Structural reconfigurable antenna

Patent metadata

Field	Value
Publication number	US-9899732-B2
Application number	US-201615342094-A
Country	US
Kind code	B2
Filing date	Nov 2, 2016
Priority date	Feb 15, 2016
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A reconfigurable antenna is provided having a liquid metal in contact with an electrolyte with the liquid metal being in a first configuration. A plurality of electrodes includes a first electrode in contact with the liquid metal and a second electrode in contact with the electrolyte. A voltage source connected across the first and second electrodes applies a voltage of a predetermined magnitude and a predetermined polarity in order to move the liquid metal from the first configuration to a second configuration and to measure resultant current flow and modify the applied voltage based on the resultant current flow. Cessation of the applied voltage locks the liquid metal in this second configuration.

First claim

We claim:

1. A selectively reconfigurable antenna system ( 100 ), comprising:
a first material layer ( 105 ) and a second material layer ( 106 ) defining a cavity ( 104 ) there between;
a first reservoir ( 207 ) and a liquid metal ( 205 ) at least partially in the first reservoir;
a second reservoir ( 215 ) and a liquid electrolyte ( 209 ) at least partially in the second reservoir such that the liquid metal and the electrolyte are in contact at a metal oxide layer ( 108 ) in the cavity; and
a plurality of electrodes ( 107 , 111 , and 203 ) in electrical communication with the cavity, with a first electrode ( 107 ) being in contact with the liquid metal and a second electrode ( 111 ) being in contact with the electrolyte such that the metal oxide layer breaks down when a negative potential ( 113 ) is applied to the second electrode relative to the first electrode.

2. The system in accordance with claim 1 , wherein the liquid metal is attracted to the second electrode by virtue of the negative potential thereof.

3. The system in accordance with claim 1 , wherein a first portion ( 211 ) of the plurality of electrodes is attached to the first material layer and a second portion ( 203 ) of the plurality of electrodes is attached to the second material layer.

4. The system in accordance with claim 1 , wherein the liquid metal comprises one of Gallium and Mercury.

5. The system in accordance with claim 4 , wherein the liquid metal comprises a eutectic alloy of Gallium and Indium “EGaIn”.

6. The system in accordance with claim 1 , wherein the electrolyte is sodium hydroxide “NaOH”.

7. The system in accordance with claim 1 , further comprising a liquid metal structure ( 401 , 600 , 602 , 604 , 606 ) within the cavity formed by selectively breaking the oxide layer and moving the liquid metal via the application of potential between at least one pair of the electrodes.

8. The system in accordance with claim 7 , wherein the liquid metal structure is one of a curtain, a window, an aperture, a frequency-selective surface, and a thermal sink.

9. The system in accordance with claim 7 , wherein the liquid metal structure comprises at least one of a monopole antenna, a dipole antenna, a Vivaldi horn element, a bowtie element, and a patch element.

10. The system in accordance with claim 1 , wherein the first and second material layers are planar.

11. The system in accordance with claim 1 , wherein the first and second material layers conform to a curved surface ( 608 ).

12. The system in accordance with claim 11 , wherein the curved surface in an aircraft outer mold line.

13. The system in accordance with claim 1 , wherein at least one of the plurality of electrodes is an electrical connector ( 211 ) linked to the liquid metal at an edge of the cavity.

14. The system in accordance with claim 13 , wherein the electrical connector is an elongate shape ( 211 ) configured to contact the liquid metal internally with respect to any surface layer.

15. A phased array ( 400 ) comprising a plurality of the selectively reconfigurable antenna systems according to claim 1 .

16. A method ( 700 ) of configuring an antenna, the method comprising:
placing ( 702 ) a liquid metal ( 205 ) and an electrolyte ( 209 ) between two surfaces ( 105 , 106 ) such that the liquid metal and the electrolyte are in contact at an interface layer ( 108 ) which includes a surface oxide;
initiating ( 704 ) application of a voltage ( 113 ) between the electrolyte and a portion of the liquid metal to generate an electric field at the interface layer, at least party breaking down ( 706 ) the surface oxide and causing movement of the portion of the liquid metal toward the electrolyte; and
ceasing ( 708 ) application of the voltage between the electrolyte and the portion of the liquid metal to freeze the interface layer in place when the liquid metal reaches a predetermined configuration.

17. The method in accordance with claim 16 , wherein the interface layer is an oxide of the liquid metal.

18. The method in accordance with claim 17 , wherein the application of the voltage breaks down the interface layer.

19. The method in accordance with claim 16 , wherein the liquid metal comprises Gallium and the electrolyte comprises sodium hydroxide “NaOH”.

20. The method in accordance with claim 16 , wherein ceasing application of the voltage between the electrolyte and the portion of the liquid metal causes the surface oxide layer to re-form.

21. A reconfigurable antenna ( 401 , 600 , 602 , 604 , 606 ) comprising:
a liquid metal ( 205 ) in contact with an electrolyte ( 209 ) and being in a first configuration ( 206 );
a plurality of electrodes ( 203 , 211 ) including a first electrode ( 211 ) in contact with the liquid metal and a second electrode ( 203 ) in contact with the electrolyte; and
a voltage source ( 115 ) connected across the first and second electrodes and configured to apply a voltage ( 113 ) of a predetermined magnitude and a predetermined polarity in order to move the liquid metal from the first configuration to a second configuration and to measure resultant current flow and modify the applied voltage based on the resultant current flow.

22. The antenna of claim 21 , wherein cessation of the applied voltage locks the liquid metal in the second configuration.

23. The reconfigurable antenna of claim 21 , wherein at least one of the first configuration and the second configuration is a two-dimensional configuration.

Assignees

• Boeing Co

Inventors

• Urcia Jr Manny S
• Adams Alec
• White Edward V

Classifications

• H01Q1/364 Primary

  using a particular conducting material, e.g. superconductor · CPC title

• H01Q3/01

  varying the shape of the antenna or antenna system · CPC title

• H01Q1/286

  substantially flush mounted with the skin of the craft · CPC title

• H01Q21/22

  Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array · CPC title

• H01Q1/085

  Flexible aerials; Whip aerials with a resilient base · CPC title