Adaptive lighting system for an aircraft interior

Patent metadata

Field	Value
Publication number	US-10118545-B2
Application number	US-201715788596-A
Country	US
Kind code	B2
Filing date	Oct 19, 2017
Priority date	Apr 4, 2017
Publication date	Nov 6, 2018
Grant date	Nov 6, 2018

Abstract

Systems and methods for adaptively controlling lighting within a passenger suite of an aircraft cabin include a light sensor disposed on or within a surface of a static element of the passenger suite that detects illumination characteristics of external lighting system(s) within the aircraft cabin. The illumination characteristics may include lighting color and intensity. A controller may cause illumination of one or more illumination devices disposed near surfaces of the passenger suite such that the illumination of the surfaces matches or complements the sensed illumination characteristics of the external lighting system(s) independent of any communications received from the external lighting systems, thereby allowing additional ambient lighting systems to be added to the aircraft cabin without having to be integrated with other aircraft lighting systems.

First claim

What is claimed is:

1. A system for adaptively controlling ambient lighting within a passenger suite of an aircraft cabin comprising:
a suite light sensor disposed on or within a surface of a static element of the passenger suite, the suite light sensor configured to detect illumination characteristics within a first region of the aircraft cabin;
a plurality of illumination devices disposed proximate one or more surfaces of the passenger suite, the plurality of illumination devices configured to illuminate the one or more surfaces of the passenger suite;
at least one external light sensor disposed externally to the passenger suite and configured to detect illumination characteristics within a second region of the aircraft cabin proximate the first region; and
a controller coupled to the suite light sensor, the at least one external light sensor, and the plurality of illumination devices, wherein the controller comprises control circuitry configured to:
receive a plurality of signals from each of the suite light sensor and the external light sensor, wherein the plurality of signals each represent at least one of a lighting color and a light intensity,
analyze the plurality of signals to determine combined illumination characteristics representing at least one of a combined lighting color and a combined light intensity, and
cause illumination of the one or more surfaces of the passenger suite by the plurality of illumination devices such that the illumination of the one or more surfaces matches or complements the combined illumination characteristics.

2. The system of claim 1 , wherein:
the suite light sensor is configured to detect light intensity entering the passenger suite through a fuselage window of the aircraft cabin; and
the controller is configured to adjust the amount of light output by the plurality of illumination devices based on the light intensity to compensate for illumination provided via the fuselage window.

3. The system of claim 1 , further comprising one or more lighting zones within the passenger suite, wherein:
each lighting zone of the one or more lighting zones includes one or more individually controllable illumination devices of the plurality of illumination devices; and
the one or more individually controllable illumination devices for each lighting zone are configured to output light in at least one of a different color and a different intensity of illumination than other zones of the one or more lighting zones.

4. The system of claim 1 , wherein the plurality of illumination devices is configured to modulate at least one of light intensity and light color in a predetermined pattern.

5. The system of claim 1 , wherein:
the static element includes an orifice disposed on an upper surface configured to provide a path for light to reach; and
the suite light sensor is located within a hollowed-out portion of the static element below the orifice.

6. The system of claim 5 , wherein the hollowed-out portion is positioned at a distance below the upper surface, wherein the distance is determined based at least in part on average illumination characteristics of one or more external lighting systems detectable by the suite light sensor at the distance.

7. The system of claim 5 , wherein the orifice is oriented at an angle from the suite light sensor configured to allows a greatest amount of light from one or more external lighting systems to enter the hollowed-out portion of the static element through the orifice.

8. The system of claim 1 , wherein the plurality of illumination devices includes at least two washlights, wherein the at least two washlights are configured to output light in a plurality of coordinated combinations of individual intensities of each of the at least two washlights, wherein the plurality of coordinated combinations is configured to represent a plurality of different colors of light.

9. The system of claim 1 , wherein the suite light sensor is configured to sense at least one of infrared, ultraviolet, and near-ultraviolet spectrum light.

10. The system of claim 1 , wherein the suite light sensor is configured to send and/or receive visible-light communication.

11. The system of claim 1 , further comprising a control panel in communication with the controller, the control panel configured to receive an adjustment setting for the ambient lighting system submitted by a passenger of the passenger suite.

12. The system of claim 1 , wherein the controller further includes control circuitry configured to adjust the illumination characteristics output by the plurality of illumination devices based on a sensed passenger status.

13. The system of claim 12 , wherein the sensed passenger status is based on at least one of i) one or more motion detectors proximate the passenger suite and ii) one or more pressure sensors disposed in the passenger suite proximate a passenger.

14. The system of claim 1 , wherein the suite light sensor includes a RGBW color sensor configured to sense an amount of red, green, blue, and white light.

15. A method for controlling an ambient lighting system within an aircraft passenger suite, the method comprising:
providing a plurality of illumination devices disposed within or proximate the aircraft passenger suite;
receiving, at a controller in communication with the plurality of illumination devices, a plurality of signals from at least one of a) a passenger entertainment computing system, b) a seating control computing system, and c) one or more presence sensors to detect at least one of movement and pressure;
identifying, by processing circuitry of the controller, a change of status of the passenger based on the plurality of signals;
receiving, from a light sensor associated with the passenger suite, signals identifying illumination characteristics of the passenger suite;
monitoring, by the processing circuitry, one or more external light sensors from an external lighting system, wherein the external lighting system comprises at least one of another passenger suite and another lighting zone;
determining, by the processing circuitry, at least one illumination characteristic of the external lighting system by weighting the plurality of other signals based on a relative proximity of each light sensor of the one or more external light sensors to the passenger suite; and
adjusting, based on the change of status, at least one of a light color, a light intensity, and a light modulation output by at least a portion of the plurality of illumination devices; and
wherein adjusting at least one of the light color, the light intensity, and the light modulation comprises adjusting further in part based upon the signals identifying illumination characteristics of the passenger suite and a plurality of other signals collected from at least one of the one or more external light sensors.

16. The method of claim 15 , wherein the change of status represents an activity level of the passenger.

17. The method of claim 15 , wherein:
identifying the change of status comprises determining the passenger has moved a passenger seat into a lie-flat position; and
adjusting comprises lowering light intensity for sleep conditions.

Assignees

• Be Aerospace Inc

Inventors

• Garing Francis Xavier L
• Pozzi Alexander Nicholas

Classifications

• B64D47/02

  Arrangements or adaptations of signal or lighting devices · CPC title

• B60Q3/80

  Circuits; Control arrangements (for dashboards B60Q3/16; for mass transit vehicles B60Q3/47) · CPC title

• B64D2011/0038

  Illumination systems for cabins as a whole · CPC title

• B60Q3/43

  General lighting · CPC title

• B64D11/00

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title