Steerable satellite antenna assembly with fixed antenna feed and associated methods

Patent metadata

Field	Value
Publication number	US-9871292-B2
Application number	US-201514818521-A
Country	US
Kind code	B2
Filing date	Aug 5, 2015
Priority date	Aug 5, 2015
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

An antenna assembly to be carried by a satellite includes an antenna feed configured to extend outwardly from the satellite, and a frame rotatably carried by the antenna feed and is rotatable about a first rotation axis. A main reflector is carried by the frame and is aligned with the antenna feed. A splash plate is carried by the frame in spaced apart relation from the main reflector and is rotatable about a second rotation axis.

First claim

That which is claimed is:

1. An antenna assembly to be carried by a satellite and comprising:
an antenna feed configured to extend outwardly from the satellite;
a frame rotatably carried by said antenna feed and being rotatable about a first rotation axis;
a main reflector carried by said frame and aligned with said antenna feed; and
a splash plate carried by said frame, and positioned in spaced apart relation from said main reflector without a subreflector therebetween so that said main reflector is positioned along a path between said antenna feed and said splash plate, and so that said splash plate is rotatable about a second rotation axis.

2. The antenna assembly according to claim 1 wherein said antenna feed has an L-shape.

3. The antenna assembly according to claim 1 wherein said main reflector is fixed to said frame.

4. The antenna assembly according to claim 1 further comprising a first rotational actuator coupled between said antenna feed and said frame.

5. The antenna assembly according to claim 1 further comprising a second rotational actuator coupled between said frame and said splash plate.

6. The antenna assembly according to claim 1 wherein the first rotation axis provides azimuthal positioning, and wherein the second rotation axis provides elevational positioning.

7. The antenna assembly according to claim 1 wherein said main reflector has a parabolic shape, and said splash plate has a flat shape.

8. The antenna assembly according to claim 1 wherein said main reflector is configured to operate in at least one of the Ka-frequency band and the Ku-frequency band.

9. A satellite comprising:
a housing;
communications circuitry carried by said housing; and
an antenna assembly comprising
an antenna feed configured to extend outwardly from said housing and coupled to said communications circuitry,
a frame rotatably carried by said antenna feed and being rotatable about a first rotation axis,
a main reflector carried by said frame and aligned with said antenna feed, and
a splash plate carried by said frame, and positioned in spaced apart relation from said main reflector without a subreflector therebetween so that said main reflector is positioned along a path between said antenna feed and said splash plate, and so that said splash plate is rotatable about a second rotation axis.

10. The satellite according to claim 9 wherein said antenna feed has an L-shape.

11. The satellite according to claim 9 wherein said main reflector is fixed to said frame.

12. The satellite according to claim 9 further comprising a first rotational actuator coupled between said antenna feed and said frame; and a second rotational actuator coupled between said frame and said splash plate.

13. The satellite according to claim 9 wherein the first rotation axis provides azimuthal positioning, and wherein the second rotation axis provides elevational positioning.

14. The satellite according to claim 9 wherein said main reflector has a parabolic shape, and said splash plate has a flat shape.

15. The satellite according to claim 9 wherein said communications circuitry and said main reflector are each configured to operate in at least one of the Ka-frequency band and the Ku-frequency band.

16. A method for making an antenna assembly to be carried by a satellite and comprising:
positioning an antenna feed to extend outwardly from the satellite;
positioning a frame to be rotatably carried by the antenna feed, with the frame being rotatable about a first rotation axis;
positioning a main reflector to be carried by the frame and aligned with the antenna feed; and
positioning a splash plate to be carried by the frame, and positioning the splash plate in spaced apart relation from the main reflector without a subreflector therebetween so that the main reflector is positioned along a path between the antenna feed and the splash plate, and so that the splash plate is rotatable about a second rotation axis.

17. The method according to claim 16 wherein the antenna feed has an L-shape.

18. The method according to claim 16 wherein the main reflector is fixed to the frame.

19. The method according to claim 16 further comprising:
coupling a first rotational actuator between the antenna feed and the frame; and
coupling a second rotational actuator between the frame and the splash plate.

20. The method according to claim 16 wherein the first rotation axis provides azimuthal positioning, and wherein the second rotation axis provides elevational positioning.

21. The method according to claim 16 wherein the main reflector has a parabolic shape, and the splash plate has a flat shape.

22. The method according to claim 16 wherein the main reflector is configured to operate in at least one of the Ka-frequency band and the Ku-frequency band.

Assignees

• Harris Corp

Inventors

• Turner Gregory M

Classifications

• H01Q3/20 Primary

  wherein the primary active element is fixed and the reflecting device is movable · CPC title

• H01Q1/288

  Satellite antennas · CPC title

• H01Q19/192

  with dual offset reflectors · CPC title