Antenna element with high gain toward the horizon

Patent metadata

Field	Value
Publication number	US-9627778-B2
Application number	US-201615017726-A
Country	US
Kind code	B2
Filing date	Feb 8, 2016
Priority date	Mar 13, 2013
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

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 1π from the groundplane.

First claim

What is claimed is:

1. An air-to-ground network communication device, the device comprising:
a conductive groundplane formed at a skin of an aircraft; 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 monopole element, and
wherein the groundplane is formed as a metallic mesh provided within a composite material forming the skin of the aircraft.

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 an underside of a body portion of the aircraft.

4. The device of claim 1 , wherein the groundplane is formed at an underside of a wing of the aircraft.

5. An air-to-ground network communication device, the device comprising:
a conductive groundplane formed at a skin of an aircraft; 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 monopole element, and
wherein the groundplane is formed as a conductive material provided over a composite material forming the skin of the aircraft.

6. The device of claim 1 , wherein the antenna element is end fed.

7. The device of claim 1 , wherein the antenna element is center fed.

8. The device of claim 1 , wherein the antenna element is neither end fed nor center fed.

9. A mobile platform comprising:
a conductive groundplane formed at a skin of an aircraft; 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 monopole element, and
wherein the antenna element is end fed.

10. The mobile platform of claim 9 , wherein the effective length of the antenna element is about 1.2λ and the distance from the groundplane is about 0.68λ.

11. The mobile platform of claim 9 , wherein the groundplane is formed at an underside of a body portion of the aircraft.

12. The mobile platform of claim 9 , wherein the groundplane is formed at an underside of a wing of the aircraft.

13. The mobile platform of claim 9 , wherein the groundplane is formed as a metallic mesh provided within a composite material forming the skin of the aircraft.

14. The mobile platform of claim 9 , wherein the groundplane is formed as a conductive material provided over a composite material forming the skin of the aircraft.

15. A mobile platform comprising:
a conductive groundplane formed at a skin of an aircraft; 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 monopole element, and
wherein the antenna element is center fed.

16. The mobile platform of claim 9 , A mobile platform comprising:
a conductive groundplane formed at a skin of an aircraft; 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 monopole element, and
wherein the antenna element is one of a plurality of antenna elements, and wherein a controller is employed to selectively connect or disconnect the antenna element relative to other antenna elements of the plurality of antenna elements to configure a desired antenna arrangement.

17. The device of claim 5 , wherein the antenna element is end fed.

18. The device of claim 5 , wherein the antenna element is center fed.

19. The device of claim 5 , wherein the antenna element is neither end fed nor center fed.

20. The mobile platform of claim 15 , wherein the groundplane is formed at an underside of a wing of the aircraft.

Assignees

• Smartsky Networks LLC

Inventors

• Schmidt Stefan
• Hayes Gerard James

Classifications

• H01Q9/16

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

• H01Q1/287

  integrated in a wing or a stabiliser · CPC title

• H01Q9/18

  Vertical disposition of the antenna · CPC title

• H01Q13/085

  Slot-line radiating ends · CPC title

• H01Q9/32

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