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公开(公告)号：US07746037B2
公开(公告)日：2010-06-29
申请号：US11656879
申请日：2007-01-23
申请人： Mikael Stavaeus , Bodo Wisch , Wolfgang Suess , Lars Rowold
发明人： Mikael Stavaeus , Bodo Wisch , Wolfgang Suess , Lars Rowold
CPC分类号： B64C1/1476 , B60J3/04 , B64D2011/0061
摘要： An electric window dimming device for reducing the light transmission of a window for an aircraft. The electric window dimming device comprises a capacitance. The electric window dimming device is adapted for being connected to the capacitance and to a primary energy source that provides energy. If the primary energy source fails, the capacitance supplies energy for electric window dimming device.
摘要翻译： 一种用于减少飞行器窗口的光透射的电动窗调光装置。 电动窗调光装置包括电容。 电动窗调光装置适于连接到电容和提供能量的一次能量源。 如果主能源发生故障，电容器为电动窗户调光装置提供能量。
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公开(公告)号：US20080144158A1
公开(公告)日：2008-06-19
申请号：US11656879
申请日：2007-01-23
申请人： Mikael Stavaeus , Bodo Wisch , Wolfgang Suess , Lars Rowold
发明人： Mikael Stavaeus , Bodo Wisch , Wolfgang Suess , Lars Rowold
CPC分类号： B64C1/1476 , B60J3/04 , B64D2011/0061
摘要： An electric window dimming device for reducing the light transmission of a window for an aircraft. The electric window dimming device comprises a capacitance. The electric window dimming device is adapted for being connected to the capacitance and to a primary energy source that provides energy. If the primary energy source fails, the capacitance supplies energy for electric window dimming device.
摘要翻译： 一种用于减少飞行器窗口的光透射的电动窗调光装置。 电动窗调光装置包括电容。 电动窗调光装置适于连接到电容和提供能量的一次能量源。 如果主能源发生故障，电容器为电动窗户调光装置提供能量。
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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
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。
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公开(公告)号：US07534016B2
公开(公告)日：2009-05-19
申请号：US11702001
申请日：2007-02-02
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。
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公开(公告)号：US20070186477A1
公开(公告)日：2007-08-16
申请号：US11702001
申请日：2007-02-02
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。
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公开(公告)号：US08116975B2
公开(公告)日：2012-02-14
申请号：US11704888
申请日：2007-02-09
申请人： Mikael Stavaeus , Jan Peter , Wolfgang Suess , Lars Rowold
发明人： Mikael Stavaeus , Jan Peter , Wolfgang Suess , Lars Rowold
IPC分类号： G01C21/00
CPC分类号： G08G5/0021 , G01C23/005
摘要： A landmark information system in an aircraft, by which landmark information system data relating to informing, instructing and entertaining passengers may be visually presented. An aircraft equipped with a landmark information system is also provided. The landmark information system comprises an aircraft window with at least one pane and a control unit. The at least one pane is coated with a translucent display that is coupled to the control unit, which, for the purpose of presenting information, is equipped to supply electrical current in a targeted manner to the display. Furthermore, the landmark information system comprises a landmark determination device which may provide geographic data relating to landmarks, for presentation on the translucent display.
摘要翻译： 航空器中的地标性信息系统，可以通过视觉呈现与通知，指导和娱乐乘客有关的地标信息系统数据。 还提供了配备地标信息系统的飞机。 地标信息系统包括具有至少一个窗格和控制单元的飞机窗。 所述至少一个窗格被涂覆有半透明显示器，所述半透明显示器耦合到所述控制单元，为了呈现信息，所述控制单元被配备成以目标方式向所述显示器提供电流。 此外，地标信息系统包括可以提供与地标有关的地理数据的地标确定装置，用于呈现在半透明显示器上。
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公开(公告)号：US20080021636A1
公开(公告)日：2008-01-24
申请号：US11704888
申请日：2007-02-09
申请人： Mikael Stavaeus , Jan Peter , Wolfgang Suess , Lars Rowold
发明人： Mikael Stavaeus , Jan Peter , Wolfgang Suess , Lars Rowold
IPC分类号： G01C21/00
CPC分类号： G08G5/0021 , G01C23/005
摘要： A landmark information system in an aircraft, by which landmark information system data relating to informing, instructing and entertaining passengers may be visually presented. An aircraft equipped with a landmark information system is also provided. The landmark information system comprises an aircraft window with at least one pane and a control unit. The at least one pane is coated with a translucent display that is coupled to the control unit, which, for the purpose of presenting information, is equipped to supply electrical current in a targeted manner to the display. Furthermore, the landmark information system comprises a landmark determination device which may provide geographic data relating to landmarks, for presentation on the translucent display.
摘要翻译： 航空器中的地标性信息系统，可以通过视觉呈现与通知，指导和娱乐乘客有关的地标信息系统数据。 还提供了配备地标信息系统的飞机。 地标信息系统包括具有至少一个窗格和控制单元的飞机窗。 所述至少一个窗格被涂覆有半透明显示器，所述半透明显示器耦合到所述控制单元，为了呈现信息，所述控制单元被配备成以目标方式向所述显示器提供电流。 此外，地标信息系统包括可以提供与地标有关的地理数据的地标确定装置，用于呈现在半透明显示器上。
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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
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。
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9.发明授权Emergency lighting arrangement with decentralized emergency power supply for an aircraft 有权应急照明安排，配有飞机分散应急电源公开(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
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。
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公开(公告)号：US20100005495A1
公开(公告)日：2010-01-07
申请号：US12223728
申请日：2007-02-09
申请人： Mikael Stavaeus , Olaf Von Wieding , Wolfgang Süss , Lars Rowold
发明人： Mikael Stavaeus , Olaf Von Wieding , Wolfgang Süss , Lars Rowold
CPC分类号： B64C1/1484 , B64D11/0015 , B64D11/00153 , B64D2011/0061 , G09F9/33 , G09G3/3208 , Y02T50/46
摘要： An information system in an aircraft, whereby information system data relating to informing, instructing and entertaining passengers can be visually presented. The information system includes an aircraft window with at least one pane and a control unit. The at least one pane, is coated with a translucent display that is coupled to the control unit, which, for the purpose of presenting information, is equipped to supply electrical current in a targeted manner to the display.
摘要翻译： 一种飞机中的信息系统，可以直观地呈现与告知，指导和娱乐乘客有关的信息系统数据。 信息系统包括具有至少一个窗格和控制单元的飞机窗口。 所述至少一个窗格被涂覆有半透明显示器，所述半透明显示器耦合到所述控制单元，为了呈现信息，所述控制单元被配备成以目标方式向所述显示器提供电流。
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