Small wave-guide radiators for closely spaced feeds on multi-beam antennas

• US 7,224,320 B2
• Filed: 05/18/2005
• Issued: 05/29/2007
• Est. Priority Date: 05/18/2004
• Status: Expired due to Fees

• Current Assignee: Probrand International Incorporated
• Original Assignee: Probrand International Incorporated
• Inventors: Cook, Scott J.
• Primary Examiner(s): Dinh; Trinh Vo
• Application Number:
  US11/132,761
• Publication Number:
  US 20050259025A1
• Time in Patent Office: 741 Days
• Field of Search: 343/772, 343/779, 343/776
• US Class Current: 343/772
• CPC Class Codes: H01Q 13/0225 of non-circular cross-section H01Q13/0216 takes precedence
• CPC Class Codes: H01Q 19/17 the primary radiating source comprising two or more radiating elements H01Q19/15, H01Q25/00 take precedence
• CPC Class Codes: H01Q 25/007 using two or more primary active elements in the focal region of a focusing device for operation on different wavebands H01Q5/22

Abstract

A relatively low cost, easy to install and aesthetically pleasing digital video broadcast from satellite (DVBS) elliptical horn antenna designed to receive satellite television broadcast signals with circular polarity. This type antenna may be implemented as a multi-beam, multi-band antenna with closely spaced antenna feed horns operable for simultaneously receiving signals from multiple satellites that are closely spaced from the perspective of the antenna.

Claims

1. An antenna configured to simultaneously receive signals from multiple satellites that are closely spaced from the perspective of the antenna;

comprising;

at least three closely spaced antenna feed horns arranged in a substantially linear array along a linear axis;

a substantially elliptical reflector defining a major axis for feeding signals to the closely spaced antenna feed horns;

a first feed horn of the array having an exterior contour that defines a first indentation;

a second feed horn of the array having an exterior contour that defines a portion received within the first indentation of the first feed horn; and

wherein the linear axis of the array is substantially aligned with the major axis of the reflector.

2. The antenna of claim 1, wherein the three closely spaced antenna feed horns are disposed within a common housing.

3. The antenna of claim 2, wherein the common housing further comprises a low noise block down converter.

4. The antenna of claim 2, wherein the common housing further comprises a circular polarizer.

5. The antenna of claim 1, herein the first feed horn defines a second indentation, further comprising a third feed horn having an exterior contour that defines a portion received within the second indentation of the first feed horn.

6. The antenna of claim 5, wherein the first feed horn comprises a substantially cross shape.

7. The antenna of claim 6, wherein the second and third feed horns each comprise a substantially square or rectangular shape.

8. The antenna of claim 6, wherein the second and third feed horns each comprise a substantially round or oval shape.

9. The antenna of claim 6, wherein the second feed horn comprises a substantially round or oval shape and the third feed horn comprises a substantially square or rectangular shape.

10. The antenna of claim 1, wherein the first feed horn comprises a substantially cross shape.

11. The antenna of claim 10, wherein the second feed horn comprises a substantially square or rectangular shape.

12. The antenna of claim 10, wherein the second feed horn comprises a substantially round or oval shape.

13. An antenna configured to simultaneously receive signals from multiple satellites that are closely spaced from the perspective of the antenna;

comprising;

a common housing containing at least three closely spaced antenna feed horns arranged in a linear array along a linear axis, a low noise block down converter, and a circular polarizer;

a substantially elliptical reflector defining a major axis for feeding signals to the closely spaced antenna feed horns;

a first feed horn of the array having an exterior contour that defines a first indentation; and

a second feed of the array horn having an exterior contour that defines a portion received within the first indentation of the first feed horn; and

wherein the linear axis of the array is substantially aligned with the major axis of the reflector.

14. The antenna of claim 13, wherein the first feed horn defines a second indentation, further comprising a third feed horn having an exterior contour that defines a portion received within the second indentation of the first feed horn.

15. The antenna of claim 14, wherein the first feed horn comprises a substantially cross shape.

16. An antenna configured to simultaneously receive signals from multiple satellites that are closely spaced from the perspective of the antenna, comprising:

a common housing containing at least three closely spaced antenna feed horns arranged in a substantially linear array along a linear axis and a low noise block down converter;

a substantially elliptical reflector defining a major axis for feeding signals to the closely spaced antenna feed horns;

a first feed horn of the array having an exterior contour that defines first and second indentations;

a second feed horn of the array having an exterior contour that defines a portion received within the first indentation of the first feed horn; and

a third feed horn of the array having an exterior contour that defines a portion received within the second indentation of the first feed horn; and

wherein the linear axis of the array is substantially aligned with the major axis of the reflector.