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公开(公告)号：US10974847B2
公开(公告)日：2021-04-13
申请号：US16712396
申请日：2019-12-12
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling-von Heimendahl , Anil Kumar Jha , Frank Klein
IPC: B64D47/06 , F21S4/28 , F21S10/06 , F21Y103/33
Abstract: An aircraft beacon light for being mounted to an aircraft fuselage includes: a support structure, having a carrier, and a stem for supporting the carrier and for spacing the carrier from the aircraft fuselage; and a lighting system, supported by the support structure, the lighting system having a plurality of light sources, light optics for redirecting at least a portion of the light emitted by the plurality of light sources, and a lens cover, with the plurality of light sources and the light optics being arranged between the carrier and the lens cover; wherein the aircraft beacon light is configured to emit a red-flashing beacon light output in operation.
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公开(公告)号：US10299343B2
公开(公告)日：2019-05-21
申请号：US15705517
申请日：2017-09-15
Applicant: Goodrich Lighting Systems GmbH
Inventor： Frank Klein , Andre Hessling-Von Heimendahl , Robert Trinschek
Abstract: An exterior aircraft light unit includes a power input coupleable to an aircraft on-board power supply; at least one LED coupled to the power input for receiving power from the aircraft on-board power supply and configured to emit a light output; an optical sensor arranged for sensing an intensity detection portion of the light output and configured to output a detection signal indicative of an intensity level of the light output; an end of life detector, coupled to the optical sensor for receiving the detection signal and configured to determine an end of life condition; and a fuse circuit coupled to the end of life detector; wherein the fuse circuit is configured to irreversibly disable an LED circuit board upon the end of life detector communicating the end of life condition to the fuse circuit.
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Patent Agency Ranking
3.发明授权公开(公告)号：US09655186B2
公开(公告)日：2017-05-16
申请号：US14504867
申请日：2014-10-02
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling Von Heimendahl , Frank Klein , Benno Heissig
CPC classification number: H05B33/0842 , B60Q3/46 , B60Q3/47 , B64D11/00 , B64D47/02 , B64D2011/0038 , B64D2203/00 , H02J9/065 , Y02T50/53
Abstract: An emergency lighting system for an aircraft includes an emergency light control unit, having an external power input and at least one external control input for receiving external control commands from at least one of a cockpit crew, a cabin crew, a board computer and an autopilot, and a plurality of autonomous emergency light units, each of the plurality of autonomous emergency light units comprising at least one LED and a rechargeable capacitor. The emergency light control unit is configured to process the external control commands and to communicate emergency light control commands to the plurality of autonomous emergency light units as a response to the external control commands.
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4.发明授权Dimmable LED reading light unit, arrangement of power supply and dimmable LED reading light unit and method of replacing a dimmable light unit by a dimmable LED reading light unit 有权可调光LED阅读灯单元，电源和可调光LED阅读灯单元的布置以及通过可调光LED阅读灯单元替换可调光单元的方法公开(公告)号：US09474112B2
公开(公告)日：2016-10-18
申请号：US14197862
申请日：2014-03-05
Applicant: GOODRICH LIGHTING SYSTEMS GMBH
Inventor： Robert Trinschek , Tomasz Kordecki , Frank Klein , Ralf Rehbein
CPC classification number: H05B33/0815 , H05B33/0845 , H05B33/0851 , Y02B20/347
Abstract: A dimmable LED reading light unit includes a dimming module and an LED module, connected in series. The dimming module has an input being connectable to a power supply supplying direct voltage and includes a potentiometer allowing section of a dimming rate and a current controller providing an operating current for the LED module. The LED module includes at least one LED and a current consumer connected in parallel and the current controller is configured to supply direct current to the LED module that substantially corresponds to the sum of the driving current necessary for driving the at least one LED to emit light with an intensity of illumination corresponding to the dimming rate of the potentiometer, and the current consumption of the current consumer.
