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1. 发明申请

WO2011144236A1 LIGHT FOR THE INTERIOR OF AN AIRCRAFT 审中-公开
标题翻译：飞机内部的光
公开(公告)号：WO2011144236A1
公开(公告)日：2011-11-24
申请号：PCT/EP2010/056741
申请日：2010-05-17
申请人： GOODRICH LIGHTING SYSTEMS GMBH , BRÖLEMANN, Rolf
发明人： BRÖLEMANN, Rolf
IPC分类号： F21K99/00 , B60Q3/00 , B63B45/00 , B64D11/00 , H01L33/48
CPC分类号： B60Q3/43 , B64D11/00 , B64D2011/0038 , F21K9/00
摘要： The present invention provides a light for the interior of an aircraft, in particular wash light for an aircraft, comprising a first group of white LEDs (18) each having an InGaN semiconductor material chip, and a second group of amber colored LEDs (20) each having an InGaN semiconductor material chip.
摘要翻译：本发明提供一种用于飞行器内部的光，特别是用于飞行器的洗涤光，其包括每组具有InGaN半导体材料芯片的第一组白色LED（18）和第二组琥珀色LED（20）每个都具有InGaN半导体材料芯片。

2. 发明申请

WO2009156349A1 WARNING LAMP FOR AN AIRCRAFT 审中-公开
标题翻译：警告用于飞机的灯
公开(公告)号：WO2009156349A1
公开(公告)日：2009-12-30
申请号：PCT/EP2009/057675
申请日：2009-06-19
申请人： GOODRICH LIGHTING SYSTEMS GMBH , AIRBUS DEUTSCHLAND GMBH , KOHLMEIER-BECKMANN, Carsten , GRIESBACH, Martin , MÜLLER, Bernhard , FERLING, Sonja , HESSLING, Andre , LÜDER, Sascha
发明人： KOHLMEIER-BECKMANN, Carsten , GRIESBACH, Martin , MÜLLER, Bernhard , FERLING, Sonja , HESSLING, Andre , LÜDER, Sascha
IPC分类号： B64D47/06
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 materia!. 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正面覆盖元件（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）。

3. 发明申请

WO2008125672A1 FARBVERSTELLBARE LED-LEUCHTE, INSBESONDERE ZUR FAHRZEUGINNENBELEUCHTUNG 审中-公开
标题翻译：灰度可调LED灯，尤其是室内照明
公开(公告)号：WO2008125672A1
公开(公告)日：2008-10-23
申请号：PCT/EP2008/054550
申请日：2008-04-15
申请人： GOODRICH LIGHTING SYSTEMS GMBH , HESSLING, Andre
发明人： HESSLING, Andre
IPC分类号： F21K7/00 , B60Q3/02 , B60Q3/00 , F21W101/08 , H01L33/00 , H05B33/08
CPC分类号： H05B33/086 , B60Q3/44 , B60Q3/47 , B60Q3/68 , F21K9/00 , F21W2106/00 , H01L25/0753 , H01L2924/0002 , H01L2924/00
摘要： Die LED-Leuchte, insbesondere Lese- bzw. Sitzplatzleuchte für Fahrzeuge wie Reisebusse oder Flugzeuge ist mit einem Gehäuse (36), mehreren LEDs, die erste LEDs ( 16) umfassen, welche elektromagnetische Strahlung in einem ersten Wellenlängenbereich aussenden, und einer Ansteuereinheit (12) zum Ansteuern der ersten LEDs (16) versehen. Ferner weist 'die LED-Leuchte ein Konversionsmaterial (24) auf, das bei Anregung durch zumindest einen Teil der elektromagnetischen Strahlung der ersten LEDs (1.6) elektromagnetische Strahlung in einem Konversionswelleniängenbereich aussendet, der im sichtbaren Bereich des Spektrums Siegt und zumindest teilweise verschieden ist von dem ersten Wellenlängenbereich versehen. Die LEDs umfassen ferner zumindest zweite LEDs (18), die zur Farbverschiebung der von dem Konversiopismaterial (24) bei Anregung durch die ersten LEDs (16) ausgesandten elektromagnetischen Strahlung eine elektromagnetische Strahlung in einem zweiten Wellenlängenbereich aussenden. Die zweiten LEDs (18) sind von der Ansteuereinheit (12) wahlweise zusätzlich zu den ersten LEDs (16) ansteuerbar, wobei die elektromagnetische Strahlung der zweiten LEDs (18) zumindest teilweise im sichtbaren Bereich des Spektrums liegt sowie zumindest teilweise verschieden ist von dem Wellenlängenbereich der ersten LEDs (16) und das Konversionsmaterial (24) im wesentlichen ohne Anregung derselben passiert und/oder wobei die elektromagnetische Strahlung der zweiten LEDs (18) das Konversionsmaterial (24) zusätzlich anregt, elektromagnetische Strahlung, deren Wellenlängenbereich innerhalb oder ausserhalb des Konversionswellenlängenbereichs liegt, auszusenden.
摘要翻译： LED灯，特别是读出用或车辆如公共汽车或飞机座椅的光被设置有外壳（36），多个发光二极管，所述第一发光二极管（16）包括在第一波长范围内什么发射电磁辐射，以及控制单元（12 ）（用于驱动第一发光二极管16）被提供。此外，“包括LED灯，其发射转换材料（24），当由所述第一发光二极管的电磁辐射（1.6）的电磁辐射在Konversionswelleniängenbereich，这是在光谱Siegt的可见区域的至少一个部分和至少部分地不同的激发设置在第一波长范围内。所述LED还包括在从所述Konversiopismaterial（24）当由所发射的第一LED激发（16）的电磁辐射发射电磁辐射中的第二波长范围至少第二LED（18），用于色移。所述驱动单元（12），无论是在除了第一发光二极管（16）的第二LED（18）可以被控制，其中所述第二LED的电磁辐射（18）位于至少部分地在光谱的可见区域，并且至少部分地从所述波长范围内的不同第一发光二极管（16）和所述转换材料（24）基本上没有激励同样的情况，和/或第二LED的电磁辐射（18）转换材料（24）进一步刺激，电磁辐射，其波长范围位于内部或外部的转换波长区域的送出去。

