公开(公告)号：US20250100712A1

公开(公告)日：2025-03-27

申请号：US18887326

申请日：2024-09-17

Applicant: Goodrich Lighting Systems GmbH & Co. KG

Inventor： Anil Kumar Jha ,  Andre Hessling-von Heimendahl ,  Elmar Schrewe

IPC: B64D47/04 ,  B64D11/00 ,  B64D47/06 ,  F21V29/503 ,  F21Y113/00

Abstract: An aircraft light comprises a light source support board, having a light source side and a back side; and a light source, arranged on the light source side of the light source support board; wherein the light source support board comprises a first metallic layer, the first metallic layer forming conductive traces on the light source side of the light source support board; an isolating layer; a second metallic layer, wherein the isolating layer is arranged between the first metallic layer and the second metallic layer and isolates the second metallic layer from the first metallic layer; and a support board core layer. A cavity is provided in the support board core layer.

公开(公告)号：US20240369202A1

公开(公告)日：2024-11-07

申请号：US18644588

申请日：2024-04-24

Applicant: Goodrich Lighting Systems GmbH and Co. KG

Inventor： Marion Depta ,  Anil Kumar Jha ,  Carsten Pawliczek

IPC: F21S41/20 ,  B64D47/04 ,  F21S41/32

Abstract: An exterior aircraft light comprise at least one light emission assembly that includes at least one light source; a cup-shaped reflector; and a light transmissive cover for the cup-shaped reflector. The at least one light source is arranged at a bottom portion of the cup-shaped reflector and a light output opening is provided at a top portion of the cup-shaped reflector. The light transmissive cover comprises a lid portion, extending across the light output opening of the cup-shaped reflector; and a column-shaped light collimating portion, extending from the lid portion into the cup-shaped reflector towards the at least on light source and comprising a light collimation surface facing the at least one light source. The lid portion comprises, on at least one side thereof, a light dispersing profile.

公开(公告)号：US12024290B2

公开(公告)日：2024-07-02

申请号：US18319836

申请日：2023-05-18

Applicant: Goodrich Lighting Systems Gmbh & Co. KG

Inventor： Anil Kumar Jha ,  Jens Leuschner

IPC: B64D11/00 ,  B60Q3/44 ,  B60Q3/60 ,  B65D47/08 ,  H04N5/33

CPC classification number: B64D11/00 ,  B60Q3/44 ,  B60Q3/60 ,  B65D47/08 ,  H04N5/33 ,  B64D2011/0053

Abstract: An aircraft passenger reading light comprises at least one reading light source, which is arranged for emitting visible light in a reading light emission direction; and at least one infrared light source, which is arranged for emitting infrared light in an infrared light emission direction. The infrared light emission direction is inclined with respect to the reading light emission direction.

公开(公告)号：US11913630B2

公开(公告)日：2024-02-27

申请号：US17973863

申请日：2022-10-26

Applicant: Goodrich Lighting Systems Gmbh & Co. KG

Inventor： Marion Depta ,  Anil Kumar Jha ,  Robert Trinschek

IPC: F21S45/60 ,  F21V29/90 ,  B64D47/04 ,  F21V29/10 ,  F21W107/30

CPC classification number: F21V29/10 ,  B64D47/04 ,  F21W2107/30

Abstract: Aircraft headlight includes at least one light source; and a light transmissive cover, at least partially covering the at least one light source. The light transmissive cover includes a first layer made of a first material; a second layer made of a second material, which differs from the first material; and at least one electric heating wire for heating the light transmissive cover by passing an electric current through the electric heating wire. The at least one electric heating wire is embedded into the first layer.

公开(公告)号：US11905035B2

公开(公告)日：2024-02-20

申请号：US18163087

申请日：2023-02-01

Applicant: Goodrich Lighting Systems Gmbh & Co. KG

Inventor： Anil Kumar Jha ,  Andre Hessling von Heimendahl ,  Andreas Ueberschaer

IPC: B64D47/06 ,  F21S43/20 ,  B60Q1/26 ,  B64D45/08 ,  B64D47/02 ,  F21V17/16 ,  B64D11/00

CPC classification number: B64D47/06 ,  B60Q1/2615 ,  B64D45/08 ,  B64D47/02 ,  F21S43/26 ,  F21V17/16 ,  B60Q2800/30 ,  B64D2011/0038 ,  B64D2011/0053 ,  B64D2203/00

Abstract: An aircraft light comprises a support board; a light source, arranged on the support board; a first optical element, which is at least partially light transmissive, which is arranged over the light source, and which is fixed to the support board; and a second optical element, which is at least partially light transmissive, wherein the first optical element is interposed between the light source and the second optical element. The first optical element has a first engagement portion and the second optical element has a second engagement portion. The first engagement portion and the second engagement portion establish a positive fit between the first optical element and the second optical element. At least a portion of light, which is emitted by the light source in operation, passes through the first optical element and through the second optical element.

