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    FLEXIBLE CONNECTION ASSEMBLY WITH INTEGRATED VIBRATION DAMPER
    1.
    发明公开
    FLEXIBLE CONNECTION ASSEMBLY WITH INTEGRATED VIBRATION DAMPER 审中-公开

    公开(公告)号：US20230264802A1

    公开(公告)日：2023-08-24

    申请号：US18172645

    申请日：2023-02-22

    申请人： Airbus Operations GmbH

    发明人： Hermann BENTHIEN ,  Andreas POPPE

    IPC分类号： B64C1/06 ,  F16F1/373 ,  F16B5/02

    CPC分类号： B64C1/066 ,  F16F1/3732 ,  F16B5/02

    摘要： A connection assembly for connecting a first element to a second element is provided. The connection assembly has a male element and a female element. The female element has a barrel nut. The barrel nut has a conical inner portion positioned at a first longitudinal region and a cylindrical inner portion positioned at a second longitudinal region. The barrel nut has a first engaging element portion and a first plain portion arranged alternatingly around a circumferential direction of the barrel nut. The male element has a cylindrical bolt-like shape and has a second engaging element portion and a second plain portion arranged alternatingly around a circumferential direction of the male element. The male element further has flattened sides at the second plain portion. The second engaging element portion of the male element is configured to engage with a respective one of the first engaging element portion of the barrel nut.

    AIRCRAFT FUSELAGE STRUCTURE
    2.
    发明申请
    AIRCRAFT FUSELAGE STRUCTURE 有权
    飞机融合结构

    公开(公告)号：US20150102168A1

    公开(公告)日：2015-04-16

    申请号：US14487727

    申请日：2014-09-16

    申请人： Airbus Operations GmbH

    发明人： Hermann BENTHIEN ,  Cord HAACK ,  Andreas POPPE ,  Michael BURRICHTER ,  Torsten ABRAHAM ,  Michael BRINCKMANN ,  Christoph DIERKER ,  Frank WERTH ,  Wulf BINDEWALD

    IPC分类号： B64C1/06

    CPC分类号： B64C1/068 ,  B64C1/26

    摘要： An aircraft fuselage structure is disclosed herein and includes an outer skin, with circumferential ribs, such that a recess is provided for receiving a wing torsion box in the outer skin, and the ribs are interrupted in the region of the recess. An object of the disclosure includes providing an aircraft fuselage structure designed such that the wing torsion box is able to extend at least partially through the upper region of the fuselage, without the stability of the fuselage being significantly reduced. This can include providing first longitudinal members which are adjacent to the recess and which extend along the longitudinal edges beyond the entire length thereof. End regions of the first longitudinal members are connected to ribs which extend circumferentially at intervals from the transverse edges of the recess along the outer skin over the vertical longitudinal central plane.

    摘要翻译： 本文公开了一种飞机机身结构，并且包括具有周向肋的外皮，使得设置用于在外皮中接收翼扭转盒的凹部，并且肋在凹部的区域中断。 本公开的目的包括提供一种设计成使得机翼扭转箱能够至少部分地延伸穿过机身的上部区域的飞行器机身结构，而不会显着减小机身的稳定性。 这可以包括提供与凹部相邻并且沿着纵向边缘延伸超过其整个长度的第一纵向构件。 第一纵向构件的端部区域连接到肋，其沿垂直纵向中心平面沿着外皮从凹部的横向边缘周向延伸。

    METHOD FOR JOINING TWO SUBSTANTIALLY PLANAR FIBER-COMPOSITE STRUCTURAL COMPONENTS WITH EACH OTHER
    4.
    发明申请
    METHOD FOR JOINING TWO SUBSTANTIALLY PLANAR FIBER-COMPOSITE STRUCTURAL COMPONENTS WITH EACH OTHER 有权

    公开(公告)号：US20230052939A1

    公开(公告)日：2023-02-16

    申请号：US17882841

    申请日：2022-08-08

    申请人： Airbus Operations GmbH

    发明人： Andreas POPPE ,  Hermann BENTHIEN ,  Thomas BEUMLER

    IPC分类号： B29C65/48 ,  B29C65/56 ,  B64C1/12 ,  B64F5/10

    摘要： A method for joining two substantially planar fiber-composite structural components, includes stacking the two components on a support jig to overlap along a joining region. A lower component end section within the joining region borders a gap between the upper component and the jig, where the upper component is unsupported by the jig. The gap is bordered on an opposite side of the lower component end section by a filling portion of the upper component or a planar filler element supported by the jig. The lower component is joined to the upper component within the joining region by applying temperature and pressure to the components. A width of the gap allows the upper component to elastically deform along the gap under the pressure and bend down into the gap to abut the jig along the gap and thereby compensate thickness tolerances between the components during the pressure application.

