Satellite communication terminal with reconfigurable support structures

Patent metadata

Field	Value
Publication number	US-10135113-B2
Application number	US-201715598238-A
Country	US
Kind code	B2
Filing date	May 17, 2017
Priority date	May 20, 2016
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

Techniques and mechanisms for enabling the positioning of a communication terminal in or on a vehicle, building or other structure. In an embodiment, the communication terminal includes an electronically steerable antenna which is disposed in a housing. A plurality of support legs, coupled to the housing, are each configured to rotate about a respective first axis, and to further rotate about a respective second axis. For a given support leg, an orientation of the respective second axis varies with rotation of that support leg about the respective first axis. Two such support legs are mechanically coupled to one another with respect to their respective first axis rotations or with respect to their respective second axis rotations. In another embodiment, the communication terminal is operable by a user to selectively enable or disable first axis rotation and/or second axis rotation of a given support leg.

First claim

What is claimed is:

1. An apparatus comprising:
a housing;
an electronically steerable antenna disposed in the housing, the electronically steerable antenna to communicate signals through the housing; and
a plurality of support legs each hingedly coupled to the housing, wherein, for each support leg of the plurality of support legs:
the support leg is configured to rotate about a respective first axis which is fixed relative to the housing;
the support leg is configured to further rotate about a respective second axis which is variable with rotation of the support leg about the respective first axis.

2. The apparatus of claim 1 , wherein the plurality of support legs includes a first support leg and a second support leg, wherein the plurality of support legs is configured to provide a respective first rotation of the second support leg in response to a respective first rotation of the first support leg.

3. The apparatus of claim 2 , wherein the plurality of support legs is further configured to provide a respective second rotation of the second support leg in response to a respective second rotation of the first support leg.

4. The apparatus of claim 1 , wherein the plurality of support legs includes a first support leg and a second support leg, wherein the plurality of support legs is configured to provide a respective second rotation of the second support leg in response to a respective second rotation of the first support leg.

5. The apparatus of claim 1 , wherein the plurality of support legs includes a first support leg, the apparatus further comprising an actuator operable by a user to selectively enable or disable a respective first rotation of the first support leg.

6. The apparatus of claim 5 , wherein the plurality of support legs further includes a second support leg, wherein the plurality of support legs is configured to enable the respective first rotation of the first support leg only while a respective second rotation of the first support leg is disabled.

7. The apparatus of claim 5 , wherein the plurality of support legs further includes a second support leg, wherein the actuator is operable by the user to further selectively enable or disable a respective first rotation of the second support leg.

8. The apparatus of claim 5 , further comprising another actuator operable by the user to selectively enable or disable a respective second rotation of the first support leg.

9. The apparatus of claim 1 , wherein the plurality of support legs includes a first support leg, the apparatus further comprising an actuator operable by a user to selectively enable or disable a respective second rotation of the first support leg.

10. The apparatus of claim 9 , wherein the plurality of support legs further includes a second support leg, wherein the plurality of support legs is configured to enable the respective second rotation of the first support leg only while a respective first rotation of the first support leg is disabled.

11. The apparatus of claim 9 , wherein the plurality of support legs further includes a second support leg, wherein the actuator is operable by the user to further selectively enable or disable a respective second rotation of the second support leg.

12. The apparatus of claim 1 , the apparatus further comprising an actuator operable by a user to selectively enable or disable one of a respective first rotation of the first support leg or a respective second rotation of the first support leg, wherein the actuator moves with the respective first rotation of the first support leg, and wherein the actuator moves with the respective second rotation of the first support leg.

13. A method comprising:
communicating signals through a housing with an electronically steerable antenna which is disposed in the housing; and
positioning the housing and the electronically steerable antenna with a plurality of support legs each hingedly coupled to the housing, the positioning including, for each of the plurality of support legs:
rotating the support leg about a respective first axis which is fixed relative to the housing; and
rotating the support leg about a respective second axis which is variable with rotation of the support leg about the respective first axis.

14. The method of claim 13 , wherein the plurality of support legs includes a first support leg and a second support leg, wherein a respective first rotation of the second support leg is in response to a respective first rotation of the first support leg.

15. The method of claim 14 , wherein a respective second rotation of the second support leg is in response to a respective second rotation of the first support leg.

16. The method of claim 13 , wherein the plurality of support legs includes a first support leg and a second support leg, wherein a respective second rotation of the second support leg is in response to a respective second rotation of the first support leg.

17. The method of claim 13 , wherein the plurality of support legs includes a first support leg, the method further comprising selectively enabling or disabling a respective first rotation of the first support leg.

18. The method of claim 17 , wherein the plurality of support legs further includes a second support leg, wherein the respective first rotation of the first support leg is enabled only while a respective second rotation of the first support leg is disabled.

19. The method of claim 17 , wherein the plurality of support legs further includes a second support leg, the method further comprising selectively enabling or disabling a respective first rotation of the second support leg.

20. The method of claim 17 , the method further comprising selectively enabling or disabling a respective second rotation of the first support leg.

21. The method of claim 13 , wherein the plurality of support legs includes a first support leg, the method further comprising selectively enabling or disabling a respective second rotation of the first support leg.

22. The method of claim 21 , wherein the plurality of support legs further includes a second support leg, wherein the respective second rotation of the first support leg is enabled only while a respective first rotation of the first support leg is disabled.

23. The method of claim 21 , wherein the plurality of support legs further includes a second support leg, the method further comprising selectively enabling or disabling a respective second rotation of the second support leg.

24. The method of claim 13 , the method further comprising selectively enabling or disabling one of a respective first rotation of the first support leg or a respective second rotation of the first support leg, the selective enabling or disabling in response to operation of an actuator which moves with the respective first rotation of the first support leg, wherein the actuator further moves with the respective second rotation of the first support leg.

Assignees

• Fotheringham David
• Nonis Adam
• Kymeta Corp

Inventors

• Fotheringham David
• Nonis Adam

Classifications

• H01Q21/065

  Patch antenna array · CPC title

• H01Q1/3208

  characterised by the application wherein the antenna is used · CPC title

• H04B7/18515

  Transmission equipment in satellites or space-based relays · CPC title

• H01Q21/24

  Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction {(circularly polarised patch antennas H01Q9/0428; circularly polarised horns H01Q13/0241; cross-polarised horns H01Q13/0258; polarisation converters H01Q15/242; cross-polarised rear feeds H01Q19/136; crossed polarisation dual antenna H01Q25/001)} · CPC title

• H01Q1/288

  Satellite antennas · CPC title