a method for producing a fiber composite component comprising a device of this type are disclosed.
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公开(公告)号：US10166729B2
公开(公告)日：2019-01-01
申请号：US14976915
申请日：2015-12-21
Applicant: Airbus Defence and Space GmbH
Inventor： Christian Weimer , Franz Engel , Tilman Orth
IPC: B29C70/42 , B29B11/16 , B29K105/00 , B29K105/12 , B29K307/04 , B29L31/00 , B29K101/12 , B29C70/34 , B29K105/08
Abstract: A device for consolidating a thermoplastic preform, in particular a carbon fiber thermoplastic preform includes a heating element, e.g., an LED array, for heating the preform and a consolidation element, e.g., a consolidation roller, for exposing the preform to pressure and for cooling the preform. In order to consolidate the preform, the heating element and consolidation element are arranged and movable relative to each other in such a way that the preform can be exposed to pressure and cooled by the consolidation element after heated by means of the heating element.
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Patent Agency Ranking
公开(公告)号：US10081443B2
公开(公告)日：2018-09-25
申请号：US15361607
申请日：2016-11-28
Applicant: Airbus Defence and Space GmbH
Inventor： Franz Engel , Daniel Bauer , Tilman Orth , Christian Weimer
CPC classification number: B64F5/60 , B64D15/20 , B64D45/00 , G01M5/0016 , G01N21/8851 , G01N2021/8867 , H04L67/12
Abstract: In order to provide a simplified inspection of an aircraft for the pilot, an aircraft inspection system is provided which includes at least one movable inspection unit, a position detection arrangement, and at least one data transfer interface. The at least one moveable inspection unit is moveable relative to an aircraft to be inspected. The at least one movable inspection unit includes at least one sensor for detecting a characteristic value, for verifying a characteristic and/or for determining a defect of an aircraft. The movable inspection unit is configured to generate monitoring data. When a defect or a characteristic value is detected, the position detection arrangement detects position data of the movable inspection unit in relation to the aircraft to be inspected, and assigns the position data to the monitoring data. The data transfer interface provides the position data with the assigned monitoring data as inspection data.
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公开(公告)号：US20180169952A1
公开(公告)日：2018-06-21
申请号：US15735282
申请日：2016-05-23
Applicant: Airbus Defence and Space GmbH
Inventor： Franz Engel , Andreas Nick , Wolfgang Rehm , Christian Weimer
IPC: B29C64/393 , B29C64/153 , B29C64/371 , B33Y30/00 , B33Y50/02 , B23K26/03 , G01J3/44 , B23K26/12 , B23K26/342
Abstract: A device for the layer-wise additive production of a complex three-dimensional component has a measuring mechanism for continuously monitoring quality indicators during the production of the component, wherein the measuring mechanism and a bed with a material powder are surrounded, at least in regions, by a processing cell filled with a protective gas atmosphere and the material powder of an uppermost layer can be melted in a locally limited manner in a melting zone by means of at least one laser. The measuring mechanism has the at least one laser and at least one optical sensor for the priority detection of the quality indicators in the region of the melting zone, in particular by means of Raman spectroscopy. Consequently, any construction errors in the component can be recognised, evaluated and, if necessary, corrected in a resource-saving manner without delay.
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公开(公告)号：US20170015070A1
公开(公告)日：2017-01-19
申请号：US15208106
申请日：2016-07-12
Applicant: Airbus Defence and Space GmbH
Inventor： Daniel Bauer , Franz Engel , Tilman Orth , Christian Weimer
CPC classification number: B29C70/30 , B29C70/54 , G01M5/0033 , G01M5/0075 , G01M5/0091
Abstract: A testing arrangement serves for controlling the manufacturing of a fiber reinforced component. The testing arrangement includes an inspection device with a sensor system, with the inspection device being configured to move on and/or above one or more material layer(s) and/or a surface of the component and to examine the material layer(s) or the surface with the sensor system. A device serves for automated manufacturing of a fiber reinforced plastic laminate. The device includes a forming tool, a laying head for automated laying of material layers in the forming tool as well as a testing arrangement.
Abstract translation: 测试装置用于控制纤维增强部件的制造。 测试装置包括具有传感器系统的检查装置，其中检查装置被配置为在部件的一个或多个材料层和/或表面上和/或上方移动并检查材料层， 或表面与传感器系统。 一种装置用于纤维增强塑料层压板的自动化生产。 该装置包括成形工具，用于在成形工具中自动铺设材料层的铺设头以及测试装置。
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公开(公告)号：US10940650B2
公开(公告)日：2021-03-09
申请号：US16665382
申请日：2019-10-28
Applicant: AIRBUS DEFENCE AND SPACE GMBH
Inventor： Franz Engel , Christian Weimer , Tilman Orth
Abstract: A laying unit for producing a fiber composite component includes a drive device which is formed for magnetic cooperation with a running face, which provides a magnetic field and/or is ferromagnetic, to advance the laying unit on the running face. A device for producing a fiber composite component including a laying unit of this type and a method for producing a fiber composite component including a device of this type are disclosed.
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公开(公告)号：US10322550B2
公开(公告)日：2019-06-18
申请号：US14728399
申请日：2015-06-02
Applicant: Airbus Defence and Space GmbH
Inventor： Christian Weimer , Juergen Filsinger
Abstract: The invention relates to a device for the infiltration of fibrous material with resin for the production of a fiber composite component, comprising a mold tool with a cavity enclosed by at least two tool parts, wherein the mold tool is designed for a relative movement of the at least two tool parts, in such a manner that space can be provided inside the cavity, in a first tool position, to hold the fibrous material, and additional space can be provided to accommodate resin, and the size of the cavity can then be reduced by a movement of the mold tool from the first tool position into a second tool position. According to the invention, a flow promoter is included in the cavity, comprising at least one first layer and one second layer, connected to each other in an edge region of the flow promoter to enclose a flow space, wherein the first layer is impermeable to resin while the second layer provides an outlet for guiding resin out of the flow space and into the fibrous material, and wherein the flow space of the flow promoter is filled with resin and/or the flow promoter has an inlet for conveying resin into the flow space. The invention further relates to a corresponding infiltration process and to a use of the device and/or the method.
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