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1. 发明申请

US20180170577A1 METHOD OF OPERATING AN AIRCRAFT HEADLIGHT SYSTEM, AIRCRAFT HEADLIGHT SYSTEM, AND AIRCRAFT COMPRISING THE SAME 审中-公开
公开(公告)号：US20180170577A1
公开(公告)日：2018-06-21
申请号：US15845106
申请日：2017-12-18
申请人： Goodrich Lighting Systems GmbH
发明人： Andre HESSLING-VON HEIMENDAHL , Christian SCHOEN
IPC分类号： B64D47/04 , F21S41/141 , F21S41/663 , H05B33/08 , F21S41/32 , F21S41/20 , B64D47/06 , F21S41/19
CPC分类号： B64D47/04 , B64D47/06 , B64D2203/00 , F21S41/141 , F21S41/143 , F21S41/145 , F21S41/147 , F21S41/153 , F21S41/192 , F21S41/25 , F21S41/285 , F21S41/321 , F21S41/663 , F21W2107/30 , F21Y2115/10 , H05B33/0845
摘要： A method of operating an aircraft headlight system of an aircraft, the aircraft headlight system having at least one headlight, includes the steps of operating the aircraft headlight system in a landing light mode during a descent of the aircraft, with the at least one headlight emitting a landing light output in the landing light mode; operating the aircraft headlight system in a taxi light mode during taxiing of the aircraft, with the at least one headlight emitting a taxi light output in the taxi light mode; and transforming the landing light output into the taxi light output after touch-down of the aircraft by operating the aircraft headlight system in at least one intermediate lighting mode between operating the aircraft headlight system in the landing light mode and operating the aircraft headlight system in the taxi light mode.

2. 发明授权

US09777903B2 Exterior aircraft light 有权
公开(公告)号：US09777903B2
公开(公告)日：2017-10-03
申请号：US14980544
申请日：2015-12-28
申请人： Goodrich Lighting Systems GmbH
发明人： Anil Kumar Jha , Andre Hessling-von Heimendahl
IPC分类号： B64D47/02 , F21V5/04 , B64D47/04 , F21S8/10 , F21V7/06 , F21W101/06 , F21Y115/10
CPC分类号： F21V5/048 , B64D47/02 , B64D47/04 , B64D2203/00 , F21S41/143 , F21V7/06 , F21W2107/30 , F21Y2115/10
摘要： An exterior aircraft light includes a base plate and a plurality of lighting units arranged on the base plate, wherein each of the plurality of lighting units includes an elongated LED light source for emitting light, the elongated LED light source having a light emitting surface with a longitudinal extension and a transverse extension, with the longitudinal extension being greater than the transverse extension and with a projection of the longitudinal extension onto the base plate defining an orientation direction of the elongated LED light source, and a collimating optical system for collimating the light emitted by the elongated LED light source towards a main output direction, wherein the plurality of lighting units has at least a first lighting unit and a second lighting unit.

3. 发明授权

US09618671B2 LED lighting device 有权
公开(公告)号：US09618671B2
公开(公告)日：2017-04-11
申请号：US14007787
申请日：2012-01-30
申请人： Ekkehard Gaydoul , Armin Plichta , Juergen Meinl , Bjoern Bleisinger , Martin Cramer , Thomas Reichert , Marc Timon Sprzagala , Sandra Mattheis
发明人： Ekkehard Gaydoul , Armin Plichta , Juergen Meinl , Bjoern Bleisinger , Martin Cramer , Thomas Reichert , Marc Timon Sprzagala , Sandra Mattheis
IPC分类号： F21V8/00 , B60Q3/00 , B60Q3/02 , F21S8/10
CPC分类号： G02B6/001 , B60Q3/43 , B60Q3/62 , B60Q3/64 , B64D11/00 , F21S2/00 , F21S41/14 , F21S41/141 , F21S41/24 , F21S43/13 , F21S43/237 , F21S43/245 , F21W2106/00 , F21W2107/30 , F21W2121/00 , F21Y2115/10 , G02B5/04 , G02B6/0038 , G02B6/0068 , G02B6/0073 , G02B6/008 , G02B6/02
摘要： LED lighting devices are provided that include two optical waveguides and at least one LED in an intermediate region between end faces of the optical waveguides so that radiation from the LED is coupled into the optical waveguides through the end faces. A de-coupler is on outer circumferential surface regions of each of the two separate optical waveguides. The de-coupler reflects the radiation guided in the optical waveguides so that the radiation passes through the optical waveguides and is coupled out of the optical waveguides laterally. The intermediate region has a length that is selected so that a brightness difference, measured perpendicular to an axis of the optical waveguides in the center of the intermediate region, at a distance of 10 mm perpendicular to the axis of the optical waveguides is at most 25% based on a maximum value of brightness along the axis of the optical waveguides.

