公开(公告)号：US20080295407A1

公开(公告)日：2008-12-04

申请号：US11630308

申请日：2005-06-14

申请人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

发明人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

IPC分类号： B64D11/00 ,  E05F15/00 ,  G01R27/26

CPC分类号： G05G15/08 ,  B64D11/003

摘要： This device is provided for a luggage compartment designed to be placed overhead. The compartment comprises a mobile part (4) between an open position and a closed position and a mechanism for acting on said mobile part (4) to promote its closing. Said mobile part (4) presents an opening (14) designed for introducing and retrieving luggage as well as a lower exterior surface (12). The control device comprises detection means reacting when pressure is exerted on a predetermined zone of the lower exterior surface (12) of the mobile part (4) as well as for sending a control signal to the mechanism acting on the mobile part (4) to close the part when pressure is exerted on said detection means. The detection means are disposed at the lower exterior surface (12) of the mobile part (4).

摘要翻译： 该设备提供用于设置在顶部的行李舱。 隔间包括在打开位置和关闭位置之间的可移动部件（4）和用于作用在所述移动部件（4）上以促进其关闭的机构。 所述移动部件（4）具有用于引入和取回行李以及下部外表面（12）的开口（14）。 控制装置包括当压力施加在可移动部件（4）的下部外表面（12）的预定区域上并且用于向作用在移动部件（4）上的机构发送控制信号时响应的检测装置 当对所述检测装置施加压力时，关闭该部件。 检测装置设置在移动部件（4）的下外表面（12）处。

公开(公告)号：US20090189733A1

公开(公告)日：2009-07-30

申请号：US12321211

申请日：2009-01-16

申请人： Olaf von Wieding ,  Lars Rowold ,  Bodo Wisch

发明人： Olaf von Wieding ,  Lars Rowold ,  Bodo Wisch

IPC分类号： G08B29/00

CPC分类号： G05G15/08 ,  B64D11/003

摘要： A detection unit for integration in a luggage compartment of an airplane, having a capacitive sensor with an active layer, wherein the capacitive sensor is adapted to detect a first event triggered by a user, wherein the detection unit is adapted to transmit a first control signal to a control mechanism, wherein the first control signal corresponds to the first event and wherein the active layer comprises carbon fibre electrically isolated from a surrounding compartment structure.

摘要翻译： 一种用于集成在具有有源层的电容传感器的飞机行李舱中的检测单元，其中所述电容传感器适于检测由用户触发的第一事件，其中所述检测单元适于发送第一控制信号 涉及控制机构，其中所述第一控制信号对应于所述第一事件，并且其中所述有源层包括与周围隔室结构电隔离的碳纤维。

公开(公告)号：US07988091B2

公开(公告)日：2011-08-02

申请号：US11630308

申请日：2005-06-14

申请人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

发明人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

IPC分类号： B64D11/00

CPC分类号： G05G15/08 ,  B64D11/003

摘要： This device is provided for a luggage compartment designed to be placed overhead. The compartment comprises a mobile part (4) between an open position and a closed position and a mechanism for acting on said mobile part (4) to promote its closing. Said mobile part (4) presents an opening (14) designed for introducing and retrieving luggage as well as a lower exterior surface (12). The control device comprises detection means reacting when pressure is exerted on a predetermined zone of the lower exterior surface (12) of the mobile part (4) as well as for sending a control signal to the mechanism acting on the mobile part (4) to close the part when pressure is exerted on said detection means. The detection means are disposed at the lower exterior surface (12) of the mobile part (4).

摘要翻译： 该设备提供用于设置在顶部的行李舱。 隔间包括在打开位置和关闭位置之间的可移动部件（4）和用于作用在所述移动部件（4）上以促进其关闭的机构。 所述移动部件（4）具有用于引入和取回行李以及下部外表面（12）的开口（14）。 控制装置包括当压力施加在可移动部件（4）的下部外表面（12）的预定区域上并且用于向作用在移动部件（4）上的机构发送控制信号时响应的检测装置 当对所述检测装置施加压力时，关闭该部件。 检测装置设置在移动部件（4）的下外表面（12）处。

公开(公告)号：US07934678B2

公开(公告)日：2011-05-03

申请号：US12321211

申请日：2009-01-16

申请人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch

发明人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch

IPC分类号： B64D11/00

CPC分类号： G05G15/08 ,  B64D11/003

摘要： A detection unit for integration in a luggage compartment of an airplane, having a capacitive sensor with an active layer, wherein the capacitive sensor is adapted to detect a first event triggered by a user, wherein the detection unit is adapted to transmit a first control signal to a control mechanism, wherein the first control signal corresponds to the first event and wherein the active layer comprises carbon fiber electrically isolated from a surrounding compartment structure.