4. 发明授权

US12091190B2 Aircraft passenger service unit 有权
公开(公告)号：US12091190B2
公开(公告)日：2024-09-17
申请号：US17703062
申请日：2022-03-24
申请人： Goodrich Lighting Systems Gmbh & Co. KG
发明人： Anil Kumar Jha , Jens Leuschner , Carsten Pawliczek
IPC分类号： B64D45/00 , A62B7/14 , B64D11/06
CPC分类号： B64D45/00 , A62B7/14 , B64D11/06
摘要： An aircraft passenger service unit includes infrared sensor configured for detecting infrared radiation and for providing a corresponding sensor output, and a controller, which is configured for receiving and evaluating the sensor output provided by the infrared sensor. The infrared sensor is an infrared sensor array configured for detecting infrared radiation emitted within a plurality of spatial sectors covering a detection area below the aircraft passenger service unit; and the infrared sensor array is configured for detecting the infrared radiation individually for each spatial sector and for providing individual sensor signals for the plurality of spatial sectors. The infrared sensor array is configured such that each passenger seat arranged within the detection area is covered by at least two of the plurality of spatial sectors, respectively; and the controller is configured for determining a passenger seating position within a passenger seat from the individual sensor signals.

5. 发明授权

US12078326B2 Aircraft light with support board and kinematic coupling fixture and aircraft comprising the same 有权
公开(公告)号：US12078326B2
公开(公告)日：2024-09-03
申请号：US18167465
申请日：2023-02-10
申请人： Goodrich Lighting Systems GmbH & Co. KG
发明人： Thomas Ebbers , Lars Christian Schröder , Markus Katzenmayer
IPC分类号： F21V21/14 , B64D11/00 , B64D47/04
CPC分类号： F21V21/14 , B64D11/00 , B64D47/04 , B64D2011/0038 , B64D2011/0053 , B64D2203/00
摘要： An aircraft light includes a support board; a light source, arranged on the support board; an optical element, arranged over the light source; and a kinematic coupling fixture, establishing a fixed position of the optical element with respect to the support board.

6. 发明授权

US12072078B2 Protective cover for a fuselage-mounted exterior aircraft light and exterior aircraft light 有权
公开(公告)号：US12072078B2
公开(公告)日：2024-08-27
申请号：US18452001
申请日：2023-08-18
申请人： Goodrich Lighting Systems GmbH & Co. KG
发明人： Anil Kumar Jha , Andre Hessling-von Heimendahl , Christian Schön , Christo Tsibadze
IPC分类号： F21V15/01 , B64D47/06
CPC分类号： F21V15/01 , B64D47/06
摘要： A protective cover for a fuselage-mounted exterior aircraft light includes a fuselage-facing mounting side for mounting the protective cover to an exterior aircraft light housing or to an exterior skin of an aircraft; a light transmissive forward facing light emission surface; and an air deflection zone, which is shaped to direct a portion of an impinging air stream (A) along and over the forward facing light emission surface for shielding the forward facing light emission surface from the impinging air stream (A).

