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    Aircraft LED Light Unit
    61.
    发明申请
    Aircraft LED Light Unit 审中-公开
    飞机LED灯单元

    公开(公告)号：US20170015435A1

    公开(公告)日：2017-01-19

    申请号：US15209895

    申请日：2016-07-14

    Applicant: Goodrich Lighting Systems GmbH

    Inventor： Anil Kumar Jha ,  Norbert Menne ,  Elmar Schrewe ,  Robert Trinschek ,  Andre Hessling-von Heimendahl

    IPC: B64D47/02 ,  F21V23/04 ,  H05K1/18

    CPC classification number: B64D47/02 ,  F21V23/04 ,  H05K1/053 ,  H05K1/056 ,  H05K1/181 ,  H05K3/3431 ,  H05K2201/10106 ,  H05K2201/10484 ,  Y02P70/611

    Abstract: An aircraft LED light unit comprises at least one printed circuit board which comprises at least one metal core layer and at least one dielectric layer, and at least one LED disposed on the printed circuit board and which comprises an anode and a cathode for electrically coupling to a power source. One of the anode and cathode of the at least one LED is connected to an electrical conductor which is disposed on the dielectric layer and is coupled to a first terminal of the power source, wherein the dielectric layer electrically isolates the electrical conductor from the metal core layer, and the other one of the anode and cathode of the at least one LED is connected to the metal core layer of the at least one printed circuit board, wherein the metal core layer is coupled to a second terminal of the power source.

    Abstract translation: 飞机LED灯单元包括至少一个包括至少一个金属芯层和至少一个介电层的印刷电路板，以及布置在印刷电路板上的至少一个LED，并且包括用于电耦合到 电源。 至少一个LED的阳极和阴极之一连接到电导体，电导体设置在电介质层上并且耦合到电源的第一端子，其中电介质层将电导体与金属芯电隔离 层，并且所述至少一个LED的阳极和阴极中的另一个连接到所述至少一个印刷电路板的金属芯层，其中所述金属芯层耦合到所述电源的第二端子。

    DYNAMIC EXTERIOR AIRCRAFT LIGHT UNIT AND METHOD OF OPERATING A DYNAMIC EXTERIOR AIRCRAFT LIGHT UNIT
    62.
    发明申请
    DYNAMIC EXTERIOR AIRCRAFT LIGHT UNIT AND METHOD OF OPERATING A DYNAMIC EXTERIOR AIRCRAFT LIGHT UNIT 有权
    动态外部飞机灯光单元及动态外部飞机灯光单元的操作方法

    公开(公告)号：US20160345408A1

    公开(公告)日：2016-11-24

    申请号：US15158911

    申请日：2016-05-19

    Applicant: Goodrich Lighting Systems GmbH

    Inventor： Christian Schoen ,  Andre Hessling-Von Heimendahl ,  Anil Kumar Jha

    IPC: H05B37/02 ,  G01S17/02 ,  B64D47/04 ,  G01S17/42 ,  H05B33/08 ,  B64D47/06

    CPC classification number: H05B37/0227 ,  B64D47/04 ,  B64D47/06 ,  G01S17/026 ,  G01S17/42 ,  H05B33/0854

    Abstract: A dynamic exterior aircraft light unit includes a plurality of LEDs, with at least two subsets of the plurality of LEDs being separately, an optical system for transforming light output from the plurality of LEDs into at least two light emission distributions, a control unit for controlling the plurality of LEDs, and a photo detector arranged to detect light, emitted by the dynamic exterior aircraft light unit as part of the at least two light emission distributions and reflected by the aircraft environment, and configured to output a light detection signal.

    Abstract translation: 动态外部飞机灯单元包括多个LED，其中多个LED中的至少两个子集是分开的，用于将从多个LED输出的光变换为至少两个发光分布的光学系统，用于控制的控制单元 所述多个LED和光检测器被布置成检测由所述动态外部飞行器光单元发射的光，作为所述至少两个发光分布的一部分并被所述飞行器环境反射，并被配置为输出光检测信号。

    AIRCRAFT LANDING LIGHT UNIT, EXTERIOR AIRCRAFT LIGHTING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT LANDING LIGHT UNIT
    63.
    发明申请
    AIRCRAFT LANDING LIGHT UNIT, EXTERIOR AIRCRAFT LIGHTING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT LANDING LIGHT UNIT 有权
    飞机着陆灯，外部飞机照明系统及操作飞机着陆灯的方法

    公开(公告)号：US20160345401A1

    公开(公告)日：2016-11-24

    申请号：US15158874

    申请日：2016-05-19

    Applicant: Goodrich Lighting Systems GmbH

    Inventor： Andre Hessling-Von Heimendahl ,  Christian Schoen ,  Anil Kumar Jha

    IPC: H05B33/08 ,  H05B37/02 ,  F21V5/04 ,  B64D47/04 ,  B64D47/06

    CPC classification number: H05B33/0854 ,  B60Q1/1423 ,  B64D47/04 ,  B64D47/06 ,  B64D2203/00 ,  F21V5/04 ,  F21Y2101/00 ,  H05B37/0218 ,  Y02B20/46

    Abstract: An aircraft landing light unit includes a plurality of LEDs, an optical system associated with the plurality of LEDs for shaping a light output of the aircraft landing light unit for illuminating an aircraft environment, a control unit for controlling the plurality of LEDs, and a photo detector arranged for detecting light, emitted by the plurality of LEDs, output via the optical system and reflected by atmospheric haze, such as clouds, fog, rain and snow, wherein the control unit is coupled to the photo detector and is configured to control the plurality of LEDs on the basis of the light detected by the photo detector, thereby adjusting the light output of the aircraft landing light unit to the atmospheric haze.