摘要翻译： 一种用于集成在具有有源层的电容传感器的飞机行李舱中的检测单元，其中所述电容传感器适于检测由用户触发的第一事件，其中所述检测单元适于发送第一控制信号 涉及控制机构，其中所述第一控制信号对应于所述第一事件，并且其中所述有源层包括与周围隔室结构电隔离的碳纤维。

公开(公告)号：US07378989B2

公开(公告)日：2008-05-27

申请号：US11027562

申请日：2004-12-30

申请人： Bodo Wisch ,  Lars Rowold

发明人： Bodo Wisch ,  Lars Rowold

IPC分类号： B64D47/06

CPC分类号： B64D25/00 ,  A62B3/00 ,  B64D11/00 ,  B64D47/02 ,  B64D2011/0038 ,  Y02T50/46

摘要： An emergency lighting arrangement preferably includes plural emergency light units connected to an on-board power supply network of an aircraft, and plural emergency current sources that each include at least one capacitor. Each emergency light unit includes an emergency light emitting element and a control unit that automatically connects the capacitor of the emergency current source to the emergency light emitting element upon the failure of the on-board power supply network. Preferably, the emergency current source including the capacitor is integrated into the emergency light unit. The emergency light unit may further include normal operation light emitting elements selectively connected by the control unit to the on-board power supply network. The control unit switches between normal operation of the normal light emitting elements and charging of the capacitor, and emergency operation in which the capacitor discharges through the emergency light emitting element.

摘要翻译： 紧急照明装置优选地包括连接到飞行器的车载电源网络的多个应急灯单元和各自包括至少一个电容器的多个应急电流源。 每个应急灯单元包括应急发光元件和一个控制单元，当车载电源网络发生故障时，自动将应急电流源的电容器连接到应急发光元件。 优选地，包括电容器的应急电流源集成到应急灯单元中。 应急灯单元还可以包括由控制单元选择性地连接到车载电源网络的正常操作发光元件。 控制单元在普通发光元件的正常工作和电容器的充电之间切换，电容器通过应急发光元件放电的紧急动作。

公开(公告)号：US08368244B2

公开(公告)日：2013-02-05

申请号：US11813465

申请日：2006-01-18

申请人： Bodo Wisch ,  Lars Rowold

发明人： Bodo Wisch ,  Lars Rowold

IPC分类号： H02J7/34

CPC分类号： H02J4/00 ,  H02J7/345 ,  Y10T307/527

摘要： An energy buffer device supplies energy to a consumer in an aircraft, and an electrical system for an aircraft. In one example, the device includes an energy feed device, an energy storage device and an energy supply device. The energy supply device may have line with a larger cross-sectional area than a corresponding line of the energy feed device. With the use of an energy buffer device, power may be switched on only for a short period of time. In addition, in case of a voltage breakdown in an on-board network, energy may be stored in an energy storage device. Supply of energy may thus occur over a short time at correspondingly high power, without placing a load on an on-board network or a generator.

摘要翻译： 能量缓冲装置为飞机上的消费者和飞机的电气系统提供能量。 在一个示例中，该装置包括能量馈送装置，能量存储装置和能量供应装置。 能量供应装置可以具有比能量馈送装置的相应线更大的横截面积的线。 通过使用能量缓冲装置，可以在短时间内接通电源。 此外，在车载网络中的电压故障的情况下，能量可以存储在能量存储装置中。 因此，能够在相当大的功率下在短时间内进行能量供给，而不会在车载网络或发电机上施加负载。

公开(公告)号：US20050211834A1

公开(公告)日：2005-09-29

申请号：US11022114

申请日：2004-12-23

申请人： Bodo Wisch ,  Lars Rowold

发明人： Bodo Wisch ,  Lars Rowold

IPC分类号： B60R5/00 ,  B61D37/00 ,  B64D11/00

CPC分类号： B64D11/003 ,  B60R5/003

摘要： The application concerns a lifting device for a luggage compartment in an aircraft, wherein the luggage compartment can be moved between an open and closed position, and the lifting device includes a power generation element that exerts a lifting force on the luggage compartment. The application also concerns an aircraft with a lifting device for a luggage compartment. The power generation element is an electrical power generation element, and the lifting device has a rechargeable energy accumulator to store energy for operation of the electrical power generation element.

