IP Library › Granted Patent US 8,045,329
Granted Patent B2
US 8,045,329 · App. 12/432,496 · Granted Oct 25, 2011

Thermal dissipation mechanism for an antenna

Assignee: Raytheon Company
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Quick Facts
Patent No.
US 8,045,329
App. No.
12/432,496
Granted
Oct 25, 2011
Kind
B2
Abstract

According to one embodiment, a heat dissipation system includes an elongated radar absorbing member configured with a thermal dissipation mechanism. The radar absorbing member extends proximate a junction of a microwave antenna enclosure that houses an antenna and a radome that covers an opening in the microwave antenna enclosure. The radar absorbing member absorbs electro-magnetic energy incident upon the junction. The thermal dissipation mechanism absorbs heat generated by the absorbed electro-magnetic energy.

Claims (33)

1. A microwave transmission system comprising:

a microwave antenna enclosure;

a radome that covers an opening in the microwave antenna enclosure, the microwave antenna enclosure and the radome made of differing materials such that an electrical discontinuity is formed at a junction of the microwave antenna enclosure and the radome;

an elongated radar absorbing member extending proximate the junction, the radar absorbing member operable to absorb electro-magnetic energy incident upon the junction; and

one or more hollow tubes operable to convey a coolant through the elongated radar absorbing member, the one or more hollow tubes fluidly coupled to a cooling system of a microwave antenna configured in the microwave antenna enclosure having one or more radiating elements, the cooling system operable to remove heat from the radiating elements and the radar absorbing member.

2. A heat dissipation system comprising:

an elongated radar absorbing member extending proximate a junction of a microwave antenna enclosure and a radome that covers an opening in the microwave antenna enclosure, the microwave antenna enclosure and the radome made of differing materials such that an electrical discontinuity is formed at the junction, the radar absorbing member operable to absorb electro-magnetic energy incident upon the junction; and

a thermal dissipation mechanism configured in the elongated radar absorbing member and operable to remove heat away from the elongated radar absorbing member, wherein the thermal dissipation mechanism comprises one or more hollow tubes that are operable to convey a coolant through the elongated radar absorbing member for removing heat from the elongated radar absorbing member.

3. The heat dissipation system of claim 2 , wherein the coolant is operable to be conveyed through the one or more hollow tubes using a convective action of the coolant.

4. The heat dissipation system of claim 2 , wherein the coolant is operable to be conveyed through the one or more hollow tubes using a pump.

5. The heat dissipation system of claim 2 , wherein the one or more hollow tubes are fluidly coupled to a cooling system of a microwave antenna configured in the microwave antenna enclosure having one or more radiating elements, the cooling system operable to remove heat from the radiating elements and the radar absorbing member.

6. The heat dissipation system of claim 2 , wherein the one or more hollow tubes are thermally coupled to a support frame of the microwave antenna enclosure such that the support frame receives heat from the one or more hollow tubes.

7. The heat dissipation system of claim 2 , wherein the one or more tubes have a circular cross-sectional shape.

8. The heat dissipation system of claim 2 , wherein the one or more hollow tubes comprises a single tube having a cross-sectional shape generally similar to the cross-sectional shape of the radar absorbing member.

9. The heat dissipation system of claim 8 , wherein the radar absorbing member has a wedge cross-sectional shape.

10. The heat dissipation system of claim 2 , wherein the antenna is operable to generate the electro-magnetic energy having a power density greater than 5 Watts per square inch.

11. The heat dissipation system of claim 2 , wherein the thermal dissipation mechanism comprises a thermally conductive material that thermally couples the elongated radar absorbing member to the microwave antenna enclosure.

12. The heat dissipation system of claim 11 , wherein the thermally conductive material comprises a metallic material.

13. A microwave transmission system comprising:

a microwave antenna enclosure;

a radome that covers an opening in the microwave antenna enclosure, the microwave antenna enclosure and the radome made of differing materials such that an electrical discontinuity is formed at a junction of the microwave antenna enclosure and the radome;

an elongated radar absorbing member extending proximate the junction, the radar absorbing member operable to absorb electro-magnetic energy incident upon the junction; and

a thermal dissipation mechanism configured in the elongated radar absorbing member and operable to remove heat away from the elongated radar absorbing member, wherein the thermal dissipation mechanism comprises one or more hollow tubes that are operable to convey a coolant through the elongated radar absorbing member for removing heat from the elongated radar absorbing member.

14. The microwave transmission system of claim 13 , wherein the thermal dissipation mechanism comprises a thermally conductive material that thermally couples the elongated radar absorbing member to the microwave antenna enclosure.

15. The microwave transmission system of claim 14 , wherein the thermally conductive material comprises a metallic material.

16. The microwave transmission system of claim 13 , wherein the coolant is operable to be conveyed through the one or more hollow tubes using a convective action of the coolant.

17. The microwave transmission system of claim 13 , wherein the coolant is operable to be conveyed through the one or more hollow tubes using a pump.

18. The microwave transmission system of claim 13 , wherein the one or more hollow tubes are fluidly coupled to a cooling system of a microwave antenna configured in the microwave antenna enclosure having one or more radiating elements, the cooling system operable to remove heat from the radiating elements and the radar absorbing member.

19. The microwave transmission system of claim 13 , wherein the one or more hollow tubes are thermally coupled to a support frame of the microwave antenna enclosure such that the support frame receives heat from the one or more hollow tubes.

20. The microwave transmission system of claim 13 , wherein the one or more tubes have a circular cross-sectional shape.

21. The microwave transmission system of claim 13 , wherein the one or more hollow tubes comprises a single tube having a cross-sectional shape generally similar to the cross-sectional shape of the radar absorbing member.

22. The microwave transmission system of claim 21 , wherein the radar absorbing member has a wedge cross-sectional shape.

23. The microwave transmission system of claim 13 , wherein the antenna is operable to generate the electro-magnetic energy having a power density greater than 5 Watts per square inch.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 29, 2009
From: CHEN, KEVIN W.; HAROKOPUS, WILLIAM P.; CUNNINGHAM, PATRICK W.
To: RAYTHEON COMPANY
Reel/Frame 022616/0094 →
Continuity (1)
Related Publication 20100277867A1 · Nov 4, 2010