Aircraft interior light unit and method of operating an aircraft interior light unit

Patent metadata

Field	Value
Publication number	US-9731840-B2
Application number	US-201615210167-A
Country	US
Kind code	B2
Filing date	Jul 14, 2016
Priority date	Jul 17, 2015
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

An aircraft interior light unit having a light output over an extended light emission area includes a flat light distribution body having a front surface, through which the light output is coupled out, and a back surface, wherein at least one of the front surface and the back surface of the flat light distribution body has a plurality of surface irregularities.

First claim

The invention claimed is:

1. An aircraft interior light unit having a light output over an extended light emission area, comprising:
a flat light distribution body having a front surface, through which the light output is coupled out, and a back surface, wherein at least one of the front surface and the back surface of the flat light distribution body has a plurality of surface irregularities;
at least one general illumination LED positioned at a lateral outside of the flat light distribution body, with light emitted by the at least one general illumination LED being coupled into the flat light distribution body and being propagated within the flat light distribution body via total internal reflection at the front and back surfaces and with light from the at least one general illumination LED being re-directed at the plurality of surface irregularities for being coupled out of the flat light distribution body and for providing a general illumination over the extended light emission area;
a plurality of signalling LEDs being arranged outside of the flat light distribution body and facing towards the back surface of the flat light distribution body; and
a translucent panel arranged between the back surface of the flat light distribution body and the plurality of signalling LEDs, with light emitted from the plurality of signalling LEDs passing through the translucent panel and the flat light distribution body, forming high luminance spots in the light output.

2. An aircraft interior light unit according to claim 1 , wherein the back surface of the flat light distribution body has a plurality of surface irregularities, with light from the at least one general illumination LED being re-directed at the plurality of surface irregularities of the back surface for being coupled out of the flat light distribution body at the front surface thereof.

3. An aircraft interior light unit according to claim 1 , wherein the translucent panel is reflective on its side facing the flat light distribution body and wherein the front surface of the flat light distribution body has a plurality of surface irregularities, with light from the at least one general illumination LED being redirected at the plurality of surface irregularities of the front surface for being coupled out of the flat light distribution body at the back surface thereof, for being reflected at the translucent panel, and for being passed through the flat light distribution body and out of the front surface thereof.

4. An aircraft interior light unit according to claim 1 , wherein the translucent panel is a diffuse reflector, in particular a white diffuse reflector, on its side facing the flat light distribution body.

5. An aircraft interior light unit according to claim 1 , wherein the translucent panel diffusely passes light emitted by the plurality of signalling LEDs.

6. An aircraft interior light unit according to claim 1 , wherein the high luminance spots have an extension of at least 2 mm, in particular of between 5 mm and 10 mm, in the extended light emission area.

7. An aircraft interior light unit according to claim 1 , wherein the translucent panel passes between 1% and 10%, in particular between 2% and 5%, of the light emitted by the plurality of signalling LEDs.

8. An aircraft interior light unit according to claim 1 , wherein a luminance of the high luminance spots in the light output is between 2 times and 10 times as high as a luminance generated by the at least one general illumination LED in the light output.

9. An aircraft interior light unit according to claim 1 , wherein the translucent panel is made of rigid foam material.

10. An aircraft interior light unit according to claim 1 , wherein a distribution of the plurality of surface irregularities is such that a luminance distribution of the light output across the extended light emission area, generated by the at least one general illumination LED, has a ratio between its maximum luminance value and its minimum luminance value of at most 3.

11. An aircraft interior light unit according to claim 1 , wherein the plurality of surface irregularities comprises surface holes and/or wherein the plurality of surface irregularities comprises dots attached to the at least one of the front and back surfaces.

12. An aircraft interior light unit according to claim 1 ,
wherein the plurality of signalling LEDs are arranged in a set manner such that the high luminance spots convey predetermined signalling information to an aircraft passenger and/or aircraft crew member upon operation of the plurality of signalling LEDs, or
wherein the plurality of signalling LEDs are arranged in a grid and wherein the plurality of signalling LEDs are individually controllable, with the aircraft interior light unit being capable of providing different signalling information to an aircraft passenger and/or aircraft crew member via selective operation of different subsets of the plurality of signalling LEDs.

13. An aircraft interior light unit according to claim 1 , wherein the high luminance spots form at least one of a wash room usage sign, a fasten seat belt sign, a non-smoking sign, and a letter arrangement.

14. An aircraft, such as an air plane or a helicopter, having at least one aircraft interior light unit according to claim 1 , disposed in an interior of the aircraft for providing general illumination and for conveying signalling information to an aircraft passenger and/or aircraft crew member.

15. A method of operating an aircraft interior light unit having a flat light distribution body with a front surface and a back surface, wherein at least one of the front surface and the back surface has a plurality of surface irregularities, at least one general illumination LED positioned at a lateral outside of the flat light distribution body, a plurality of signalling LEDs arranged outside of the flat light distribution body and facing towards the back surface thereof, and a translucent panel arranged between the back surface of the flat light distribution body and the plurality of signalling LEDs, the method comprising the steps of:
providing a general illumination over an extended light emission area by operating the at least one general illumination LED, with light from the at least one general illumination LED being coupled into the flat light distribution body, being propagated therein via total internal reflection, and being re-directed at the plurality of surface irregularities for being coupled out of the flat light distribution body; and
providing signalling information to an aircraft passenger and/or air crew member by operating the plurality of signalling LEDs, with light emitted from the plurality of signalling LEDs passing through the translucent panel and the flat light distribution body, forming high luminance spots that jointly contain the signalling information.

Assignees

• Goodrich Lighting Systems Gmbh

Inventors

• Schoen Christian
• Schallenberg Bjoern

Classifications

• G09F2013/227

  Electroluminescent displays for vehicles · CPC title

• G09F2013/222

  with LEDs · CPC title

• G02B6/00

  Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings · CPC title

• G09F13/04

  Signs, boards or panels, illuminated from behind the insignia · CPC title

• G09F9/302 Primary

  characterised by the form or geometrical disposition of the individual elements · CPC title