Low cost high performance aircraft antenna for advanced ground to air internet system

• US 10,103,428 B2
• Filed: 09/20/2013
• Issued: 10/16/2018
• Est. Priority Date: 05/02/2013
• Status: Active Grant

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Ozaki, Ernest Tadashi, Tassoudji, Mohammad Ali, Tran, Allen Minh-Triet, Jalali, Ahmad
• Primary Examiner(s): McGue, Frank J
• Application Number:
  US14/033,351
• Publication Number:
  US 20140327577A1
• Time in Patent Office: 1,852 Days
• Field of Search: 342367
• CPC Class Codes: H01Q 1/283 Blade, stub antennas
• CPC Class Codes: H01Q 21/005 Slotted waveguides arrays
• CPC Class Codes: H01Q 21/065 Patch antenna array
• CPC Class Codes: H01Q 25/00 Antennas or antenna systems providing at least two radiating patterns arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence
• CPC Class Codes: H01Q 3/34 by electrical means active lenses or reflecting arrays H01Q3/46
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

A high gain multi-beam aircraft blade antenna of an air-to-ground antenna systems includes multiple columnar matrix antenna elements housed within a blade. The elements are arranged to create independently steerable directed beams. A first independently steerable beam is used to provide communication. A second independently steerable beam is used to simultaneously search other signals.

Claims

1. A high gain multi-beam aircraft blade antenna comprising:

a plurality of columnar matrix antenna elements arranged to create a plurality of independently steerable directional beams, wherein at least a first independently steerable beam is configured to provide communication, and at least a second independently steerable beam is configured to simultaneously search for other signals;

a beam steering unit coupled to each of the columnar matrix antenna elements and configured to cause at least two of the columnar matrix antenna elements to transmit both of the first and second independently steerable beams simultaneously; and

a plurality of pre-amplification circuits coupled between the columnar matrix antenna elements and the beam steering unit, at least two of the plurality of pre-amplification circuits coupled to different ones of the columnar matrix antenna elements and each of the pre-amplification circuits comprising a plurality of amplifiers, wherein;

at least a first one of the plurality of amplifiers is configured to amplify transmission of the first independently steerable beam via at least one of the plurality of the columnar matrix antenna elements; and

at least a second one of the of amplifiers is configured to receive signals from the at least one of the columnar matrix antenna elements.

2. The high gain multi-beam aircraft blade antenna of claim 1, wherein the plurality of columnar matrix antenna elements comprises an array of slot waveguides.

3. The high gain multi-beam aircraft blade antenna of claim 2, further comprising:

an antenna vane placed between each of the slot waveguides.

4. The high gain multi-beam aircraft blade antenna of claim 2, wherein the slot waveguide array is scanned in azimuth of at least one of the plurality of independently steerable directed beams.

5. The high gain multi-beam aircraft blade antenna of claim 1, wherein the plurality of columnar matrix antenna elements comprises a patch array.

6. The high gain multi-beam aircraft blade antenna of claim 5, wherein the patch array is scanned in azimuth and elevation of at least one of the plurality of independently steerable directed beams.

7. The high gain multi-beam aircraft blade antenna of claim 5, wherein the patch array is configured to shape a desired gain pattern in an elevation plane of at least one of the plurality of independently steerable directed beams.

8. The high gain multi-beam aircraft blade antenna of claim 5, further comprising a transceiver coupled to each of the plurality of columnar matrix antenna elements and configured to enable simultaneous access to the plurality of columnar matrix antenna elements.

9. The high gain multi-beam aircraft blade antenna of claim 1, wherein the plurality of columnar matrix antenna elements structurally cooperate to create a desired gain pattern in a yaw direction of an aircraft while reducing deleterious scattering interference from a surface of the aircraft.

10. The high gain multi-beam aircraft blade antenna of claim 1, wherein the plurality of amplifiers comprise a first amplifier configured to amplify transmission of both of the first and second independently steerable beam and a second amplifier configured to amplify reception of both of the first and second independently steerable beam.

11. The high gain multi-beam aircraft blade antenna of claim 1, wherein each of the plurality of amplifiers is configured to amplify only one of transmission or reception of the first and second independently steerable beams.

12. The high gain multi-beam aircraft blade antenna of claim 1, wherein the at least a first one of the plurality of amplifiers is a power amplifier and at least a second one of the plurality of amplifiers is a low noise amplifier.

13. The high gain multi-beam aircraft blade antenna of claim 1, wherein the power amplifier and the low noise amplifier are both coupled to at least one transmit/receive switch.

14. The high gain multi-beam aircraft blade antenna of claim 1, wherein the first and second independently steerable beams are phase shifted beams.

15. A high gain multi-beam aircraft blade antenna comprising:

means for housing a plurality of columnar matrix antenna elements arranged to create a plurality of independently steerable directional beams, wherein at least a first independently steerable beam is configured to provide communication, and at least a second independently steerable beam is configured to simultaneously search other signals;

means for causing at least two of the columnar matrix antenna elements to transmit both of the first and second independently steerable beams simultaneously;

means for amplifying transmission of the first independently steerable beam via at least one of the plurality of the columnar matrix antenna elements; and

means for receiving signals from the at least one of the columnar matrix antenna elements.

16. The high gain multi-beam aircraft blade antenna of claim 15, wherein the plurality of columnar matrix antenna elements comprises an array of slot waveguides.

17. The high gain multi-beam aircraft blade antenna of claim 16, further comprising:

an antenna vane placed between each of the slot waveguides.

18. The high gain multi-beam aircraft blade antenna of claim 17, wherein the slot waveguide array is scanned in azimuth of at least one of the plurality of independently steerable directed beams.

19. The high gain multi-beam aircraft blade antenna of claim 15, wherein the plurality of columnar matrix antenna elements comprises a patch array.

20. The high gain multi-beam aircraft blade antenna of claim 19, wherein the patch array is scanned in azimuth and elevation of at least one of the plurality of independently steerable directed beams.

21. The high gain multi-beam aircraft blade antenna of claim 19, wherein the patch array is configured to shape a desired gain pattern in an elevation plane of at least one of the plurality of independently steerable directed beams.

22. The high gain multi-beam aircraft blade antenna of claim 19, further comprising:

means for enabling simultaneous access to the plurality of columnar matrix antenna elements.

23. The high gain multi-beam aircraft blade antenna of claim 19, wherein the plurality of columnar matrix antenna elements comprises two sets of a plurality of columns arranged to face port and starboard faces of the means for housing.

24. A method of wireless communication using a high gain multi-beam aircraft blade antenna, the method comprising:

operating a plurality of columnar matrix antenna elements;

steering at least a first independently steerable directional beam to provide communication;

steering at least a second independently steerable directed beam to simultaneously search other signals while the first independently steerable directional beam is providing communication;

feeding, using a beam steering unit, each of the columnar matrix antenna elements to cause at least two of the columnar matrix antenna elements to transmit both of the first and second independently steerable beams simultaneously;

amplifying, using a first amplifier, transmission of the first independently steerable beam via at least one of the plurality of the columnar matrix antenna elements; and

receiving, using a second amplifier, signals from the at least one of the columnar matrix antenna elements.

25. The method of claim 24, wherein the plurality of columnar matrix antenna elements comprises an array of slot waveguides.

26. The method of claim 25, further comprising:

scanning the slot waveguide array in azimuth of at least one of the first and second independently steerable directed beams.

27. The method of claim 24, wherein the plurality of columnar matrix antenna elements comprises a patch array.

28. The method of claim 27, further comprising:

scanning the patch array in azimuth and elevation of at least one of the first and second independently steerable directed beams.