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公开(公告)号：US08348451B2
公开(公告)日：2013-01-08
申请号：US11776312
申请日：2007-07-11
IPC分类号： F21S8/02
CPC分类号： B60Q3/46 , B64D2011/0038 , B64D2203/00
摘要： Emergency cabin illumination for an aircraft, including: at least one cabin component of an aircraft and at least one emergency lighting device, the at least one emergency lighting device being arranged in the cabin component so that the emergency lighting device in its switched-off state has no contrast to its environment, and in the switched-on state of the emergency lighting device, the light emitted emerges from the cabin component.
摘要翻译： 一种用于飞机的紧急舱照明，包括：飞机的至少一个客舱部件和至少一个应急照明装置，所述至少一个应急照明装置布置在所述舱室部件中，使得所述应急照明装置处于关闭状态 与其环境没有对比，并且在应急照明装置的接通状态下，从舱室部件发出的光发射出来。
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公开(公告)号：US20080013332A1
公开(公告)日：2008-01-17
申请号：US11776312
申请日：2007-07-11
IPC分类号： B64D47/00
CPC分类号： B60Q3/46 , B64D2011/0038 , B64D2203/00
摘要： Emergency cabin illumination for an aircraft, comprising: at least one cabin component (2, 10, 20, 30) of an aircraft and at least one emergency lighting means (6, 16, 22, 34), the at least one emergency lighting means (6, 16, 22, 34) being arranged in or on the cabin component (2, 10, 20, 30) so that the emergency lighting means (6, 16, 22, 34) in its switched-off state has no contrast to its environment, and in the switched-on state of the emergency lighting means (6, 16, 22, 34) the light which it emits emerges from or on the cabin component (2, 10, 20, 30).
摘要翻译： 一种用于飞机的紧急舱照明，包括：飞机的至少一个客舱部件（2,10,20,30）和至少一个紧急照明装置（6,16,22,34），所述至少一个应急照明装置 （6,16,22,34）布置在所述客舱部件（2,10,20,30）中或其上，使得处于其关闭状态的应急照明装置（6,16,22,34）没有对比度 在其环境中，并且在紧急照明装置（6,16,22,34）的接通状态下，其发射的光从舱室部件（2,10,20,30）中排出。
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公开(公告)号：US06842120B2
公开(公告)日：2005-01-11
申请号：US10434211
申请日：2003-05-09
摘要： A device comprises a luminous indicator intended to indicate an emergency exit and capable of being placed in at least one of three different states, a standby state, in which it emits a first luminous radiation which is continuous and which exhibits a first intensity, an alert state, in which it emits a second luminous radiation which is discontinuous and which exhibits a second intensity greater than the first intensity, and a third state, and an operating unit for operating the luminous indicator in such a way as to place it in the standby state, in a normal situation, in the alert state, during an emergency evacuation via the emergency exit, which is passable, and in the third state, during an emergency evacuation when the emergency exit is impassable.
摘要翻译： 一种装置包括用于指示紧急出口并能够被放置在三种不同状态中的至少一种状态的待发光指示器，待机状态中，其发射连续的第一发光辐射并且呈现第一强度，警报 状态，其中发射不连续的并且表现出大于第一强度的第二强度的第二发光和第三状态;以及操作单元，用于以将其置于待机状态的方式操作发光指示器 在正常情况下处于警戒状态，在通过紧急出口的紧急撤离期间，在第三状态下，在紧急撤离期间，当紧急出口不通时。
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公开(公告)号：US08579479B2
公开(公告)日：2013-11-12
申请号：US12996831
申请日：2009-06-19
申请人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
发明人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
IPC分类号： B64D47/02
CPC分类号： B64D47/06 , B64D2203/00 , F21S43/14 , F21S45/43 , F21S45/47 , F21V29/70 , F21V29/74 , F21V29/83 , F21W2107/30 , F21W2111/00 , F21Y2115/10
摘要： The warning lamp for an aircraft is provided with a housing (10) which possesses a light permeable cover (12) that is exposed to the surrounding air when the housing is mounted on the aircraft, with a frontal cover area and a rear cover area, a mounting element (44) to fasten the cover to a lower part (14) of the housing (10), wherein one edge (41) of the cover (12) is covered by an edge of the mounting element (44) and protrudes from it, a lamp with at least one LED (42,46,58,60), which is arranged within an area that is covered by the cover (12), and a cooling body (18) for the at least one LED (42,46,58,60), wherein the cooling body (18) possesses a cooling surface (32) that is exposed to the surrounding air when the housing (10) is mounted on the aircraft. The frontal cover area is formed by a frontal cover element (22) which is made from a light permeable first material. The rear cover area is formed by a rear cover element (28), which is made from a light permeable second material. The cooling body (18), while separating the frontal cover element (22) from the rear cover element (28), is arranged between them, wherein its cooling surface (32) is a part of the external contours of the cover (12) of the housing (10) that is given by the frontal and rear cover elements (22,28) and possesses an upper region (38) as well as adjacent, opposing side areas (40).
