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    SEAT RAIL FOR SUPPORTING SEATS IN AN AIRCRAFT AND A METHOD OF MANUFACTURING A SEAT RAIL
    22.
    发明申请
    SEAT RAIL FOR SUPPORTING SEATS IN AN AIRCRAFT AND A METHOD OF MANUFACTURING A SEAT RAIL 审中-公开
    用于支持飞机座椅的座椅和制造座椅的方法

    公开(公告)号：US20160130004A1

    公开(公告)日：2016-05-12

    申请号：US14938532

    申请日：2015-11-11

    Applicant: AIRBUS OPERATIONS GMBH

    Inventor： Alexei Vichniakov ,  Alexander Gillessen

    IPC: B64D11/06

    CPC classification number: B64D11/0696 ,  B64C1/20 ,  Y02T50/46

    Abstract: A seat rail for supporting seats in an aircraft comprises a support portion for connection with the cabin floor and a seat receiving portion having a groove for receiving the end portions of connector elements coupled with the support frame of a seat. The support portion comprises a profile arrangement of a fiber-reinforced polymer, preferably carbon fiber-reinforced polymer, having a central main portion and flanges which extend outwardly from and perpendicular with respect so the main portion to form a support surface for the seat rail. The main portion comprises a slot open at least at its end remote from the flanges. At least one metal element comprising the groove for receiving the end portions of the connector elements has a leg which is inserted into the slot of the main portion and is secured therein. The seat rail may be manufactured in a continuous process.

    Abstract translation: 用于在飞行器中支撑座椅的座椅轨道包括用于与机舱地板连接的支撑部分和具有用于接收与座椅的支撑框架联接的连接器元件的端部的凹槽的座椅接收部分。 支撑部分包括纤维增强聚合物，优选碳纤维增强聚合物的轮廓布置，其具有中心主要部分和从主体部分向外延伸并且垂直于主要部分形成用于座椅导轨的支撑表面的凸缘。 主要部分包括至少在其远离法兰的端部开口的狭槽。 至少一个包括用于接收连接器元件的端部的槽的金属元件具有插入到主要部分的槽中并固定在其中的支脚。 座椅导轨可以以连续的方式制造。

    Method And Apparatus For Producing A Fiber-Reinforced Plastics Casting
    23.
    发明申请
    Method And Apparatus For Producing A Fiber-Reinforced Plastics Casting 有权
    用于生产纤维增强塑料铸件的方法和装置

    公开(公告)号：US20140306372A1

    公开(公告)日：2014-10-16

    申请号：US14248508

    申请日：2014-04-09

    Applicant: Airbus Operations GmbH

    Inventor： Alexander Gillessen ,  Johannes Born ,  Sascha Backhaus ,  Joachim Piepenbrock

    IPC: B29C33/38

    CPC classification number: B29C33/38 ,  B29C33/3807 ,  B29C70/36 ,  B29C70/542

    Abstract: An apparatus and method for producing a fiber-reinforced plastics casting (FRP), includes a moulding box filled with free flowing moulding material, in what a prototype of casting or a textile preform is inserted, forming a mould cavity for infiltration the inserted preform of textile with synthetic resin material in order to form a fiber-reinforced plastics casting (FRP).

    Abstract translation: 一种用于生产纤维增强塑料铸件（FRP）的装置和方法，包括填充有自由流动的模制材料的模制盒，在铸造或织物预制件的原型中插入什么，形成用于使插入的预成型件渗透的模具腔 用合成树脂材料纺织以形成纤维增强塑料铸件（FRP）。

    PROCESS FOR PRODUCING A COMPONENT HAVING A THERMOPLASTIC FIBER COMPOSITE AND COMPONENTS MADE BY THE PROCESS
    25.
    发明申请
    PROCESS FOR PRODUCING A COMPONENT HAVING A THERMOPLASTIC FIBER COMPOSITE AND COMPONENTS MADE BY THE PROCESS 有权

    公开(公告)号：US20220204182A1

    公开(公告)日：2022-06-30

    申请号：US17582068

    申请日：2022-01-24

    Applicant: Airbus Operations GmbH

    Inventor： Alexander Gillessen ,  Paul Jörn

    IPC: B64F5/10 ,  B29C70/50 ,  B29C70/38 ,  B29C70/20 ,  B29C70/00

    Abstract: A process for producing a component for an aircraft for the frame, e.g. formers and stringers. Aircraft are being increasingly constructed of polymeric fiber composite to reduce weight. Here, fiber composites were originally composed of thermoset polymer and carbon fibers. Thermoplastic fiber composites are increasingly a research focus. An example is poly(ether ether ketone). However, production of components of thermoplastic fiber composites is complex. An improved process for producing such components includes producing a sheet-like object with a thermoplastic fiber composite having a thermoplastic polymer material and reinforcing fibers embedded therein, forming the sheet-like object for a semifinished part, and solidification of the semifinished part to give the component. Components obtainable by this process are also disclosed.

    Device for lacquer transfer
    26.
    发明授权
    Device for lacquer transfer 有权

    公开(公告)号：US11331688B2

    公开(公告)日：2022-05-17

    申请号：US16829914

    申请日：2020-03-25

    Applicant: Airbus Operations GmbH ,  Airbus (S.A.S.)

