公开(公告)号：US10047465B2

公开(公告)日：2018-08-14

申请号：US14845468

申请日：2015-09-04

Applicant: Airbus Defence and Space GmbH

Inventor： Thomas Meer

IPC: B29C70/24 ,  D05C15/16 ,  B32B5/26 ,  B32B7/12 ,  D06M17/04

Abstract: A fiber composite component includes a composite including cured matrix material and a fiber material embedded therein. At least one partial area of the fiber composite component is provided with at least one thread, which undulates as it extends along a surface area of the composite, so that sections of the thread alternately run inside of the composite and outside of the composite. An adhesive arrangement for such fiber composite components is also disclosed. Finally, methods for manufacturing such a fiber composite component or for manufacturing such an adhesive arrangement are disclosed.

公开(公告)号：US20170122871A1

公开(公告)日：2017-05-04

申请号：US15335067

申请日：2016-10-26

Applicant: Airbus Defence and Space GmbH

Inventor： Thomas Meer

IPC: G01N21/64 ,  G01N21/88

CPC classification number: G01N21/6456 ,  G01N21/645 ,  G01N21/8806 ,  G01N21/8851 ,  G01N21/94 ,  G01N2021/646 ,  G01N2021/8472 ,  G01N2201/061

Abstract: A method for detecting surface residues on fiber composite plastic material components using ultraviolet radiation includes irradiating a surface of the component with ultraviolet radiation using an ultraviolet radiation source, detecting fluorescent radiation which is emitted from the surface of the component as a result of the irradiation with the ultraviolet radiation, and characterizing surface residues on the basis of the detected fluorescent radiation.

公开(公告)号：US10705034B2

公开(公告)日：2020-07-07

申请号：US15337153

申请日：2016-10-28

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Sebastian Heckner ,  Georg Wachinger ,  Thomas Meer ,  Matthias Geistbeck

IPC: G01N23/223

Abstract: A method for detecting surface impurities on a surface of a component by X-ray fluorescence analysis uses a hand spectroscope for application to the surface of a component. The hand spectroscope comprises an X-ray source, a fluorescent radiation detector, an analyzer and a display. The method comprises irradiating the surface of the component with X-rays using the X-ray source; detecting fluorescent radiation, which is emitted by the surface of the component as a result of the irradiation with the X-rays, using the fluorescent radiation detector; measuring a radiation spectrum of the detected fluorescent radiation; generating an evaluation result by analyzing the measured radiation spectrum using the analyzer, the evaluation result comprising a quantitative measure of the surface impurity of the surface due to predetermined characteristic substances; and outputting the generated evaluation result on the display.

公开(公告)号：US20160334380A1

公开(公告)日：2016-11-17

申请号：US15151795

申请日：2016-05-11

Applicant: Airbus Defence and Space GmbH

Inventor： Georg Wachinger ,  Andreas Helwig ,  Thomas Meer ,  Matthias Geistbeck ,  Alois Friedberger ,  Sebastian Heckner

IPC: G01N33/00

CPC classification number: G01N33/0036 ,  G01N1/2226 ,  G01N1/44 ,  G01N25/56 ,  G01N2001/2241 ,  G01N2033/0003

Abstract: A method for testing a component for contamination. The method comprises a heating of a specimen surface of the component under a measuring bell defining a measurement volume, an at least two-time measuring of a contamination of the measurement volume with at least one contaminant, and a purging of the measurement volume with gas. An apparatus for testing a component for contamination is also disclosed. The apparatus comprises a measuring bell configured to form a measurement volume about the component or contacting the component. A heating element is configured to heat at least one specimen surface of the component. A purging unit is configured to purge the measurement volume with gas. A sensor system is configured to measure a contamination of the measurement volume with at least one contaminant.