    CONNECTION SYSTEM, CONNECTION ARRANGEMENT AND METHOD
    6.
    发明申请
    CONNECTION SYSTEM, CONNECTION ARRANGEMENT AND METHOD 审中-公开
    连接系统，连接布置和方法

    公开(公告)号：US20160272295A1

    公开(公告)日：2016-09-22

    申请号：US15073244

    申请日：2016-03-17

    申请人： AIRBUS OPERATIONS GMBH

    发明人： Hermann BENTHIEN ,  Andreas POPPE ,  Bastian SCHÄFER

    IPC分类号： B64C1/00 ,  B32B7/12 ,  B64G1/10 ,  B32B3/26

    摘要： A connection system includes a first adhesion segment, on which a first planar bonding region is formed; a second adhesion segment, on which a second planar bonding region is formed, which is shaped so as to be complementary to the first planar bonding region, and a solidifiable, liquid bonding substance. The first planar bonding region and/or the second planar bonding region are each provided with receiving openings. The receiving openings extend like capillaries through each bonding region into the interior of each adhesion segment and, in order to form an integral bond between the first adhesion segment and the second adhesion segment, are designed such that the receiving openings receive the liquid bonding substance due to capillary ascension during application of the liquid bonding substance onto each bonding region.

    摘要翻译： 连接系统包括：第一粘附段，其上形成有第一平面结合区域; 形成有与第一平面结合区域互补的第二平面结合区域的第二粘附段和可固化的液体粘合物质。 第一平面结合区域和/或第二平面结合区域各自设置有接收开口。 接收开口通过每个结合区域延伸到每个粘合区段的内部，并且为了形成第一粘附段和第二粘合段之间的整体结合，设计成接收开口接收液体粘合物质 在将液体粘合物质施加到每个接合区域时的毛细管升高。

    FLOOR SYSTEM FOR A CABIN OF A VEHICLE WITH FORM-FITTING FLOOR PANEL CONNECTION
    7.
    发明公开
    FLOOR SYSTEM FOR A CABIN OF A VEHICLE WITH FORM-FITTING FLOOR PANEL CONNECTION 审中-公开

    公开(公告)号：US20240174341A1

    公开(公告)日：2024-05-30

    申请号：US18520217

    申请日：2023-11-27

    申请人： Airbus Operations GmbH

    发明人： Andreas POPPE ,  Hermann BENTHIEN ,  Jens WIENTING

    IPC分类号： B64C1/18 ,  B64D11/06

    CPC分类号： B64C1/18 ,  B64D11/0696

    摘要： A floor system for a cabin of a vehicle is proposed, including a floor panel, a seat rail having an installation surface, a base surface underneath the installation surface at a distance thereto, and at least one recess between the installation surface and the base surface and extending along the seat rail. The floor panel has a top surface, a bottom surface and at least one connection edge extending between the top surface and the bottom surface. The seat rail is configured to vertically clamp the floor panel inside the at least one recess. The at least one connection edge has a continuously undulating or serrated edge surface. The at least one recess comprises an outward-facing lateral receiving surface that is at least partially complementary to the edge surface of the at least one connection edge to provide a form-fit engagement with the floor panel.

    SEAT RAIL SYSTEM FOR AN INTERIOR SPACE OF A VEHICLE
    8.
    发明申请
    SEAT RAIL SYSTEM FOR AN INTERIOR SPACE OF A VEHICLE 有权

    公开(公告)号：US20230027418A1

    公开(公告)日：2023-01-26

    申请号：US17870018

    申请日：2022-07-21

    申请人： Airbus Operations GmbH

    发明人： Andreas POPPE ,  Hermann BENTHIEN

    IPC分类号： B64D11/06

    摘要： A seat rail system for an interior space of a vehicle includes a seat rail having a plurality of attachment sockets arranged in a row along a longitudinal extension of the seat rail. Each attachment socket has an at least partly spheroid concave bearing surface. Two coupling openings are embedded in each concave bearing surface; an attachment stud having an at least partly spheroid or cylindroid convex bearing surface with a curvature corresponding to a curvature of the concave bearing surface of the attachment sockets. A coupling pin is arranged on or in the convex bearing surface and configured to enter one of the attachment openings to couple the attachment stud to the seat rail. A locking pin is configured to enter the respective other attachment opening through a through hole in the attachment stud and thereby lock the attachment stud to the seat rail.

    TROLLEY LIFT AND AIRCRAFT AREA, AND AIRCRAFT WITH TROLLEY LIFT
    9.
    发明申请
    TROLLEY LIFT AND AIRCRAFT AREA, AND AIRCRAFT WITH TROLLEY LIFT 审中-公开

    公开(公告)号：US20200269984A1

    公开(公告)日：2020-08-27

    申请号：US16797589

    申请日：2020-02-21

    申请人： Airbus Operations GmbH

    发明人： Hermann BENTHIEN ,  Andreas POPPE

    IPC分类号： B64D11/00 ,  B66B9/00

    摘要： A trolley lift for connecting a lower aircraft deck to an upper aircraft deck. The trolley lift comprises a platform configured to accommodate at least one trolley, wherein the platform delimits a lift compartment at the bottom, and a cover which delimits the lift compartment at the top. In particular, on a side facing away from the lift compartment, the cover at least partly forms a floor of the upper aircraft deck. Furthermore, an aircraft area having a trolley lift and an aircraft having a trolley lift and/or an aircraft area are described.