IP Library › Granted Patent US 7,239,285
Granted Patent B2
US 7,239,285 · App. 11/132,763 · Granted Jul 3, 2007

Circular polarity elliptical horn antenna

Assignee: ProBrand International, Inc.
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Quick Facts
Patent No.
US 7,239,285
App. No.
11/132,763
Granted
Jul 3, 2007
Kind
B2
Abstract

A relatively low cost, easy to install and aesthetically pleasing digital video broadcast from satellite (DVBS) elliptical horn antenna designed as part of a reflector antenna system to receive satellite television broadcast signals with circular polarity. This type antenna may be implemented with a single antenna feed horn with multiple feed horns that may be arranged separately or in one or more integral feed horn blocks. The antennas may be designed to achieve acceptable circular polarity performance over broad and multiple frequency bands through the use of oppositely sloped differential phase differential sections.

Claims (39)

1. An antenna feed horn extending in a signal propagation direction, comprising:

a reception end defined by an undivided, oblong input aperture;

an output aperture spaced apart from the input aperture in the signal propagation direction;

a phase adjustment structure extending from the input aperture to the output aperture comprising an interior surface defining an oblong, undivided cross-section perpendicular to the signal propagation direction over a substantial portion of the phase adjustment structure in the signal propagation direction; and

for a signal propagating at a desired frequency and exhibiting circular polarity expressed by orthogonal linear components when incident at the input aperture, the interior surface of the phase adjustment structure configured to differentially phase shift the linear components by approximately 90 degrees to convert the signal from circular polarity to linearly polarity as the signal propagates through the phase adjustment structure.

2. The antenna feed horn of claim 1 , wherein the phase adjustment structure comprises a transition section that differentially phase shifts the linear components in a first direction by an initial amount less than 90 degrees and an additive phase differential section that differentially phase shifts the linear components by an additive amount in the first direction to impart a total differential phase shift through the phase adjustment structure of approximately 90 degrees.

3. The antenna feed horn of claim 1 , wherein the phase adjustment structure comprises a transition section that differentially phase shifts the linear components in a first direction by an initial amount greater than 90 degrees and an oppositely sloped phase differential section that differentially phase shifts the linear components by a subtractive amount in a second direction opposing the first direction to impart a total differential phase shift through the phase adjustment structure of approximately 90 degrees.

4. The antenna feed horn of claim 3 , wherein:

the transition section exhibits a phase differential versus frequency transfer function that slopes in a first direction across an operational frequency band of the antenna feed horn; and

the oppositely sloped phase differential section exhibits a phase differential versus frequency transfer function that slopes in a direction opposing the first direction across the operational frequency band of the antenna feed horn.

5. The antenna feed horn of claim 4 , wherein, for an operational frequency band between a low-end frequency of 18.3 GHz and a high-end frequency 20.2 GHz, the differential phase shift through the antenna feed horn differs from 90 degrees by no more than ten degrees over the operational frequency band.

6. The antenna feed horn of claim 4 , wherein, for an operational frequency band between a low-end frequency of 11.7 GHz and a high-end frequency 12.7 GHz, the differential phase shift through the antenna feed horn differs from 90 degrees by no more than ten degrees over the operational frequency band.

7. The antenna feed horn of claim 1 , wherein the oblong, undivided cross-section of the interior surface of the phase adjustment structure is substantially elliptical or substantially rectangular.

8. The antenna feed horn of claim 1 , wherein the interior surface of the phase adjustment structure is smooth-walled, comprises one or more ridges extending in the signal propagation direction, or comprises a smooth-walled first portion and a second portion comprising one or more ridges extending in the propagation direction.

9. The antenna feed horn of claim 1 , further comprising two additional antenna feed horns as described in claim 1 disposed within a common integral housing, and wherein each antenna feed horn is positioned to receive signals from an associated satellite, and the satellites are located approximately within a four degree longitudinal zone.

