Low profile active electronically scanned antenna (AESA) for Ka-band radar systems

• US 7,132,990 B2
• Filed: 02/18/2005
• Issued: 11/07/2006
• Est. Priority Date: 02/05/2003
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Corporation
• Inventors: Wise, Carl D., Stenger, Peter A., McMonagle, Brian T., Sisk, Robert, Heffner, Craig, LaCour, Kevin, Hinton, Tujuana, Krafcsik, David, Walters, Andrew, Paquin, Joseph, Block, Steven D., Handley, Steven S., Kuss, Fred C.
• Primary Examiner(s): Dinh, Trinh
• Assistant Examiner(s): Mancuso, Huedung
• Application Number:
  US11/060,774
• Publication Number:
  US 20050146479A1
• Time in Patent Office: 627 Days
• Field of Search: 343/754, 343/772, 343/762, 343/700.MS, 343/755, 342/175, 333/125, 333/250, 333/286, 455/90.3, 455/82
• US Class Current: 343/754
• CPC Class Codes: H01P 1/047 Strip line joints
• CPC Class Codes: H01P 1/268 Strip line terminations H01P1/262 takes precedence
• CPC Class Codes: H01P 5/085 Coaxial-line/strip-line transitions
• CPC Class Codes: H01P 5/107 Hollow-waveguide/strip-line transitions
• CPC Class Codes: H01Q 1/422 comprising two or more layers of dielectric material H01Q1/425 takes precedence
• CPC Class Codes: H01Q 21/0037 linear waveguide fed arrays
• CPC Class Codes: H01Q 21/0087 Apparatus or processes specially adapted for manufacturing antenna arrays manufacturing waveguides H01P11/00
• CPC Class Codes: H01Q 21/064 using horn or slot aerials slotted waveguides arrays H01Q21/005
• CPC Class Codes: H01Q 23/00 Antennas with active circuits or circuit elements integrated within them or attached to them
• 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 vertically integrated Ka-band active electronically scanned antenna including, among other things, a transitioning RF waveguide relocator panel located behind a radiator faceplate and an array of beam control tiles respectively coupled to one of a plurality of transceiver modules via an RF manifold. Each of the beam control tiles includes a respective plurality of high power transmit/receive (T/R) cells as well as dielectric waveguides, RF stripline and coaxial transmission line elements. The waveguide relocator panel is preferably fabricated by a diffusion bonded copper laminate stack up with dielectric filling. The beam control tiles are preferably fabricated by the use of multiple layers of low temperature co-fired ceramic (LTCC) material laminated together. The waveguide relocator panel and the beam control tiles are designed to route RF signals to and from a respective transceiver module of four transceiver modules and a quadrature array of antenna radiators matched to free space formed in the faceplate. Planar type metal spring gaskets are provided between the interfacing layers so as to provide and ensure interconnection between mutually facing waveguide ports and to prevent RF leakage from around the perimeter of the waveguide ports. Cooling of the various components is achieved by a pair of planar forced air heat sink members which are located on either side of the array of beam control tiles. DC power and control of the T/R cells is provided by a printed circuit wiring board assembly located adjacent to the array of beam controlled tiles with solderless DC connections being provided by an arrangement of “fuzz button” electrical connector elements.

Claims

1. Heat sink apparatus for a Ka-band active electronically scanned antenna comprising:

an internal air cooled planar heat sink member located between a planar array of beam control elements and a waveguide relocator panel for dissipating heat generated by active circuit components of one or more RF signal amplifier circuits located in said beam control elements, and including a plurality of raised elongated substantially parallel heat sink body portions including respective sets of waveguides formed therethrough for coupling waveguide ports in a front face of an array of beam control elements to waveguide ports in a back face of a waveguide relocator element.

2. The heat sink apparatus according to claim 1 wherein said planar array of beam control elements comprise beam control tiles.

3. The heat sink apparatus according to claim 1 wherein said waveguide relocator elements comprise a generally flat panel including a plurality of like waveguide relocator sub-sections.

4. The heat sink apparatus according to claim 1 wherein each set of waveguides includes at least two mutually parallel subsets of waveguides located along the length of a predetermined member of said heat sink body portions on a surface of the heat sink member facing the waveguide relocator panel.

5. The heat sink apparatus according to claim 4 wherein each said set of waveguides comprise RF dielectric filled waveguides.

6. The heat sink apparatus according to claim 4 wherein each said subset of parallel waveguides are arranged substantially linearly on respective heat sink body portions.

7. The heat sink apparatus according to claim 6 wherein the waveguides of said at least two mutually parallel subsets of waveguides are mutually offset from one another.

8. The heat sink apparatus according to claim 6 wherein a predetermined number of said heat sink body portions include two subsets of waveguides and a predetermined number of said heat sink body portions include four subsets of waveguides.

9. The heat sink apparatus according to claim 8 wherein said sink body portions including two subsets of waveguides are located on either side of said sink body portions including four subsets of waveguides.

10. The heat sink apparatus according to claim 4 wherein said heat sink member includes a surface having a relatively large cavity facing the planar array of beam control elements.

11. The heat sink apparatus according to claim 10 and additionally including a set of apertured spring gaskets located in the cavity intermediate the heat sink member and the beam control elements.

12. Heat sink apparatus for a Ka-band active electronically scanned antenna, comprising:

an internal air-cooled planar heat sink member located between an array of beam control elements and at least one RF transceiver module for dissipating heat generated by one or more active RF signal amplifier circuits located in said beam control elements and said transceiver module and including RF coupling apparatus and a plurality of waveguide ports for coupling an input/output signal port of the transceiver modules to a waveguide port in each of the beam control elements.

13. The heat sink apparatus according to claim 12 wherein the array of beam control elements comprises a planar array of beam control tiles.

14. The heat sink apparatus according to claim 12 wherein the RF coupling apparatus in said inner heat sink member includes dielectric waveguide to air waveguide transition elements.

15. The heat sink apparatus according to claim 14 wherein said dielectric waveguide to air waveguide transition elements include a dielectric waveguide base portion and a plurality of intermediate stepped air waveguide matching portions and a top portion including an elongated RE signal port.

16. The heat sink apparatus according to claim 12 and additionally including an RF signal manifold member bonded to an outer face of the heat sink member and wherein the RF coupling means comprises a magic tee coupler formed in the RF signal manifold member.

17. The heat sink apparatus according to claim 14 wherein said heat sink member includes a plurality of mutually opposing side walls defining a cavity in an inner face of the heat sink member and in which is located an assembly of said dielectric waveguide to air waveguide transition elements.

18. The heat sink apparatus according to claim 17 and wherein a pair of mutually opposing side walls of said plurality of side walls each include at least one cross ventilating cooling opening for cross ventilating the assembly of waveguide transition elements.

19. The heat sink apparatus according to claim 18 wherein said at least one cooling opening comprises a plurality of cooling openings.

20. The heat sink apparatus according to claim 19 wherein pairs of said plurality of cooling openings oppose each other so as to provide a plurality of cross ventilation channels in a region of the cavity including the dielectric waveguide to air waveguide transition elements.