Multi-step circular horn system

• US 6,384,795 B1
• Filed: 09/21/2000
• Issued: 05/07/2002
• Est. Priority Date: 09/21/2000
• Status: Expired due to Fees

• Current Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Original Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Inventors: Bhattacharyya, Arun K., Goyette, Guy
• Primary Examiner(s): Wong, Don
• Assistant Examiner(s): CHEN, SHIH CHAO
• Application Number:
  US09/666,203
• Time in Patent Office: 593 Days
• Field of Search: 343/725, 343/756, 343/772, 343/776, 343/781.R, 343/786
• US Class Current: 343/786
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 13/025 Multimode horn antennas; Horns using higher mode of propagation H01Q13/0241 takes precedence; multiple beam H01Q25/04

Abstract

A multi-step circular horn system may have several steps and may use more than one flared section based upon design considerations. In order to achieve high aperture efficiency, the aperture field distribution is close to uniform. For good cross-polar performance, the field distribution is circularly symmetric. Location and shape of the steps is determined by the wavelength of the signal being transmitted and the space constraints imposed by the antenna design. The step discontinuities generate desired modes of operation in the right proportion.

Claims

1. A multi-step horn system comprising:

a horn having an aperture opening and a radiating opening, said horn receiving a relatively uniform, circularly symmetric field distribution at said aperture opening, wherein said field has a given wavelength;

a first flare located on said horn between said aperture opening and said radiating opening;

a first step coupled to said first flare and located between said first flare and said aperture opening, said first step shape and location on said horn based upon said wavelength to generate a desired first mode; and

a third flare coupled to a first flange and located between said first flange and said aperture opening.

2. The multi-step horn system as recited in claim 1, further comprising a second flare coupled to said first flange and located between said first flange and said aperture opening.

3. The multi-step horn system as recited in claim 2, further comprising a second step located between said second flare and said aperture opening, said second step shape and location on said horn based upon said wavelength to generate a desired second mode.

4. The multi-step horn system as recited in claim 3, wherein said third flare is coupled to said second step and located between said second step and said aperture opening, wherein said third flare is used for input matching.

5. The multi-step horn system as recited in claim 4, wherein said aperture opening comprises said first flange coupled to said third flare.

6. A satellite communications system, comprising;

a ground station;

a satellite in orbit and in communication with said ground station, said satellite having a multi-step circular horn system comprising;

a horn having an aperture opening and a radiating opening, said horn receiving a relatively uniform, circularly symmetric field distribution at said aperture opening, wherein said field has a given wavelength;

a first flare located on said horn between said aperture opening and said radiating opening;

a first step coupled to said first flare and located between said first flare and said aperture opening, said first step shape and location on said horn based upon said wavelength to generate a desired first mode; and

a third flare coupled to a first flange and located between said first flange and said aperture opening.

7. The multi-step horn system as recited in claim 6, further comprising a second flare coupled to said first flange and located between said first flange and said aperture opening.

8. The multi-step horn system as recited in claim 7, further comprising a second step located between said second flare and said aperture opening, said second step shape and location on said horn based upon said wavelength to generate a desired second mode.

9. The multi-step horn system as recited in claim 8, further comprising a third flare coupled to said second flange and located between said second flange and said aperture opening, wherein said third flare is used for input matching.

10. The multi-step horn system as recited in claim 9, wherein said aperture opening comprises said first flange coupled to said third flare.

11. The multi-step horn system as recited in claim 6, wherein said horn is circular in shape.

12. The multi-step circular horn system as recited in claim 6, wherein said horn is rectangular in shape.

13. The multi-step circular horn system as recited in claim 6, wherein said horn is square in shape.