Abstract translation: 一种用于测试污染成分的方法。 该方法包括在限定测量体积的测量钟下加热组件的样本表面，至少两次测量具有至少一种污染物的测量体积的污染物，以及用气体吹扫测量体积 。 还公开了一种用于测试污染成分的装置。 该装置包括测量钟，其配置成形成关于部件的测量体积或接触该部件。 加热元件构造成加热组件的至少一个样品表面。 清洗单元配置成用气体吹扫测量体积。 传感器系统被配置成用至少一种污染物测量测量体积的污染。

公开(公告)号：US20160069009A1

公开(公告)日：2016-03-10

申请号：US14845468

申请日：2015-09-04

Applicant: Airbus Defence and Space GmbH

Inventor： Thomas Meer

IPC: D05C15/16 ,  B32B5/26 ,  D06M17/04 ,  B32B7/12

CPC classification number: D05C15/16 ,  B29C70/24 ,  B32B5/26 ,  B32B7/12 ,  B32B2260/00 ,  B32B2605/18 ,  D06M17/04 ,  Y10T29/49801

Abstract: A fiber composite component includes a composite including cured matrix material and a fiber material embedded therein. At least one partial area of the fiber composite component is provided with at least one thread, which undulates as it extends along a surface area of the composite, so that sections of the thread alternately run inside of the composite and outside of the composite. An adhesive arrangement for such fiber composite components is also disclosed. Finally, methods for manufacturing such a fiber composite component or for manufacturing such an adhesive arrangement are disclosed.

Abstract translation: 纤维复合材料组分包括包含固化的基质材料和嵌入其中的纤维材料的复合材料。 所述纤维复合部件的至少一个部分区域设置有至少一个螺纹，所述至少一个螺纹沿着所述复合材料的表面区域延伸而波动，使得所述线材的部分交替地在所述复合材料内部并且在所述复合材料的外部延伸。 还公开了这种纤维复合材料部件的粘合装置。 最后，公开了制造这种纤维复合材料部件或制造这种粘合剂装置的方法。

公开(公告)号：US10414116B2

公开(公告)日：2019-09-17

申请号：US14719774

申请日：2015-05-22

Applicant: Airbus Defence and Space GmbH

Inventor： Jonas Gruenewald ,  Patricia Parlevliet ,  Thomas Meer

IPC: B32B3/12 ,  B32B7/00 ,  B32B37/04 ,  B32B38/00 ,  B29B11/04 ,  B29B11/14 ,  B32B27/08 ,  B32B27/28 ,  B32B7/04 ,  B32B27/04 ,  B32B37/14 ,  B32B37/00 ,  B32B37/18 ,  B29C53/04 ,  B29C65/00 ,  B29C65/48 ,  B29K671/00 ,  B29K679/00 ,  B29K71/00 ,  B29K79/00

Abstract: A sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced thermoplast material having greater resistance to a certain solvent and, fused therewith, an inner layer made of a thermoplast material having lower resistance to the solvent. The core has outer layers, each of which is formed from a thermoplast material having lower resistance to the solvent, and an inner structure, which is formed entirely or partially from a thermoplast material having greater resistance to the solvent. The inner layers of the cover layers were each fused with one of the outer layers of the core with the use of the solvent.

公开(公告)号：US10343373B2

公开(公告)日：2019-07-09

申请号：US15381678

申请日：2016-12-16

Applicant: Airbus Defence and Space GmbH

Inventor： Thomas Koerwien ,  Michael Hoffmann ,  Robert Meissner ,  Helmut Wehlan ,  Andreas Roessmann ,  Jens Holtmannspoetter ,  Sebastian Heckner ,  Thomas Meer ,  Matthias Geistbeck

IPC: B23B7/06 ,  B29C65/00 ,  B32B3/24 ,  B29C33/68 ,  B32B7/06 ,  B32B33/00 ,  B32B27/12 ,  B32B3/08 ,  B32B3/26 ,  B32B5/14 ,  B32B27/08 ,  B32B5/28 ,  B32B27/32 ,  B32B5/02 ,  B32B27/04 ,  B29C37/00 ,  B29C70/42 ,  B29C70/54 ,  D03D15/00 ,  D06M17/00 ,  B32B15/08 ,  B32B15/14 ,  B32B27/30 ,  B32B43/00 ,  B32B3/14

Abstract: A coated composite component includes, in this order, a composite component, a fluorine-containing film and/or a fluorine-containing woven fabric, knitted fabric or crocheted fabric, and a tear-off fabric. A method for producing a coated composite component including, in this order, a composite component, a fluorine-containing film and/or a fluorine-containing woven fabric, knitted fabric or crocheted fabric, and a tear-off fabric.