摘要翻译： 用于飞行器的警示灯设置有壳体（10），该壳体具有透光罩（12），当壳体安装在飞行器上时，该透光罩暴露于周围的空气，具有正面盖区域和后盖区域， 安装元件（44），用于将盖子紧固到壳体（10）的下部（14），其中盖（12）的一个边缘（41）被安装元件（44）的边缘覆盖并且突出 一种具有至少一个LED（42,46,58,60）的灯，其布置在由所述盖（12）覆盖的区域内，以及用于所述至少一个LED的冷却体（18） 42,46,58,60），其中所述冷却体（18）具有当壳体（10）安装在飞机上时暴露于周围空气的冷却表面（32）。 正面覆盖区域是由可透光的第一材料制成的前盖元件（22）形成的。 后盖区域由可透光的第二材料制成的后盖元件（28）形成。 冷却体（18）在将前盖元件（22）与后盖元件（28）分离的同时被布置在它们之间，其中其冷却表面（32）是盖子（12）的外部轮廓的一部分， 由前侧和后盖元件（22,28）给出并具有上部区域（38）以及相邻的相对的侧部区域（40）的壳体（10）。
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公开(公告)号：US07186012B2
公开(公告)日：2007-03-06
申请号：US10888277
申请日：2004-07-09
IPC分类号： F21V7/04
CPC分类号： F21S8/02 , B60Q3/43 , B64D11/00 , B64D2011/0038 , F21V21/04 , F21V31/04 , F21Y2115/10 , G02B6/4298 , Y10S362/80
摘要： A lighting element has a light emitting diode that is installed in a light carrier. The lighting element has a light guide element that is optically coupled to the light emitting diode and the light guide element has a smaller light exit surface than the light emitting diode. With a plurality of such lighting elements it is possible to embody an effect lighting configuration for example in an aircraft cabin.
摘要翻译： 照明元件具有安装在光载体中的发光二极管。 照明元件具有与发光二极管光学耦合的导光元件，并且导光元件具有比发光二极管更小的光出射表面。 利用多个这样的照明元件，可以例如在飞机机舱中体现效果照明配置。
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公开(公告)号：US20060114683A1
公开(公告)日：2006-06-01
申请号：US11252447
申请日：2005-10-18
IPC分类号： F21V11/00
CPC分类号： B64D11/00 , B60K2370/343 , B60Q3/43 , B60Q3/44 , B60Q3/46 , B60Q3/745 , B64D2011/0038 , B64D2011/0053 , B64D2011/0061
摘要： In present-day passenger aircraft, fluorescent lamps in tubular form, are used as general illumination. An illumination unit for aircraft having a two-dimensional light source, an aperture which is at least partly translucent, and an attachment element. In this arrangement, the aperture is an interior fitting element of an aircraft cabin so that the entire illumination unit can be integrated in the aircraft cabin when the interior fitting element is installed. The flat design of the light source makes the installation of the light source possible in spaces of limited depth.
摘要翻译： 在当今的客机中，以管状形式的荧光灯被用作一般照明。 用于具有二维光源的飞行器的照明单元，至少部分半透明的孔和附接元件。 在这种布置中，孔是飞机机舱的内部装配元件，使得当安装内部装配元件时，整个照明单元可以集成在飞机机舱中。 光源的平面设计使得光源的安装可能在有限深度的空间中。
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公开(公告)号：US07731399B2
公开(公告)日：2010-06-08
申请号：US12064412
申请日：2006-08-21
IPC分类号： F21V21/005
CPC分类号： B64D11/00 , B60Q3/43 , B60Q3/44 , B60Q3/47 , B60Q3/51 , B60Q3/78 , B64D2011/0038 , B64D2203/00
摘要： The present invention relates to an illumination strip for illuminating a handrail recess that itself at the same time forms a handrail; to a hatrack for installation in an aircraft cabin with a correspondingly designed handrail recess that at least in sections can be illuminated; as well as to the use of an illumination strip or a hatrack in an aircraft. The illumination strip comprises a carrier module for accommodating the illumination unit and illumination units accommodated by the carrier module. The carrier module is strip shaped and includes a positive locking member to secure the carrier module of the illumination strip into the handrail in an exchangeable manner.
摘要翻译： 本发明涉及一种用于照亮扶手凹部的照明条，其自身同时形成扶手; 用于安装在具有相应设计的扶手凹部的飞机机舱中，至少可以照亮部分; 以及在飞机上使用照明条或吊竿。 照明条包括用于容纳照明单元的载体模块和由载体模块容纳的照明单元。 载体模块是带状的并且包括正的锁定构件，以将照明条的载体模块以可更换的方式固定到扶手中。
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公开(公告)号：US20100012780A1
公开(公告)日：2010-01-21
申请号：US12503742
申请日：2009-07-15
IPC分类号： B64D11/00
CPC分类号： B64D11/00 , B60Q3/44 , B60Q3/47 , B64D2011/0053
摘要： The present invention concerns a system for servicing a plurality of service positions which are assigned to a plurality of installation elements, in particular passenger seats in an aircraft, comprising: a plurality of service units, in particular lighting units, wherein the number of service units exceeds the number of service positions to be serviced, and a control unit, wherein the control unit is adapted to receive a respective item of control information including an identification in respect of an installation element and to control a predetermined service unit on the basis of the identification, and a method of servicing a plurality of service positions which are assigned to a plurality of installation elements, in particular passenger seats in an aircraft, and a corresponding computer program.