公开(公告)号：US11565826B2

公开(公告)日：2023-01-31

申请号：US17156800

申请日：2021-01-25

Applicant: Goodrich Lighting Systems GmbH

Inventor： Anil Kumar Jha ,  Andre Hessling-Von Heimendahl

IPC: B64D47/02 ,  H05B47/105 ,  B64C39/02

Abstract: A navigation light system for an unmanned aerial vehicle, such as a multicopter type unmanned aerial vehicle, includes: a plurality of light emission units. E of the plurality of light emission units has a unit-specific light emission direction and is configured to provide a light output around the unit-specific light emission direction. Each of the plurality of light emission units includes a multi-color light source capable of emitting red light, green light, and white light. The plurality of light emission units are arranged to jointly provide a navigation light pattern around the unmanned aerial vehicle and wherein the light outputs of adjacent light emission units have an overlap the navigation light system is configured to operate each of the plurality of light emission units depending on a relation between a momentary flight direction of the unmanned aerial vehicle and the respective unit-specific light emission direction.

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.

公开(公告)号：US11226081B2

公开(公告)日：2022-01-18

申请号：US16700069

申请日：2019-12-02

Applicant: Goodrich Lighting Systems GmbH

Inventor： Andre Hessling-Von Heimendahl ,  Anil Kumar Jha

IPC: B64D47/04 ,  F21V7/04 ,  F21V7/06 ,  F21Y115/10 ,  B64D11/00

Abstract: A lighting arrangement includes a light source configured for emitting light; a first reflector configured for collimating a first portion of the light emitted by the light source around a main light emission direction (D); and a second reflector arranged opposite to the light source. The second reflector is configured for reflecting a second portion of the light emitted by the light source back towards the light source for being diffusely reflected from the light source.

公开(公告)号：US11225336B2

公开(公告)日：2022-01-18

申请号：US17077106

申请日：2020-10-22

Applicant: Goodrich Lighting Systems GmbH

Inventor： Andre Hessling-Von Heimendahl ,  Robert Trinschek ,  Anil Kumar Jha ,  Matthias Krause

IPC: B64D47/06 ,  H05B47/20 ,  H05B47/105 ,  F21S10/06 ,  G08G5/04 ,  F21Y115/10 ,  F21W107/30 ,  B64D47/04

Abstract: A combined aircraft navigation and anti-collision light, includes: at least one navigation light source and one anti-collision light source; a navigation light sensor, in operation outputting a light detection signal corresponding to an amount of light detected by the navigation light sensor; first and second optical systems, associated with navigation and collision light sources, wherein the first optical system is configured for shaping a navigation light output from light emitted by the at least one navigation light source and is configured for directing stray light from the at least one navigation light source to the navigation light sensor and a second optical system, associated with the at least one anti-collision light source and configured for shaping an anti-collision light output from light emitted by the at least one anti-collision light source; a lens cover, arranged over the light sources and optical systems for passing light therethrough.

公开(公告)号：US11097855B2

公开(公告)日：2021-08-24

申请号：US16441548

申请日：2019-06-14

Applicant: Goodrich Lighting Systems GmbH

Inventor： Anil Kumar Jha ,  Andre Hessling-Von Heimendahl

IPC: B64D47/06 ,  F21V7/00 ,  F21V7/06 ,  F21V5/04 ,  B64D47/04 ,  F21Y115/10 ,  F21W107/30

Abstract: An aircraft beacon light includes a mounting plate having a central portion; a plurality of light sources arranged on the mounting plate around the central portion and facing away from the mounting plate; and a lens structure arranged over the plurality of light sources, wherein the lens structure is configured to reflect a first portion of light emitted by the plurality of light sources laterally outwards via total internal reflection; wherein the aircraft beacon light is configured to emit flashes of red light in operation.