公开(公告)号：US10150277B2

公开(公告)日：2018-12-11

申请号：US15371890

申请日：2016-12-07

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Thomas Meer

IPC: B29C65/08 ,  B32B37/04 ,  B32B7/10 ,  B32B27/08 ,  B32B27/38 ,  B29C65/06 ,  B32B27/28 ,  B32B27/36

Abstract: A connection element includes a composite component with a cured epoxy resin, a first layer including a first thermoplastic polymer and an intermediate layer arranged between the composite component and the first layer, the first layer containing both the cured epoxy resin of the composite component and the first thermoplastic polymer of the first layer. The first thermoplastic polymer has a melting point above a curing temperature of the epoxy resin and is soluble at a temperature of at least 150° C. in the epoxy resin used for producing the composite component.

公开(公告)号：US20160334377A1

公开(公告)日：2016-11-17

申请号：US15152230

申请日：2016-05-11

Applicant: Airbus Defence and Space GmbH

Inventor： Georg Wachinger ,  Andreas Helwig ,  Thomas Meer ,  Matthias Geistbeck ,  Alois Friedberger ,  Sebastian Heckner ,  Johann Goebel

IPC: G01N30/72

CPC classification number: G01N30/7206 ,  G01N1/04 ,  G01N27/622 ,  G01N30/12 ,  G01N30/64 ,  G01N2001/045 ,  G01N2001/2241 ,  G01N2030/009 ,  G01N2030/0095 ,  G01N2030/062 ,  G01N2033/0003

Abstract: An apparatus used for the surface examination of components. The apparatus comprises: a radiation source configured to convert at least one non-volatile substance at least partially into a gas by irradiating a sample surface of a component; and a detector unit configured to qualitatively and/or quantitatively detect the at least one substance converted into gas. A method provided for a surface examination of components. The method comprises irradiating a sample surface of a component with a radiation source configured to convert at least one non-volatile substance at least partially into a gas; and a qualitative and/or quantitative detection of the at least one substance converted into gas via a detector unit.

Abstract translation: 用于表面检查部件的装置。 该装置包括：辐射源，被配置为通过照射部件的样品表面将至少一种非挥发性物质至少部分地转化成气体; 以及检测器单元，其被配置为定性和/或定量地检测转化为气体的至少一种物质。 一种用于组件表面检查的方法。 该方法包括用配置成将至少一种非挥发性物质至少部分地转化为气体的辐射源照射部件的样品表面; 以及通过检测器单元定性和/或定量地检测转化成气体的至少一种物质。

公开(公告)号：US20160334309A1

公开(公告)日：2016-11-17

申请号：US15151723

申请日：2016-05-11

Applicant: Airbus Defence and Space GmbH

Inventor： Georg Wachinger ,  Andreas Helwig ,  Thomas Meer ,  Matthias Geistbeck ,  Alois Friedberger ,  Sebastian Heckner

IPC: G01N1/22

CPC classification number: G01N1/2214 ,  G01N1/2226 ,  G01N25/56 ,  G01N33/442 ,  G01N2001/2241 ,  G01N2033/0003

Abstract: A device used to examine layer material for contamination. The device comprises a heating device to heat a test area of the layer material and a detector device to detect at least one contaminant desorbed from the layer material. The heating device comprises at least one infra-red heating element. A method comprises heating a test area of the layer material and detecting at least one contaminant desorbed from the layer material. The heating takes place via an infra-red heating element.

Abstract translation: 用于检查污染层的材料的装置。 该装置包括用于加热层材料的测试区域的加热装置和用于检测从层材料解吸的至少一种污染物的检测器装置。 加热装置包括至少一个红外加热元件。 一种方法包括加热层材料的测试区域并检测从层材料解吸的至少一种污染物。 加热通过红外加热元件进行。