Antenna element with high gain toward the horizon

Patent metadata

Field	Value
Publication number	US-9293830-B2
Application number	US-201414208656-A
Country	US
Kind code	B2
Filing date	Mar 13, 2014
Priority date	Mar 13, 2013
Publication date	Mar 22, 2016
Grant date	Mar 22, 2016

Abstract

An air-to-ground network communication device may include a conductive groundplane and an antenna element. The conductive groundplane may be disposed to be substantially parallel to a surface of the earth. The antenna element may extend substantially perpendicularly away from the groundplane and may have an effective length between about 1λ to about 1.5λ. The antenna element may be disposed at a distance of about 0.5λ to about 1λ from the groundplane.

First claim

What is claimed is:

1. An air-to-ground network communication device, the device comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane,
wherein the antenna element comprises a dipole element.

2. The device of claim 1 , wherein the effective length of the antenna element is about 1.2λ and the distance from the groundplane is about 0.68λ.

3. The device of claim 1 , wherein the groundplane is formed at a skin of an aircraft.

4. The device of claim 1 , wherein the groundplane is formed at a platform of a ground transmission station.

5. An air-to-ground network communication device, the device comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the goundplane,
wherein the antenna element comprises a Vivaldi-antenna.

6. An air-to-ground network communication device, the device comprising:
a conduction groundplane disposed to be substantially parallel to a surface of the earth; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane,
wherein the antenna element comprises non-linear shaped elements.

7. An air-to-ground network communication device, the device comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth;
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ about 1 λ from the groundplane; and
an impedance matcher operable coupled to the antenna element to cancel reactive components of impedance of the antenna element.

8. The device of claim 7 , wherein the impedance matcher is operably coupled to the antenna controller that is configured to enable modification of the impedance matcher to cancel different reactive component values associated with different switchable antenna element configurations of the antenna element.

9. An air-to-ground network communication device, the device comprising:
a conductive groundplane disposed to the substantially parallel to a surface of the earth; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane,
wherein the antenna element includes switchable components that are configured to be arranged in at least two different configurations that each have the effective length between about 1λ to about 1.5λ.

10. A mobile platform comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth while the mobile platform is in motion; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane,
wherein the antenna element comprises a dipole element.

11. A mobile platform of claim 10 , wherein the effective length of the antenna element is about 1.2λ and the distance from the groundplane is about 0.68λ.

12. The mobile platform of claim 10 , wherein the groundplane is formed at a skin of an aircraft.

13. The mobile platform of claim 10 , wherein the groundplane extends for at least three feet in every direction away from the antenna element.

14. The mobile platform comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth while the mobile platform is in motion; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ from the groundplane,
wherein the antenna element comprises a Vivaldi-antenna.

15. The mobile platform comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth while the mobile platform is in motion; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane,
wherein the antenna element comprises non-linear shaped elements.

16. A mobile platform comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth while the mobile platform is in motion;
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane; and
an impedance matcher operable coupled to the antenna element to cancel reactive components of impedance of the antenna element.

17. The mobile platform of claim 16 , wherein the impedance matcher is operable coupled to an antenna controller that is configured to enable modification of the impedance matcher to cancel different reactive component values associated with different switchable antenna element configurations of the antenna element.

18. A mobile platform comprising:
a conductive groundplane disposed to be substantially parallel to a surface of the earth while the mobile platform is in motion; and
an antenna element having an omni-directional radiation pattern, the antenna element extending substantially perpendicularly away from the groundplane and having an effective length between about 1λ to about 1.5λ, wherein the antenna element is disposed at a distance of about 0.5λ to about 1λ from the groundplane,
wherein the antenna element includes switchable components that are configured to be arranged in at least two different configurations that each have the effective length between about 1λ to about 1.5λ.

Assignees

• Smartsky Networks LLC

Inventors

• Schmidt Stefan
• Hayes Gerard James

Classifications

• H01Q9/16 Primary

  with feed intermediate between the extremities of the antenna, e.g. centre-fed dipole (H01Q9/44 takes precedence) · CPC title

• H01Q9/18

  Vertical disposition of the antenna · CPC title

• H01Q1/286 Primary

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

• H01Q13/085

  Slot-line radiating ends · CPC title

• H01Q9/32

  Vertical arrangement of element (H01Q9/40 takes precedence) · CPC title