    Inventor： Pierre C. Zahlen ,  Alexander Gillessen ,  Christian Schepp ,  Daniel Kress ,  Waldemar Kümmel

    IPC: B05C1/08 ,  B05C21/00

    Abstract: A device for a lacquer transfer includes a transfer roller mounted at and rotatable relative to a frame. The roller includes a cylindrical support-body, first ring-element, second ring-element, and a tire including a middle-section forming a circumferential outer contact surface with depressions, the roller configured to roll with the outer contract surface on a work surface of a workpiece for transferring lacquer from the outer contact surface and the depressions to the work surface. The tire includes two annular end-sections attached to a cylindrical outer shell of the support-body resulting in two axially separated and circumferentially extending connections, the tire, connections, and outer shell of the support-body being fluid-tight. The first and second ring-elements are in the first cavity seated on the support-body at a distance in an axial direction of the roller from one another and the middle-section of the tire between the first and second ring-elements is prestrained in the axial direction.

    DEVICE AND SYSTEM
    27.
    发明申请
    DEVICE AND SYSTEM 审中-公开

    公开(公告)号：US20200306786A1

    公开(公告)日：2020-10-01

    申请号：US16829925

    申请日：2020-03-25

    Applicant: Airbus Operations GmbH

    Inventor： Pierre C. Zahlen ,  Alexander Gillessen ,  Sebastian Kerger

    IPC: B05C1/08 ,  B05C21/00

    Abstract: A device and a system for a lacquer transfer with a frame, transfer roller with a circumferential lateral wall, a drive unit, a slit nozzle, the slit nozzle at least indirectly connected to the frame, an outside contact surface of the lateral wall including depressions, the transfer roller mounted rotatably about an axis of rotation at the frame, the drive unit configured to drive the transfer roller for the transfer roller to rotate about the axis of rotation. The slit nozzle includes a supply connection, nozzle-cavity, slit-shaped nozzle-channel and at least one limiter, the supply connection coupled to the nozzle-cavity for supplying lacquer to the nozzle-cavity, the nozzle-channel extending from the nozzle-cavity to a muzzle end formed by the slit nozzle at the end of the nozzle-channel for dispensing lacquer, the slit nozzle configured by the limiter to adjust a cross-section in a restriction area of the nozzle-channel.

    Method for producing a rail-shaped hybrid component, and such a hybrid component
    28.
    发明授权
    Method for producing a rail-shaped hybrid component, and such a hybrid component 有权

    公开(公告)号：US10472070B2

    公开(公告)日：2019-11-12

    申请号：US15598462

    申请日：2017-05-18

    Applicant: Airbus Operations GmbH

    Inventor： Johannes Born ,  Alexander Gillessen ,  Carsten Rowedder

    IPC: B64D11/06 ,  B64G1/60

    Abstract: In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.

    METHOD FOR PRODUCING A THREE-DIMENSIONAL PREFORM FROM REINFORCING FIBERS
    29.
    发明申请
    METHOD FOR PRODUCING A THREE-DIMENSIONAL PREFORM FROM REINFORCING FIBERS 审中-公开

    公开(公告)号：US20190329456A1

    公开(公告)日：2019-10-31

    申请号：US16354882

    申请日：2019-03-15

    Applicant: Airbus Operations GmbH

    Inventor： Thore Sdunnus ,  Alexander Gillessen

    IPC: B29B11/12 ,  B29B11/16 ,  B29C70/34

    Abstract: A method for producing a three-dimensional preform from reinforcing fibers for producing a component from a fiber-reinforced plastic comprises the steps of introducing at least one layer of fibers having a binder into a draping mold, forming the at least one layer of fibers by at least one forming element which is displaceable along the draping mold, applying an airtight film to the at least one layer of fibers during or directly after the forming, creating a negative pressure in the intermediate space between the airtight film and the draping mold, activating the binder and removing the negative pressure after curing of the binder.

    APPARATUS FOR CARRYING A FIBER COMPOSITE RESIN SYSTEM IN A HEAT TRANSFER DEVICE
    30.
    发明申请
    APPARATUS FOR CARRYING A FIBER COMPOSITE RESIN SYSTEM IN A HEAT TRANSFER DEVICE 审中-公开

    公开(公告)号：US20180141242A1

    公开(公告)日：2018-05-24

    申请号：US15816081

    申请日：2017-11-17

    Applicant: Airbus Operations GmbH

    Inventor： Heike Lindhorst ,  Alexander Gillessen ,  Paulin Fideu Siagam ,  Konstantin Schubert

    IPC: B29C35/02

    CPC classification number: B29C35/0227 ,  B29C31/08 ,  B29K2307/04 ,  B29L2031/3076

    Abstract: An apparatus for carrying a fiber composite resin system in a heat transfer device, in particular an autoclave, for transferring heat between the fiber composite resin system and a directed gas flow, to produce a fiber composite aircraft component. The apparatus comprises a carrier structure for carrying the fiber composite resin system, the carrier structure having at least one flow path which, when the apparatus is accommodated in the heat transfer device, extends from an inlet on a side facing the directed gas flow along the fiber composite resin system accommodated by the carrier structure, to allow heat exchange between the gas flow in the flow path and the fiber composite resin system, and a diverting device for diverting at least a part of the directed gas flow when the apparatus is accommodated in the heat transfer device, to feed this part to the carrier structure flow path.

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