Lighting system for an aircraft cabin

• US 5,677,603 A
• Filed: 12/23/1994
• Issued: 10/14/1997
• Est. Priority Date: 08/04/1994
• Status: Expired due to Fees

• Current Assignee: British Airways PLC (International Consolidated Airlines Group SA)
• Original Assignee: British Airways PLC (International Consolidated Airlines Group SA)
• Inventors: Speirs, Jonathan Laycock, Fozard, Anthony Roy
• Primary Examiner(s): Pascal, Robert
• Assistant Examiner(s): Kinkead, Arnold
• Application Number:
  US08/362,407
• Time in Patent Office: 1,026 Days
• Field of Search: 362/17, 362/18, 362/61, 362/16, 362/348, 362/62, 362/75, 362/32, 362/293, 307/10.8, 315/324, 315/76, 315/77, 315/307, 315/316, 315/317, 315/318, 315/291, 244/118.5, 359/889, 359/890, 250/227.11
• US Class Current: 315/324
• CPC Class Codes: B60Q 3/47 Circuits; Control arrangements
• CPC Class Codes: B60Q 3/66 for distributing light among several lighting devices
• CPC Class Codes: B60Q 3/80 Circuits; Control arrangements for dashboards B60Q3/16; for mass transit vehicles B60Q3/47
• CPC Class Codes: B60Q 3/85 for manual control of the light, e.g. of colour, orientation or intensity
• 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: F21S 10/005 using light guides light guides specially adapted for lighting devices G02B6/0001
• CPC Class Codes: F21S 10/007 using rotating transparent or colored disks, e.g. gobo wheels
• CPC Class Codes: F21S 10/02 changing colors F21S10/002 - F21S10/007, F21S10/04 take precedence
• CPC Class Codes: F21V 9/40 with provision for controlling spectral properties, e.g. colour, or intensity
• CPC Class Codes: H05B 47/155 Coordinated control of two or more light sources

Abstract

The lighting system for an aircraft cabin includes multiple illuminating units for distribution about a cabin. Each illuminating unit includes at least one variable light source providing light of a known characteristic and that is energizeable independently of other illuminating units. A controller controls energization of the illuminating units by way of dimming and switching units associated respectively with the illuminating units. The controller is operable to create different predetermined combinations of energizations of the illuminating units so that a desired lighting scene is created within the cabin by the energized illuminating units. The controller is arranged to effect a gradual transition to the energizations of the illuminating units when changing from one predetermined combination to another. As a result, there is a corresponding gradual change between scenes created in the cabin.

Claims

1. A lighting system for an aircraft cabin which simulates natural lighting transitions within a daily cycle, the system comprising:

a first illuminating unit for distributing light about the cabin, said first illuminating trait comprising at least one first light source providing light of a first known characteristic;

a second illuminating unit for distributing light about the cabin, said second illuminating unit comprising at least one second light source providing light of a second known characteristic different than that provided by said first light source in said first illuminating unit, said first and second illuminating units being energizable and controllable independently of each other; and

a controller for controlling energization of said first and second illuminating units, said controller being operable to create different predetermined combinations of energizations of said first and second illuminating units so that in use a first desired light scenic can be created within the cabin by energizing said first and second light sources of said first and second illuminating units to a respective first level of energization, and a second desired lighting scene can be created within the cabin by energizing said first and second light sources of said first and second illuminating units to a respective second level of energization, whereby different lighting scenes are created within the cabin at different times, and

said controller being arranged to effect a gradual transition between said first and second levels of energization of said first and second light sources in said first and second illuminating units when changing between said first desired lighting scene and said second desired lighting scene so that there is a corresponding gradual change between said first and second desired lighting scenes which simulates natural illumination in a sequence representing at least a portion of a full day to create a lighting atmosphere in the cabin which is comfortable and natural to a passenger.

