Patent classifications
H05B47/20
Aircraft light unit and aircraft having such aircraft light unit
An aircraft light unit (2), has a support portion (4), a light source having at least one LED (6), the light source being arranged on the support portion (4) and in operation emitting light with a source-side light intensity distribution, and an optical element (8) for transforming the source-side light intensity distribution into an output light intensity distribution. The optical element (8) has at least two transformation segments (10, 20, 30), covering different angular ranges of the source-side light intensity distribution in a first cross-sectional plane. The at least two transformation segments (10, 20, 30) include a first transformation segment (10), with the light from the light source experiencing total internal reflection within the optical element (8) in the first transformation segment (10) and being bundled in a peak region of the output light intensity distribution, and at least one further transformation segment (20, 30), with the light from the light source experiencing refraction only in the at least one further transformation segment (20, 30).
Projector light source unit having intensity controller
A light source unit includes: a plurality of elemental light sources; an optical sensor; a light quantity measurement circuit; and a control circuit. The plurality of elemental light sources each include one or more light emitting elements, one or more drive circuits, a focusing optical system, and an optical fiber. The one or more drive circuits selectively operate in a driving state or in a non-driving state. The control circuit performs a sequence that sequentially acquires light quantity measurement data by sequentially selecting one of the plurality of elemental light sources, putting at least one of the one or more drive circuits included in the selected elemental light source into a first state, and putting the plurality of drive circuits other than the at least one drive circuit into a second state, and detects abnormality based on a plurality of pieces of the acquired light quantity measurement data.
Methods and systems of proactive monitoring of LED lights
Various embodiments of methods and systems of proactive monitoring of LED lights are described herein. An LED light monitoring system may include a specification database of LED lamps and drivers, a usage database that records the usage of LED lamps and drivers, a data acquisition subsystem that obtains the identity and the usage data of LED lamps or drivers in use, and a data processing subsystem that calculates, for each LED lamp, its current lumen output statistically and, for each LED driver, its remaining lifetime, and provides replacement recommendations for LED lamps and drivers.
Guidance system
To provide a guidance system that can quickly guide a person along a guidance route without anxiety. Provided are: a plurality of unit control apparatuses; and a plurality of unit light emitting apparatuses controlled by the unit control apparatuses, wherein at normal times, light emitting elements of a plurality of light emitting apparatuses of the plurality of unit light emitting apparatuses are continuously lit at an illuminance of 100%, and at guidance, the illuminance of the light emitting elements of the plurality of light emitting apparatuses of the plurality of unit display apparatuses is attenuated to 30%, and then the illuminance of the light emitting elements of the plurality of light emitting apparatuses of the plurality of unit display apparatuses is sequentially controlled to 100% based on count values stored in an emergency exit number count value storage unit to generate an optical flow toward a guidance direction.
LED DRIVING DEVICE WITH DETACHABLE SURGE PROTECTION
An LED driving device includes a converter module configured to receive an input voltage and generate an output voltage for driving a plurality of LEDs. A surge protection module is electrically connected to the converter module. A case holds the converter module and the surge protection module, and provides electrical coupling therebetween.
SYSTEMS AND METHODS FOR SENSIC DEVICE LOCALIZATION
Disclosed are systems and methods for automatically detecting an error in commissioning of a system device in a physical environment comprising a plurality of system devices, comprising the steps: (i) receiving (1352), by each the plurality of system devices, a wireless signal from one or more neighboring system devices; (ii) determining (1354), by each the plurality of system devices, a strength of the received wireless signal; (iii) receiving (1356), from an installer (610), a request to commission a first system device within the physical environment, wherein the request comprises an intended location of the first system device; (iv) receiving (1358) the commissioning request and determined wireless signal strengths from at least one system device neighboring the first system device, wherein the location of the at least one system device neighboring the first system device is known; (v) determining (1360), based at least in part on the received wireless signal strength from the at least one neighboring system device, that the first system device is not located at the intended location; and (vi) alerting (1362) the installer that the first system device is not located at the intended location.
SWITCH CONTROL SYSTEMS FOR LIGHT EMITTING DIODES AND METHODS THEREOF
System and method for controlling one or more light emitting diodes. For example, the system for controlling one or more light emitting diodes includes a current generator configured to generate a first current flowing through one or more light emitting diodes. The one or more light emitting diodes are configured to receive a rectified voltage generated by a rectifying bridge coupled to a TRIAC dimmer. Additionally, the system includes a bleeder configured to receive the rectified voltage, and a controller configured to receive a sensing voltage from the current generator and output a control signal to the bleeder. The sensing voltage indicates a magnitude of the first current.
PROVISIONAL OVERVOLTAGE PROTECTION FOR A LUMINAIRE
The invention is related to a luminaire comprising a lighting module for emitting light, a driver for driving operation of the lighting module, a runtime overvoltage protection device for protecting the lighting module and the driver from exposure to overvoltage above a first overvoltage tripping limit, and a provisional overvoltage protection device that is connected in parallel to the runtime overvoltage protection device and has a second overvoltage tripping limit. The second tripping limit smaller than the first overvoltage tripping limit so that the provisional overvoltage protection device provides overvoltage protection to the runtime overvoltage protection device. Moreover, the provisional overvoltage protection device is deactivatable.
PROVISIONAL OVERVOLTAGE PROTECTION FOR A LUMINAIRE
The invention is related to a luminaire comprising a lighting module for emitting light, a driver for driving operation of the lighting module, a runtime overvoltage protection device for protecting the lighting module and the driver from exposure to overvoltage above a first overvoltage tripping limit, and a provisional overvoltage protection device that is connected in parallel to the runtime overvoltage protection device and has a second overvoltage tripping limit. The second tripping limit smaller than the first overvoltage tripping limit so that the provisional overvoltage protection device provides overvoltage protection to the runtime overvoltage protection device. Moreover, the provisional overvoltage protection device is deactivatable.
Exterior Aircraft Light And Aircraft Comprising The Same
An exterior aircraft light includes a mounting board, having an upper side, a lower side and a plurality of side faces; at least one LED, arranged on the upper side of the mounting board; and a mounting board enclosure and lens structure, wherein the mounting board enclosure and lens structure comprises a lens arranged over the at least one LED for shaping an output light intensity distribution of the exterior aircraft light and a covering layer arranged on the upper side, the lower side and the plurality of side faces of the mounting board, wherein the mounting board enclosure and lens structure is an integral silicone structure.