IP Library Granted Patent US 12,586,898
Granted Patent B2
US 12,586,898 · App. 18/098,598 · Granted Mar 24, 2026

Power planes for a radio frequency (RF) metamaterial antenna

Inventors: Cagdas Varel (Seattle, WA); Steven Howard Linn (Hillsboro, WA)
Assignee: KYMETA CORPORATION
H01Q3/26H01Q21/00H01Q1/288H01Q3/36H01Q21/0031
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Quick Facts
Patent No.
US 12,586,898
App. No.
18/098,598
Granted
Mar 24, 2026
Kind
B2
Abstract

A radio-frequency (RF) antenna and method for using the same are disclosed. In some embodiments, an antenna includes an array of RF radiating antenna elements, a plurality of RF antenna element driving circuits coupled to the array of RF radiating antenna elements to supply tuning voltages to the RF radiating antenna elements, and one or more metal power planes, each of the one or more metal power planes coupled to supply a common voltage to two or more of the plurality of RF antenna driving circuits.

Claims (42)

1 . An antenna comprising:

an array of radio-frequency (RF) radiating antenna elements;

a plurality of RF antenna element driving circuits coupled to the array of RF radiating antenna elements to supply tuning voltages to the RF radiating antenna elements; and

one or more metal power planes, each of the one or more metal power planes coupled to supply a common voltage to two or more of the plurality of RF antenna driving circuits, wherein said each one or more metal power planes is electrically connected to two or more of the plurality of RF antenna driving circuits using vias.

2 . The antenna of claim 1 wherein each of the plurality of RF antenna driving circuits has a footprint and the via extends from a location within the footprint to one of the one or more metal power planes.

3 . The antenna of claim 1 wherein at least one RF antenna driving circuit of the plurality of RF antenna driving circuits is electrically connected to one metal power plane of said each one or more metal power planes by coupling an extension of the one metal power plane into the at least one RF antenna driving circuit.

4 . The antenna of claim 1 wherein the voltage of each of the one or more metal power planes is operable to transfer a direct current (DC) voltage to all of RF antenna driving circuits electrically connected to said each of the one or more metal power planes.

5 . The antenna of claim 1 further comprising:

a substrate; and

a plurality of layers deposited on top of the substrate, wherein the plurality of layers includes

an iris metal layer coupled to the substrate and containing irises, each of the irises being part of one of the RF radiating antenna elements,

one or more additional layers on the iris metal layer, wherein the one or more metal power planes are on top of the one or more additional layers.

6 . The antenna of claim 5 wherein the one or more layers comprises:

at least one passivation layer between the iris metal layer and the one or more routing lines, and further wherein the one or more metal power planes geometrically in parallel with the iris metal layer.

7 . The antenna of claim 1 wherein the one or more metal power planes are not beneath routing lines routing variable voltages to one RF antenna driving circuit of the plurality of RF antenna driving circuits.

8 . The antenna of claim 1 further comprising a bridge to electrically connect a pair of power plane segments on opposite sides of a set of one or more routing lines coupled to one or more of the RF antenna driving circuits of the plurality of RF antenna driving circuits.

9 . The antenna of claim 1 wherein the RF radiating antenna elements comprise metamaterial antenna elements.

10 . The antenna of claim 9 wherein the RF radiating antenna drive circuits are part of the active-matrix drive.

11 . An antenna comprising:

an array of radio-frequency (RF) radiating antenna elements;

a plurality of RF antenna element driving circuits coupled to the array of RF radiating antenna elements to supply tuning voltages to the RF radiating antenna elements;

one or more metal power planes, each of the one or more metal power planes coupled to supply a common Direct Current (DC) voltage to two or more of the plurality of RF antenna driving circuits, wherein said each one or more metal power planes is electrically connected to two or more of the plurality of RF antenna driving circuits using via structures; and

a bridge to electrically connect a pair of power plane segments on opposite sides of a set of one or more routing lines coupled to one or more of the RF antenna driving circuits of the plurality of RF antenna driving circuits.

12 . The antenna of claim 11 wherein each of the plurality of RF antenna driving circuits has a footprint and the via extends from a location within the footprint to one of the one or more metal power planes.

13 . The antenna of claim 11 wherein the voltage of each of the one or more metal power planes is operable to transfer the DC voltage to all of RF antenna driving circuits electrically connected to said each of the one or more metal power planes.

14 . The antenna of claim 11 wherein the one or more metal power planes are not beneath routing lines routing variable voltages to one RF antenna driving circuit of the plurality of RF antenna driving circuits.

15 . A satellite communications terminal comprising an antenna having:

a plurality of metal power planes to supply a common voltage;

an array of radio-frequency (RF) radiating antenna elements;

a plurality of RF antenna element driving circuits coupled to the array of RF radiating antenna elements to supply tuning voltages to the RF radiating antenna elements, each of the plurality of RF antenna element driving circuits having one or more nodes, wherein the one or more nodes in the plurality of RF antenna element driving circuits maintained at one or more constant voltages by coupling each the one or more nodes to one power plane of the plurality of power planes.

16 . The antenna of claim 15 further comprising:

a substrate; and

a plurality of layers deposited on top of the substrate, wherein the plurality of layers includes

an iris metal layer coupled to the substrate and containing irises, each of the irises being part of one of the RF radiating antenna elements,

one or more additional layers on the iris metal layer, wherein the one or more metal power planes are on top of the one or more additional layers and are in parallel geometrically with the iris metal layer, and further wherein at least one passivation layer between the iris metal layer and the one or more routing lines.

17 . An antenna comprising:

an array of radio-frequency (RF) radiating antenna elements, each of the RF radiating antenna elements having an iris;

a plurality of RF antenna element driving circuits coupled to the array of RF radiating antenna elements to supply tuning voltages to the RF radiating antenna elements; and

two or more metal power planes, each metal power plane of the two or more metal power planes coupled to supply a common voltage to two or more of the plurality of RF antenna driving circuits without overlapping irises of the RF radiating antenna elements in the array of RF radiating antenna elements, wherein the two or more power planes are electrically isolated from each other.

18 . The antenna of claim 17 wherein the two or more power planes are electrically isolated from each other by one or more thin film passivation layers.

19 . The antenna of claim 17 wherein each of the two or more power planes comprises power plane segments of one power plane that has been that have been connected into two or more different power planes connected to two or more different common voltages.

20 . The antenna of claim 17 further comprising a stack that includes the one or more passivation layers, routing lines, and iris metal in an iris metal layer for forming a portion of the RF antenna elements, wherein the routing lines are coupled to the RF antenna driving circuits and are isolated with passivation from iris metal in an iris metal plane.

Assignments (4)
SECURITY INTEREST Recorded Feb 7, 2025
From: KYMETA CORPORATION
To: GATES FRONTIER, LLC
Reel/Frame 070154/0001 →
SECURITY INTEREST Recorded Jul 11, 2024
From: KYMETA CORPORATION
To: TRINITY CAPITAL INC.
Reel/Frame 068276/0105 →
SECURITY INTEREST Recorded Apr 12, 2024
From: KYMETA CORPORATION
To: GATES FRONTIER, LLC
Reel/Frame 067095/0862 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 25, 2023
From: VAREL, CAGDAS; LINN, STEVEN HOWARD
To: KYMETA CORPORATION
Reel/Frame 063762/0422 →
Continuity (2)
Provisional Application 63301585 · Jan 21, 2022
Related Publication 20230238697A1 · Jul 27, 2023
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