Aircraft air duct system for transmitting electrical power and visible light

Patent metadata

Field	Value
Publication number	US-11535384-B2
Application number	US-202117552675-A
Country	US
Kind code	B2
Filing date	Dec 16, 2021
Priority date	Feb 5, 2020
Publication date	Dec 27, 2022
Grant date	Dec 27, 2022

Abstract

An air duct system comprising an air duct having a main body, a visible light source, an emitter configured to emit radio frequency waves, and one or more antennas. 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. The visible light source directs the visible light along the reflective inner surface of the air duct. The emitter directs the radio frequency waves along the reflective inner surface of the air duct. The one or more antennas are each connected to a corresponding power harvesting circuit, where the radio frequency waves are received by the one or more antennas and are converted into electrical power by the corresponding power harvesting circuit.

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;
an emitter configured to emit radio frequency waves, wherein the emitter directs the radio frequency waves along the reflective inner surface of the air duct; and
one or more antennas that are each connected to a corresponding power harvesting circuit, wherein the radio frequency waves are received by the one or more antennas and are converted into electrical power by the corresponding power harvesting circuit.

2. The air duct system of claim 1 , wherein the corresponding power harvesting circuit includes an impedance matching network, a combined rectifier and voltage multiplier, and a power management module.

3. The air duct system of claim 2 , wherein the impedance matching network is configured to transform an impedance of the one or more antennas into a transmission impedance of the corresponding power harvesting circuit.

4. The air duct system of claim 2 , wherein the combined rectifier and voltage multiplier is configured to convert the radio frequency waves into direct current (DC) power.

5. 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.

6. The air duct system of claim 5 , 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.

7. The air duct system of claim 6 , further comprising one or more ultraviolet optical filters, wherein an ultraviolet optical filter is placed over each of the one or more lighting apertures.

8. The air duct system of claim 6 , wherein the ultraviolet light includes a germicidal wavelength ranging from 185 to 400 nanometers.

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

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 fifty percent.

11. 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.

12. The air duct system of claim 1 , wherein the reflective inner surface of the air duct reflects the radio frequency waves.

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

14. The air duct system of claim 13 , wherein each LED of the array of LEDs emit white light at ten kilowatts.

15. The air duct system of claim 1 , wherein the visible light source includes an array of lamps, wherein each lamp of the array of lamps emit a light beam.

16. The air duct system of claim 15 , wherein the array of lamps include parabolic aluminized reflector lamps.

17. The air duct system of claim 1 , wherein the reflective inner surface is coated with one of the following: an optical supermirror, a Bragg grating, photonic crystal, and nanostructured materials.

18. 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;
emitting radio frequency waves by an emitter, wherein the radio frequency waves are directed along the reflective inner surface of the air duct;
receiving the radio frequency waves by one or more antennas, wherein the one or more antennas are each connected to a corresponding power harvesting circuit; and
converting the radio frequency waves are into electrical power by the corresponding power harvesting circuit.

19. The method of claim 18 , 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.

20. The method of claim 18 , further comprising:
releasing the conditioned air by one or more air valves disposed along a main body of the air duct.

Assignees

• Boeing Co

Inventors

• Hiller Nathan D

Classifications

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• F21W2107/30

  for aircraft · CPC title

• B64D2013/0644

  including electric motors or generators · CPC title

• B60Q3/41

  for mass transit vehicles, e.g. buses · CPC title

• F21V9/06

  for filtering out ultraviolet radiation · CPC title