    Abstract translation: 飞机着陆灯单元包括多个LED，与多个LED相关联的光学系统，用于对用于照射飞行器环境的飞机着陆灯单元的光输出进行整形，用于控制多个LED的控制单元和照片 检测器，被布置成用于检测由多个LED发射的光，经由光学系统输出并被诸如云，雾，雨和雪的大气雾度反射，其中控制单元耦合到光电检测器，并且被配置为控制 基于由光检测器检测的光的多个LED，从而将飞机着陆灯单元的光输出调节到大气雾度。

    AEROSPACE GROUND MANEUVER LIGHT
    64.
    发明申请
    AEROSPACE GROUND MANEUVER LIGHT 有权
    航空地面漫游灯

    公开(公告)号：US20130314256A1

    公开(公告)日：2013-11-28

    申请号：US13901754

    申请日：2013-05-24

    Applicant: Goodrich Lighting Systems GmbH

    Inventor： Andre Hessling ,  Alexander Wernicke ,  Anil Kumar Jha ,  Christian Schoen

    IPC: B64F1/00 ,  F21K99/00 ,  B64F1/18

    CPC classification number: F21V29/60 ,  B60Q1/2696 ,  B64D2203/00 ,  B64F1/002 ,  B64F1/18 ,  B64F1/205 ,  F21K9/60 ,  F21V3/061 ,  F21V3/062 ,  F21V7/0008 ,  F21V7/0025 ,  F21V7/048 ,  F21V7/09 ,  F21V29/54 ,  F21V29/70 ,  F21W2111/06 ,  F21Y2115/10 ,  G08B5/36

    Abstract: Aerospace ground maneuver light, comprises a reflector (14), the reflector (14) defining a light exit plane (18), an LED light source (26) arranged outside of the area defined by the reflector (14) and its light exit plane (18), and a mounting bar (22) which has a longitudinal extension and at which the LED light source (26) is mounted. The mounting bar (22) extends across the reflector (14) and is spaced apart from the light exit plane (18) of the reflector (14) and comprises a mounting side (24) facing towards the reflector (14) and its light exit plane (18), with the LED light source (26) arranged on the mounting side (24) for emitting light towards the reflector (14).

    Abstract translation: 航空地面机动灯包括反射器（14），反射器（14）限定光出射平面（18），布置在由反射器（14）限定的区域的外部的LED光源（26）和其光出射平面 （18），以及安装杆（22），其具有纵向延伸并且安装有所述LED光源（26）。 安装杆（22）延伸穿过反射器（14）并且与反射器（14）的光出射平面（18）间隔开并且包括面向反射器（14）的安装侧（24）和其光出口 平面（18），其中LED光源（26）布置在安装侧（24）上，用于向反射器（14）发射光。

    Aircraft navigation light and aircraft comprising the same
    68.
    发明授权
    Aircraft navigation light and aircraft comprising the same 有权

    公开(公告)号：US11891190B2

    公开(公告)日：2024-02-06

    申请号：US18164427

    申请日：2023-02-03

    Applicant: Goodrich Lighting Systems GmbH & Co. KG

    Inventor： Marion Depta ,  Anil Kumar Jha

    IPC: B64D47/06 ,  B60Q1/26

    CPC classification number: B64D47/06 ,  B60Q1/2607

    Abstract: An aircraft navigation light, configured to be usable as any of a left forward navigation light, a right forward navigation light, and a tail navigation light of an aircraft, comprises a common support plate which is substantially vertical in the aircraft frame of reference; a first light source arranged on the common support plate for emitting red light; a second light source arranged on the common support plate for emitting green light; a third light source arranged on the common support plate for emitting white light; a driving circuit coupled to the first light source, the second light source and the third light source and configured to supply power to a selected one of the first light source, the second light source, and the third light source; and a blocking element arranged to limit the light output of the aircraft navigation light to one lateral side.

    Aircraft passenger reading light
    70.
    发明授权
    Aircraft passenger reading light 有权

    公开(公告)号：US11305689B2

    公开(公告)日：2022-04-19

    申请号：US17077297

    申请日：2020-10-22

    Applicant: Goodrich Lighting Systems GmbH

    Inventor： Anil Kumar Jha ,  Jens Leuschner

    IPC: B60Q3/44 ,  B60Q3/76 ,  B60Q3/47 ,  B60Q3/82 ,  B64D11/00 ,  B64D11/06

    Abstract: An aircraft passenger reading light include comprises: a light source arrangement having a plurality of rows of reading light sources, with each of the rows having a plurality of reading light sources for passenger-specific illumination of a plurality of seats of a seating row of an aircraft and with the plurality of rows having different illumination directions in a longitudinal direction (L) of the aircraft, whereinach of the light sources first and second electrical terminals; first and second power supply connectors; and a multi-state switching arrangement having a plurality of switching states. The first power supply connector is coupled to the first electrical terminals of the plurality of reading light sources. The second power supply connector is coupled to the second electrical terminals of the plurality of reading light sources via the multi-state switching arrangement.

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