4. 发明申请

US20170089532A1 HYBRID EMERGENCY EXIT LIGHTING SYSTEM 有权
公开(公告)号：US20170089532A1
公开(公告)日：2017-03-30
申请号：US14870930
申请日：2015-09-30
申请人： Erik John Oltheten
发明人： Erik John Oltheten
IPC分类号： F21S9/02 , B64D11/00 , F21V23/04 , B64C27/04 , H05B33/08 , B64D47/02 , B64D41/00 , F21K99/00 , F21V7/00
CPC分类号： F21S9/022 , B64C27/04 , B64D11/00 , B64D41/00 , B64D47/02 , B64D2011/0038 , F21V7/0008 , F21V23/04 , F21W2106/00 , F21W2107/30 , H02J9/065 , H05B33/0812 , H05B33/0845 , Y02B20/343
摘要： An emergency lighting system (ELS) for an aircraft has a capacitor, a light emitting diode (LED) selectively powered by the capacitor, and at least one of a photoluminescent sign and a photoluminescent panel configured to receive light emitted from the LED.

5. 发明申请

US20160076722A1 Dynamic Aircraft Headlight and Method of Operating a Dynamic Aircraft Headlight 有权
标题翻译：动态飞机头灯和操作动力飞机头灯的方法
公开(公告)号：US20160076722A1
公开(公告)日：2016-03-17
申请号：US14851957
申请日：2015-09-11
申请人： Goodrich Lighting Systems GmbH
发明人： Andre HESSLING von HEIMENDAHL
IPC分类号： F21S8/10
CPC分类号： B64D47/04 , B64D47/02 , B64D47/06 , F21W2107/30 , F21W2111/06 , F21Y2115/10
摘要： A dynamic aircraft headlight, includes an LED group, having a plurality of LEDs, and an optical system, comprising at least one optical element, for shaping an output light intensity distribution from the light emitted by the LED group. The LED group and the optical system are stationary within the dynamic aircraft light unit, with each LED of the LED group has a set position with respect to the optical system and with a light output of each LED being affected differently by the optical system.
摘要翻译：一种动态飞行器头灯，包括具有多个LED的LED组，以及包括至少一个光学元件的光学系统，用于对来自LED组发射的光进行输出光强分布的整形。 LED组和光学系统在动态飞行器光单元内是静止的，LED组的每个LED相对于光学系统具有设定位置，并且每个LED的光输出受到光学系统的不同影响。

6. 发明申请

US20150377452A1 PARABOLIC QUADRANT LED LIGHT FIXTURE 审中-公开
标题翻译： PARABOLIC QUADRANT LED灯具
公开(公告)号：US20150377452A1
公开(公告)日：2015-12-31
申请号：US14556717
申请日：2014-12-01
申请人： Phillip Walesa
发明人： Phillip Walesa
IPC分类号： F21V7/06 , F21V13/04 , F21V29/71 , F21S8/00
CPC分类号： F21V7/06 , B64D47/04 , B64D2203/00 , F21S41/147 , F21S41/19 , F21S41/321 , F21S45/47 , F21S45/50 , F21V29/717 , F21V29/83 , F21W2102/00 , F21W2107/30 , F21Y2101/00 , F21Y2107/30 , F21Y2115/10
摘要： The present invention is a lighting fixture device with a frustoconical housing. The frustoconical housing has a housing edge and an inner housing chamber accessible by a housing aperture. This inner housing chamber includes a parabolic reflective surface with multiple symmetrical reflective sections. Each reflective section includes at least one focal point. The device also includes an LED board mounting post forming a vertical axis through the vertex of the parabolic reflective surface. The LED board mounting post includes at least one mounting surface, to which is mounted multiple LED boards. Each LED board includes at least one LED. A central axis of each LED is aligned with at least one of the focal points.
摘要翻译：本发明是具有截头圆锥形壳体的照明器具。截头圆锥形壳体具有壳体边缘和通过壳体孔可接近的内部壳体腔室。该内壳体室包括具有多个对称反射部分的抛物面反射表面。每个反射部分包括至少一个焦点。该装置还包括通过抛物面反射表面的顶点形成垂直轴线的LED板安装柱。 LED板安装柱包括至少一个安装表面，多个LED板安装在该安装表面上。每个LED板包括至少一个LED。每个LED的中心轴与至少一个焦点对准。