摘要翻译： 该应用涉及一种用于飞行器中的行李箱的提升装置，其中行李箱可以在打开和关闭位置之间移动，并且提升装置包括在行李箱上施加提升力的发电元件。 该应用还涉及具有用于行李箱的提升装置的飞机。 发电元件是发电元件，并且提升装置具有用于存储用于发电元件的操作的能量的可再充电能量蓄能器。

公开(公告)号：US20100014009A1

公开(公告)日：2010-01-21

申请号：US12224029

申请日：2007-02-14

申请人： Mikael Stavaeus ,  Bodo Wisch ,  Wolfgang Süss ,  Lars Rowold

发明人： Mikael Stavaeus ,  Bodo Wisch ,  Wolfgang Süss ,  Lars Rowold

IPC分类号： H04N5/64 ,  B64D11/00

CPC分类号： B64D11/0015 ,  B64D11/00153 ,  B64D2011/0061 ,  G06F3/1438 ,  G09F9/33 ,  G09G3/3208 ,  Y02T50/46

摘要： A visualization system in the passenger cabin of an aircraft, by which visualization system data relating to informing, instructing and entertaining passengers can be visually presented, along with graphic effects. The visualization system includes a lining panel to line the passenger cabin, and a control unit. The lining panel is coated with a flexible display that is coupled to the control unit, which, for the purpose of presenting information, is equipped to supply electricity in a targeted manner to the display.

摘要翻译： 航空器客舱中的可视化系统，通过该可视化系统可以视觉呈现与通知，指导和娱乐乘客有关的可视化系统数据以及图形效果。 可视化系统包括用于排列客舱的衬板和控制单元。 衬里面板涂有柔性显示器，该柔性显示器耦合到控制单元，为了呈现信息，该控制单元被配备成以目标方式向显示器供电。

公开(公告)号：US07534016B2

公开(公告)日：2009-05-19

申请号：US11702001

申请日：2007-02-02

申请人： Mikael Stavaeus ,  Bodo Wisch ,  Carsten Kohlmeier Beckmann ,  Lars Rowold

发明人： Mikael Stavaeus ,  Bodo Wisch ,  Carsten Kohlmeier Beckmann ,  Lars Rowold

IPC分类号： F21V33/00 ,  B64D47/02

CPC分类号： B64C1/1484 ,  B64D2011/0061 ,  E06B9/24 ,  E06B2009/2464

摘要： A window unit for an aircraft with which individual lighting scenarios can be produced. In addition, an aircraft is equipped with at least one window unit. The window unit includes a window pane, which is coated with an electrically actuatable shading device for reducing incidental light entering through the window page. In addition, the window unit includes a control unit for operating the shading device as well as a lighting device for producing a light effect in the region of the window unit. In this connection, the control unit has an interface via which the control unit is connected to a network system of the aircraft for operation of the shading device. Likewise, the lighting device is coupled with the control unit, so that the lighting device can be operated with the network system of the aircraft via the interface of the control unit.

摘要翻译： 用于可以生产各种照明场景的飞机的窗单元。 另外，一架飞机配有至少一个窗单元。 窗户单元包括窗玻璃，其被涂覆有电致动阴影装置，用于减少通过窗页进入的附带光。 此外，窗单元包括用于操作遮光装置的控制单元以及用于在窗单元的区域中产生光效果的照明装置。 在这方面，控制单元具有接口，通过该接口，控制单元连接到飞行器的网络系统以用于遮蔽装置的操作。 同样地，照明装置与控制单元相连，使得照明装置可以通过控制单元的接口与飞行器的网络系统一起操作。

公开(公告)号：US20070186477A1

公开(公告)日：2007-08-16

申请号：US11702001

申请日：2007-02-02

申请人： Mikael Stavaeus ,  Bodo Wisch ,  Carsten Kohlmeier Beckmann ,  Lars Rowold

发明人： Mikael Stavaeus ,  Bodo Wisch ,  Carsten Kohlmeier Beckmann ,  Lars Rowold

IPC分类号： E05F17/00

CPC分类号： B64C1/1484 ,  B64D2011/0061 ,  E06B9/24 ,  E06B2009/2464

摘要： A window unit for an aircraft with which individual lighting scenarios can be produced. In addition, an aircraft is equipped with at least one window unit. The window unit includes a window pane, which is coated with an electrically actuatable shading device for reducing incidental light entering through the window page. In addition, the window unit includes a control unit for operating the shading device as well as a lighting device for producing a light effect in the region of the window unit. In this connection, the control unit has an interface via which the control unit is connected to a network system of the aircraft for operation of the shading device. Likewise, the lighting device is coupled with the control unit, so that the lighting device can be operated with the network system of the aircraft via the interface of the control unit.

摘要翻译： 用于可以生产各种照明场景的飞机的窗单元。 另外，一架飞机配有至少一个窗单元。 窗户单元包括窗玻璃，其被涂覆有电致动阴影装置，用于减少通过窗页进入的附带光。 此外，窗单元包括用于操作遮光装置的控制单元以及用于在窗单元的区域中产生光效果的照明装置。 在这方面，控制单元具有接口，通过该接口，控制单元连接到飞行器的网络系统以用于遮蔽装置的操作。 同样地，照明装置与控制单元相连，使得照明装置可以通过控制单元的接口与飞行器的网络系统一起操作。