Fast, digital frequency tuning, winglet dipole antenna system

• US 8,525,745 B2
• Filed: 10/25/2010
• Issued: 09/03/2013
• Est. Priority Date: 10/25/2010
• Status: Active Grant

• Current Assignee: Sensor Systems
• Original Assignee: Sensor Systems
• Inventors: Lin, Zhen Biao, Lin, Jack J. Q., Robin, Seymour
• Primary Examiner(s): LE, HOANGANH T
• Application Number:
  US12/911,529
• Publication Number:
  US 20120098714A1
• Time in Patent Office: 1,044 Days
• Field of Search: 343/705, 343/708, 343/795, 343/725, 343/729, 343/802
• US Class Current: 343/705
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 1/50 Structural association of antennas with earthing switches, lead-in devices or lightning protectors
• CPC Class Codes: H01Q 21/28 Combinations of substantially independent non-interacting antenna units or systems multiple beam H01Q25/00
• CPC Class Codes: H01Q 21/30 Combinations of separate antenna units operating in different wavebands and connected to a common feeder system
• CPC Class Codes: H01Q 9/285 Planar dipole H01Q9/065 takes precedence; patch antenna H01Q9/0407
• CPC Class Codes: H01Q 9/36 with top loading

Abstract

Antenna system embodiments are illustrated that include a planar, top-loaded dipole antenna and a planar elliptical dipole antenna arranged substantially coplanar and within the top-loaded dipole antenna. These antenna structures facilitate their combination with tuning coil chains, baluns and impedance matching circuits to operate over multiple frequency bands. System embodiments exhibit high gain and selectivity and may be digitally tuned over wide frequency bands (e.g., 30-600 MHz). The embodiments may be digitally tuned to support operational modes such as frequency hopping to thereby realize a secure communication system. Because these embodiments are configured to operate in the absence of a ground plane, they are especially suited for mounting on various portions of an aircraft'"'"'s structure. For example, they may be configured as winglets and situated far out on wingtips to thus free the remainder of an aircraft'"'"'s structure for other operational systems.

Claims

1. An antenna system, comprising:

a planar, top-loaded dipole antenna to provide signals to a system output port, wherein said top-loaded dipole antenna comprises first and second top-loaded blades; and

first and second strings of inductors coupled to respective blades, said system arranged such that the inductors in each string can be selectively connected in series to tune said top-loaded dipole antenna to a selected tuning frequency.

2. The system of claim 1, further including:

a planar elliptical dipole antenna arranged substantially coplanar with said top-loaded dipole antenna to provide signals to said system output port.

3. The system of claim 2, wherein said elliptical dipole antenna comprises:

a first set of nested elliptical rings; and

a second set of nested elliptical rings arranged in a dipole relationship with said first set.

4. The system of claim 3, wherein centers of elliptical rings in each of said first and second sets are progressively spaced towards the other of said first and second sets.

5. The system of claim 1, further including diodes arranged across each of said inductors to enable selection thereof.

6. The system of claim 5, wherein said diodes are switching diodes, opposed pairs of which are connected in parallel with respective inductors, such that each inductor can be selectively connected in series with one of said first or second strings of inductors in response to a signal applied to the junction between the opposed pair of diodes connected in parallel with said inductor.

7. The system of claim 5, wherein said diodes are PIN diodes.

8. The system of claim 1, wherein said further including:

a balun with said first and second strings respectively coupled between said first and second top-loaded blades and said balun; and

an impedance-matching circuit coupled to said balun.

9. The system of claim 1, further including:

a second balun;

first and second diodes each arranged to selectively couple a respective one of said first and second blades to said second balun; and

a second impedance-matching circuit coupled to said second balun.

10. The system of claim 9, further including:

a planar elliptical dipole antenna arranged substantially coplanar with said top-loaded dipole antenna to provide signals to said output port;

a third impedance-matching circuit;

a third balun coupling said third impedance-matching circuit to said elliptical dipole antenna; and

a diplexer coupled to said second and third impedance-matching circuits.

11. The system of claim 1, wherein said top-loaded dipole antenna is arranged to operate over a frequency band of 30-88 MHz.