7. 发明授权

US09169017B2 Aircraft interior lighting system using structured micro lens arrays 有权
标题翻译：使用结构化微透镜阵列的飞机内部照明系统
公开(公告)号：US09169017B2
公开(公告)日：2015-10-27
申请号：US13397171
申请日：2012-02-15
申请人： Michael Palagashvili , Timothy Todd King
发明人： Michael Palagashvili , Timothy Todd King
IPC分类号： F21V5/00 , B64D11/00 , F21W101/06 , F21Y101/02
CPC分类号： B64D11/00 , B60Q3/43 , B60Q3/44 , B60Q3/60 , B60Q3/64 , B64D2011/0038 , B64D2203/00 , F21V5/004 , F21V5/007 , F21V5/008 , F21W2106/00 , F21W2107/30 , F21Y2115/10
摘要： An illumination system for an aircraft interior has an illumination source. An optical module is coupled to the illumination source. The optical module collects the light emissions from the light source and distributes the collected light over a desired area with a specified intensity profile.
摘要翻译：用于飞机内部的照明系统具有照明源。光学模块耦合到照明源。光学模块收集来自光源的光发射，并将所收集的光以特定的强度分布分布在期望的区域上。

8. 发明申请

US20150252951A1 METHOD FOR PRODUCING AN ESCAPE ROUTE MARKING FOR AIRPLANES, AND SAID ESCAPE ROUTE MARKING 有权
标题翻译：生产航空公司ESCAPE路线标记的方法，并规定ESCAPE路线标记
公开(公告)号：US20150252951A1
公开(公告)日：2015-09-10
申请号：US14421559
申请日：2013-08-14
申请人： Lufthansa Technik AG
发明人： Torben Biehl , Hans-Christian Lierow
IPC分类号： F21K2/00 , B29C51/12 , B29C51/30 , B29C51/00
CPC分类号： F21K2/00 , B29C51/002 , B29C51/12 , B29C51/30 , B29K2069/00 , B29K2883/005 , B29K2995/0035 , B29L2009/00 , B29L2031/772 , B60Q3/46 , B60Q3/78 , C09D5/22 , F21W2107/30 , F21W2111/00
摘要： A method for producing an escape route marking in a heatable and malleable support mold is described. The escape route marking has a transparent covering, a supporting element and a photoluminescent material. The method includes procuring the heatable and malleable support mold, inserting a supporting element into the support mold, arranging the photoluminescent material on the supporting element, arranging the transparent covering on the supporting element, heating and deforming the escape route marking in the support mold and solidifying the escape route marking in the support mold in a predetermined position. The resulting escape route marking is also described.
摘要翻译：描述了一种用于在可加热和可延展的支撑模具中生产逃生路线标记的方法。逃生路线标记具有透明覆盖物，支撑元件和光致发光材料。该方法包括采购可加热和可延展的支撑模具，将支撑元件插入支撑模具中，将光致发光材料布置在支撑元件上，将透明覆盖物布置在支撑元件上，加热和变形支撑模具中的逃生路线标记，将支撑模具中的逃生路线标记固化在预定位置。还描述了所得到的逃生路线标记。

9. 发明申请

US20150232168A1 CEILING TRIM ELEMENT FOR AN INTERIOR TRIM ARRANGEMENT OF AN AIRCRAFT CABIN 审中-公开
标题翻译：航空客舱内部装配的天花板元件
公开(公告)号：US20150232168A1
公开(公告)日：2015-08-20
申请号：US14619723
申请日：2015-02-11
申请人： Airbus Operations GmbH
发明人： Benedikt Kircher , Paul Edwards
IPC分类号： B64C1/06 , B64D11/00 , F21V3/04 , B64D47/02
CPC分类号： B64C1/066 , B64D11/00 , B64D47/02 , B64D2011/0038 , F21V3/049 , F21W2107/30
摘要： A ceiling trim element for a passenger cabin of a vehicle, in particular for an aircraft cabin of an aircraft which has a planar panel element with a front side and a rear side, wherein the front side is provided to point towards the interior of the passenger cabin, and the rear side is provided to point away from the interior of the passenger cabin, wherein an image surface is provided in the panel element, wherein the image surface is assigned a varying pattern generator in order to illuminate the image surface with varying patterns, and having an illuminating ring generator to generate an illuminating ring which surrounds the image surface.
摘要翻译：一种用于车辆客舱的天花板装饰元件，特别是用于具有前侧和后侧的平面面板元件的飞机的飞机机舱，其中前侧设置成指向乘客的内部并且后侧被设置为指向远离客舱的内部，其中在面板元件中设置图像表面，其中图像表面被分配有变化的图案发生器以便以变化的图案照亮图像表面并且具有照明环发生器以产生围绕图像表面的照明环。

10. 发明授权

US08579479B2 Warning lamp for an aircraft 有权
标题翻译：飞机警示灯
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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