IP Library Granted Patent US 8,537,068
Granted Patent B2
US 8,537,068 · App. 12/693,494 · Granted Sep 17, 2013

Method and apparatus for tri-band feed with pseudo-monopulse tracking

Inventors: Larry C. Martin (Los Angeles, CA); Yueh-Chi Chang (Northborough, MA); John J. Hanlin (Worcester, MA); William F. Call (Milford, MA)
Assignee: Raytheon Company
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Quick Facts
Patent No.
US 8,537,068
App. No.
12/693,494
Granted
Sep 17, 2013
Kind
B2
Abstract

Methods and apparatus for a feed assembly for a reflector antenna including an aperture common to low, mid, and high frequency bands, a polyrod design to launch signals in the mid and high frequency bands, a horn to launch signals in the low frequency band, a co-located phase center for launching signals in the low, mid, and high frequency bands, and a low-band monopulse array located on a surface about the aperture to track a satellite.

Claims (28)

1. A feed assembly for a reflector antenna, comprising:

an antenna aperture common to low, mid, and high frequency bands;

a polyrod to launch signals from the aperture in the mid and high frequency bands while supporting the low band;

a horn to launch signals from the aperture in the low frequency band;

a co-located phase center for launching signals in the low, mid, and high frequency bands; and

a low-band monopulse array located on a surface about a perimeter of the aperture to track a satellite.

2. The feed assembly according to claim 1 , wherein respective beamwidths for the low, mid, and high frequency bands is approximately equal.

3. The feed assembly according to claim 2 , wherein the respective beamwidths are about 10 dB.

4. The feed assembly according to claim 1 , wherein the monopulse array includes a four patch antenna array.

5. The feed assembly according to claim 1 , wherein a waveguide network for the low frequency band is elongated to minimize blockage of the reflector antenna.

6. The feed assembly according to claim 1 , wherein a length of a polarizer for the mid and high frequency bands is reduced to minimize blockage of the reflector antenna.

7. The feed assembly according to claim 1 , wherein a length of a feed is less than six inches.

8. The feed assembly according to claim 1 , wherein a diameter of the aperture is less than 2.5 inches.

9. The feed assembly according to claim 1 , wherein the monopulse array is implemented in a single stripline layer.

10. The feed assembly according to claim 1 , wherein the monopulse array provides sum, delta azimuth, and delta elevation beams in a downlink band and a single beam in an uplink band.

11. The feed assembly according to claim 1 , further including a turnstile junction coupled to the horn for coupling low-band energy to four symmetric waveguide channels.

12. A method, comprising:

receiving and transmitting signals using a feed assembly for a reflector antenna having an antenna aperture common to low, mid, and high frequency bands;

employing a polyrod to launch signals from the aperture in the mid and high frequency bands while supporting the low band and employing a compact horn to launch signals from the aperture in the low frequency band, wherein a phase center for launching signals in the low, mid, and high frequency bands is co-located; and

employing a low-band monopulse array located on a surface about a perimeter of the aperture to track a satellite.

13. The method according to claim 12 , further including employing respective beamwidths for the low, mid, and high frequency bands that are approximately equal.

14. The method according to claim 13 , wherein the respective beamwidths are about 10 dB.

15. The method according to claim 13 , wherein the monopulse array includes a four patch antenna array.

16. The method according to claim 13 , further including elongating a waveguide network for the low frequency band to minimize blockage of the reflector antenna.

17. The method according to claim 13 , further including reducing a length of a polarizer for the mid and high frequency bands to minimize blockage of the reflector antenna.

18. The method according to claim 13 , wherein a length of a feed is less than six inches.

19. The method according to claim 13 , wherein a diameter of the aperture is less than 2.5 inches.

20. The method according to claim 13 , further including implementing the monopulse array in a single stripline layer.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 2, 2010
From: MARTIN, LARRY C.; CHANG, YUEH-CHI; HANLIN, JOHN J.; CALL, WILLIAM F.
To: RAYTHEON COMPANY
Reel/Frame 023885/0439 →
Continuity (1)
Related Publication 20110181479A1 · Jul 28, 2011