摘要翻译： 本发明涉及一种用于维修分配给飞行器中的多个安装元件，特别是乘客座椅的多个维修位置的系统，包括：多个服务单元，特别是照明单元，其中服务单元的数量 超过要维修的服务位置的数量;以及控制单元，其中，所述控制单元适于接收包括关于安装元件的标识的各个控制信息项，并且基于所述控制单元来控制预定的服务单元 识别和维护分配给飞行器中的多个安装元件，特别是乘客座位的多个维修位置的方法以及相应的计算机程序。
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公开(公告)号：US20080219012A1
公开(公告)日：2008-09-11
申请号：US12064412
申请日：2006-08-21
IPC分类号： B64D47/02
CPC分类号： B64D11/00 , B60Q3/43 , B60Q3/44 , B60Q3/47 , B60Q3/51 , B60Q3/78 , B64D2011/0038 , B64D2203/00
摘要： The present invention relates to an illumination strip by means of which a handrail recess that itself at the same time forms a handrail can be illuminated; to a hatrack for installation in an aircraft cabin with a correspondingly designed handrail recess that at least in sections can be illuminated; as well as to the use of an illumination strip or a hatrack in an aircraft. The illumination strip comprises carrier module for accommodating an illumination means and a multitude of illumination means that are accommodated by the carrier module. The carrier module is strip shaped and comprises at least one positive locking means by means of which, for the purpose of illuminating the handrail recess, the carrier module can be fitted into the handrail so as to provide a positive-locking fit and so as to be exchangeable.
摘要翻译： 本发明涉及照明条，通过该照明条可以照亮自身同时形成扶手的扶手凹部; 用于安装在具有相应设计的扶手凹部的飞机机舱中，至少可以照亮部分; 以及在飞机上使用照明条或吊竿。 照明条包括用于容纳照明装置的载体模块和由载体模块容纳的多个照明装置。 托架模块是带状的，并且包括至少一个正锁定装置，借助于该锁定装置，为了照亮扶手凹槽，托架模块可以装配到扶手中，以便提供正锁定配合，并且 可交换
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公开(公告)号：US20110261577A1
公开(公告)日：2011-10-27
申请号：US12996831
申请日：2009-06-19
申请人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
发明人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
IPC分类号： F21S8/10
CPC分类号： B64D47/06 , B64D2203/00 , F21S43/14 , F21S45/43 , F21S45/47 , F21V29/70 , F21V29/74 , F21V29/83 , F21W2107/30 , F21W2111/00 , F21Y2115/10
摘要： The warning lamp for an aircraft is provided with a housing (10) which possesses a light permeable cover (12) that is exposed to the surrounding air when the housing is mounted on the aircraft, with a frontal cover area and a rear cover area, a mounting element (44) to fasten the cover to a lower part (14) of the housing (10), wherein one edge (41) of the cover (12) is covered by an edge of the mounting element (44) and protrudes from it, a lamp with at least one LED (42,46,58,60), which is arranged within an area that is covered by the cover (12), and a cooling body (18) for the at least one LED (42,46,58,60), wherein the cooling body (18) possesses a cooling surface (32) that is exposed to the surrounding air when the housing (10) is mounted on the aircraft. The frontal cover area is formed by a frontal cover element (22) which is made from a light permeable first material. The rear cover area is formed by a rear cover element (28), which is made from a light permeable second material. The cooling body (18), while separating the frontal cover element (22) from the rear cover element (28), is arranged between them, wherein its cooling surface (32) is a part of the external contours of the cover (12) of the housing (10) that is given by the frontal and rear cover elements (22,28) and possesses an upper region (38) as well as adjacent, opposing side areas (40).
摘要翻译： 用于飞行器的警示灯设置有壳体（10），该壳体具有透光罩（12），当壳体安装在飞行器上时，该透光罩暴露于周围的空气，具有正面盖区域和后盖区域， 安装元件（44），用于将盖子紧固到壳体（10）的下部（14），其中盖（12）的一个边缘（41）被安装元件（44）的边缘覆盖并且突出 一种具有至少一个LED（42,46,58,60）的灯，其布置在由所述盖（12）覆盖的区域内，以及用于所述至少一个LED的冷却体（18） 42,46,58,60），其中所述冷却体（18）具有当壳体（10）安装在飞机上时暴露于周围空气的冷却表面（32）。 正面覆盖区域是由可透光的第一材料制成的前盖元件（22）形成的。 后盖区域由可透光的第二材料制成的后盖元件（28）形成。 冷却体（18）在将前盖元件（22）与后盖元件（28）分离的同时被布置在它们之间，其中其冷却表面（32）是盖子（12）的外部轮廓的一部分， 由前侧和后盖元件（22,28）给出并具有上部区域（38）以及相邻的相对的侧部区域（40）的壳体（10）。
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