Plasma aviation antenna

Patent metadata

Field	Value
Publication number	US-10276930-B2
Application number	US-201615237825-A
Country	US
Kind code	B2
Filing date	Aug 16, 2016
Priority date	May 13, 2013
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

An aircraft communications system may include a RF-transparent enclosure, a plasma antenna element and a controller. The RF-transparent enclosure may be disposed substantially conformal with a portion of the aircraft. The plasma antenna element may be housed within the RF-transparent enclosure. The controller may be operably coupled to the plasma antenna element to provide control of operation of the plasma antenna element. The plasma antenna element may include one or more RF-conductive plasma devices that are selectively ionized to a plasma state under control of the controller.

First claim

What is claimed is:

1. An aircraft window comprising:
an enclosure configured to be provided in a window opening of an aircraft;
a receiving space defined in the enclosure; and
a plasma antenna element provided within the receiving space, the plasma antenna element being operably coupled to a controller to provide control of operation of the plasma antenna element over a selectable range of frequencies, the plasma antenna element including one or more RF-conductive plasma discharge tubes that are selectively ionizable to a plasma state under control of the controller,
wherein the controller is operably coupled to one or more switching devices, the one or more switching devices modulating application of power to the plasma antenna element during ionization of the plasma antenna element.

2. The aircraft window of claim 1 , wherein the plasma antenna element is controlled by the controller to facilitate beam steering.

3. The aircraft window of claim 1 , wherein the switching devices modulate the application of power to provide sufficient energy to ionize gas to a plasma state when the plasma antenna element is functionally on, and modulate the application of power to provide insufficient energy to ionize the gas to the plasma state when the plasma antenna element is functionally off.

4. The aircraft window of claim 1 , wherein the aircraft window is a cockpit window.

5. The aircraft window of claim 1 , wherein the aircraft window is an aircraft side window.

6. The aircraft window of claim 1 , wherein the controller is configured to alternately tune the plasma antenna element to be reflective or absorptive of multiple frequencies.

7. The aircraft window of claim 1 , wherein the controller is configured to scan a plurality of frequencies and tune the plasma antenna element to a targeted frequency identified during the scan.

8. The aircraft window of claim 1 , further comprising a plurality of plasma antenna elements, wherein the controller is configured to ionize selected ones of the plurality of plasma antenna elements to define an array of a desired length.

9. The aircraft window of claim 1 , wherein the one or more switching devices are switchable in nanoseconds.

10. The aircraft window of claim 9 , wherein the one or more switching devices are configured to enable fast switching to enable the plasma antenna element to communicate with multiple devices using time-division duplex.

11. An apparatus comprising:
an enclosure;
a controller; and
a plasma antenna element provided within the enclosure, the plasma antenna element being operably coupled to the controller to provide control of operation of the plasma antenna element over a selectable range of frequencies, the plasma antenna element including one or more RF-conductive plasma discharge tubes that are selectively ionizable to a plasma state under control of the controller,
wherein the controller is operably coupled to one or more switching devices, the one or more switching devices modulating application of power to the plasma antenna element during ionization of the plasma antenna element.

12. The apparatus of claim 11 , wherein the plasma antenna element is controlled by the controller to facilitate beam steering.

13. The apparatus of claim 11 , wherein the switching devices modulate the application of power to provide sufficient energy to ionize gas to a plasma state when the plasma antenna element is functionally on, and modulate the application of power to provide insufficient energy to ionize the gas to the plasma state when the plasma antenna element is functionally off.

14. The apparatus of claim 11 , wherein the apparatus is an aircraft cockpit window.

15. The apparatus of claim 11 , wherein the apparatus is an aircraft side window.

16. The apparatus of claim 11 , wherein the controller is configured to alternately tune the plasma antenna element to be reflective or absorptive of multiple frequencies.

17. The apparatus of claim 11 , wherein the controller is configured to scan a plurality of frequencies and tune the plasma antenna element to a targeted frequency identified during the scan.

18. The apparatus of claim 11 , further comprising a plurality of plasma antenna elements, wherein the controller is configured to ionize selected ones of the plurality of plasma antenna elements to define an array of a desired length.

19. The apparatus of claim 11 , wherein the one or more switching devices are switchable in nanoseconds.

20. The apparatus of claim 19 , wherein the one or more switching devices are configured to enable fast switching to enable the plasma antenna element to communicate with multiple devices using time-division duplex.

Assignees

• Smartsky Networks LLC

Inventors

• Stone Ryan Mitchell
• Eskridge Jr Elbert Stanford

Classifications

• H01Q1/26

  with electric discharge tube · CPC title

• H01Q1/1271

  for mounting on windscreens · CPC title

• H01Q1/366 Primary

  using an ionized gas · CPC title

• H01Q1/286

  substantially flush mounted with the skin of the craft · CPC title

• H01Q3/22

  varying the orientation in accordance with variation of frequency of radiated wave · CPC title