Hybrid-mode horn antenna with selective gain

• US 6,992,639 B1
• Filed: 12/18/2003
• Issued: 01/31/2006
• Est. Priority Date: 01/16/2003
• Status: Active Grant

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Lier, Erik
• Primary Examiner(s): Chen, Shih-Chao
• Assistant Examiner(s): A, Minh Dieu
• Application Number:
  US10/742,464
• Time in Patent Office: 775 Days
• Field of Search: 343/785, 343/786, 343/787, 343/911.R, 343/872, 333/21.R, 333/240, 333/248, 333/251
• US Class Current: 343/786
• CPC Class Codes: H01Q 13/025 Multimode horn antennas; Horns using higher mode of propagation H01Q13/0241 takes precedence; multiple beam H01Q25/04

Abstract

The present invention provides a new class of hybrid-mode horn antennas. The present invention facilitates the design of boundary conditions between soft and hard, supporting modes under balanced hybrid condition with uniform as well as tapered aperture distribution. In one embodiment, the horn antenna (100) is relatively simple mechanically, has a reasonably large bandwidth, supports linear as well as circular polarization, and is designed for a wide range of aperture sizes.

Claims

1. A horn antenna, comprising:

a conducting horn;

a first dielectric layer lining substantially the entire inner wall of said conducting horn;

a second dielectric layer disposed over at least a portion of the first dielectric layer; and

a third dielectric layer disposed over at least a portion of the second dielectric layer;

wherein the second dielectric layer comprises a higher dielectric constant than the third dielectric layer, and the third dielectric layer comprises a higher dielectric constant than the first dielectric layer.

2. The horn antenna as in claim 1 wherein the first dielectric layer comprises an air-filled gap.

3. The horn antenna as in claim 1 wherein the first and second dielectric layers have a generally uniform thickness in an axial direction of the conducting horn.

4. The horn antenna as in claim 1 wherein the first dielectric layer has a variable thickness in an axial direction of the conducting horn.

5. The horn antenna as in claim 1 wherein the second dielectric layer has a variable thickness in an axial direction of the conducting horn.

6. The horn antenna as in claim 1 wherein the conducting horn comprises an inner wall surface, and wherein the second dielectric layer is spaced apart from the inner wall surface by a plurality of spacers.

7. The horn antenna as in claim 6 wherein at least one of the spacers is aligned axially relative to the conducting horn.

8. The horn antenna as in claim 6 wherein at least one of the spacers is aligned circumferentially relative to the conducting horn.

9. The horn antenna as in claim 1 wherein the second dielectric layer further comprises an impedance matching layer near an aperture of the conducting horn.

10. The horn antenna as in claim 9 wherein the impedance matching layer comprises a corrugated impedance matching layer.

11. The horn antenna as in claim 1 wherein the third dielectric layer further comprises an impedance matching layer near an aperture of the conducting horn.

12. The horn antenna as in claim 11 wherein the impedance matching layer comprises a plurality of spaced holes.

13. The horn antenna as in claim 1 further comprising an impedance matched horn throat defined by at least a portion of the second and third dielectric layers.

14. A horn antenna, comprising:

a conducting horn; and

a dielectric core coupled to the conducting horn by a plurality of spacers to define a gap between the horn and core;

wherein the dielectric core comprises an outer portion lining substantially the entire inner wall of said conducting horn, and an inner portion, the outer and inner portions each comprising a dielectric material, with the outer portion dielectric material having a greater dielectric constant than the dielectric constant of the inner portion dielectric material.

15. The horn antenna as in claim 14 wherein the gap is at least partially filled with a gas.

16. The horn antenna as in claim 14 wherein the gap comprises a vacuum region.

17. The horn antenna as in claim 14 wherein the gap is at least partially filled with a third dielectric material having a lower dielectric constant than the dielectric constants of both the inner and outer portion dielectric materials.

18. The horn antenna as in claim 17 wherein the spacers comprise the third dielectric material.

19. The horn antenna as in claim 14 wherein the gap is substantially filled with a third dielectric material having a lower dielectric constant than the dielectric constants of both the inner and outer portion dielectric materials.

20. A reflector antenna comprising:

a reflective dish; and

at least one horn antenna, the horn antenna comprising;

a conducting horn; and

a dielectric core coupled to the conducting horn by a plurality of spacers to define a gap between the horn and core;

the dielectric core comprising an outer portion lining substantially the entire inner wall of said conducting horn, and an inner portion having different dielectric constants, with the outer portion dielectric constant being greater than the inner portion dielectric constant; and

wherein the at least one horn antenna is adapted to direct a signal towards the reflective dish.

21. The reflector antenna as in claim 20 wherein the gap comprises a third dielectric material having a lower dielectric constant than the dielectric core inner and outer portions.

22. An antenna array system, comprising:

at least two horn antennas, each horn antenna comprising;

a conducting horn; and

a dielectric core coupled to the conducting horn by a plurality of spacers to define a gap between the horn and core;

wherein the dielectric core comprises an outer portion lining substantially the entire inner wall of said conducting horn, and an inner portion, the outer and inner portions each comprising a dielectric material, with the outer portion dielectric material having a greater dielectric constant than the dielectric constant of the inner portion dielectric material.

23. A spacecraft, comprising:

a spacecraft bus; and

a horn antenna coupled to the bus, the antenna comprising;

a conducting horn; and

a dielectric core coupled to the conducting horn by a plurality of spacers to define a gap between the horn and core;

the dielectric core comprising an outer portion lining substantially the entire inner wall of said conducting horn, and an inner portion having different dielectric constants, with the outer portion dielectric constant being greater than the inner portion dielectric constant.

24. A spacecraft, comprising:

a spacecraft bus; and

a horn antenna coupled to the bus, the antenna comprising;

a conducting horn;

a first dielectric layer lining substantially the entire inner wall of said conducting horn;

a second dielectric layer disposed over at least a portion of the first dielectric layer; and

a third dielectric layer disposed over at least a portion of the second dielectric layer;

wherein the second dielectric layer comprises a higher dielectric constant than the third dielectric layer, and the third dielectric layer comprises a higher dielectric constant than the first dielectric layer.