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    Flow Body For An Aircraft With A Selectively Activatable Shock Bump
    2.
    发明申请
    Flow Body For An Aircraft With A Selectively Activatable Shock Bump 有权

    公开(公告)号：US20220258853A1

    公开(公告)日：2022-08-18

    申请号：US17737550

    申请日：2022-05-05

    Applicant: Airbus Operations GmbH ,  Airbus Defence and Space GmbH

    Inventor： Peter Linde ,  Wolfgang Machunze

    IPC: B64C23/04 ,  B29C70/54 ,  B64C3/20 ,  B64C39/00

    Abstract: A flow body for an aircraft includes a skin having a first flow surface, having a flow influencing section with at least one first layer, at least one separator layer, at least one third layer, and at least one base layer. The first layer includes lithiated carbon fibers embedded into a matrix to form a negative electrode. The third layer includes carbon fibers with an electrode active material coating to form a positive electrode. The separator layer includes a non-conductive material for electrically isolating the first layer and the third layer from each other. The flow influencing section is configured for selectively raising a region of the arrangement of first layer, separator layer and third layer from the base layer upon application of a voltage between the first and third layers to form a bump on the flow body.

    Battery core for a sandwich component
    3.
    发明授权
    Battery core for a sandwich component 有权

    公开(公告)号：US11296360B2

    公开(公告)日：2022-04-05

    申请号：US16152810

    申请日：2018-10-05

    Applicant: Airbus Operations GmbH

    Inventor： Peter Linde

    IPC: H01M10/0583 ,  H01M4/587 ,  H01M4/58 ,  B64D41/00 ,  H01M4/62 ,  H01M10/04 ,  H01M10/0525 ,  H01M50/44 ,  H01M50/431 ,  H01M50/429

    Abstract: A battery core has a positive electrode layer, a separator layer and a negative electrode layer. The separator layer is arranged between the positive electrode layer and the negative electrode layer. The positive electrode layer, the separator layer and the negative electrode layer have nanocellulose fibres. The battery core is folded and forms a cellular structure as a core for a sandwich component. The sandwich component has an upper covering layer, a lower covering layer and a battery core. The battery core is arranged between the upper covering layer and the lower covering layer. A method for producing such a battery core is also described.

    Structural component having an integrated battery construction
    4.
    发明授权
    Structural component having an integrated battery construction 有权

    公开(公告)号：US11038200B2

    公开(公告)日：2021-06-15

    申请号：US16388311

    申请日：2019-04-18

    Applicant: Airbus Operations GmbH ,  Airbus Defence and Space GmbH

    Inventor： Peter Linde ,  Christian Karch

    IPC: H01M10/0562 ,  B60L50/64 ,  H01M4/04 ,  H01M4/131 ,  H01M4/66

    Abstract: A structural component for a vehicle has a battery construction having a solid-electrolyte matrix material, a first layer of carbon fibres having a cathode-active coating, embedded in said solid-electrolyte matrix material, a second layer of carbon fibres without a cathode-active coating, embedded in said solid-electrolyte matrix material, and at least one electrically isolating barrier layer disposed between said first layer and said second layer. The structural component has a first collector layer and a second collector layer disposed on the first layer and the second layer, respectively, on a side that faces away from the barrier layer. The first collector layer and the second collector layer are configured from a flexible, moldable and porous layer of carbon allotropes.

    Autoclave and method for welding thermoplastic composite parts
    6.
    发明授权
    Autoclave and method for welding thermoplastic composite parts 有权

    公开(公告)号：US10654021B2

    公开(公告)日：2020-05-19

    申请号：US15807447

    申请日：2017-11-08

    Applicant: Airbus Operations GmbH

    Inventor： Peter Linde

    IPC: B01J19/12 ,  B29C65/14 ,  B29C65/78 ,  H05B6/80 ,  B29C65/00 ,  B01J3/04 ,  B29K101/12 ,  B29L31/00

    Abstract: An autoclave for welding thermoplastic composite parts comprises a sealed process chamber, a pressure source, a microwave source and a workpiece supporting member configured to support at least two thermoplastic composite parts which contact each other in an abutting section within the process chamber. The pressure source is configured to generate positive pressure in the process chamber which is higher than an ambient pressure surrounding the process chamber while the microwave source emits microwaves towards the abutting section in order to locally melt the thermoplastic composite parts and weld them together in the region of the abutting section.

    Welding system
    8.
    发明授权
    Welding system 有权

    公开(公告)号：US10144180B2

    公开(公告)日：2018-12-04

    申请号：US15386518

    申请日：2016-12-21

    Applicant: Airbus Operations GmbH

    Inventor： Peter Linde

    IPC: B29C65/00 ,  B29C65/16 ,  B32B27/08 ,  B32B37/00 ,  B32B37/06 ,  B32B38/00 ,  H01L39/00 ,  H02N15/04 ,  B29K101/12 ,  B29L31/30 ,  B29C65/08

    Abstract: A system for welding an elongate element along a longitudinal direction to a component including a support element comprising a support surface, a magnetic field generating arrangement generating a predefined magnetic field, a carriage comprising contacts supporting an elongate element against movement along the surface of the component in directions perpendicular to the longitudinal direction, a superconducting element being fixedly connected to the carriage, an element cooling device for cooling the superconducting element below its transition temperature, a mover operable to linearly move the carriage, and a welding device for welding the elongate element to the component. The predefined magnetic field defines a linear path along the support surface for the superconducting element when the superconducting element has a temperature below its transition temperature.

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