Aircraft Interior Surface and Method of Illuminating an Aircraft Interior Surface

Patent metadata

Field	Value
Publication number	US-2017283065-A1
Application number	US-201715478568-A
Country	US
Kind code	A1
Filing date	Apr 4, 2017
Priority date	Apr 4, 2016
Publication date	Oct 5, 2017
Grant date	—

Abstract

An aircraft interior surface for partitioning, dividing, or establishing privacy within a cabin space includes a transparent material that provides for transmission of light within the aircraft cabin. A graphical design may be applied to the transparent material, the graphical design including indicia arranged in predetermined patterns based on a location or function of the transparent material. A light source located proximate to the transparent material may wash light across a surface of the transparent material such that the graphical design exhibits predetermined properties when illuminated by the light source. The transparent material may be selectively dimmable to increase opacity.

First claim

What is claimed is:

1 . An aircraft partition, comprising:
a panel or frame portion residing substantially in a first plane, the panel or frame portion being opaque and constructed of a material that does not transmit visible light; a planar dimmable portion, the dimmable portion being substantially co-planar with the panel or frame portion, the dimmable portion configured to operate in a transparent condition and in an opaque condition, the dimmable portion further being located to permit crew line of sight through the partition system when the dimmable portion is in the transparent condition; control circuitry communicatively coupled to the dimmable portion comprising processing circuitry, and a non-transitory computer readable medium having instructions stored thereon, wherein the instructions, when executed by the control circuitry, cause the control circuitry to receive at least one selection from a computing device related to a dimmable panel setting and translate the at least one setting into at least one control signal to switch the dimmable portion between the transparent condition and the opaque condition.

2 . The aircraft partition of claim 1 , further comprising a graphical design element applied to the dimmable portion.

3 . The aircraft partition of claim 2 , further comprising a light source disposed in the panel or frame portion.

4 . The aircraft partition of claim 3 , wherein the light source is configured to illuminate the graphical design element.

5 . The partition of claim 2 , wherein the graphical design element includes retail or branded content.

6 . The aircraft partition of claim 1 , wherein the control circuitry is configured to set the dimmable panel to at least two selectable opacities, said opacities being at least 70 percent.

7 . The aircraft partition of claim 1 , wherein the control circuitry is configured to set the panel to a transparent condition during taxi, take-off and landing.

8 . The aircraft partition of claim 1 , wherein the panel or frame portion at least partially separates a passenger suite from an adjacent aisle region.

9 . The aircraft partition of claim 1 , wherein the panel or frame portion at least partially separates a fore cabin of an aircraft from an aft cabin of an aircraft.

10 . The partition of claim 1 , wherein the panel or frame portion at least partially separates a passenger suite from an adjacent passenger suite.

11 . The partition of claim 1 , wherein the transparent portion comprises electronic glass.

12 . The partition of claim 11 , wherein the electronic glass material comprises an electrochromic layer.

13 . An aircraft partition, comprising:
a panel or frame portion residing substantially in a first plane, the panel or frame portion being opaque and constructed of a material that does not transmit visible light; a planar non-opaque portion, the non-opaque portion being substantially co-planar with the panel or frame portion, non-opaque portion further being located to permit crew line of sight through the partition; a graphical design element applied to the non-opaque portion; and a light source disposed in the panel or frame portion and configured to illuminate the graphical design element.

14 . The aircraft partition of claim 13 , wherein the non-opaque portion comprises a planar dimmable portion configured to operate in a transparent condition and in an opaque condition, the dimmable portion further being located to permit crew line of sight through the partition system when the dimmable portion is in the transparent condition.

15 . The aircraft partition of claim 14 , further comprising control circuitry communicatively coupled to the dimmable portion comprising processing circuitry, and a non-transitory computer readable medium having instructions stored thereon, wherein the instructions, when executed by the control circuitry, cause the control circuitry to receive at least one selection from a computing device related to a dimmable panel setting and translate the at least one setting into at least one control signal to switch the dimmable portion between the transparent condition and the opaque condition.

16 . The aircraft partition of claim 15 , wherein the control circuitry is configured to set the dimmable panel to at least two selectable opacities, said opacities being at least 70 percent.

17 . The aircraft partition of claim 15 , wherein the control circuitry is configured to set the panel to a transparent condition during taxi, take-off and landing.

18 . The aircraft partition of claim 13 , wherein the panel or frame portion at least partially separates a passenger suite from an adjacent aisle region.

19 . The aircraft partition of claim 13 , wherein the panel or frame portion at least partially separates a fore cabin of an aircraft from an aft cabin of an aircraft.

20 . The aircraft partition of claim 13 , wherein the panel or frame portion at least partially separates a passenger suite from an adjacent passenger suite.

21 . The aircraft partition of claim 13 , wherein the graphical design element includes retail or branded content.

22 . The partition of claim 14 , wherein the transparent portion comprises electronic glass.

23 . The partition of claim 22 , wherein the electronic glass material comprises an electrochromic layer.

Assignees

• Be Aerospace Inc

Inventors

• Papke Robert
• Claflin Shawn
• Lightbody Stephanie
• Mckee Jefferey

Classifications

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• G09F21/06 Primary

  by aeroplanes, airships, balloons, or kites · CPC title

• E06B2009/2464

  featuring transparency control by applying voltage, e.g. LCD, electrochromic panels · CPC title

• B64D11/0606 Primary

  with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title

• E06B2009/2417

  Light path control; means to control reflection · CPC title