Abstract: A lighting arrangement for the interior of an automotive vehicle in which the light source, such as an LED, is recessed into the interior structure of the vehicle and covered with a layer of fabric. The light source is invisible when not in use, but shines through the fabric/foam layer when illuminated, and can be associated with a light transmitting member, such as a light bar and a light pipe. Such lighting arrangements can be disposed within the headliner to direct light where desired and for different functions, such as a map light or for area lighting. The lighting arrangement can be mounted in non-traditional locations, such as on vertically oriented pillars, visors, door panels, seat backs, seat fronts, and console sides. The light source is preferably one or more LEDs associated with a light transmitting medium to direct the discharge of light as desired within the automotive interior.

Abstract: A light bar proximity switch is provided that includes a light pipe having a first surface and a second surface, wherein the first and second surface define an area. The light bar proximity sensor further includes an at least partially reflective surface adjacent the second surface, at least one circuit board spaced from the light pipe and the at least partially reflective surface, at least one proximity sensor electrically connected to the at least one circuit board, and at least one light source configured to project light along the area, wherein the emitted light is reflected by the at least partially reflective surface and viewed through the first surface.

Abstract: A vehicle component is provided that includes a console surface, at least one circuit board proximate the console surface, and an array of proximity sensors electrically connected to the at least one circuit board. Each of the proximity sensors emit a field that combine to form an activation field, wherein a lateral direction of the activation field extending approximately parallel to the console surface is greater than a longitudinal direction of the activation field extending approximately perpendicular to the console surface.

Abstract: A vehicle interior panel is provided that includes an interior panel substrate defining an aperture for a light source to extend through the interior panel substrate, a lens attached to the interior panel substrate, wherein the lens extends over at least a portion of the aperture for the light source, an at least partially transparent material that extends over the lens, and a plurality of positioning holes defined by the interior panel substrate, such that at least a portion of the plurality of positioning holes are configured to correspond to a plurality of positioning pins of an interior panel mold.

Abstract: An interior light in a vehicle and method of compensating for a change of color of emitted light are provided. The interior light includes a circuit board configured to be attached to a roof support structure of the vehicle, an at least partially transparent material proximate to the circuit board and attached to the roof support structure, wherein the at least partially transparent material changes a perceived color and of light propagating there-through, and at least one light source electrically connected to the circuit board, such that the at least one light source is between the circuit board and the at least partially transparent material, wherein the at least one light source is configured to emit light that propagates through the at least partially transparent material, and further configured to compensate for the change of the color and the intensity of light propagating through the at least partially transparent material.

Abstract: A luminous decorative vehicle trim insert having an opaque carrier structure. A reflective layer is disposed over the opaque carrier structure. A light pipe is adjacent the reflective layer and operably connected to a light source. An optic layer is disposed in the light pipe. A total internal reflection (TIR) protective layer is disposed over the light pipe. A diffusing layer is disposed over the TIR protective layer. A decorative transmitting layer is disposed over the diffusing layer. An optic layer creates a luminous effect in the trim insert visible only when the light source is activated. An environmental layer is disposed over the transmitting layer.

Abstract: A light bar system for a vehicle compartment includes a circuit board having a plurality of capacitive-type, user-activated switches, an electrical power source coupled to the circuit board, a light emitting diode (LED) coupled to the circuit board, and a light bar affixed to the circuit board. The user-activated switches are coupled to a vehicle accessory to control the level of operation of the vehicle accessory. The most recently actuated one of the user-actuated switches is detected by the circuit board and the circuit board provides a pulse width modulated (PWM) signal to the LED with a duty cycle of the PWM signal based on the most recently actuated switch. A higher duty cycle PWM signal corresponds to a higher setting of the accessory.

Abstract: A vehicle interior panel having a substrate with a receiving slot. A support lens is disposed in the receiving slot and includes a light source. A sensor is operably connected to the light source and disposed proximate the support lens. A connector operably links the sensor to the light source through the support lens. A decorative layer extends over the support lens and the sensor.

Abstract: A method for making a vehicle interior panel including positioning a slipsheet on a film or fabric liner. The liner is placed on a substrate board. The liner and substrate board are formed into an interior panel. A cavity is formed by removing a portion of the substrate board from the interior panel adjacent to the slipsheet position. A lamp is positioned in the cavity.

Abstract: A lighting arrangement for the interior of an automotive vehicle in which the light source, such as an LED, is recessed into the interior structure of the vehicle and covered with a layer of fabric. The light source is invisible when not in use, but shines through the fabric/foam layer when illuminated, and can be associated with a light transmitting member, such as a light bar and a light pipe. Such lighting arrangements can be disposed within the headliner to direct light where desired and for different functions, such as a map light or for area lighting. The lighting arrangement can be mounted in non-traditional locations, such as on vertically oriented pillars, visors, door panels, seat backs, seat fronts, and console sides. The light source is preferably one or more LEDs associated with a light transmitting medium to direct the discharge of light as desired within the automotive interior.