10. An antenna feed horn extending in a signal propagation direction and, for a signal propagating through the antenna feed horn at a desired frequency and exhibiting a polarity expressed by linear components, the phase adjustment structure comprising:

a transition section that differentially phase shifts the linear components in a first direction; and

an oppositely sloped phase differential section that differentially phase shifts the linear components by a subtractive amount in a second direction opposing the first direction.

11. The antenna feed horn of claim 10 , wherein:

the transition section exhibits a phase differential versus frequency transfer function that slopes in a first direction across an operational frequency band of the antenna feed horn;

the oppositely sloped phase differential section exhibits a phase differential versus frequency transfer function that slopes in a second direction opposing the first direction across the operational frequency band of the antenna feed horn.

12. The antenna feed horn of claim 11 , wherein, for an operational frequency band between a low-end frequency of 18.3 GHz and a high-end frequency 20.2 GHz, the differential phase shift through the antenna feed horn differs from 90 degrees by no more than ten degrees over the operational frequency band.

13. The antenna feed horn of claim 11 , wherein, for an operational frequency band between a low-end frequency of 11.7 GHz and a high-end frequency 12.7 GHz, the differential phase shift through the antenna feed horn differs from 90 degrees by no more than ten degrees over the operational frequency band.

14. An antenna feed horn comprising a phase adjustment structure extending in a signal propagation direction, the phase adjustment structure comprising:

a non-corrugated interior surface extending in the signal propagation direction and defining an oblong, undivided cross-section perpendicular to the signal propagation direction over a substantial portion of the phase adjustment structure in the signal propagation direction; and

for a signal propagating at a desired frequency and exhibiting circular polarity expressed by orthogonal linear components when incident at the input aperture, the interior surface of the phase adjustment structure configured to deliver the signal to the output aperture exhibiting circular polarity.

15. The antenna feed horn of claim 14 , wherein the interior surface of the phase adjustment structure is smooth-walled, comprises one or more ridges extending in the signal propagation direction, or comprises a smooth-walled first portion and a second portion comprising one or more ridges extending in the propagation direction.

16. An antenna comprising an oblong reflector and an antenna feed horn positioned and configured to illuminate substantially all of the oblong reflector, the antenna feed horn comprising:

a reception end defined by an undivided, oblong input aperture;

an output aperture spaced apart from the input aperture in the signal propagation direction;

a phase adjustment structure extending from the input aperture to the output aperture comprising a interior surface defining an oblong, undivided cross-section perpendicular to the signal propagation direction over a substantial portion of the phase adjustment structure in the signal propagation direction; and

for a signal propagating at a desired frequency and exhibiting circular polarity expressed by orthogonal linear components when incident at the input aperture, the interior surface of the phase adjustment structure configured to differentially phase shift the linear components by approximately 90 degrees to convert the signal from circular polarity to linearly polarity as the signal propagates through the phase adjustment structure.

17. The antenna of claim 16 , further comprising two additional antenna feed horns as described in claim 16 disposed within a common integral housing, and wherein:

each feed horn is positioned to receive signals from an associated satellite; and

the satellites are located approximately within a four degree longitudinal zone.

18. The antenna of claim 17 , wherein, for each antenna feed horn, the phase adjustment structure of comprises a transition section that differentially phase shifts the linear components in a first direction by an initial amount greater than 90 degrees and an oppositely sloped phase differential section that differentially phase shifts the linear components by a subtractive amount in a second direction opposing the first direction to impart a total differential phase shift through the phase adjustment structure of approximately 90 degrees.

19. The antenna of claim 18 , wherein, for each antenna feed horn:

the transition section exhibits a phase differential versus frequency transfer function that slopes in a first direction across an operational frequency band of the antenna feed horn; and

the oppositely sloped phase differential section exhibits a phase differential versus frequency transfer function that slopes in a direction opposing the first direction across the operational frequency band of the antenna feed horn.

Continuity (3)
Provisional Application 6057208000 · May 18, 2004
Provisional Application 6057198800 · May 18, 2004
Related Publication 20050259026A1 · Nov 24, 2005