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公开(公告)号：US20230027737A1
公开(公告)日：2023-01-26
申请号：US17385690
申请日：2021-07-26
Applicant: B/E AEROSPACE, INC.
Inventor： Eric Johannessen
Abstract: A method may comprise: commanding, by a processor, a lighting system to generate a first desired effect in accordance with a first spectral weighting mode; determining, by the processor, a first optimized predetermined variable within a first predetermined domain to generate the desired effect based on the first spectral weighting mode; commanding, by the processor, the lighting system to transition from the first desired effect to a second desired effect, the second desired effect in accordance with a second spectral weighting mode; and determining by the processor, a second optimized predetermined variable within a second predetermined domain to generate the second desired effect based on the second spectral weighting mode, the first optimized predetermined variable being different from the second optimized predetermined variable.
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公开(公告)号：US11318882B2
公开(公告)日：2022-05-03
申请号：US16823826
申请日：2020-03-19
Applicant: B/E AEROSPACE, INC.
Inventor： Eric Johannessen , Jameson Mauzy
IPC: B60Q3/43 , B60Q3/47 , B64D11/00 , F21V5/04 , F21Y113/13 , F21Y105/10 , F21Y115/10 , F21W107/30 , F21W106/00
Abstract: A lighting device is disclosed. In various embodiments, the lighting device includes an optical system; a plurality of light sources arranged in a matrix, the plurality of light sources including a first plurality of light sources configured to irradiate a first region of the optical system with a first light color, a second plurality of light sources configured to irradiate a second region of the optical system with a second light color; and a processor configured to control interaction of the first plurality of light sources and the second plurality of light sources with a third plurality of light sources and to control mixing of the first light color and the second light color.
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公开(公告)号：US20200002024A1
公开(公告)日：2020-01-02
申请号：US16558773
申请日：2019-09-03
Applicant: B/E Aerospace, Inc.
Abstract: An integrated aircraft lighting and display panel includes high-density arrays of micro-scale light-emitting diodes (LED) set into arrays (e.g., linear, two-dimensional, freeform) to form tiles, the LED tiles combined and interconnected to form LED panels conformable to any interior surface within an aircraft cabin. The PCB and LED arrays may be set into structural layers corresponding to overhead panels, side panels, bin panels, divider panels, doorway panels, galley and monument panels, or other interior structural panels of the aircraft. The LED arrays may be activated by an onboard video processor and local panel-level controllers to provide cabin lighting, indicate aircraft signage, display high-resolution image or video graphics, or simultaneously blend any combination thereof, either on command or in response to detected conditions.
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公开(公告)号：US10317053B2
公开(公告)日：2019-06-11
申请号：US15460555
申请日：2017-03-16
Applicant: B/E AEROSPACE, INC.
Inventor： Matthew Dunn , Anthony Catania , Eric Johannessen
IPC: F21S4/24 , F21V21/02 , F21V21/088 , F21Y103/10 , F21Y107/70 , F21Y115/10
Abstract: A clamp for holding a twisted lighting unit includes a body member having a slot extending from its top wall to its base. The slot extends from an end wall to a side wall to create a passage for receiving a twisted portion of a lighting unit. Parallel surfaces are provided over a portion of the width of the passage to hold the lighting unit in its intended position. Various curves in the slot receive the twist itself and facilitate insertion of the clamp on the lighting unit and reduce the strain experienced along the edge of the lighting unit.
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公开(公告)号：US10128654B2
公开(公告)日：2018-11-13
申请号：US15682882
申请日：2017-08-22
Applicant: B/E AEROSPACE, INC.
Inventor： Eric Johannessen , Brendan Upton , Luis Sam
Abstract: A light-emitting diode (“LED”) lighting unit includes an operational, a sense resistor electrically connected to the input of the operational amplifier, a first field effect transistor (“FET”) whose gate is electrically connected to the output such that the input voltage at the gate of the first FET rises and falls with the output voltage, a second FET whose gate is electrically connected to the output such that the input voltage at the gate of the second FET rises and falls with the output voltage, and a string of LED lights connected such that when the voltage across the string drops below a level to operate, the voltage across a sense resistor drops, causing the operational amplifier to increase its output until the input voltage at the gate of the second FET increases allowing one bank of LED lights to operate.
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Patent Agency Ranking
公开(公告)号：US09999109B2
公开(公告)日：2018-06-12
申请号：US15331698
申请日：2016-10-21
Applicant: B/E AEROSPACE, INC.
