IP Library Granted Patent US 8,279,604
Granted Patent B2
US 8,279,604 · App. 12/851,289 · Granted Oct 2, 2012

Cooling system for cylindrical antenna

Assignee: Raytheon Company
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,279,604
App. No.
12/851,289
Granted
Oct 2, 2012
Kind
B2
Abstract

According to one embodiment, an antenna cooling system, comprises a first cylinder and a second cylinder substantially concentric to the first cylinder. The first and second cylinders form a chamber between the first cylinder and the second cylinder. The chamber is configured to receive a fluid flow. A plurality of fins are disposed within the chamber and rigidly coupled to the first cylinder and the second cylinder. The plurality of fins are configured to transmit thermal energy to the fluid flow. A plurality of ports are coupled to the second cylinder. Each port is configured to receive an antenna unit.

Claims (49)

1. An antenna cooling system, comprising:

a first cylinder;

a second cylinder substantially concentric to the first cylinder, and forming a chamber between the first cylinder and the second cylinder, the chamber configured to receive a fluid flow;

a plurality of fins disposed within the chamber and rigidly coupled to the first cylinder and the second cylinder, the plurality of fins configured to transmit thermal energy to the fluid flow; and

a plurality of ports coupled to the second cylinder, each port configured to receive an antenna unit.

2. The antenna cooling system of claim 1 , each port of the plurality of ports coupling to the second cylinder opposite from a corresponding fin of the plurality of fins.

3. The antenna cooling system of claim 1 , further comprising a plurality of feedlines, each feedline of the plurality of feedlines aligned parallel with a corresponding fin of the plurality of fins, the plurality of feedlines configured to electronically couple the plurality of ports to electronics disposed within the first cylinder.

4. The antenna cooling system of claim 1 , further comprising a power supply disposed within the first cylinder.

5. The antenna cooling system of claim 1 , further comprising a cylinder cover coupled to the first cylinder and configured to prevent at least some of the fluid flow from entering the first cylinder.

6. The antenna cooling system of claim 1 , each port configured to receive a transmit/receive integrated microwave module (TRIMM) card.

7. The antenna cooling system of claim 1 , further comprising a flow diverter coupled to the second cylinder and configured to:

receive the fluid flow in a first direction;

direct the fluid flow in a second direction substantially perpendicular to the first direction; and

provide the fluid flow to the chamber in the second direction.

8. A method of cooling an antenna system, comprising:

receiving a fluid flow through a chamber, the chamber formed between a first cylinder and a second cylinder substantially concentric to the first cylinder;

transferring thermal energy from a plurality of fins to the fluid flow, the plurality of fins disposed within the chamber and rigidly coupled to the first cylinder and the second cylinder; and

electronically communicating with a plurality of antenna units through a plurality of ports of the second cylinder, each port configured to receive an antenna unit.

9. The method of claim 8 , each port of the plurality of ports coupling to the second cylinder opposite from a corresponding fin of the plurality of fins.

10. The method of claim 8 , electronically communicating with the plurality of antenna units comprising electronically coupling the plurality of ports to electronics disposed within the first cylinder.

11. An antenna cooling system, comprising:

a first cylinder;

a second cylinder substantially concentric to the first cylinder, and forming a chamber between the first cylinder and the second cylinder, the chamber configured to receive a fluid flow;

a plurality of fins disposed within the chamber and rigidly coupled to the first cylinder and the second cylinder, the plurality of fins configured to transmit thermal energy to the fluid flow; and

a plurality of heat pipes disposed between the first cylinder and the second cylinder, the plurality of heat pipes configured to be in thermal communication with a plurality of antenna units.

12. The antenna cooling system of claim 11 , further comprising:

a control circuit card disposed within the first cylinder; and

a plurality of feedlines configured to electronically couple the control circuit card to the plurality of antenna units.

13. The antenna cooling system of claim 11 , further comprising a power supply disposed within the first cylinder.

14. The antenna cooling system of claim 11 , further comprising an EMI filter disposed within the first cylinder.

15. The antenna cooling system of claim 11 , further comprising a cylinder cover coupled to the first cylinder and configured to prevent at least some of the fluid from entering the first cylinder.

16. The antenna cooling system of claim 11 , further comprising a flow diverter coupled to the second cylinder and configured to:

receive the fluid flow in a first direction;

direct the fluid flow in a second direction substantially perpendicular to the first direction; and

provide the fluid flow to the chamber in the second direction.

17. The antenna cooling system of claim 11 , further comprising a flow diverter coupled to the second cylinder and configured to:

receive the fluid flow from the chamber in a first direction; and

direct the fluid flow in a second direction substantially perpendicular to the first direction.

18. A method of cooling an antenna system, comprising:

receiving a fluid flow through a chamber, the chamber formed between a first cylinder and a second cylinder substantially concentric to the first cylinder;

transferring thermal energy from a plurality of fins to the fluid flow, the plurality of fins disposed within the chamber and rigidly coupled to the first cylinder and the second cylinder; and

transferring thermal energy from a plurality of heat pipes to the fluid flow, the plurality of heat pipes disposed between the first cylinder and the second cylinder, the plurality of heat pipes in thermal communication with a plurality of antenna units.

19. The method of claim 18 , further comprising:

receiving the fluid flow in a first direction;

directing the fluid flow in a second direction substantially perpendicular to the first direction; and

providing the fluid flow to the chamber in the second direction.

20. The method of claim 18 , further comprising:

receiving the fluid flow from the chamber in a first direction; and

directing the fluid flow in a second direction substantially perpendicular to the first direction.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 5, 2010
From: JONES, DANIEL P.; BURNSED, MILLAGE G.; COSTAS, CARLOS R.
To: RAYTHEON COMPANY
Reel/Frame 024797/0325 →
Continuity (1)
Related Publication 20120033383A1 · Feb 9, 2012