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公开(公告)号：US10815004B2
公开(公告)日：2020-10-27
申请号：US16034585
申请日：2018-07-13
Applicant: Goodrich Lighting Systems GmbH
Inventor： Marion Depta , Norbert Menne , Elmar Schrewe
Abstract: A lens structure for placement over a light source and for attachment to a circuit board around the light source includes a circuit board engagement portion for being placed towards the circuit board, a recess provided in the circuit board engagement portion for receiving the light source upon attachment of the lens structure to the circuit board, a light entry surface around the recess, a lens body, a light exit surface distal from the circuit board engagement portion, and an attachment structure, the attachment structure being partially molded into the lens body and partially extending from the lens body for attaching the lens structure to the circuit board.
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公开(公告)号：US09694913B2
公开(公告)日：2017-07-04
申请号：US14446528
申请日：2014-07-30
Applicant: Goodrich Lighting Systems GmbH
Inventor： Norbert Menne , Elmar Schrewe , Klaus Gierse-Plogmeier
IPC: B64D47/02 , F21V23/00 , F21V29/80 , F21V29/89 , F21W111/06 , F21Y115/10 , F21Y107/60
CPC classification number: B64D47/02 , B64D2203/00 , F21V23/007 , F21V29/80 , F21V29/89 , F21W2111/06 , F21Y2107/60 , F21Y2115/10
Abstract: An aircraft LED light unit is disclosed that includes a flat electric circuit device having a first main surface, a second main surface and at least one side surface extending between the first main surface and the second main surface, power supply circuitry, disposed in the electric circuit device, at least one heat transport element, disposed in the electric circuit device, and at least one LED. The at least one LED is arranged on the at least one side surface of the electric circuit device, is electrically coupled to the power supply circuitry, and is in heat exchange relationship with the at least one heat transport element.
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公开(公告)号：US11260989B2
公开(公告)日：2022-03-01
申请号：US16659739
申请日：2019-10-22
Applicant: Goodrich Lighting Systems GmbH
Inventor： Anil Kumar Jha , Andre Hessling-Von Heimendahl , Marion Depta , Norbert Menne
IPC: B64D47/06 , F21S43/20 , F21S43/14 , F21Y115/10 , F21W107/30 , F21W103/15
Abstract: An aircraft beacon light for an aircraft wing with a foldable wing tip includes a housing, a lens cover, and at least one light source arranged between the housing and the lens cover, wherein the aircraft beacon light is configured to emit flashes of red light in operation, and wherein the housing and the lens cover are shaped to embed the aircraft beacon light into a hinge assembly coupling the foldable wing tip to a main wing portion of the aircraft wing.
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4.发明申请公开(公告)号：US20200094988A1
公开(公告)日：2020-03-26
申请号：US16564506
申请日：2019-09-09
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling-Von Heimendahl , Anil Kumar Jha , Marion Depta , Norbert Menne
Abstract: An exterior aircraft light for indicating a movement of a foldable wing tip between a folded up position and a laterally extended position includes a light source; and a control unit; wherein the control unit is configured to operate the light source to emit a warning light output in response to a warning light control signal indicative of the movement of the foldable wing tip.
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Patent Agency Ranking
公开(公告)号：US11136139B2
公开(公告)日：2021-10-05
申请号：US16564177
申请日：2019-09-09
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling-Von Heimendahl , Anil Kumar Jha , Marion Depta , Norbert Menne
IPC: B64D47/06 , F21S43/14 , B64C3/56 , F21V23/04 , F21Y113/13 , F21Y115/10 , F21W103/10 , F21W107/30
Abstract: An aircraft light for a foldable wing tip of an aircraft includes a first lighting structure, including at least one first light source and a first optical system, with the at least one first light source and the first optical system in operation generating a first light output; a second lighting structure, including at least one second light source and a second optical system, with the at least one second light source and the second optical system in operation generating a second light output; wherein the first light output and the second light output are of the same color and wherein the first light output and the second light output are angled with respect to each other; and wherein the aircraft light is configured to control the at least one first light source and the at least one second light source depending on a wing tip orientation signal, which is indicative of an orientation of the foldable wing tip.
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公开(公告)号：US10273022B2
公开(公告)日：2019-04-30
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
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.
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公开(公告)号：US20200094987A1
公开(公告)日：2020-03-26
申请号：US16564177
申请日：2019-09-09
Applicant: Goodrich Lighting Systems GmbH
Inventor： Andre Hessling-Von Heimendahl , Anil Kumar Jha , Marion Depta , Norbert Menne
Abstract: An aircraft light for a foldable wing tip of an aircraft includes a first lighting structure, including at least one first light source and a first optical system, with the at least one first light source and the first optical system in operation generating a first light output; a second lighting structure, including at least one second light source and a second optical system, with the at least one second light source and the second optical system in operation generating a second light output; wherein the first light output and the second light output are of the same color and wherein the first light output and the second light output are angled with respect to each other; and wherein the aircraft light is configured to control the at least one first light source and the at least one second light source depending on a wing tip orientation signal, which is indicative of an orientation of the foldable wing tip.
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公开(公告)号：US10513349B2
公开(公告)日：2019-12-24
申请号：US15983153
申请日：2018-05-18
Applicant: Goodrich Lighting Systems GmbH
Inventor： Anil Kumar Jha , Andre Hessling-Von Heimendahl , Norbert Menne
Abstract: A combined aircraft take-off and tower signal light unit comprises a mounting portion for mounting the combined aircraft take-off and tower signal light unit to an aircraft, wherein the mounting portion is configured for orienting a horizontal cross-sectional plane (H) of the combined aircraft take-off and tower signal light unit substantially horizontally with respect to the aircraft; and at least one light source. The combined aircraft take-off and tower signal light unit has a take-off light output, which is centered on a take-off light emission axis and which has a take-off light peak intensity, and a tower signal light output, which is centered on a tower light emission axis (B) and which has a tower light peak intensity.
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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
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。
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