System and apparatus for driving antenna

Patent metadata

Field	Value
Publication number	US-9680199-B2
Application number	US-201514752232-A
Country	US
Kind code	B2
Filing date	Jun 26, 2015
Priority date	Jun 27, 2014
Publication date	Jun 13, 2017
Grant date	Jun 13, 2017

Abstract

A multiple-antenna positioning system with a single drive element, providing reduced weight and complexity over systems that have a drive element for each antenna. In certain examples, each antenna can be coupled with a rotating spindle, with each antenna spindle being coupled with a pair of link arms. By driving a single drive spindle, each of the antenna spindles in the system can be rotated by the associated pair of link arms. The link arms can have an adjustable length, such as through a turnbuckle mechanism, to reduce backlash in the system, and in some examples can apply a preload to the system. By reducing backlash, the multiple antenna positioning system can have improved responsiveness to a rotation of the single drive element, as well as improved stability of the positioning of each antenna when the drive element is held in a fixed position.

First claim

What is claimed is:

1. An antenna system comprising:
a first spindle coupled with a first antenna, the first antenna having a first boresight;
a second spindle coupled with a second antenna, the second antenna having a second boresight that is not parallel to the first boresight;
a first pair of link arms coupling the first spindle with a third spindle;
a second pair of link arms coupling the second spindle with the third spindle; and
a drive element coupled with the third spindle to simultaneously rotate the first antenna via the first pair of link arms and the second antenna via the second pair of link arms.

2. The antenna system of claim 1 , wherein a link arm of the first or second pairs of link arms has a fixed length.

3. The antenna system of claim 1 , wherein a link arm of the first or second pairs of link arms includes a turnbuckle.

4. The antenna system of claim 3 , wherein the turnbuckle comprises two bearing rod ends, each bearing rod end being coupled with one of the first spindle, the second spindle, or the third spindle.

5. An antenna system, comprising:
a first spindle coupled with a first antenna;
a second spindle coupled with a second antenna;
a first pair of link arms coupling the first spindle with a third spindle;
a second pair of link arms coupling the second spindle with the third spindle; and
a drive element coupled with the third spindle to simultaneously rotate the first antenna via the first pair of link arms and the second antenna via the second pair of link arms,
wherein a link arm from the first pair of link arms or a link arm from the second pair of link arms is adjustable to change a first amount of backlash between the first spindle and the third spindle, or to change a second amount of backlash between the second spindle and the third spindle.

6. The antenna system of claim 1 , wherein the first pair of link arms are separated by a first distance, and the second pair of link arms are separated by a second distance, the second distance being different from the first distance.

7. The antenna system of claim 1 , wherein one of the first pair of link arms, the second pair of link arms, and the drive element may be installed or removed irrespective of the presence or absence of the others of the first pair of link arms, the second pair of link arms, and the drive element.

8. The antenna system of claim 1 , wherein an end of one link arm of the first pair of link arms and an end of one link arm of the second pair of link arms are both coupled with the third spindle at a first radial distance as measured from an axis of the third spindle.

9. The antenna system of claim 8 , wherein an end of the other link arm of the first pair of link arms and an end of the other link arm of the second pair of link arms are coupled with the third spindle at a second radial distance as measured from the axis of the third spindle.

10. The antenna system of claim 1 , wherein the first antenna and the second antenna operate over different frequency bands.

11. The antenna system of claim 1 , wherein the drive element comprises a motor.

12. The antenna system of claim 1 , wherein the first spindle and the second spindle are on opposing sides of the third spindle.

13. The antenna system of claim 1 , wherein the

14. The antenna system of claim 1 , wherein each link arm of the first and second pairs of link arms are made of the same material.

15. The antenna system of claim 1 , wherein the drive element comprises a gearbox.

16. An antenna system, comprising:
a first spindle coupled with a first antenna;
a second spindle coupled with a second antenna;
a first pair of link arms coupling the first spindle with a third spindle;
a second pair of link arms coupling the second spindle with the third spindle;
a drive element coupled with the third spindle to simultaneously rotate the first antenna via the first pair of link arms and the second antenna via the second pair of link arms;
an azimuth base element, the first spindle, the second spindle, and the third spindle each being rotatably coupled with the azimuth base element; and
an azimuth drive element coupled with the azimuth base element, the azimuth drive element being configured to rotate the azimuth base element about an azimuth axis orthogonal to axes of the first and second spindles.

17. A method of rotationally coupling antennas comprising:
coupling a first spindle to a first antenna, the first antenna having a first boresight;
coupling a second spindle to a second antenna, the second antenna having a second boresight that is not parallel to the first boresight;
coupling a first pair of link arms between the first spindle and a third spindle;
coupling a second pair of link arms between the second spindle and the third spindle; and
coupling a drive element to the third spindle to simultaneously rotate the first antenna via the first pair of link arms and the second antenna via the second pair of link arms.

18. The method of claim 17 , wherein a link arm of the first and second pairs of link arms has a fixed length.

19. The method of claim 17 , wherein a link arm of the first and second pairs of link arms includes a turnbuckle.

20. The method of claim 18 , wherein the turnbuckle comprises two bearing rod ends, each bearing rod end being coupled with one of the first or second spindles.

21. A method of rotationally coupling antennas, comprising:
coupling a first spindle to a first antenna;
coupling a second spindle to a second antenna;
coupling a first pair of link arms between the first spindle and a third spindle;
coupling a second pair of link arms between the second spindle and the third spindle, wherein a link arm from the first pair of link arms or a link arm from the second pair of link arms is adjustable to change a first amount of backlash between the first spindle and the third spindle, or to change a second amount of backlash between the second spindle and the third spindle; and
coupling a drive element to the third spindle to simultaneously rotate the first antenna via the first pair of link arms and the second antenna via the second pair of link arms.

22. The method of claim 17 , wherein the first pair of link arms are separated by a first distance, and the second pair of link arms are separated by a second distance, the second distance being different from the first distance.

23. The method of claim 17 , wherein one of the first pair of link arms, the second pair of link arms, and the drive element may be installed or removed irrespective of the presence or absence of the others of the first pair of link arms, the second pair of link arms, and the drive element.

24. The method of claim 17 , wherein an end of one link arm of the first pair of link arms and an end of one link arm of the second pair of link arms are both coupled with the third spindle at a first radial distance as measured from an axis of the third spindle.

25. The method of claim 24 , wherein an end of the other link arm of the first pair of link arms and an end of the other link arm of the second pair of link arms are both coupled with the third spindle at a second radial distance as measured from the axis of the third spindle.

26. The method of claim 17 , wherein the first antenna and the second antenna operate over different frequency bands.

27. The method of claim 17 , wherein the drive element comprises a mot

Assignees

• Viasat Inc

Inventors

• Newkirk Jack C
• Holt B Wayne
• Smith Bradley H
• Skinner Kevin M
• Blalock E Mitchell

Classifications

• H01Q3/08

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• H04B7/18508

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