Wide-band linked-ring antenna element for phased arrays

• US 8,749,446 B2
• Filed: 07/29/2011
• Issued: 06/10/2014
• Est. Priority Date: 07/29/2011
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Manry, Charles W. Jr., Cai, Lixin
• Primary Examiner(s): Ho, Tan
• Application Number:
  US13/194,344
• Publication Number:
  US 20130028298A1
• Time in Patent Office: 1,047 Days
• Field of Search: 343/700.MS, 343/841, 343/866, 343/867
• US Class Current: 343/866
• CPC Class Codes: H01Q 5/40 Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
• CPC Class Codes: H01Q 5/45 using two or more feeds in association with a common reflecting, diffracting or refracting device
• CPC Class Codes: H01Q 9/0464 Annular ring patch

Abstract

Technologies for a wide-band linked-ring antenna element covering two adjacent K-band military and/or commercial receive bands are provided. The antenna element comprises a linked-ring conductive resonator that is electromagnetically coupled to at least one feed line. The conductive resonator and feed line are further surrounded by a Faraday cage that is conductively coupled to an electromagnetically-shielding ground plane and operable to shield the conductive resonator and the feed line.

Claims

1. An antenna element comprising:

a multi-layer circuit board;

a linked-ring conductive resonator located on a top layer of the multi-layer circuit board and comprising a plurality of ring elements connected by one or more tuning tabs;

a first feed line and a second feed line located on a middle layer of the multi-layer circuit board and capacitively coupled to the linked-ring conductive resonator;

an electromagnetically-shielding ground plane located on a bottom layer of the multi-layer circuit board; and

a Faraday cage surrounding the linked-ring conductive resonator, the first feed line, and the second feed line and conductively coupled to the electromagnetically-shielding ground plane.

2. The antenna element of claim 1, wherein the linked-ring conductive resonator comprises an inner ring element and an outer ring element connected by four tuning tabs.

3. The antenna element of claim 1, wherein the first feed line is oriented at substantially 90 degrees with respect to the second feed line such that the antenna element may receive both right-hand circular polarized and left-hand circular polarized signals.

4. The antenna element of claim 1, wherein the Faraday cage comprises a conductive strip located on each layer of the multi-layer circuit board above the bottom layer and a plurality of conductive vias connecting the conductive strips to the electromagnetically-shielding ground plane.

5. The antenna element of claim 1, wherein each layer of the multi-layer circuit board is separated by a low-loss low-dielectric-constant material.

6. The antenna element of claim 1, wherein the antenna element is configured to be constructed with a plurality of antenna elements to form a phased array antenna.

7. A system for communicating on at least two adjacent satellite communication bands, the system comprising:

a plurality of antenna elements configured in a phased array, at least one of the plurality of antenna elements comprising a linked-ring conductive resonator having an inner ring element and an outer ring element connected by four tuning tabs, a first feed line and a second feed line capacitively coupled to the linked-ring conductive resonator, and a Faraday cage operable to shield the conductive resonator, the first feed line, and the second feed line; and

communication electronics electrically coupled to the first feed line and the second feed line and configured to provide independent signaling to the at least one of the plurality of antenna elements.

8. The system of claim 7, wherein the first feed line and the second feed line are further operative to drive the linked-ring conductive resonator.

9. The system of claim 7, wherein the first feed line is oriented at substantially 90 degrees with respect to the second feed line.

10. The system of claim 7, wherein the Faraday cage comprises an electromagnetically-shielding ground plane coupled to a plurality of conductive strips by at least one conductive via.

11. An antenna element comprising:

a plurality of layers, each of the plurality of layers separated by a low-loss low-dielectric-constant material;

a linked-ring conductive resonator comprising a plurality of ring elements connected by one or more tuning tabs;

a feed line electromagnetically coupled to the conductive resonator; and

a Faraday cage operable to shield the conductive resonator and the feed line, the linked-ring conductive resonator, the feed line, and the Faraday cage positioned among the plurality of layers.

12. The antenna element of claim 11, wherein the linked-ring conductive resonator comprises an inner ring element and an outer ring element connected by four tuning tabs.

13. The antenna element of claim 11, wherein the feed line is operable to drive the linked-ring conductive resonator.

14. The antenna element of claim 11, wherein the feed line is operable to receive a signal from the linked-ring conductive resonator.

15. The antenna element of claim 11, further comprising a first feed line and a second feed line, wherein the first feed line is oriented at substantially 90 degrees with respect to the second feed line.

16. The antenna element of claim 15, wherein the first feed line and the second feed line are located beneath the linked-ring conductive resonator in the antenna element and are capacitively coupled to the linked-ring conductive resonator.

17. The antenna element of claim 11, wherein the Faraday cage comprises an electromagnetically-shielding ground plane coupled to a plurality of conductive strips by at least one conductive via.

18. The antenna element of claim 17, wherein the linked-ring conductive resonator is located on a top layer, the feed line is located on a middle layer below the linked-ring conductive resonator, and the electromagnetically-shielding ground plane is located on a bottom layer, and wherein one of the plurality of conductive strips is located on each of the plurality of layers above the bottom layer.

19. The antenna element of claim 11, wherein the antenna element is configured to be constructed with a plurality of the antenna elements to form a phased array antenna.

20. A method for performing wide-band satellite communications (“

SATCOM”

) over a conformal phased array, the method comprising;

implementing a phased array of a plurality of antenna elements, at least one of the antenna elements comprising a linked-ring conductive resonator comprising a plurality of ring elements connected by one or more tuning tabs, a feed line electromagnetically coupled to the conductive resonator, and a Faraday cage operable to shield the conductive resonator and the feed line from electrical fields of neighboring antenna elements in the phased array;

coupling the feed line of the at least one antenna element to communication electronics;

utilizing the communication electronics to drive the linked-ring resonator to receive a signal in a first SATCOM receive band; and

utilizing the communication electronics to drive the linked-ring resonator to receive a signal in a second SATCOM receive band.

21. The method of claim 20, further comprising:

receiving a signal in a SATCOM band at the communication electronics through the conductive resonator and feed line of the at least one antenna element.

22. The method of claim 20, wherein the conductive resonator comprises an inner ring element and an outer ring element connected by four tuning tabs.

23. The method of claim 20, wherein a first feed line is oriented at substantially 90 degrees with respect to a second feed line in at least one antenna element such that the communication electronics may selectively receive both right-hand circular polarized and left-hand circular polarized signals.

24. The method of claim 20, wherein the Faraday cage comprises a hexagonal shape such that conductive strips and conductive vias of the Faraday cage are shared with the neighboring antenna elements in the phased array.