2. A lighting system as claimed in claim 1, wherein at least one of said first and second light sources in said first and second illuminating units comprises a plurality of lamps.

3. A lighting system as claimed in claim 2, wherein, if one of said plurality of lamps fails, another of said plurality of lamps can be selected.

4. A lighting system as claimed in claim 1, wherein at least one of said first and second light sources in said first and second illuminating units comprises means for varying an intensity of light emitted therefrom.

5. A lighting system as claimed in claim 1, wherein at least one of said first and second light sources in said first and second illuminating units comprises a means for varying a color of light emitted therefrom.

6. A lighting system as claimed in claim 5, wherein said means for varying said color comprises a color wheel having a plurality of different color filters.

7. A lighting system as claimed in claim 1, wherein at least one of said first and second illuminating units comprises a light transmitting rod.

8. A lighting system as claimed in claim 7, wherein said light transmitting rod is arranged to emit light substantially from a side wall thereof.

9. A lighting system as claimed in claim 7, wherein said light transmitting rod is arranged to emit light substantially from an end face thereof.

10. A lighting system as claimed in claim 1, wherein at least one of said first and second illuminating units comprises a fiber optic.

11. A lighting system as claimed in claim 10, wherein said fiber optic is arranged to emit light substantially from a side wall thereof.

12. A lighting system as claimed in claim 10, wherein said fiber optic is arranged to emit light substantially from an end face thereof.

13. A lighting system as claimed in claim 1, wherein at least one of said first and second illuminating units comprises a patterned light obstructing member for causing a section of said patterned light obstructing member in use to emit a pattern of shadow and light.

14. A lighting system as claimed in claim 13, wherein said pattern of said patterned light obstructing member is irregular.

15. A lighting system as claimed in claim 13, wherein said pattern of said patterned light obstructing member is graphical.

16. A lighting system as claimed in claim 13, wherein said patterned light obstructing member comprises a gobo.

17. A lighting system as claimed in claim 13, wherein said patterned light obstructing member comprises a liquid crystal screen.

18. A lighting system as claimed in claim 17, wherein said liquid crystal screen comprises a size sufficient to at least partly partition the cabin.

19. A lighting system as claimed in claim 1, wherein at least one of said first and second illuminating units comprises means for capturing natural light from outside the cabin for use as a respective one of said first and second light sources.

20. A lighting system as claimed in claim 1, wherein said controller comprises a memory for storing data defining each of said first and second desired lighting scenes and a processor for effecting operation of said controller in accordance with said stored data.

21. A lighting system as claimed in claim 20, further comprising:

means for generating said data off-line and for down loading said data to said memory.

22. A lighting system as claimed in claim 21, wherein said means for generating said data comprises a computer.

23. A lighting system as claimed in claim 20, wherein time of transition data defining a time of a transition from one scene to another lighting scene is stored in said memory.

24. A lighting system as claimed in claim 1, wherein said controller is further operable to create sets of scenes selectable for use during a given type of flight, wherein said sets of scenes contain predetermined ones of said different lighting scenes.

25. A lighting system as claimed in claim 24, further comprising:

a display for displaying information identifying different lighting scenes in a first set of scenes selected from said sets of scenes.

26. A lighting system as claimed in claim 25, further comprising:

user operable selecting means for selecting a scene from said first set of scenes, wherein said selected scene is to be created in the cabin.

27. A lighting system as claimed in claim 26, wherein said selecting means comprises an array of push buttons, said controller being responsive to actuation of said push buttons.

28. A lighting system as claimed in claim 26, wherein said display comprises a touch sensitive screen which serves as said a operable selecting means.

