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    Connection of cabin components, cabin component and method for connecting cabin components
    1.
    发明授权
    Connection of cabin components, cabin component and method for connecting cabin components 有权
    客舱部件连接，客舱部件和连接客舱部件的方法

    公开(公告)号：US08496207B2

    公开(公告)日：2013-07-30

    申请号：US12836641

    申请日：2010-07-15

    申请人： Robert Alexander Goehlich ,  Daniel Wenninger

    发明人： Robert Alexander Goehlich ,  Daniel Wenninger

    IPC分类号： B64C1/22 ,  B64D11/00

    CPC分类号： B64D11/003

    摘要： A connection device for a plurality of cabin components of an aircraft includes a rail extending in a longitudinal direction of an aircraft structure, wherein the plurality of cabin components is disposed on the rail; and a plurality of adjustment devices configured to self-adjust each of the plurality of cabin components in the longitudinal direction.

    摘要翻译： 用于飞行器的多个舱室部件的连接装置包括沿飞行器结构的纵向方向延伸的轨道，其中多个舱室部件设置在轨道上; 以及多个调整装置，其被配置为在纵向方向上自适应地调节所述多个客舱部件中的每一个。

    Passenger supply arrangement for an aeroplane
    5.
    发明授权
    Passenger supply arrangement for an aeroplane 失效
    飞机的乘客供应安排

    公开(公告)号：US08740144B2

    公开(公告)日：2014-06-03

    申请号：US13097262

    申请日：2011-04-29

    申请人： Robert Alexander Goehlich ,  Holger Frauen ,  Cihangir Sayilgan

    发明人： Robert Alexander Goehlich ,  Holger Frauen ,  Cihangir Sayilgan

    IPC分类号： B64D11/00

    CPC分类号： B64D11/00151 ,  B64D11/0015 ,  B64D11/00155 ,  B64D11/003 ,  B64D11/0624 ,  B64D11/0649 ,  B64D13/00 ,  Y02T50/44 ,  Y02T50/46

    摘要： A passenger supply arrangement provides a communications system and comfort system for a passenger of an aeroplane. The passenger supply arrangement includes a presentation surface configured to be integrated into a backrest of a passenger seat of an aeroplane and a passenger supply module configured to be disposed above the passengers seats of the aeroplane. The passenger supply module includes at least one projector configured to project an image onto the presentation surface. The image includes a monitoring area for playback of video and an operating area for displaying and for actuation of operating elements of the passenger supply module.

    摘要翻译： 乘客供应安排为飞机乘客提供通信系统和舒适系统。 乘客供应装置包括配置成集成到飞机的乘客座椅的靠背中的演示表面和被配置为设置在飞机的乘客座位上方的乘客供应模块。 乘客供应模块包括至少一个投影仪，其配置成将图像投影到呈现表面上。 图像包括用于播放视频的监视区域和用于显示和用于驾驶乘客供应模块的操作元件的操作区域。

    Holder for fixing components, in particular lines, inside an aircraft without using holes
    6.
    发明授权
    Holder for fixing components, in particular lines, inside an aircraft without using holes 有权
    用于固定组件，特别是线路内的飞机内，不使用孔

    公开(公告)号：US08087621B2

    公开(公告)日：2012-01-03

    申请号：US12273075

    申请日：2008-11-18

    申请人： Cihangir Sayilgan ,  Holger Frauen ,  Frank Neuhaus ,  Robert Alexander Goehlich ,  Rainer Schildt

    发明人： Cihangir Sayilgan ,  Holger Frauen ,  Frank Neuhaus ,  Robert Alexander Goehlich ,  Rainer Schildt

    IPC分类号： F16L3/08

    CPC分类号： B64C1/406 ,  B64D11/0015 ,  B64D11/00155 ,  B64D11/02 ,  B64D11/04 ,  B64D13/00 ,  H02G3/0456

    摘要： Disclosed is a holder for fixing all types of component, in particular lines, without using holes and largely without using tools inside a conventional fuselage structure of an aircraft with stringers and annular formers, the formers each being provided with an angle bracket at crossing points between a stringer and an annular former. The holder is configured so as to be split in two with a lower part and an upper part which can be connected thereto, the lower part being slidable onto an angle bracket. By attaching the upper part to the lower part, the holder is positionally fixed at the crossing point in the top region of an annular former. It is fixed in its final position by connecting the holder to a transverse line holder as a function element by means of an expansion pin or other connection elements. Other alternative function elements for fixing the components, such as a longitudinal line holder, a transverse batten or a longitudinal batten for specific installation requirements, may, if necessary, be combined with at least one holder so as to form holder arrangement with any desired degree of complexity.

