公开(公告)号：US20170175307A1

公开(公告)日：2017-06-22

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: D03D15/00 ,  D06M17/00

CPC classification number: D03D15/00 ,  B29C33/68 ,  B29C37/0075 ,  B29C66/02 ,  B29C66/721 ,  B29C66/7316 ,  B29C66/73751 ,  B29C66/7392 ,  B29C70/42 ,  B29C70/542 ,  B32B3/08 ,  B32B3/14 ,  B32B3/266 ,  B32B5/02 ,  B32B5/142 ,  B32B5/28 ,  B32B7/06 ,  B32B15/08 ,  B32B15/14 ,  B32B27/04 ,  B32B27/08 ,  B32B27/12 ,  B32B27/304 ,  B32B27/322 ,  B32B33/00 ,  B32B43/006 ,  B32B2250/44 ,  B32B2260/021 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/106 ,  B32B2305/07 ,  B32B2305/076 ,  B32B2305/18 ,  B32B2305/72 ,  B32B2305/77 ,  B32B2307/748 ,  B32B2605/00 ,  D06M17/00 ,  Y10T428/24331 ,  Y10T428/24752 ,  Y10T428/2476 ,  Y10T428/31

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：US10328682B2

公开(公告)日：2019-06-25

申请号：US15607019

申请日：2017-05-26

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Thomas Koerwien ,  Alois Friedberger ,  Andreas Helwig ,  Uwe Beier ,  Frank Weiland

IPC: B32B41/00 ,  B32B5/26 ,  B32B27/08 ,  B32B37/10 ,  B32B37/18 ,  B29C70/44 ,  B29C70/54 ,  B29C70/00 ,  B32B27/28 ,  B29C65/48 ,  B29C65/50 ,  B29C65/00 ,  B29C65/02 ,  B64D45/00 ,  B64C1/00 ,  B64C27/473

Abstract: A method for joining structural elements to a component made of at least one fiber-reinforced plastics material, includes providing at least two structural elements made of at least one fiber-reinforced plastics material having a particular matrix; providing at least one film element made of a thermoplastic heavy-duty material; arranging the at least one film element on a surface of one of the structural elements or between surfaces to be joined of the at least two structural elements to be joined; and producing the component to be joined in a curing process.

公开(公告)号：US10071817B2

公开(公告)日：2018-09-11

申请号：US14649830

申请日：2013-12-02

Applicant: Airbus Defence and Space GmbH

Inventor： Stefan Niedermeier ,  Thomas Koerwien

IPC: B25G3/00 ,  F16C11/06 ,  F16D1/00 ,  F16G11/00 ,  B64D45/00 ,  F16B11/00 ,  F16B19/02 ,  F16B31/02 ,  F16B5/04

CPC classification number: B64D45/00 ,  F16B5/04 ,  F16B11/006 ,  F16B19/02 ,  F16B31/02 ,  Y10T403/20

Abstract: A structural element includes a first component and a second component; a bonded joint, by which the first component and the second component are interconnected; and an indication bolt, which is fixed to the first component and the second component. The indication bolt is designed to indicate when the first component and the second component have moved relative one another.

公开(公告)号：US10166724B2

公开(公告)日：2019-01-01

申请号：US14678189

申请日：2015-04-03

Applicant: Airbus Defence and Space GmbH

Inventor： Thomas Koerwien

IPC: B32B3/10 ,  B29C65/70 ,  B29C73/00 ,  B32B27/08 ,  C09J5/00 ,  B32B7/00 ,  B32B7/12 ,  B32B27/00 ,  B32B27/06 ,  B32B27/30 ,  B32B27/32 ,  B32B3/00 ,  B32B3/02 ,  B32B3/30 ,  F16B11/00 ,  B29K63/00

Abstract: A method for providing spacers on a construction component to be adhered involves applying a planar formation, including passages, on the construction component to be adhered, and inserting a setting liquid in the passages of the planar formation, so that the liquid forms spacer on the construction component to be adhered after setting and peeling off the planar formation. The spacer ensures a predetermined minimum bondline when adhering the construction component.

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：US09548531B2

公开(公告)日：2017-01-17

申请号：US14748892

申请日：2015-06-24

Applicant: Airbus Defence and Space GmbH

Inventor： Bernhard Schoenlinner ,  Ulrich Prechtel ,  Thomas Schuster ,  Michael Sabielny ,  Herbert Zippold ,  Kay W. Dittrich ,  Franz Stadler ,  Markus Rothenhaeusler ,  Wilhelm Wulbrand ,  Thomas Koerwien

IPC: H01Q1/42 ,  H01Q15/14 ,  H01Q1/40 ,  H01Q1/28 ,  H01Q1/32 ,  H01Q1/38 ,  H01Q3/08

CPC classification number: H01Q1/42 ,  H01Q1/28 ,  H01Q1/3275 ,  H01Q1/38 ,  H01Q1/40 ,  H01Q1/422 ,  H01Q3/08 ,  H01Q15/141 ,  Y02T50/43

Abstract: A method is provided for manufacturing a radome. The method has the following steps: creation of a contoured fit of at least one section of an inner surface of a wall of the radome; arrangement of a plurality of planar photosensitive semiconductor elements on an outer surface of the contoured fit; placement of the contoured fit with the plurality of planar photosensitive semiconductor elements on the at least one section of the inner surface of the wall; establishing of a connection between the plurality of planar photosensitive semiconductor elements and the wall; and removal of the contoured fit from the radome. This method enables the simple manufacture of a radome with a layer having several semiconductor elements for the electromagnetic shielding of the interior of the radome.

Abstract translation: 提供了制造天线罩的方法。 该方法具有以下步骤：产生天线罩的壁的内表面的至少一个部分的轮廓拟合; 多个平面光敏半导体元件在轮廓配合的外表面上的布置; 将所述轮廓配合与所述多个平面光敏半导体元件放置在所述壁的内表面的所述至少一个部分上; 建立所述多个平面光敏半导体元件与所述壁之间的连接; 并从天线罩中移除轮廓拟合。 该方法能够简单地制造具有用于雷达罩内部的电磁屏蔽的具有若干半导体元件的层的雷达罩。