AC driven LED light with digital control of color and intensity

• US 9,699,841 B2
• Filed: 04/09/2015
• Issued: 07/04/2017
• Est. Priority Date: 06/17/2014
• Status: Active Grant

• Current Assignee: BAE Systems Controls Incorporated (BAE Systems Plc)
• Original Assignee: BAE Systems Controls Incorporated (BAE Systems Plc)
• Inventors: Heimes, Felix O.
• Primary Examiner(s): Vo, Tuyet
• Application Number:
  US14/912,461
• Publication Number:
  US 20160205735A1
• Time in Patent Office: 817 Days
• Field of Search: 315247, 315185 S, 315224, 315225, 315209 R, 315291, 315307-326
• CPC Class Codes: B64D 11/00 Passenger or crew accommodation; Flight-deck installations not otherwise provided for
• CPC Class Codes: B64D 2011/0038 Illumination systems for cabins as a whole
• CPC Class Codes: H05B 45/24 using electrical feedback from LEDs or from LED modules
• CPC Class Codes: H05B 45/395 Linear regulators
• CPC Class Codes: H05B 45/48 having LEDs organised in strings and incorporating parallel shunting devices
• CPC Class Codes: H05B 45/58 involving end of life detection of LEDs
• CPC Class Codes: H05B 47/18 via data-bus transmission
• CPC Class Codes: Y02B 20/30 Semiconductor lamps, e.g. solid state lamps [SSL] light emitting diodes [LED] or organic LED [OLED]

Abstract

A full color LED light for aircraft interiors is described, comprising a housing containing at least three differently colored groups of light emitting diodes, a controller for the groups of light emitting diodes and an alternating current power source. The controller distributes the alternating current to LED groups, providing a desired intensity of each differently colored group, producing a desired blended output color. At least one switching circuit receives input current from the power source, via the controller, and directs current to LED subgroups such that a near optimal voltage drop is maintained, given the varied voltage drops of the LED subgroups, regardless of the input voltage, in light of the voltage rating of the LEDs. Embodiments provide for measurement or estimation of current profiles, thermal profiles, and series resistance, allowing accurate measurement of lumen depreciation over time. Additional embodiments include a feedback circuit to temper input power fluctuations.

Claims

1. A full color array of light emitting diode for aircraft interiors which runs on alternating current, without transformation to direct current, comprising:

a plurality of light emitting diodes comprising substantially equal numbers of light emitting diodes of at least three different colors, wherein light emitting diodes of each color are arranged in a series configuration;

said plurality of light emitting diodes in operative communication with a closed loop feedback circuit;

said closed loop feedback circuit in operative communication with a source of alternating current;

wherein said closed loop feedback circuit is configured to smooth and direct said source of alternating current to said light emitting diodes, thereby maintaining a substantially constant power to said light emitting diodes by accommodating changes in voltage of the alternating current through adjustment of the current provided to said plurality of light emitting diodes, whereby flicker is reduced to levels imperceptible to a typical human observer, and

wherein said closed loop feedback circuit comprises a proportional-integral-derivative controller in operative communication with an analog to digital converter, configured to provide monitor line voltage communicate this information to the proportional-integral-derivative controller, and a current sense circuit, configured to monitor current and communicate this information to the proportional-integral-derivative controller.

2. The full color light emitting diode array for aircraft interiors of claim 1, wherein said closed loop feedback circuit is implemented in software.

3. The full color light emitting diode array for aircraft interiors of claim 1, wherein said closed loop feedback circuit is implemented in a field programmable gate array.

4. The full color light emitting diode array for aircraft interiors of claim 1, wherein said proportional-integral-derivative controller is used to compute nominal light emitting diode intensity and direct the necessary current to said plurality of light emitting diodes.

5. The full color light emitting diode array for aircraft interiors of claim 1, wherein said proportional-integral-derivative controller also takes into account information regarding current, temperature and series resistance of the light emitting diodes when calculating said nominal intensity.