    摘要翻译： 公开了一种用于固定所有类型的部件，特别是线，而不使用孔并且在具有桁条和环形成形器的飞行器的常规机身结构内部大部分不使用工具的情况下，各个部件都设置有尖角支架， 桁条和环形成形机。 保持器构造成可以分为两部分，下部和上部可以连接到其上，下部可滑动到角度支架上。 通过将上部附接到下部，保持器被定位在环形成形器的顶部区域中的交叉点处。 通过借助于膨胀销或其他连接元件将支架连接到作为功能元件的横线支架固定在其最终位置。 用于固定组件的其他替代功能元件，例如用于特定安装要求的纵向线支架，横向板条或纵向板条，如果需要，可以与至少一个支架组合，以便形成具有任何所需程度的支架装置 的复杂性。

    Fuselage Section of an Aircraft and Method for the Production of the Fuselage Section
    7.
    发明申请
    Fuselage Section of an Aircraft and Method for the Production of the Fuselage Section 有权
    飞机机身部分和生产机身部分的方法

    公开(公告)号：US20110303791A1

    公开(公告)日：2011-12-15

    申请号：US13154899

    申请日：2011-06-07

    申请人： Holger Frauen ,  Robert Alexander Goehlich

    发明人： Holger Frauen ,  Robert Alexander Goehlich

    IPC分类号： B64C1/00 ,  B64C1/06

    CPC分类号： B29C70/202 ,  B29D99/001 ,  B29L2031/3082 ,  B64C1/068 ,  B64C2001/0072 ,  Y02T50/43

    摘要： In accordance with the method, an inside layer of a fuselage section skin made from first fibers is placed on a manufacturing surface, the first fibers being placed in one or more first fiber directions. On the inside layer, a stiffening structure is formed from stiffening fibers, the stiffening fibers being placed in one or more stiffening fiber directions. An outside layer of the fuselage section skin, comprising fourth fibers, is placed on the stiffening structure formed from stiffening fibers, the fourth fibers being placed in one or more fourth fiber directions. The stiffening structure is designed and developed in such a way that the fuselage section does not require an additional stiffening structure, is connected with the fuselage section skin, and comprises the inside layer, the stiffening structure, and the outside layer; in particular, an additional stiffening structure in the form of stringers and frames is not required.

    摘要翻译： 根据该方法，将由第一纤维制成的机身部分皮肤的内层放置在制造表面上，将第一纤维放置在一个或多个第一纤维方向上。 在内层中，加强结构由加强纤维形成，加强纤维被放置在一个或多个加强纤维方向上。 包括第四纤维的机身部分皮肤的外层被放置在由加强纤维形成的加强结构上，第四纤维被放置在一个或多个第四纤维方向上。 加固结构的设计和开发方式使得机身部分不需要额外的加强结构，与机身部分皮肤相连，并且包括内层，加强结构和外层; 特别地，不需要桁条和框架形式的附加加强结构。

    HOLDER FOR FIXING COMPONENTS, IN PARTICULAR LINES, INSIDE AN AIRCRAFT WITHOUT USING HOLES
    8.
    发明申请
    HOLDER FOR FIXING COMPONENTS, IN PARTICULAR LINES, INSIDE AN AIRCRAFT WITHOUT USING HOLES 有权
    固定组件，特殊线路，不使用孔的飞机内部

    公开(公告)号：US20090159750A1

    公开(公告)日：2009-06-25

    申请号：US12273075

    申请日：2008-11-18

    申请人： Cihangir Sayilgan ,  Holger Frauen ,  Frank Neuhaus ,  Robert Alexander Goehlich ,  Rainer Schildt

    发明人： Cihangir Sayilgan ,  Holger Frauen ,  Frank Neuhaus ,  Robert Alexander Goehlich ,  Rainer Schildt

    IPC分类号： B64C1/00

    CPC分类号： B64C1/406 ,  B64D11/0015 ,  B64D11/00155 ,  B64D11/02 ,  B64D11/04 ,  B64D13/00 ,  H02G3/0456

    摘要： Disclosed is a holder for fixing all types of component, in particular lines, without using holes and largely without using tools inside a conventional fuselage structure of an aircraft with stringers and annular formers, the formers each being provided with an angle bracket at crossing points between a stringer and an annular former. The holder is configured so as to be split in two with a lower part and an upper part which can be connected thereto, the lower part being slidable onto an angle bracket. By attaching the upper part to the lower part, the holder is positionally fixed at the crossing point in the top region of an annular former. It is fixed in its final position by connecting the holder to a transverse line holder as a function element by means of an expansion pin or other connection elements. Other alternative function elements for fixing the components, such as a longitudinal line holder, a transverse batten or a longitudinal batten for specific installation requirements, may, if necessary, be combined with at least one holder so as to form holder arrangement with any desired degree of complexity.

    摘要翻译： 公开了一种用于固定所有类型的部件，特别是线，而不使用孔并且在具有桁条和环形成形器的飞行器的常规机身结构内部大部分不使用工具的情况下固定所有类型的部件，所述成形器各自在 桁条和环形成形机。 保持器构造成可以分为两部分，下部和上部可以连接到其上，下部可滑动到角度支架上。 通过将上部附接到下部，保持器被定位在环形成形器的顶部区域中的交叉点处。 通过借助于膨胀销或其他连接元件将支架连接到作为功能元件的横线支架固定在其最终位置。 用于固定组件的其他替代功能元件，例如用于特定安装要求的纵向线支架，横向板条或纵向板条，如果需要，可以与至少一个支架组合，以便形成具有任何所需程度的支架装置 的复杂性。