7. 发明授权

US12054284B2 Exterior aircraft light, aircraft comprising an exterior aircraft light, and method for providing an extent of erosion of an exterior surface of a light transmissive cover of an exterior aircraft light 有权
公开(公告)号：US12054284B2
公开(公告)日：2024-08-06
申请号：US18450758
申请日：2023-08-16
申请人： Goodrich Lighting Systems GmbH & Co. KG
发明人： Andre Hessling-Von Heimendahl , Marion Depta
IPC分类号： B64D47/02 , B64D45/00 , G01N21/958
CPC分类号： B64D47/02 , G01N21/958 , B64D2045/0085
摘要： An exterior aircraft light includes a support and a light transmissive cover having a light transmissive body with an interior surface and an exterior surface. The light includes at least one light source arranged between the support and the light transmissive cover; and a first light detector. The light transmissive cover has a first light guide path within the light transmissive body from a first light entry region to a first light exit region, wherein the first light detector is arranged to receive light that travels along the first light guide path and that exits the light transmissive cover at the first light exit region. The first light detector is configured to provide sensor measurements corresponding to the amount of light incident on the first light detector.

8. 发明授权

US12050185B2 Exterior aircraft light with cover erosion monitoring, aircraft comprising such exterior aircraft light, and method of monitoring erosion of a light transmissive cover 有权
公开(公告)号：US12050185B2
公开(公告)日：2024-07-30
申请号：US18545951
申请日：2023-12-19
申请人： Goodrich Lighting Systems GmbH & Co. KG
发明人： Anil Kumar Jha , Jens Leuschner , Andre Hessling von Heimendahl , Marion Depta
IPC分类号： B64D47/06 , F21S43/20 , F21W107/30 , G01N21/958
CPC分类号： G01N21/958 , B64D47/06 , F21S43/26 , F21W2107/30
摘要： An exterior aircraft light with cover erosion monitoring, the exterior aircraft light comprises: a support; at least one light source, arranged on the support; a light transmissive cover, arranged over the at least one light source, the light transmissive cover having a forward facing portion and a rear-ward facing portion; a first light sensor, arranged to receive light emitted by the at least one light source and reflected towards the first light sensor by the forward facing portion of the light transmissive cover; and a second light sensor, arranged to receive light emitted by the at least one light source and reflected towards the second light sensor by the rearward facing portion of the light transmissive cover.

9. 发明公开

US20240149788A1 LIGHT MODULE FOR AN ELONGATED INTERIOR AIRCRAFT LIGHT, ELONGATED INTERIOR AIRCRAFT LIGHT, AIRCRAFT, AND METHOD OF INSTALLING AN ELONGATED INTERIOR AIRCRAFT LIGHT IN AN AIRCRAFT 审中-公开
公开(公告)号：US20240149788A1
公开(公告)日：2024-05-09
申请号：US18495205
申请日：2023-10-26
申请人： Goodrich Lighting Systems GmbH & Co. KG
发明人： Carsten PAWLICZEK
IPC分类号： B60Q3/43 , B60Q3/64 , B60Q3/74 , F21V7/00
CPC分类号： B60Q3/43 , B60Q3/64 , B60Q3/74 , F21V7/0066 , B60Q2800/30 , F21Y2115/10
摘要： A light module for an elongated interior aircraft light includes: a plurality of light sources, forming an array of light sources that extends between a first lateral end portion of the light module and a second lateral end portion of the light module; and an elongated light transmissive cover that is arranged over the array of light sources, wherein the elongated light transmissive cover allows a forward light output portion, emitted by the plurality of light sources towards the elongated light transmissive cover, to pass through; wherein, at at least one of the first lateral end portion and the second lateral end portion, a light output boosting lateral end cap is provided, wherein the light output boosting lateral end cap is shaped to mesh with a neighboring lateral end cap of a neighboring light module.

10. 发明授权

US11945589B2 Passenger seat canopy 有权
公开(公告)号：US11945589B2
公开(公告)日：2024-04-02
申请号：US16713563
申请日：2019-12-13
申请人： Goodrich Lighting Systems GmbH
发明人： Martin Klaus , Andre Hessling-Von Heimendahl , Robert Schulten
IPC分类号： B64D11/06 , B64D11/00
CPC分类号： B64D11/0606 , B64D11/0626 , B64D2011/0053
摘要： A canopy is configured to be mounted to a passenger seat of a passenger transport vehicle, in particular an aircraft. The canopy is foldable between a retracted storage configuration and an extended operational configuration. In the operational configuration, the canopy forms a hood establishing a passenger's personal space below the canopy. The canopy comprises at least one functional device which is configured for modifying a physical characteristics of the personal space. The at least one functional device in particular includes at least one of a lighting device configured for lighting the personal space and a venting device configured for venting the personal space.

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