Goodrich Lighting Systems Gmbh

Goodrich Lighting Systems Gmbh & Co. Kg

Goodrich Corporation

Andre Hessling Von Heimendahl

Anil Kumar Jha

Christian Schoen

Marion Depta

Sascha Lueder

Robert Trinschek

Philippe Lapujade

Franz-Josef Beermann

Jens Leuschner

Steffen Roebke

Frank Klein

Ryan Schmidt

Christoph Kallfass

Carsten Pawliczek

Andreas Ueberschaer

Steven Thomas Keller

Siegfried Schmees

Elmar Schrewe

Todd Christopher Knight

Björn Schallenberg

Alexander Wernicke

Rebecca Stoner

Jan Frederik Hildebrandt

Lars Christian Schroeder

Benno Heissig

Sascha Kueckelmann

Anthony Bartels

Christian Schön

Jörg Müller

Sascha Luwder

Jr Benjamin Elmer Bishop

Steven T Keller

Philippe G Lapujade

Jan Hildebrandt

An aircraft headlight comprises at least one light source and an integrated, single-piece optical structure. The integrated, single-piece optical structure includes a light transmissive protective cover portion, forming an outer light emission surface of the aircraft headlight, and at least one reflector portion, arranged for directing light that is emitted by the at least one light source through the light transmissive protective cover portion.

Aircraft headlight, aircraft comprising an aircraft headlight and method of manufacturing an aircraft headlight

An aircraft passenger reading light, which is operable in at least two predetermined configurations, comprises: a light source; an optical element; and an actuation mechanism, which is configured to modify a distance between the light source and the optical element. The distance (D) between the light source and the optical element differs in the at least two predetermined configurations and a spatial extension of the illumination, which results from the light output of the light source and the optical element, differs in the at least two predetermined configurations.

Aircraft passenger reading light

A multi mode aircraft beacon light comprises a mounting portion for mounting the multi mode aircraft beacon light to an aircraft fuselage; at least one visible light source for emitting a visible beacon light output; a plurality of infra-red light sources for emitting an infrared beacon light output; an orientation sensor; and a controller, coupled to the orientation sensor for receiving an orientation sensor signal from the orientation sensor. The controller is configured to determine a mounting orientation of the multi mode aircraft beacon light from the orientation sensor signal, wherein the mounting orientation is indicative of whether the multi mode aircraft beacon light has an upper fuselage mounting position or a lower fuselage mounting position; and to selectively operate the plurality of infrared light sources, depending on the mounting orientation of the multi mode aircraft beacon light.

Multi mode aircraft beacon light and aircraft comprising a multi mode aircraft beacon light

An aircraft beacon light includes: a plurality of first LEDs, wherein the plurality of first LEDs emit aviation red light in accordance with Federal Aviation Regulations section 25.1397 at an operating temperature of 25° C.; and a plurality of second LEDs, wherein the plurality of second LEDs are phosphor-converted LEDs of red or reddish orange color; wherein the aircraft beacon light is configured to jointly flash the plurality of first LEDs and the plurality of second LEDs for emitting a red beacon light output.

Aircraft beacon light, and aircraft comprising an aircraft beacon light

An aircraft light providing a white light output has a light source that comprises a light emitting semiconductor for emitting light having an initial light spectrum; a first light converting material, arranged over the light emitting semiconductor; and a light transmissive layer, covering the first light converting material. A first portion of the light, which is emitted by the light emitting semiconductor, is shifted towards longer wavelengths by the first light converting material. The aircraft light further comprises a second light converting material, which is arranged over the light transmissive layer of the light source and a lens element, which is arranged over the second light converting material, with light exiting the lens element forming at least a portion of the white light output of the aircraft light.

