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    METHOD AND DEVICE FOR PRODUCING A FIBRE COMPOSITE COMPONENT
    3.
    发明申请
    METHOD AND DEVICE FOR PRODUCING A FIBRE COMPOSITE COMPONENT 有权
    用于生产纤维复合组分的方法和装置

    公开(公告)号：US20140084508A1

    公开(公告)日：2014-03-27

    申请号：US14029242

    申请日：2013-09-17

    Applicant: AIRBUS OPERATIONS GMBH

    Inventor： Hauke Seegel ,  Paulin Fideu ,  Axel Herrmann

    IPC: B29C33/00

    CPC classification number: B29C33/0038 ,  B29C70/443 ,  B29C70/48 ,  B29C70/54 ,  F16J15/08

    Abstract: The present invention provides a method for producing a fibre composite component, comprising: arranging a first and a second mould in relation to one another in such a way that these together form a first cavity; laying a fibre material on the first and/or second mould; filling the formed first cavity with a casting material and solidifying said casting material in order to seal the first and the second mould to one another and/or interconnect them; and infiltrating the fibre material with a matrix and curing said matrix to form the fibre composite component.

    Abstract translation: 本发明提供了一种纤维复合材料成型体的制造方法，其特征在于，包括：使第一和第二模具相互相对配置，使得它们一起形成第一空腔; 在第一和/或第二模具上铺设纤维材料; 用铸造材料填充所形成的第一空腔并固化所述铸造材料，以便将第一模具和第二模具彼此密封和/或互连; 并用基质渗透纤维材料并固化所述基质以形成纤维复合材料组分。

    Aircraft structural assembly having an area element which comprises a core and an outer layer
    4.
    发明授权
    Aircraft structural assembly having an area element which comprises a core and an outer layer 有权
    具有包括芯和外层的区域元件的飞机结构组件

    公开(公告)号：US09327821B2

    公开(公告)日：2016-05-03

    申请号：US13779432

    申请日：2013-02-27

    Applicant: AIRBUS OPERATIONS GMBH

    Inventor： Pierre Zahlen ,  Ichwan Zuardy ,  Markus Mueller ,  Axel Herrmann

    IPC: B64C1/18 ,  B64C1/06 ,  B64C1/12 ,  B64C1/00

    CPC classification number: B64C1/18 ,  B64C1/00 ,  B64C1/068 ,  B64C1/12 ,  Y10T428/24612

    Abstract: An aircraft structural assembly includes an area element which has a core and an outer layer. A first surface of the area element is convexly curved, at least in certain sections, relative to an imaginary central area of the area element extending through the core of the area element. By contrast, a second surface of the area element located opposite the first surface is oriented, at least in certain sections, parallel to the imaginary central area of the area element extending through the core of the area element. The area element is configured in the form of a floor panel of a floor system. The first or the second surface of the area element is designed to form a walkable floor surface of the floor system in the state of the aircraft structural assembly when mounted in an aircraft.

    Abstract translation: 飞机结构组件包括具有芯和外层的区域元件。 区域元件的第一表面至少在某些部分中相对于延伸穿过区域元件的芯的区域元件的假想中心区域呈凸形弯曲。 相比之下，与第一表面相对的区域元件的第二表面至少在某些部分上平行于延伸穿过区域元件的芯的区域元件的假想中心区域。 区域元件被配置为地板系统的地板面板的形式。 区域元件的第一或第二表面设计成在飞机结构组件的状态下安装在飞行器中时形成地板系统的可步行地板表面。

    Apparatus and method for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material
    6.
    发明授权
    Apparatus and method for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material 审中-公开

    公开(公告)号：US10668671B2

    公开(公告)日：2020-06-02

    申请号：US15921514

    申请日：2018-03-14

    Applicant: Airbus Operations GmbH

    Inventor： Jan Schiller ,  Axel Herrmann

    IPC: B29C70/30 ,  B29C70/56 ,  B29K105/24

    Abstract: An apparatus for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material includes a mold having a mold surface that corresponds to a portion of the desired profile geometry and curvature of the profiled structural part, a clamping device for tensioning a layer of a knitted fiber fabric along a tensioning line in a prestressed state, and a movement device for producing a relative movement between the mold and the clamped-in fabric layer such that the mold surface moves close to the fabric layer in a direction perpendicular to the tensioning line and, in the further course of the relative movement, pushes through the tensioning line such that the fabric layer completely covers the mold surface. The clamping device is equipped to load the fabric layer during the entire draping operation with a tensile force acting along the tensioning line.

    APPARATUS AND METHOD FOR DRAPING KNITTED FIBER FABRICS FOR CURVED PROFILED STRUCTURAL PARTS OF FIBER COMPOSITE MATERIAL
    7.
    发明申请
    APPARATUS AND METHOD FOR DRAPING KNITTED FIBER FABRICS FOR CURVED PROFILED STRUCTURAL PARTS OF FIBER COMPOSITE MATERIAL 审中-公开

    公开(公告)号：US20180200966A1

    公开(公告)日：2018-07-19

    申请号：US15921514

    申请日：2018-03-14

    Applicant: Airbus Operations GmbH

    Inventor： Jan Schoppmeier ,  Axel Herrmann

    IPC: B29C70/30 ,  B29C70/56 ,  B29K105/24

    CPC classification number: B29C70/30 ,  B29C70/56 ,  B29K2105/243

    Abstract: An apparatus for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material includes a mold having a mold surface that corresponds to a portion of the desired profile geometry and curvature of the profiled structural part, a clamping device for tensioning a layer of a knitted fiber fabric along a tensioning line in a prestressed state, and a movement device for producing a relative movement between the mold and the clamped-in fabric layer such that the mold surface moves close to the fabric layer in a direction perpendicular to the tensioning line and, in the further course of the relative movement, pushes through the tensioning line such that the fabric layer completely covers the mold surface. The clamping device is equipped to load the fabric layer during the entire draping operation with a tensile force acting along the tensioning line.

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