Compliant, internally cooled antenna apparatus and method

• US 20070035448A1
• Filed: 08/09/2005
• Published: 02/15/2007
• Est. Priority Date: 08/09/2005
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Navarro, Julio, Bostwick, Richard, Bolster, Mark
• Granted Patent: US 7,443,354 B2
• Time in Patent Office: Days
• US Class Current: 343/700.MS
• CPC Class Codes: H01Q 1/02 Arrangements for de-icing; Arrangements for drying-out ; Arrangements for cooling; Arrangements for preventing corrosion
• CPC Class Codes: H01Q 21/0025 Modular arrays
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence

Abstract

A phased array antenna system including a mandrel having compliant portions and an internally formed cooling passageway. The compliant portions are formed by removing portions of material along one end of the mandrel to form a plurality of pairs of generally U-shaped, leaf spring-like connecting areas. The connecting areas allow a degree of movement of a lower portion of the mandrel relative to the remainder of the mandrel, when the mandrel is fixedly secured to a printed wiring board (PWB). This enables flexible electrical interconnects, positioned over the compliant portions, to make electrical contact with circuit traces on the PWB, even if the PWB has a curved or undulating surface.

Claims

1. An antenna system comprising:

an elongated mandrel for supporting a plurality of electronics subassemblies;

the mandrel having material removed at one end to form a plurality of leaf spring like sections;

each said leaf spring like section enabling a subsection of the mandrel to be able to flex relative to other subsections such that the mandrel forms a conformable support member that can be secured to an external electrical component and conform to a surface curvature of the external electrical component.

2. The antenna system of claim 1, wherein said leaf spring like sections form opposing U-shaped leaf spring like sections along a common end of said mandrel.

3. The antenna system of claim 2, wherein said leaf spring like sections further define cut-outs;

and

said antenna system further including at least one flexible electrical interconnect assembly that is disposed over said end of said mandrel.

4. The antenna system of claim 3, wherein the mandrel comprises a length of metallic material having a hollowed out portion for receiving a flowing cooling medium to cool the mandrel.

5. The antenna system of claim 4, wherein the mandrel further comprises a hollowed area adjacent the hollowed out portion for allowing air flow circulation through the mandrel.

6. The antenna system of claim 5, further comprising an antenna integrated printed wiring board having a plurality of radiating elements mounted to a surface of said mandrel opposite said end along which said leaf spring like sections are formed.

7. An antenna system comprising:

an elongated mandrel for supporting a plurality of electronic printed wiring boards along a side portion thereof;

the mandrel having material removed at opposing sides of one end to form a plurality of leaf spring like sections along a length thereof;

each said leaf spring like section enabling a subsection of the mandrel to be able to flex relative to other subsections such that the mandrel forms a conformable support member that can be secured to an external electrical component and conform to a surface curvature of the external electrical component; and

the mandrel further including a fluid passageway for enabling a cooling medium to be circulated through the mandrel to assist in cooling the mandrel during operating of the antenna system.

9. The antenna system of claim 7, further comprising a plurality of antenna wiring boards each having a plurality of radiating elements, and being supported on a surface of said mandrel opposite to said one end, and in electrical communication with an associated one of said electronic printed wiring boards.

10. The antenna system of claim 7, further comprising a flexible interconnect assembly supported on said one end of said mandrel for enabling electrical communication with an external electrical circuit component.

8. The antenna system of claim 8, further comprising a plurality of electronic printed wiring boards secured to opposite side surfaces of the mandrel and in thermal communication with the mandrel.

11. A method for forming a phased array antenna, the method comprising:

forming a metallic material into an elongated support mandrel;

forming a hollowed area in the mandrel;

forming a pair of opposing slots, in sections, at one end of the mandrel, and along a length of the mandrel such that a plurality of independent, flexible sections are formed that enable the mandrel to be secured to an undulating component while making contact with said undulating component along substantially an entire length of the mandrel; and

securing a plurality of electronic components to side surfaces of the mandrel.

12. An antenna system comprising:

a thermally conductive core component, the core component having an internal flow passage;

an electronic component supported from the core component in a manner to transmit heat generated by the electronic component to the core component; and

a cooling medium in communication with the core component for circulating a cooling medium through the core component to absorb and carry away heat absorbed by the core component, to thus cool the electronic component.

13. The system of claim 12, further comprising:

a core component having material removed from one end thereof to form a compliant end portion defined by at least one slot;

a flexible electrical circuit interconnect disposed at least partially within the slot, and in electrical communication with said electronic component; and

a printed wiring board in communication with said flexible electrical circuit interconnect.

14. The system of claim 12, wherein the manifold comprises a first manifold portion coupled to a first side of said core component for supplying said cooling medium into said core component, and a second manifold portion for receiving said cooling medium after said cooling medium has circulated through said core component.

15. The system of claim 12, wherein said core component comprises an elongated component for supporting a plurality of electronic components in side by side fashion therefrom.

16. The system of claim 15, wherein said one end of said module includes a plurality of slots for defining a plurality of distinct compliant end portions.

17. The system of claim 12, wherein said core component further includes a plurality of secondary internal passages for permitting airflow therethrough.

18. The system of claim 12, wherein said core component is comprised of a single piece of aluminum.