Aircraft light, aircraft comprising an aircraft light, and method of manufacturing an aircraft light

An exterior aircraft light with cover erosion monitoring, the exterior aircraft light comprises: a support; at least one light source, arranged on the support; a light transmissive cover, arranged over the at least one light source, the light transmissive cover having a forward facing portion and a rear-ward facing portion; a first light sensor, arranged to receive light emitted by the at least one light source and reflected towards the first light sensor by the forward facing portion of the light transmissive cover; and a second light sensor, arranged to receive light emitted by the at least one light source and reflected towards the second light sensor by the rearward facing portion of the light transmissive cover.

Exterior aircraft light with cover erosion monitoring, aircraft comprising such exterior aircraft light, and method of monitoring erosion of a light transmissive cover

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.

Aircraft light, aircraft, and method of assembling an aircraft light

An aircraft beacon light unit has an operating light emission distribution. The operating light emission distribution has a first light emission opening angle of at least 150&#xb0; in a first cross-sectional plane, and a second light emission opening angle of at most 180&#xb0; in a second cross-sectional plane orthogonal to the first cross-sectional plane. The aircraft beacon light unit is configured in such a way that it is mountable to an aircraft with the first cross-sectional plane being oriented in a vertical direction and the second cross-sectional plane being oriented in a horizontal direction, and the first light emission opening angle extends at least 75&#xb0; both above and below the second cross-sectional plane.

Aircraft beacon light unit and set of aircraft beacon light units

An exterior lamp for an aircraft may comprise a housing, a navigation light disposed within the housing, and a brake light disposed within the housing, wherein the brake light is configured to illuminate in response to a brake signal. The exterior lamp may include a controller disposed within the housing, and a tangible, non-transitory memory configured to communicate with the controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising receiving a brake signal and illuminating the brake light in response to a brake signal.

Systems and methods for aircraft braking signal

A system for transferring heat from printed circuit boards (PCBs) with light emitting diodes (LEDs) includes a PCB having a first side and a second side and configured to be coupled to an exterior portion of an aircraft. The system further includes a LED located on the first side of the PCB. The system further includes a first metal strip located on the second side of the PCB. The system further includes a heat sink configured to contact the first metal strip to dissipate heat from the PCB.

High performance heat sink for double sided printed circuit boards

An LED light unit comprises a support portion, a light source having at least one LED, the light source being arranged on the support portion and having a source-side light intensity distribution (LI), and a refractive optical element having an inner surface and an outer surface, with at least one of the inner surface and the outer surface being non-spherical, the refractive optical element being arranged over the light source and being attached to the support portion.

LED light unit and method of producing an LED light unit

An aircraft may include a first pair of forward-facing flash position lamps disposed at a first wing tip, the first pair of flash position lamps comprising a first flash position lamp and a second flash position lamp, a second pair of forward-facing flash position lamps disposed at a second wing tip, the second pair of flash position lamps comprising a third flash position lamp and a fourth flash position lamp, and a controller in electronic communication with the first pair of flash position lamps, wherein at least one of the first flash position lamp and the second flash position lamp are configured to flash, while maintaining a combined intensity of the first pair of forward-facing flash position lamps above a desired intensity, to indicate a change in direction of the aircraft.

Position lights as direction change signals

A lanyard assembly for an evacuation system may comprise a lanyard body and a pin housing. The lanyard body may comprise an actuator connect portion, a pin housing connect portion, and a center member extending between the actuator connect portion and the pin housing connect portion. The pin housing may be slidably coupled to the pin housing connect portion of the lanyard body.

Adjustable release lanyard

An LED light unit, in particular for a passenger transportation vehicle, such as an aircraft, a road vehicle, a ship or a rail car, has a support portion a light source having at least one LED, the light source being arranged on the support portion, and a refractive optical element having an inner surface and an outer surface the refractive optical element being attached to the support portion and being arranged over the light source. The refractive optical element has a chamfer portion adjacent the support portion, wherein at least one of the inner surface and the outer surface has at least one chamfer surface in the chamfer portion.

Growing community of inventors

Koblenz, Germany

Andre Hessling Von Heimendahl