IP Library Granted Patent US 10,658,758
Granted Patent B2
US 10,658,758 · App. 14/254,955 · Granted May 19, 2020

Modular antenna assembly

Inventors: Joseph L. Hafenrichter (Seattle, WA); Manny S. Urcia (Bellevue, WA); Joseph A. Marshall (Kent, WA); Charles W. Manry, Jr. (Auburn, WA); Mohammad-Nasar M. Adeeyo (Seattle, WA)
Assignee: The Boeing Company
H01Q21/0025H01Q1/40H01Q21/0087H01Q21/061
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Quick Facts
Patent No.
US 10,658,758
App. No.
14/254,955
Granted
May 19, 2020
Kind
B2
Abstract

Embodiments of the present disclosure provide an antenna assembly that includes a plurality of separate and distinct antenna modules that are interconnected together to form an antenna layer. Each of the antenna modules may include a support structure including a core frame connected to a core support, and a backskin connected to one or both of the core frame and the core support. The antenna assembly may also include an alignment grid configured to receive and align each of the antenna modules, and/or a matching layer configured to receive and align each of the antenna modules.

Claims (30)

1. An antenna assembly, comprising:

a plurality of separate and distinct antenna modules that are interconnected together to form an antenna layer, wherein portions of neighboring antenna modules abut against one another,

wherein each of the plurality of separate and distinct antenna modules comprises half-thickness outer walls that cooperate to form a full thickness outer wall when abutting against another half-thickness wall of another one of the plurality of separate and distinct antenna modules;

wherein the full thickness outer wall is defined as a thickness of internal support walls of two or more of the plurality of separate and distinct antenna modules.

2. The antenna assembly of claim 1 , further comprising an alignment grid configured to receive and align each of the plurality of separate and distinct antenna modules.

3. The antenna assembly of claim 1 , further comprising a cover layer over the plurality of separate and distinct antenna modules.

4. The antenna assembly of claim 1 , further comprising a single, unitary electronics layer operatively connected to the antenna layer, wherein the single unitary electronics layer comprises a plurality of separate and distinct electronics card modules.

5. The antenna assembly of claim 1 , wherein each of the plurality of separate and distinct antenna modules comprises a core frame connected to a core support.

6. The antenna assembly of claim 5 , wherein the core frame is separate and distinct from the core support.

7. The antenna assembly of claim 5 , wherein each of the plurality of separate and distinct antenna modules further comprises a backskin connected to one or both of the core frame and the core support.

8. The antenna assembly of claim 1 , wherein each of the plurality of separate and distinct antenna modules comprises an antenna card having a plurality of antenna elements.

9. The antenna assembly of claim 1 , wherein each of the plurality of separate and distinct antenna modules is bonded together with adhesive through rotational curing.

10. An antenna assembly, comprising:

a plurality of separate and distinct antenna modules that are interconnected together to form an antenna layer, wherein each of the plurality of separate and distinct antenna modules comprises a support structure including a core frame connected to a core support, a backskin connected to one or both of the core frame and the core support; half-thickness outer walls cooperate to form a full thickness outer wall with another half-thickness walls of another one of the plurality of separate and distinct antenna modules;

an alignment grid configured to receive and align each of the plurality of separate and distinct antenna modules; and

a cover layer configured to receive and align each of the plurality of separate and distinct antenna modules;

wherein the full thickness outer wall is defined as a thickness of internal support walls of two or more of the plurality of separate and distinct antenna modules.

11. The antenna assembly of claim 10 , further comprising an electronics layer operatively connected to the antenna layer.

12. The antenna assembly of claim 11 , wherein the electronics layer comprises a plurality of separate and distinct electronics card modules.

13. The antenna assembly of claim 10 , wherein the core frame is separate and distinct from the core support.

14. The antenna assembly of claim 10 , wherein each of the plurality of separate and distinct antenna modules further comprises an antenna card supported by the support structure, and wherein the antenna card comprises at least one antenna element.

15. The antenna assembly of claim 10 , wherein each of the plurality of separate and distinct antenna modules is bonded together with adhesive through rotational curing.

16. An antenna assembly, comprising:

a plurality of separate and distinct antenna modules that are interconnected together to form an antenna layer, wherein each of the plurality of separate and distinct antenna modules comprises half-thickness outer walls that cooperate to form a full thickness outer wall with another half-thickness walls of another one of the plurality of separate and distinct antenna modules further comprises (a) a support structure including a core frame connected to a separate and distinct core support, (b) a backskin connected to one or both of the core frame and the core support, and (c) an antenna card supported by the support structure, wherein the antenna card comprises at least one antenna element, wherein the support structure, the backskin and the antenna card are bonded together with adhesive through rotational curing;

an alignment grid configured to receive and align each of the plurality of separate and distinct antenna modules;

a cover layer configured to receive and align each of the plurality of separate and distinct antenna modules; and

an electronics layer operatively connected to the antenna layer, wherein the electronics layer comprises a plurality of separate and distinct electronics card modules;

wherein the full thickness outer wall is defined as a thickness of internal support walls of two or more of the plurality of separate and distinct antenna modules.

17. The antenna assembly of claim 16 , wherein portions of neighboring antenna modules abut against one another.

18. The antenna assembly of claim 16 , wherein the support structure, the backskin, and the antenna card are mechanically connected together, covered with a flowing adhesive, and rotated during the rotational curing so that the adhesive flows over and through the connection interfaces and interstices between the support structure, the backskin, and the antenna card.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 17, 2014
From: HAFENRICHTER, JOSEPH L.; URCIA, MANNY S.; MARSHALL, JOSEPH A.; MANRY, CHARLES W., JR.; ADEEYO, MOHAMMED-NASAR M.
To: THE BOEING COMPANY
Reel/Frame 032695/0222 →
Continuity (1)
Related Publication 20150303586A1 · Oct 22, 2015
Cited By (6)
US 12,237,575 US 12,334,630 US 12,355,148 US 12,374,772 US 12,463,333 US 12,706,374