公开(公告)号：US08500065B2

公开(公告)日：2013-08-06

申请号：US13179794

申请日：2011-07-11

申请人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Juergen Grabmann ,  Dietmar Voelkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla

发明人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Juergen Grabmann ,  Dietmar Voelkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla

IPC分类号： B64C13/00

CPC分类号： B64D11/00 ,  B64D2011/0053 ,  B64D2013/003 ,  Y02T50/46 ,  Y10T29/49826

摘要： Corresponding to reducing the number of components that need to be separately installed, in addition to a weight reduction and a reduction in the cable loom volume, improved system reliability is obtained if the loads relating to a seating space in a passenger cabin (12), in particular in an aircraft, are combined on an overhead panel (17) which is connected, via line connections which are now only short, to a spatially associated supply module (19), which is operated in cutouts (20) in a stub frame (13), in order to anchor a hat rack (11) in the fuselage structure (16) of the cabin (12).

摘要翻译： 对于减少需要单独安装的部件的数量，除了重量减轻和电缆织机体积的减少之外，如果与客舱（12）中的座位空间有关的负载，则可以获得提高的系统可靠性， 特别是在飞行器中，组合在高架板（17）上，该顶板经由现在仅短路的线路连接到空间相关的供电模块（19），空间相关的供电模块（19）在短截线框架 （13），以将帽架（11）固定在机舱（12）的机身结构（16）中。

公开(公告)号：US20120223184A1

公开(公告)日：2012-09-06

申请号：US13179794

申请日：2011-07-11

申请人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Juergen Grabmann ,  Dietmar Volkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla

发明人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Juergen Grabmann ,  Dietmar Volkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla

IPC分类号： B64D11/00

CPC分类号： B64D11/00 ,  B64D2011/0053 ,  B64D2013/003 ,  Y02T50/46 ,  Y10T29/49826

摘要： Corresponding to reducing the number of components that need to be separately installed, in addition to a weight reduction and a reduction in the cable loom volume, improved system reliability is obtained if the loads relating to a seating space in a passenger cabin (12), in particular in an aircraft, are combined on an overhead panel (17) which is connected, via line connections which are now only short, to a spatially associated supply module (19), which is operated in cutouts (20) in a stub frame (13), in order to anchor a hat rack (11) in the fuselage structure (16) of the cabin (12).

摘要翻译： 对于减少需要单独安装的部件的数量，除了重量减轻和电缆织机体积的减少之外，如果与客舱（12）中的座位空间有关的负载，则可以获得提高的系统可靠性， 特别是在飞行器中，组合在高架板（17）上，该顶板经由现在仅短路的线路连接到空间相关的供电模块（19），空间相关的供电模块（19）在短截线框架 （13），以将帽架（11）固定在机舱（12）的机身结构（16）中。

公开(公告)号：US08644022B2

公开(公告)日：2014-02-04

申请号：US13162080

申请日：2011-06-16

申请人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Jürgen Grabmann ,  Dietmar Völkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla

发明人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Jürgen Grabmann ,  Dietmar Völkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla

IPC分类号： H05K7/20

CPC分类号： B64D11/0023 ,  B64D2011/0038 ,  B64D2011/0046 ,  Y02T50/46

摘要： An internal device arrangement for a passenger cabin, for example of an aircraft, is provided. The device has an internal device element which is selected from a group including wall paneling, window panel, side panel, ceiling paneling and luggage compartment. The device has an electrical apparatus fitted in or on the internal device element; and at least one line for supplying power to the electrical apparatus. Furthermore, a heat dissipation device in the form of an integral component part of the internal device element, the electrical apparatus and/or the at least one line is provided. Such a heat dissipation device makes it possible to dispense with an additional heat sink for temperature management and thus save installation space and weight.

摘要翻译： 提供了用于例如飞行器的客舱的内部装置装置。 该装置具有从包括墙板，窗板，侧板，天花板镶板和行李箱的组中选择的内部装置元件。 该装置具有安装在内部装置元件中或之上的电气装置; 以及用于向电气设备供电的至少一条线。 此外，提供了内部装置元件，电气装置和/或至少一条线的整体部件形式的散热装置。 这样的散热装置使得可以省去用于温度管理的附加散热器，从而节省安装空间和重量。

公开(公告)号：US08800922B2

公开(公告)日：2014-08-12

申请号：US13181623

申请日：2011-07-13

申请人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Jürgen Grabmann ,  Dietmar Völkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla ,  Ralph Pätzold ,  Dirk-Achim Schevardo ,  Peter Younes

发明人： Frank Schmid ,  Marc Renz ,  Norbert Knopp ,  Jürgen Grabmann ,  Dietmar Völkle ,  Markus Klingseis ,  Wolf-Dieter Kuhnla ,  Ralph Pätzold ,  Dirk-Achim Schevardo ,  Peter Younes

IPC分类号： B64C1/00

CPC分类号： B64D11/00 ,  B29C70/86 ,  B29C70/865 ,  B64D2011/0046 ,  Y02T50/43 ,  Y10T29/49865

摘要： The description covers cabin components for aircraft, which can be produced with a sandwich structure and may have the components 1003 for signal and/or power transmission. The cabin components in this case have at least two prepreg layers 1001, 1005 and, for example, a honeycomb layer 1002, which can be connected to one another by pressing and heating. Furthermore, electrical and/or optical signal paths are shown on cabin components, which can be produced by positioning them there or printing. In addition, according to the description, signal and/or power transmission can take place beyond the boundary of cabin components, by means of a transmitter/receiver path.

摘要翻译： 描述涵盖用于飞机的舱室部件，其可以用夹层结构制造，并且可以具有用于信号和/或动力传递的部件1003。 这种情况下的舱室部件具有至少两个预浸料层1001,1005和例如蜂窝层1002，蜂窝层1002可以通过加压和加热彼此连接。 此外，电气和/或光信号路径显示在机舱部件上，可通过将其定位在那里或打印来生产。 此外，根据描述，信号和/或功率传输可以通过发射机/接收机路径发生在舱室部件的边界之外。