12. The system of claim 1, wherein each of said first and second strings of inductors comprises:

a smallest inductor having an inductance L;

a second inductor having an inductance 2L;

a third inductor having an inductance 4L;

and so on, with the inductance of each subsequent inductor increasing in accordance with a binary progression.

13. The system of claim 1, wherein said system is arranged to selectively connect said inductors in series such that the combined inductances in each string substantially cancel the capacitance of the blade to which each string is connected at said selected tuning frequency.

14. The system of claim 1, wherein said inductors in each string are selectively connected in series in response to respective control signals, further including:

a processor arranged to receive a frequency word which represents said selected tuning frequency; and

a digital lookup table arranged to receive a frequency code from said processor and to provide an output from which said control signals are derived such that said top-loaded dipole antenna is tuned to said selected tuning frequency.

16. The system of claim 1, further including:

a planar elliptical dipole antenna arranged substantially coplanar with said top-loaded dipole antenna to provide signals to said system output port;

a first balun, said first and second strings of inductors respectively coupled between said first and second top-loaded blades and said first balun;

a first impedance-matching circuit to couple said first balun to said system output port;

a diplexer coupled to said system output port;

a second balun;

first and second diodes each arranged to selectively couple a respective one of said first and second blades to said second balun;

a second impedance-matching circuit coupled between said second balun and said diplexer;

a third balun coupled to said elliptical dipole antenna; and

a third impedance-matching circuit coupled between said third balun and said diplexer.

15. An antenna system, comprising:

a planar, top-loaded dipole antenna to provide signals to a system output port; and

a planar elliptical dipole antenna arranged substantially coplanar with said top-loaded dipole antenna to provide signals to said output port;

wherein;

said top-loaded dipole antenna comprises a first blade terminating in an elongate first top load and a second blade terminating in an elongate second top load; and

said elliptical dipole antenna is positioned between said first and second top loads.

17. An antenna, comprising:

a first set of nested elliptical rings; and

a second set of nested elliptical rings arranged in a dipole relationship with said first set,

wherein the centers of the elliptical rings in each of said first and second sets are progressively spaced towards the other of said first and second sets.

18. The antenna of claim 17, wherein said rings are substantially coplanar.

19. An antenna system to be coupled to an aircraft wingtip, comprising:

a planar, top-loaded dipole antenna to provide signals to a system output port, wherein said top-loaded dipole antenna comprises first and second top-loaded blades;

a planar elliptical dipole antenna arranged substantially coplanar with said top-loaded dipole antenna to provide signals to said output port;

a planar dielectric radome aerodynamically shaped to closely surround said top-loaded dipole antenna and said elliptical dipole antenna and configured to couple to said wingtip; and

first and second strings of inductors coupled to respective blades, said system arranged such that the inductors in each string can be selectively connected in series to tune said top-loaded dipole antenna to a selected tuning frequency.

20. The system of claim 19, wherein said radome is configured to mount substantially orthogonal to said wingtip.

21. The system of claim 19, wherein said elliptical dipole antenna comprises:

a first set of nested elliptical rings; and

a second set of nested elliptical rings arranged in a dipole relationship with said first set.

22. The system of claim 19, further including:

a balun with said first and second strings respectively coupled between said first and second top-loaded blades and said balun; and

an impedance-matching circuit coupled to said balun.

23. The system of claim 22, further including:

a second balun;

first and second diodes each arranged to selectively couple a respective one of said first and second blades to said second balun; and

a second impedance-matching circuit coupled to said second balun.

24. The system of claim 22, further including:

a third impedance-matching circuit;

a third balun coupling said third impedance-matching circuit to said elliptical dipole antenna; and

a diplexer coupled to said second and third impedance-matching circuits.

25. An antenna system to be coupled to an aircraft wingtip, comprising:

a planar, top-loaded dipole antenna to provide signals to a system output port;

a planar elliptical dipole antenna arranged substantially coplanar with said top-loaded dipole antenna to provide signals to said output port; and

a planar dielectric radome aerodynamically shaped to closely surround said top-loaded dipole antenna and said elliptical dipole antenna and configured to couple to said wingtip;

wherein;

said top-loaded dipole antenna comprises a first blade terminating in an elongate first top load and a second blade terminating in an elongate second top load; and

said elliptical dipole antenna is positioned between said first and second top loads.