Aircraft air duct system for transmitting electrical power and visible light

Patent metadata

Field	Value
Publication number	US-11230383-B2
Application number	US-202016782473-A
Country	US
Kind code	B2
Filing date	Feb 5, 2020
Priority date	Feb 5, 2020
Publication date	Jan 25, 2022
Grant date	Jan 25, 2022

Abstract

An air duct system comprising an air duct having a main body, a visible light source, and one or more photovoltaic devices. The main body of the air duct defines a passageway having a reflective inner surface. The visible light source is configured to generate visible light, where the visible light source directs the visible light along the reflective inner surface of the air duct. The one or more photovoltaic devices are disposed along the reflective inner surface of the air duct, where a portion of the visible light generated by the visible light source is converted into electrical power by the one or more photovoltaic devices.

First claim

What is claimed is:

1. An air duct system, comprising:
an air duct having a main body, wherein the main body of the air duct defines a passageway having a reflective inner surface;
a visible light source configured to generate visible light, wherein the visible light source directs the visible light along the reflective inner surface of the air duct; and
one or more photovoltaic devices disposed along the reflective inner surface of the air duct, wherein a portion of the visible light generated by the visible light source is converted into electrical power by the one or more photovoltaic devices.

2. The air duct system of claim 1 , further comprising one or more lighting apertures disposed along the main body of the air duct, wherein a portion of the visible light generated by the visible light source exits the air duct through the one or more lighting apertures.

3. The air duct system of claim 2 , further comprising an ultraviolet light source configured to generate ultraviolet light, wherein the ultraviolet light source directs the ultraviolet light along the reflective inner surface of the air duct.

4. The air duct system of claim 3 , further comprising one or more ultraviolet optical filters, wherein an ultraviolet optical filter is placed over each of the one or more lighting apertures.

5. The air duct system of claim 4 , wherein the ultraviolet light includes a germicidal wavelength ranging from 185 to 400 nanometers.

6. The air duct system of claim 1 , further comprising one or more air valves disposed along the main body of the air duct.

7. The air duct system of claim 1 , wherein the visible light source comprises an array of light-emitting diodes (LEDs).

8. The air duct system of claim 1 , wherein the visible light emitted from the visible light source has an angle of divergence of ten degrees or less.

9. The air duct system of claim 1 , wherein the reflective inner surface of the main body of the air duct includes a reflectance of at least fifty percent.

10. The air duct system of claim 1 , wherein the reflective inner surface of the main body of the air duct includes a reflectance of at least ninety-nine percent.

11. The air duct system of claim 1 , further comprising a thermoelectric generator having a hot side and a cold side, wherein the hot side of the thermoelectric generator is positioned along an outer surface of the air duct.

12. The air duct system of claim 11 , wherein the thermoelectric generator is cooled by natural convection, forced convection, or solid conduction.

13. A method for transmitting air, visible light, and electrical power through an air duct of an aircraft, the method comprising:
receiving, by the air duct, conditioned air, and visible light;
directing the visible light along a reflective inner surface of the air duct, wherein the visible light reflects off of the reflective inner surface and travels along a passageway of the air duct; and
converting a portion of the visible light into electrical power by one or more photovoltaic devices disposed along the reflective inner surface of the air duct.

14. The method of claim 13 , further comprising:
allowing a portion of the visible light to exit the air duct through one or more lighting apertures disposed along a main body of the air duct.

15. The method of claim 13 , further comprising:
releasing the conditioned air by one or more air valves disposed along a main body of the air duct.

16. The method of claim 13 , further comprising:
directing ultraviolet light along the reflective inner surface of the air duct.

17. The method of claim 16 , wherein the ultraviolet light includes a germicidal wavelength ranging from 185 to 400 nanometers.

18. The method of claim 13 , wherein the visible light emitted from the visible light source has an angle of divergence of ten degrees or less.

19. The method of claim 13 , wherein the reflective inner surface of the air duct includes a reflectance of at least fifty percent.

20. The method of claim 13 , wherein the reflective inner surface of the air duct includes a reflectance of at least ninety-nine percent.

21. The method of claim 13 , wherein the air duct further comprises one or more air valves disposed along a main body of the air duct.

Assignees

• Boeing Co

Inventors

• Hiller Nathan D

Classifications

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• F21V7/0008 Primary

  providing for indirect lighting · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title

• F21V9/06

  for filtering out ultraviolet radiation · CPC title

• F21Y2115/10

  Light-emitting diodes [LED] · CPC title