Methods and devices for light distribution in an aircraft, and aircraft including such devices

• US 10,384,803 B2
• Filed: 10/07/2016
• Issued: 08/20/2019
• Est. Priority Date: 10/07/2016
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hills, Karen L., McMullin, Dianne Lynn, Camp, III, Randolph C., Valentine, Jr., William Hanson, Brown, Douglas Alan, Green, Rush Frederick, Simms, Richard K., Rezmer, Jennifer J., Burgess, Michael Joseph
• Primary Examiner(s): Badawi, Medhat
• Application Number:
  US15/288,126
• Publication Number:
  US 20180099763A1
• Time in Patent Office: 1,047 Days
• 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: B64D 2203/00 Aircraft or airfield lights using LEDs
• CPC Class Codes: B64D 47/02 Arrangements or adaptations of signal or lighting devices
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

Lighting components for illuminating an aisle portion of a cabin floor of an aircraft, and aircraft and passenger seats for an aircraft including the same are disclosed. Said lighting components are configured to illuminate at least a portion of the aisle, between adjacent passenger seats positioned on either side of the aisle. The lighting components are configured to direct light towards the cabin floor using a specially designed housing and reflector surface that are designed to illuminate objects in the aisle, while minimizing light pollution in the cabin and detection by passengers on board the aircraft. Said lighting components are optionally mounted on one or more passenger seats, and/or may be integrally formed with a passenger seat. Lighting components include a curved reflector surface configured to reflect light from a light source positioned within the housing such that it is directed towards the aisle to create the desired illumination.

Claims

1. A passenger aircraft, comprising:

a cabin floor within a passenger cabin of the passenger aircraft, wherein the cabin floor comprises an aisle having an aisle width;

a plurality of passenger seats arranged on the cabin floor, forming one or more rows of adjacent passenger seats; and

a plurality of lighting components for illuminating the cabin floor of the passenger aircraft, each respective lighting component of the plurality of lighting components comprising;

a housing defining a cavity and including a light channel configured to allow light to exit the housing, wherein the housing restricts light from exiting the housing other than through the light channel;

a light source contained within the cavity of the housing and configured to emit visible light towards the light channel, wherein the light source creates a light pattern on the aisle of the cabin floor, and wherein the light pattern has a width cone that is sufficient to span the aisle width;

a reflector surface configured to reflect visible light emanating from the light source through the light channel and towards the cabin floor of the passenger aircraft, wherein the reflector surface is curved and at least partially defines the light channel, and wherein the reflector surface is substantially concave facing the light channel of the lighting component; and

an optical absorber surface arranged with respect to the reflector surface such that the optical absorber surface is configured to restrict visible light emanating from the light source from exiting the light channel in a direction towards a cabin ceiling opposite the cabin floor of the passenger aircraft, wherein the optical absorber surface of each respective lighting component is substantially convex facing the light channel, and wherein each respective lighting component is coupled to a respective passenger seat of the plurality of passenger seats.

2. The passenger aircraft according to claim 1, wherein the optical absorber surface of each respective lighting component is arranged opposite the reflector surface of the respective lighting component, and wherein the light channel of each respective lighting component is defined between the optical absorber surface and the reflector surface of the respective lighting component.

3. The passenger aircraft according to claim 1, wherein each respective light channel extends longitudinally from a respective first end region of a respective housing to a respective second end region of the respective housing and wherein the respective reflector surface extends longitudinally from the respective first end region of the respective housing to the respective second end region of the respective housing.

4. The passenger aircraft according to claim 1, wherein a first portion of the plurality of passenger seats and a second portion of the plurality of passenger seats are arranged on either side of the aisle of the cabin floor with respect to each other, wherein each respective lighting component is configured to illuminate a respective portion of the aisle extending between respective passenger seats positioned on either side of the aisle.

5. The passenger aircraft according to claim 4, wherein each respective lighting component is configured to provide substantially uniform illumination of the respective portion of the aisle of the cabin floor between a first respective passenger seat of the plurality of passenger seats, to which the lighting component is coupled, and a second respective passenger seat of the plurality of passenger seats, wherein the first respective passenger seat and the second respective passenger seat are separated by the aisle.

6. The passenger aircraft according to claim 4, wherein each respective lighting component is configured to illuminate objects on or protruding into the respective portion of the aisle of the cabin floor, within a zone of mesopic vision.