Inventor： Luis Sam , Eric Johannessen , Brendan Upton
IPC: H05B33/08 , H05B37/02 , F21K9/278 , F21K9/272 , F21V3/02 , F21Y115/10 , F21Y103/10 , F21K9/275
CPC classification number: H05B33/0887 , F21K9/272 , F21K9/275 , F21K9/278 , F21V3/02 , F21Y2103/10 , F21Y2115/10 , H05B33/0809 , H05B33/083 , H05B33/0851 , H05B33/089 , H05B37/0227
Abstract: An LED lighting assembly includes, according to various implementations, mechanisms for protecting the LED lights from voltage or current surges, including hardware that absorbs the strike voltage and hardware that provides a bypass path. The provision of a bypass path in the event of the failure of one or LED lights in an LED string allows the string to be, in effect, “turned off” in order to protect the remaining LED lights, thereby allowing the healthy LED lights to stay lit.
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公开(公告)号：US09868390B1
公开(公告)日：2018-01-16
申请号：US15338930
申请日：2016-10-31
Applicant: B/E AEROSPACE, INC.
Inventor： Luis Sam , Eric Johannessen , Brendan Upton
CPC classification number: B60Q3/47 , B64D11/00 , B64D47/02 , H05B33/0845 , H05B33/086 , H05B33/0863
Abstract: An LED lighting assembly onboard an aircraft includes at least one light emitting diode (LED) unit and a controller. The LED unit includes any number of primary LEDs and at least two white LEDs. The controller is configured to supply respective driving signals to each of the LEDs, the respective driving signals individually controlling relative intensity outputs of the respective LEDs. The controller is further configured to display a desired color point by continuously driving the white LEDs while not driving at least one of the other LEDs.
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公开(公告)号：US20130038241A1
公开(公告)日：2013-02-14
申请号：US13650289
申请日：2012-10-12
Applicant: B/E Aerospace, Inc.
Inventor： Eric Johannessen , Andrew B. Walsh , Kevin Lawrence , Richard Waring, JR.
IPC: H05B37/02
CPC classification number: H05B33/0869 , H05B33/0827
Abstract: A system and appertaining method calibrate a color LED light unit comprising at least first-, second-, and third-color LEDs, comprising: a) defining a target color on a color map to calibrate; b) selecting initial calibration coefficients associated with the target color; c) storing the initial or updated calibration coefficients in a non-volatile memory of the light unit; d) controlling the light unit to drive the LEDs to attempt to emit the target color, producing an attempted color, utilizing the calibration coefficients; e) measuring the attempted color to determine if it matches the target color within a predefined tolerance; f) if the attempted color matches the target color, then terminating the method; g) if the attempted color does not match the target color, then performing the following; h) selecting a color component; i) adapting at least one calibration coefficient associated with the selected color component; and j) performing (c)-(i) again.
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公开(公告)号：US20250091507A1
公开(公告)日：2025-03-20
申请号：US18961182
申请日：2024-11-26
Applicant: B/E AEROSPACE, INC.
Inventor： Eric Johannessen
Abstract: A method may comprise: commanding, by a processor, a lighting system to generate a first desired effect in accordance with a first spectral weighting mode; determining, by the processor, a first optimized predetermined variable within a first predetermined domain to generate the desired effect based on the first spectral weighting mode; commanding, by the processor, the lighting system to transition from the first desired effect to a second desired effect, the second desired effect in accordance with a second spectral weighting mode; and determining by the processor, a second optimized predetermined variable within a second predetermined domain to generate the second desired effect based on the second spectral weighting mode, the first optimized predetermined variable being different from the second optimized predetermined variable.
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公开(公告)号：US11911527B2
公开(公告)日：2024-02-27
申请号：US17184913
申请日：2021-02-25
Applicant: B/E AEROSPACE, INC.
Inventor： Daniel Tilmont , Eric Johannessen , John Edquist
CPC classification number: A61L2/10 , A61L2/084 , A61L2/22 , A61L2/26 , A61L9/14 , A61L2202/11 , A61L2202/14 , A61L2202/25 , A61L2209/11 , A61L2209/16 , A61L2209/211
Abstract: A sanitization system for an aircraft cabin may comprise: a cabin of an aircraft; a light system including a lighting unit configured to emit an electromagnetic radiation output between 300 and 430 nanometers (“nm”); an external reactive oxygen species (ROS) generator in fluid communication with the cabin, wherein the sanitization system is configured to disinfect a target area of the cabin by targeting the target area with the electromagnetic radiation output and the ROS.
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