公开(公告)号：US09989234B2

公开(公告)日：2018-06-05

申请号：US15080723

申请日：2016-03-25

申请人： Goodrich Lighting Systems GmbH

发明人： Robert Trinschek ,  Elmar Schrewe ,  Tomasz Kordecki

IPC分类号： F21V29/00 ,  F21V29/10 ,  H05K1/02 ,  F21V29/70 ,  F21V29/89 ,  B64D11/00 ,  F21V23/00 ,  F21V23/02 ,  F21W101/06 ,  F21Y103/10 ,  F21Y115/10 ,  F21Y101/02

CPC分类号： F21V29/10 ,  B64D11/00 ,  B64D2011/0038 ,  B64D2203/00 ,  F21V23/005 ,  F21V23/02 ,  F21V29/70 ,  F21V29/89 ,  F21W2107/30 ,  F21Y2101/00 ,  F21Y2103/10 ,  F21Y2115/10 ,  H05K1/0209 ,  H05K2201/09781 ,  H05K2201/10106

摘要： An interior aircraft LED light unit includes at least one printed circuit board, on which a plurality of LEDs are connected to a power source, each one of the plurality of LEDs having a predetermined distance to the power source, and each one of the plurality of LEDs being associated with a respective thermal transfer member having a predetermined size, for transferring heat away from the respective LED, wherein, for at least some of the plurality of LEDs the predetermined size of the respective thermal transfer member varies with the predetermined distance of the LED to the power source.

公开(公告)号：US09771168B2

公开(公告)日：2017-09-26

申请号：US14707207

申请日：2015-05-08

申请人： GOODRICH LIGHTING SYSTEMS GMBH

发明人： Andre Hessling

IPC分类号： B64D47/02 ,  B64F1/20 ,  F21V1/20 ,  F21V21/00 ,  B64D47/06 ,  B62D47/02 ,  F21V29/02 ,  F21V29/60 ,  F21V29/71 ,  F21W101/06 ,  F21Y115/10

CPC分类号： B64D47/06 ,  B62D47/02 ,  B64D2203/00 ,  F21V29/60 ,  F21V29/713 ,  F21W2107/30 ,  F21Y2115/10

摘要： An aircraft light comprises a housing, at least one light source to be cooled, the at least one light source being arranged in the housing, a heat sink element thermally coupled to the at least one light source and defining a cooling surface exposable to a cooling airstream for the cooling airstream to flow along the cooling surface in a flow direction. The cooling surface extends between upstream and downstream end portions spaced apart in the flow direction and means for generating a pressure difference between the upstream and downstream end portions of the cooling surface. Due to the pressure difference, a cooling airstream flowing along the cooling surface is created.

公开(公告)号：US09227564B2

公开(公告)日：2016-01-05

申请号：US14640419

申请日：2015-03-06

申请人： IDD Aerospace Corporation

发明人： Birger Timm ,  Volker Antonczyk ,  Henrik Heine

IPC分类号： H05B37/02 ,  B60Q3/02 ,  B64D11/00 ,  F21K99/00 ,  H05B33/08 ,  B64D47/02 ,  F21Y101/02 ,  F21W101/06

CPC分类号： H05B33/0824 ,  B60Q3/43 ,  B60Q3/44 ,  B60Q3/47 ,  B60Q3/64 ,  B64D11/00 ,  B64D2011/0038 ,  B64D2203/00 ,  F21K9/20 ,  F21Y2115/10 ,  H05B33/0845 ,  H05B33/086 ,  Y02T50/46

摘要： The invention relates to a LED strip lighting device for a cabin of a passenger aircraft, the device comprising at least one LED strip, comprising a plurality of N independently controllable LED segments (S), wherein each LED segment (S) comprises at least four LED selected from red, green, blue, ice blue, warm white and cold white or another type of LED; a plurality of M driver units, wherein each LED section (S) is connected to a driver unit for providing a control signal to the respective LED section (S); and a bus system connecting all M driver units. The device further comprises a micro controller connected to the bus system for providing control signals for each driver unit, such that each LED segment (S) emits light in intensity and color according to a predetermined illumination pattern.

摘要翻译： 本发明涉及一种用于客机的舱室的LED条照明装置，该装置包括至少一个LED条，其包括多个N个可独立控制的LED段（S），其中每个LED段（S）包括至少四个 LED从红色，绿色，蓝色，冰蓝色，暖白色和冷白色或另一种类型的LED选择; 多个M个驱动器单元，其中每个LED部分（S）连接到驱动器单元，用于向相应的LED部分（S）提供控制信号; 以及连接所有M个驱动单元的总线系统。 该装置还包括连接到总线系统的微控制器，用于为每个驱动器单元提供控制信号，使得每个LED段（S）根据预定的照明模式发射强度和颜色的光。

公开(公告)号：US10040575B2

公开(公告)日：2018-08-07

申请号：US15211164

申请日：2016-07-15

申请人： Goodrich Lighting Systems, Inc.

发明人： David Franich ,  Philippe Lapujade

IPC分类号： B64D47/06 ,  F21V11/16 ,  F21V7/00 ,  F21Y115/10 ,  F21W101/06 ,  F21W107/30

摘要： A dual mode light assembly for a forward position light of an aircraft includes a base, a visible light source mounted to the base that is configured to emit visible light, a covert light source mounted to the base that is configured to emit covert light, and a light shield mounted to the base. The light shield is configured to restrict transmission of the visible light to a visible light pattern and to restrict transmission of the covert light to a covert light pattern.