Abstract translation: 可调光LED阅读灯单元包括串联连接的调光模块和LED模块。 调光模块具有可连接到提供直流电压的电源的输入，并且包括调光速率的电位计允许部分和为LED模块提供工作电流的电流控制器。 LED模块包括并联连接的至少一个LED和当前消费者，并且电流控制器被配置为向LED模块提供基本对应于驱动至少一个LED发光的驱动电流之和 具有对应于电位计的调光率的照明强度和当前消费者的电流消耗。
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5.发明授权Combined wing scan and winglet illumination light unit and aircraft having winglet illumination 有权组合机翼扫描和小翼照明灯单元和飞机具有小翼照明公开(公告)号：US08956023B1
公开(公告)日：2015-02-17
申请号：US14037913
申请日：2013-09-26
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling Von Heimendahl , Frank Klein , Sascha Lueder
IPC: B64D47/02
CPC classification number: B64D47/02
Abstract: A combined wing scan and winglet illumination light unit is disclosed. The light unit has at least one LED and at least one optical structure for shaping a light emission distribution of the combined wing scan and winglet illumination light unit. The wherein the light emission distribution has a first illumination region for illuminating a wing and a wing engine of an aircraft and a second illumination region for illuminating a wing tip winglet of the aircraft.
Abstract translation: 公开了组合机翼扫描和小翼照明灯单元。 光单元具有至少一个LED和用于整形组合的机翼扫描和小翼照明灯单元的发光分布的至少一个光学结构。 其中，所述发光分布具有用于照射飞行器的机翼和机翼引擎的第一照明区域和用于照射所述飞行器的翼梢小翼的第二照明区域。
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公开(公告)号：US20200331629A1
公开(公告)日：2020-10-22
申请号：US16712396
申请日：2019-12-12
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling-von Heimendahl , Anil Kumar Jha , Frank Klein
Abstract: An aircraft beacon light for being mounted to an aircraft fuselage includes: a support structure, having a carrier, and a stem for supporting the carrier and for spacing the carrier from the aircraft fuselage; and a lighting system, supported by the support structure, the lighting system having a plurality of light sources, light optics for redirecting at least a portion of the light emitted by the plurality of light sources, and a lens cover, with the plurality of light sources and the light optics being arranged between the carrier and the lens cover; wherein the aircraft beacon light is configured to emit a red-flashing beacon light output in operation.
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7.发明申请EMERGENCY LIGHTING SYSTEM FOR AN AIRCRAFT AND AIRCRAFT COMPRISING SUCH EMERGENCY LIGHTING SYSTEM 有权用于包括这种紧急照明系统的飞机和飞机的紧急照明系统公开(公告)号：US20150091438A1
公开(公告)日：2015-04-02
申请号：US14504867
申请日：2014-10-02
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling Von Heimendahl , Frank Klein , Benno Heissig
CPC classification number: H05B33/0842 , B60Q3/46 , B60Q3/47 , B64D11/00 , B64D47/02 , B64D2011/0038 , B64D2203/00 , H02J9/065 , Y02T50/53
Abstract: An emergency lighting system for an aircraft includes an emergency light control unit, having an external power input and at least one external control input for receiving external control commands from at least one of a cockpit crew, a cabin crew, a board computer and an autopilot, and a plurality of autonomous emergency light units, each of the plurality of autonomous emergency light units comprising at least one LED and a rechargeable capacitor. The emergency light control unit is configured to process the external control commands and to communicate emergency light control commands to the plurality of autonomous emergency light units as a response to the external control commands.
Abstract translation: 用于飞机的应急照明系统包括具有外部电源输入的应急灯控制单元和至少一个外部控制输入端，用于接收来自驾驶舱乘务员，客舱乘务员，车载计算机和自动驾驶仪中的至少一个的外部控制命令 和多个自主应急灯单元，所述多个自主应急灯单元中的每一个包括至少一个LED和可充电电容器。 所述应急灯控制单元被配置为处理所述外部控制命令，并且响应于所述外部控制命令，向所述多个自主应急灯单元通信应急灯控制命令。
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