29. A method of lighting an aircraft cabin which simulates natural lighting transitions within a daily cycle, the method comprising the steps of:

installing in the cabin a first illuminating unit comprising at least one first light source providing light of a first known characteristic together with a second illuminating unit comprising at least one second light source providing light of a second known characteristic different than that provided by said first light source in said first illuminating unit, said first and second illuminating units being installed so as to be energizable and controllable independently of each other; and

controlling energization of said first and second illuminating units to create different predetermined combinations of energizations of said first and second illuminating units so that a first desired lighting scene is created within the cabin when said first and second light sources of said first and second illuminating units are energized to a respective first level of energization and a second desired lighting scene is created within the cabin when said first and second light sources of said first and second illuminating units are energized to a respective second level of energization,

whereby different lighting scenes are created within the cabin at different times, and wherein a gradual transition between said first and second levels of energization of said first and second light sources in said first and second illuminating units is effected when changing between said first desired lighting scene and said second desired lighting scene so that there, is a corresponding gradual change between said first and second desired lighting scenes which simulates natural illumination in a sequence representing at least a portion of a full day to create a lighting atmosphere in the cabin which is comfortable and natural to a passenger.

30. A method as claimed in claim 29, further comprising the steps of:

dividing the cabin into a plurality of zones each containing at least one of said first and second illuminating units; and

controlling the energization of at least one of said first and second illuminating units in each of said plurality of zones individually so as to create different lighting scenes for different zones within the cabin.

31. A method as claimed in claim 29, further comprising the steps of:

varying an intensity of light emitted from at least one of said first and second light sources.

32. A method as claimed in claim 29, further comprising the steps of:

varying a color of light emitted from at least one of said first and second light sources.

33. A lighting system for an aircraft cabin which simulates natural lighting transitions within a daily cycle, the system comprising:

a first plurality of illuminating units for distribution about a cabin, each of said first plurality of illuminating units comprising a first light source providing light of a first known characteristic;

a second plurality of illuminating units for distribution about the cabin, each of said second plurality of illuminating units comprising a second light source providing light of a second known characteristic different than said first known characteristic, wherein said first plurality of illuminating units are energizable independently of said second plurality of illuminating units; and

a controller for controlling an energization of said first plurality of illuminating units, said controller being operable to create different predetermined combinations of energizations of said first plurality of illuminating units so that in use multiple different lighting scenes and subsets of scenes containing predetermined ones of said multiple different lighting scenes are selectable for use during a given type of flight, wherein said multiple different lighting scenes are created within the cabin by energization of said first plurality of illuminating units in accordance with one of said different predetermined combinations of energizations, said controller being arranged to effect a gradual transition of energizations of said first plurality of illuminating units when changing from one predetermined combination of energizations to another predetermined combination of energizations so that there is a corresponding gradual change between said multiple different lighting scenes which simulates natural illumination in a sequence representing at least a portion of a full day to create a lighting atmosphere in the cabin which is comfortable and natural to a passenger.

34. A lighting system for an aircraft cabin which simulates natural lighting transitions within a daily cycle, the system comprising:

a first plurality of illuminating units for distribution about a cabin, each of said first plurality of illuminating units comprising a first light source providing light of a first known characteristic;

a second plurality of illuminating units for distribution about the cabin, each of said second plurality of illuminating units comprising a second light source providing light of a second known characteristic different than said first known characteristic, wherein said first plurality of illuminating units are energizable independently of said second plurality of illuminating units and at least one illuminating unit in said first and second plurality of illuminating units comprises means for capturing natural light from outside the cabin as one of said first and second light source; and

a controller for controlling an energization of said first plurality of illuminating units, said controller being operable to create different predetermined combinations of energizations of said first plurality of illuminating units so that in use a desired lighting scene is created within the cabin by energization of said first plurality of illuminating units in accordance with one of said different predetermined combinations of energizations, and said controller being arranged to effect a gradual transition of energizations of said first plurality of illuminating units when changing from one predetermined combination of energizations to another predetermined combination of energizations so that there is a corresponding gradual change between scenes which simulates natural illumination in a sequence representing at least a portion of a full day to create a lighting atmosphere in the cabin which is comfortable and natural to a passenger.