IP Library › Granted Patent US 12,394,900
Granted Patent B2
US 12,394,900 · App. 18/170,847 · Granted Aug 19, 2025

Bandwidth extended balanced tightly coupled dipole array additively manufactured modular aperture

Inventors: Alexander D. Johnson (Waltham, MA); James F. Fung (Manchester, NH); Randall R. Lapierre (Hooksett, NH)
Assignee: BAE Systems Information and Electronic Systems Integration Inc.
H01Q5/48H01Q21/12
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Quick Facts
Patent No.
US 12,394,900
App. No.
18/170,847
Granted
Aug 19, 2025
Kind
B2
Abstract

An antenna assembly includes a balanced antenna feed configured to receive a differential signal and a ground plane. The assembly further includes a first conductive dipole arm in planar alignment with a surface of the ground plane and a second conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the first conductive dipole arm. The assembly further includes a first feedline in electrical communication with the first conductive dipole arm and the balanced antenna feed and a second feedline in electrical communication with the second conductive dipole arm and the balanced antenna feed. The assembly further includes a conductive wall (“H-wall”) in electrical communication with the ground plane and having an end adjacent to, and physically separate from, the second conductive dipole arm. The H-wall has an axial length orthogonal to the ground plane.

Claims (44)

1. An antenna assembly comprising:

a balanced antenna feed configured to receive a differential signal;

a ground plane;

a first conductive dipole arm in planar alignment with a surface of the ground plane;

a second conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the first conductive dipole arm;

a first feedline in electrical communication with the first conductive dipole arm and the balanced antenna feed;

a second feedline in electrical communication with the second conductive dipole arm and the balanced antenna feed; and

a conductive wall in electrical communication with the ground plane and having an end parallel with the ground plane and adjacent to, and physically separate from, the second conductive dipole arm, an axial length of the conductive wall being orthogonal to the ground plane.

2. The antenna assembly of claim 1 , further comprising at least one non-conductive structural support element between the ground plane and the first feedline, the second feedline, or both.

3. The antenna assembly of claim 2 , wherein the at least one non-conductive structural support includes a dielectric foam or resin.

4. The antenna assembly of claim 1 , further comprising:

a third conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the second conductive dipole arm;

a fourth conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the third conductive dipole arm;

a third feedline in electrical communication with the third conductive dipole arm and the balanced antenna feed; and

a fourth feedline in electrical communication with the fourth conductive dipole arm and the balanced antenna feed.

5. The antenna assembly of claim 4 , wherein the end of the conductive wall is further adjacent to, and physically separate from, the third conductive dipole arm.

6. The antenna assembly of claim 4 , wherein the third conductive dipole arm is perpendicular to the second conductive dipole arm.

7. The antenna assembly of claim 6 , wherein the first conductive dipole arm is parallel to the second conductive dipole arm, and wherein the fourth conductive dipole arm is parallel to the third conductive dipole arm.

8. The antenna assembly of claim 4 , wherein the first and second conductive dipole arms are linearly polarized with respect to a first plane of polarization, wherein the third and fourth conductive dipole arms are linearly polarized with respect to a second plane of polarization, and wherein the first plane of polarization is orthogonal to the second plane of polarization.

9. The antenna assembly of claim 1 , further comprising an integral element additively manufactured into a single continuous piece of material, the integral element including the ground plane, the first conductive dipole arm, the second conductive dipole arm, the first feedline, the second feedline, and the conductive wall.

10. The antenna assembly of claim 9 , wherein the integral element includes an electrically conductive material.

11. The antenna assembly of claim 9 , wherein the integral element includes a non-conductive material plated with an electrically conductive material.

12. The antenna assembly of claim 1 , further comprising an aperture configured to provide up to a 10:1 bandwidth ratio.

13. An antenna assembly method comprising:

additively manufacturing an integral element as a single continuous piece of material, the integral element comprising:

a balanced antenna feed configured to receive a differential signal;

a ground plane;

a first conductive dipole arm in planar alignment with a surface of the ground plane;

a second conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the first conductive dipole arm;

a first feedline in electrical communication with the first conductive dipole arm and the balanced antenna feed;

a second feedline in electrical communication with the second conductive dipole arm and the balanced antenna feed; and

a conductive wall in electrical communication with the ground plane and having an end in parallel with the ground plane and adjacent to, and physically separate from, the second conductive dipole arm, an axial length of the conductive wall being orthogonal to the ground plane; and

attaching a superstrate to the integral element.

14. The antenna assembly method of claim 13 , further comprising attaching at least one non-conductive structural support element between the ground plane and the first feedline, the second feedline, or both.

15. The antenna assembly method of claim 14 , wherein the at least one non-conductive structural support includes a dielectric foam or resin.

16. The antenna assembly method of claim 13 , wherein the integral element includes an electrically conductive material.

17. The antenna assembly method of claim 13 , wherein the integral element includes a non-conductive material plated with an electrically conductive material.

18. The antenna assembly method of claim 13 , wherein the integral element further comprises:

a third conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the second conductive dipole arm;

a fourth conductive dipole arm in planar alignment with the surface of the ground plane and adjacent to the third conductive dipole arm;

a third feedline in electrical communication with the third conductive dipole arm and the balanced antenna feed; and

a fourth feedline in electrical communication with the fourth conductive dipole arm and the balanced antenna feed.

19. The antenna assembly method of claim 18 , wherein the first and second conductive dipole arms are linearly polarized with respect to a first plane of polarization, wherein the third and fourth conductive dipole arms are linearly polarized with respect to a second plane of polarization, and wherein the first plane of polarization is orthogonal to the second plane of polarization.

20. The antenna assembly method of claim 13 , further comprising an aperture configured to provide up to a 10:1 bandwidth ratio.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 21, 2023
From: JOHNSON, ALEXANDER D.; FUNG, JAMES F.; LAPIERRE, RANDALL R.
To: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.
Reel/Frame 062756/0693 →
Continuity (1)
Related Publication 20240283154A1 · Aug 22, 2024
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