Abstract: A parking brake system for an automotive vehicle includes an internally articulated pedal arm having an upper pedal arm which is connected with a cable operated parking brake actuator, and a lower pedal arm which is pivotably attached to the upper pedal arm such that the lower pedal arm has both a stowed position and a deployed position.

Abstract: A collapsible storage system attachable to an exterior or an interior of an automobile. The storage system may include a front primary panel pivotally connected to a central primary panel at one end of the central primary panel, and a rear primary panel pivotally connected to the central primary panel at an opposite end of the central primary panel. The front, rear and/or central primary panels may include pivotally connected secondary side panels. The front and rear primary panels may be pivotally movable relative to the central primary panel and the secondary side panels may be pivotally movable laterally relative to the front, rear and/or central primary panels in predetermined directions to place the storage system in an assembled configuration, and may be movable in predetermined opposite directions to place the storage system in a collapsed configuration.

Abstract: A white anti-collision light mounted on an aircraft utilizes a set of high-power light-emitting diodes (LEDs) and dedicated reflectors to distribute the light in a particular pattern that satisfies predetermined intensity requirements along a horizontal coverage area. The anti-collision light may include heat pipes for transferring heat from the LEDs to a set of cooling fins. Also, the LEDs may be electrically connected and controlled to provide redundancy and mitigate the effects of LED failures.

Abstract: A rotationally symmetrical anti-collision light (100, 200) for an aircraft utilizing light-emitting diodes (LEDs) is mounted to the fuselage of an aircraft. The LEDs (10, 10?, 20, 20?) may be configured in one or more concentric rings. The anti-collision light includes a reflector (30, 30?) configured to redirect the light emitted by at least one of the rings, so that the light pattern satisfies predetermined specifications.

Abstract: A system and method for implementing an LED-based luminaire (100) incorporates one or more color channels (32-n). The luminaire includes a controller (50) that uses optical sensing and feedback to control LEDs (30A) in each channel to deliver a consistent intensity and/or color output. The optical feedback loop may provide measured intensity and/or color of the luminaire's output to the luminaire controller. The controller may then adjust the current, pulse width modulation (PWM) duty cycle, or both, which are delivered to discrete color channels of the luminaire to obtain the desired intensity and/or color.

Abstract: An aircraft rear position light device (1) has a modular configuration. The device utilizes solid-state light sources. In an exemplary embodiment, the light sources are side-emitting light-emitting diodes (LEDs) (40), which are attached to a heat sink (30). A reflector (200) is positioned next to each of the LEDs. The device further includes an outer lens (10) with an integrated cut-off shield (110) and optical treatments (120). The configuration of LEDs and reflectors, in conjunction with the cut-off shield and optical treatments, allows the emitted light to satisfy predetermined minimum and maximum angular intensity requirements. An electronics module (50) is also attached to the heat sink to connect the LEDs to a power source in the aircraft. Electronic updates may be made by replacing the electronics module.

Abstract: A quick attachment device for use in the repeated testing of diode light sources (30) includes a quick attachment module (10) having a fixed location with respect to a testing position (150) for the diodes (30), and a mounting assembly (20) on which each diode (30) is mounted during testing. The quick attachment module (10) includes a quick disconnect fastener and two locating pins (120a and 120b) for securing the mounting assembly (20) for testing, where the two locating pins (120a and 120b) have a locational transition fit connection with the mounting assembly (20). The mounting assembly (20) may further include a thermal-electric cooling device (260) for cooling the diode light sources (30) during testing.

Abstract: An aircraft forward position lighting device (1) has a modular configuration, including a mounting module (20) containing solid-state light sources, e.g., light-emitting diodes (LEDs) (210, 230). The mounting module also includes reflectors 220. The pattern of light emanating from the light sources and reflectors satisfy Federal Aviation Regulations (FARs) regarding minimum light intensity. The device includes a cut-off shield module (10) configured to provide angular cut-offs to the pattern of light, so that the device satisfies FARs regarding overlap between position lights. The device may also include a base assembly module (30) that contains electronic circuitry connecting the light sources to a power source in the aircraft. Electronic updates may be performed by replacing the base assembly module.

Abstract: Pilot Director Lights (PDLs) mounted on the exterior of a refueling tanker aircraft (10) utilize light emitting diodes (LEDs) (213) as a light source to provide visual information to the pilot of an approaching aircraft (30). The PDLs may include a plurality of light emitting devices (200) arranged in arrays (123 and 124), each light emitting device (200) being configured to illuminate a particular symbol/pattern. Each light emitting device (200) may include a plurality of modular banks (210) of LEDs (213), which are configured to emit light through a clear lens (230) within a particular field of view. The PDL arrays (123 and 124) may provide visual feedback regarding the elevational and fore-aft position of the approaching aircraft (30) relative to the boom envelope (14) of the tanker aircraft (10).