High-gain antenna with cavity between feed line and ground plane

Patent metadata

Field	Value
Publication number	US-11276933-B2
Application number	US-201916675357-A
Country	US
Kind code	B2
Filing date	Nov 6, 2019
Priority date	Nov 6, 2019
Publication date	Mar 15, 2022
Grant date	Mar 15, 2022

Abstract

An antenna device includes a conductive patch antenna element and a conductive feed line. The conductive feed line and the conductive patch antenna element are separated by one or more first dielectric layers. The antenna device also includes a ground plane. The ground plane is separated from the conductive feed line by a spacer structure that defines one or more walls of a cavity between the conductive feed line and the ground plane. The spacer structure includes one or more second dielectric layers.

First claim

What is claimed is:

1. An antenna device comprising:
a conductive patch antenna element;
a conductive feed line, wherein the conductive feed line and the conductive patch antenna element are separated by one or more first dielectric layers; and
a ground plane, wherein the ground plane is separated from the conductive feed line by a spacer structure defining one or more walls of a cavity between the conductive feed line and the ground plane and including one or more second dielectric layers, wherein the ground plane is separated from the conductive patch antenna element by the conductive feed line.

2. The antenna device of claim 1 , further comprising one or more additional conductive patch antenna elements separated from the conductive feed line by the one or more first dielectric layers.

3. The antenna device of claim 1 , further comprising:
a second conductive patch antenna element; and
a second conductive feed line, wherein the one or more first dielectric layers separate the second conductive patch antenna element and the second conductive feed line, wherein the cavity extends between the second conductive feed line and the ground plane.

4. The antenna device of claim 3 , further comprising a power divider structure connecting the conductive feed line and the second conductive feed line to a third conductive feed line.

5. The antenna device of claim 1 , wherein the conductive patch antenna element comprises a slotted circular metal member.

6. The antenna device of claim 1 , wherein the conductive feed line has a first width along a direction parallel to a surface of the ground plane, wherein opposing walls of the cavity are separated by a second width in the direction parallel to the surface of the ground plane, and wherein the second width is greater than the first width.

7. The antenna device of claim 1 , further comprising gas disposed within the cavity.

8. The antenna device of claim 7 , wherein the gas is air.

9. The antenna device of claim 1 , wherein the one or more first dielectric layers includes a first dielectric layer having a first layer side and a second layer side opposite the first layer side, wherein the conductive feed line has a first line side and a second line side opposite to the first line side, wherein the conductive patch antenna element is coupled to the first dielectric layer via the first layer side, wherein the first line side is coupled to the first dielectric layer via the second layer side, and wherein the ground plane and the second line side are formed on opposite sides of the cavity.

10. The antenna device of claim 9 , wherein the first dielectric layer is coupled to the conductive feed line via a second dielectric layer of the one or more first dielectric layers.

11. The antenna device of claim 1 , wherein materials of the conductive patch antenna element, the conductive feed line, the one or more first dielectric layers, the ground plane, and the spacer structure are pliable to conform to a curved surface.

12. A method of forming an antenna device, the method comprising:
forming a conductive patch antenna element on a first dielectric layer;
forming a conductive feed line on the first dielectric layer or on a second dielectric layer;
forming one or more walls defining a cavity in a third dielectric layer; and
forming a stack such that a first spacer structure separates the conductive patch antenna element and the conductive feed line and a second spacer structure separates the conductive feed line and the ground plane, wherein the first spacer structure includes the first dielectric layer, the second dielectric layer, or both, wherein the second spacer structure includes the third dielectric layer, and wherein the ground plane is separated from the conductive patch antenna element by the conductive feed line.

13. The method of claim 12 , wherein the conductive patch antenna element is formed by subtractively patterning a conductive material on the first dielectric layer to define a slotted circular member.

14. The method of claim 12 , wherein the conductive patch antenna element is formed by adding a conductive material to a surface of the first dielectric layer to define a slotted circular member.

15. The method of claim 12 , wherein the conductive feed line is formed by subtractively patterning a conductive material on the second dielectric layer to define a plurality of traces interconnected by one or more power divider structures.

16. The method of claim 12 , wherein the conductive feed line is formed by adding a conductive material to a surface of the second dielectric layer to define a plurality of traces interconnected by one or more power divider structures.

17. The method of claim 12 , wherein forming the stack includes:
aligning structures of two or more dielectric layers; and
adhering the two or more dielectric layers to one another.

18. The method of claim 12 , further comprising attaching the ground plane or a coating underlying the ground plane to a contoured surface of a structure.

19. The method of claim 18 , wherein the structure is a portion of an aircraft.

20. A system comprising:
a structure defining a surface;
communication equipment at least partially within the structure; and
an antenna device physically coupled to the surface of the structure and electrically coupled to the communication equipment, the antenna device comprising:
a conductive patch antenna element disposed on a surface of a circuit board;
a conductive feed line embedded within the circuit board;
a ground plane; and
a spacer structure separating the conductive feed line and the ground plane, the spacer structure defining one or more walls of a cavity between the conductive feed line and the ground plane and including one or more dielectric layers, wherein the ground plane is separated from the conductive patch antenna element by the conductive feed line.

21. The system of claim 20 , wherein the structure comprises an aircraft, a spacecraft, a watercraft, or a land vehicle.

Assignees

• Boeing Co

Inventors

• Rogers John E

Classifications

• H01Q1/34

  Adaptation for use in or on ships, submarines, buoys or torpedoes (for subaqueous use H01Q1/04) · CPC title

• H01Q9/0428

  radiating a circular polarised wave · CPC title

• H01Q21/0037

  linear waveguide fed arrays · CPC title

• H01Q9/0457 Primary

  electromagnetically coupled to the feed line · CPC title

• H01Q1/241

  used in mobile communications, e.g. GSM (H01Q1/247, H01Q1/248 take precedence) · CPC title