7. The passenger aircraft according to claim 4, wherein each respective lighting component is mounted on a respective passenger seat of the passenger aircraft without protruding into the aisle.

8. The passenger aircraft according to claim 1, wherein each respective light source comprises an LED.

9. The passenger aircraft according to claim 1, wherein the reflector surface is configured such that selection of one or more reflector variable values relative to one another creates a predetermined light pattern reflected onto the cabin floor of the passenger aircraft, wherein the one or more reflector variables comprise a reflector radius, a reflector conic constant, a horizontal displacement of the reflector surface relative to the light source, a reflector length, a reflector width, and a vertical displacement of the reflector surface relative to the light source.

10. The passenger aircraft according to claim 1, wherein each respective reflector surface comprises a specular adhesive film.

11. A system for illuminating a cabin floor of a passenger aircraft, the system comprising:

a plurality of lighting components, each lighting component comprising;

a housing, wherein the housing defines a cavity and a light channel configured to allow light to exit the housing, wherein the housing restricts light from exiting the housing other than through the light channel;

a light source contained within the cavity of the housing and configured to emit visible light towards the light channel, wherein the light source creates a light pattern on an aisle of the cabin floor, and wherein the light pattern has a width cone that is sufficient to span an aisle width of the aisle of the cabin floor;

a reflector surface configured to reflect visible light emanating from the light source through the light channel and towards the cabin floor of the passenger aircraft, wherein the reflector surface is curved and forms a portion of the light channel, and wherein the reflector surface is substantially concave facing the light channel of the lighting component; and

an optical absorber surface arranged with respect to the reflector surface such that the optical absorber surface is configured to restrict visible light emanating from the light source from exiting the light channel in a direction towards a cabin ceiling opposite the cabin floor of the passenger aircraft, wherein the optical absorber surface of each respective lighting component is substantially convex facing the light channel; and

a plurality of passenger seats positioned within the passenger aircraft, wherein each passenger seat of the plurality of passenger seats includes a respective lighting component of the plurality of lighting components.

12. The system according to claim 11, further comprising:

a first plurality of passenger seats arranged on a first side of the aisle of the cabin floor of the passenger aircraft; and

a second plurality of passenger seats arranged on a second side of the aisle, wherein the first side of the aisle is opposite the second side of the aisle, wherein the first plurality of passenger seats and the second plurality of passenger seats are positioned with respect to one another to form a plurality of rows of passenger seats such that the aisle is positioned between the first plurality of passenger seats and the second plurality of passenger seats, and wherein the plurality of lighting components comprises one respective lighting component per row of passenger seats.

13. A method for illuminating a cabin floor of a passenger aircraft, the method comprising:

powering a plurality of lighting components using one or more selected from the group consisting of a battery, a capacitor, solar energy, an electrical system of the passenger aircraft, and energy harvesting, wherein each lighting component of the plurality of lighting components comprises;

a housing, wherein the housing defines a cavity and a light channel configured to allow light to exit the housing, wherein the housing restricts light from exiting the housing other than through the light channel;

a light source contained within the cavity of the housing and configured to emit visible light towards the light channel;

a reflector surface configured to reflect light emanating from the light source through the light channel and towards the cabin floor of the passenger aircraft, wherein the reflector surface is curved and forms a portion of the light channel, and wherein the reflector surface is substantially concave facing the light channel of the lighting component; and

an optical absorber surface arranged with respect to the reflector surface such that the optical absorber surface is configured to restrict visible light emanating from the light source from exiting the light channel in a direction towards a cabin ceiling opposite the cabin floor of the passenger aircraft, wherein the optical absorber surface of each respective lighting component is substantially convex facing the light channel; and

forming a light pattern on an aisle portion of the cabin floor using the plurality of lighting components, wherein the light pattern has a width cone that is sufficient to span an aisle width of the aisle portion of the cabin floor.

14. The method according to claim 13, further comprising integrating a respective lighting component of the plurality of lighting components into one or more respective passenger seats of the passenger aircraft.

15. The method according to claim 13, further comprising delivering a passenger seat that includes a respective lighting component of the plurality of lighting components integrated within the passenger seat.

16. The method according to claim 13, further comprising illuminating objects in or protruding into the aisle portion of the cabin floor of the passenger aircraft using the plurality of lighting components.