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.

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。

公开(公告)号：US09851076B2

公开(公告)日：2017-12-26

申请号：US14739365

申请日：2015-06-15

申请人： PANASONIC INTELLECTUAL PROPERTY MANAGEMENT CO., LTD.

发明人： Itaru Onishi ,  Osamu Tanahashi

IPC分类号： F21V19/00 ,  F21V17/00 ,  F21V21/00 ,  F21V23/00 ,  B60Q3/43 ,  B60Q3/74 ,  F21W101/06 ,  F21Y105/00 ,  F21Y115/20

CPC分类号： F21V19/00 ,  B60Q3/43 ,  B60Q3/745 ,  F21W2107/30 ,  F21Y2105/00 ,  F21Y2115/20

摘要： A light-emitting device includes: a holder having an elongate shape and flexibility; and a flat light-emitting element held by the holder and having a rectangular shape and flexibility. The holder includes a frame portion extending in a longitudinal direction of the holder, and a holding part protruding from the frame portion in a plan view. The frame portion of the holder and the flat light-emitting element overlap in a lateral-view direction, and the flat light-emitting element is joined to and held by the holding part.

公开(公告)号：US09365156B2

公开(公告)日：2016-06-14

申请号：US14450429

申请日：2014-08-04

申请人： DIEHL AEROSPACE GmbH

发明人： Martin Bachhuber ,  Frank Schmid

IPC分类号： B60Q3/02 ,  B60Q3/00 ,  B64D11/00 ,  F21W101/02 ,  F21W101/04 ,  F21W101/06 ,  F21W101/08

CPC分类号： B64D11/00 ,  B60Q3/44 ,  B60Q3/46 ,  B60Q3/64 ,  B60Q3/76 ,  B64D2011/0053 ,  F21W2106/00 ,  F21W2107/10 ,  F21W2107/20 ,  F21W2107/30

摘要： A lighting apparatus, in particular a reading lamp, is provided. The apparatus can be recessed in a trim of a passenger cab of a vehicle, which can be a land vehicle, an aircraft, or a watercraft. The apparatus has a first light-emitting device that is pivotably mounted to a recess-mounting frame, so that a light-emitting direction of the first light-emitting device with respect to the recess-mounting frame is changeable. To simplify the design of the apparatus, a second light-emitting device is mounted to a visible side of the recess-mounting frame. The second light-emitting device at least partially surrounds the first light-emitting device and is fitted to the recess-mounting frame, so that the light-emitting direction of the second light-emitting device is invariable.

摘要翻译： 提供照明装置，特别是阅读灯。 该装置可以嵌入车辆的乘客驾驶室的装饰物中，车辆的乘客驾驶室可以是陆上车辆，飞行器或船只。 该装置具有可枢转地安装到凹部安装框架的第一发光装置，使得第一发光装置相对于凹部安装框架的发光方向是可变的。 为了简化设备的设计，将第二发光装置安装到凹部安装框架的可见侧。 第二发光装置至少部分地围绕第一发光装置，并且嵌合到凹部安装框架，使得第二发光装置的发光方向是不变的。

公开(公告)号：US09261258B2

公开(公告)日：2016-02-16

申请号：US13366520

申请日：2012-02-06

申请人： Storm S. Sears

发明人： Storm S. Sears

IPC分类号： F21V21/00 ,  F21V7/00 ,  B60Q3/02 ,  F21S4/00 ,  B64C27/82 ,  B64D11/00 ,  F21W101/06 ,  F21W101/08 ,  F21Y101/02 ,  F21Y103/00 ,  F21Y113/00

CPC分类号： F21V7/0008 ,  B60Q3/43 ,  B64C2027/8236 ,  B64D11/00 ,  B64D2011/0038 ,  B64D2203/00 ,  F21S4/28 ,  F21V7/005 ,  F21V29/507 ,  F21W2106/00 ,  F21W2107/30 ,  F21Y2103/10 ,  F21Y2113/13 ,  F21Y2115/10

摘要： A light emitting diode (LED) luminaire that produces a uniform light pattern at close distances is provided. The LED luminaire includes a housing, a printed circuit board assembly thermally coupled to the housing, a plurality of high brightness (HB) LED emitters, thermally coupled to the printed circuit board assembly to form a linear array, and a linear reflector assembly, attached to the housing, to concentrate the light generated by the LED emitters over a beam angle formed by the upper surface of the housing and the linear reflector assembly.

摘要翻译： 提供了在近距离产生均匀的光图案的发光二极管（LED）照明器。 LED灯具包括壳体，热耦合到壳体的印刷电路板组件，多个高亮度（HB）LED发射器，其热耦合到印刷电路板组件以形成线性阵列，以及附接的线性反射器组件 以将由LED发射器产生的光集中在由壳体的上表面和线性反射器组件形成的光束角上。

公开(公告)号：US09951917B2

公开(公告)日：2018-04-24

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： G09F13/04 ,  F21S9/02 ,  B64C27/04 ,  B64D11/00 ,  B64D41/00 ,  B64D47/02 ,  F21V7/00 ,  F21V23/04 ,  H05B33/08 ,  H02J9/06 ,  F21W101/06 ,  F21W101/08

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.