Hybrid matrix amplifier systems, and methods for making thermally-balanced hybrid matrix amplifier systems

• US 5,055,798 A
• Filed: 10/09/1990
• Issued: 10/08/1991
• Est. Priority Date: 10/09/1990
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Heinzelmann, Christine
• Primary Examiner(s): MOTTOLA, STEVEN J
• Application Number:
  US07/594,472
• Time in Patent Office: 364 Days
• Field of Search: 330/53, 330/124 R, 330/286, 330/295, 333/109, 333/113, 333/114, 333/115, 333/116, 333/117
• US Class Current: 330/295
• CPC Class Codes: H03F 2200/198 A hybrid coupler being used as coupling circuit between stages of an amplifier circuit
• CPC Class Codes: H03F 3/602 Combinations of several amplifiers

Abstract

A hybrid matrix amplifier system that yields balanced thermal loads with minimal input signal constraints includes an input multiport hybrid coupler system having outputs joined to a plurality of amplifiers, and an output multiport hybrid coupler system joined to the outputs of the amplifiers. The input multiport hybrid coupler system, and the output multiport hybrid coupler system, each include n stages where n is an integer equal to or greater than 1, with each stage including 2^n-1 couplers. These coupler systems may also include strategically-placed phase shifters. Such systems also include N amplifiers where N is equal to 2ⁿ, with N inputs from the outputs of the input multiport hybrid coupler system, and with the outputs of the amplifiers connected as inputs to the output multiport hybrid coupler system. This configuration permits a division of the N amplifiers into two groups that each dissipates substantially the same quantity of heat energy.

Claims

1. A hybrid matrix amplifier system for processing N input signals, including an input multiport hybrid coupler system comprising N×

2^n-1 hybrid couplers divided into n stages where n is an integer equal to or greater than 2 and where each stage includes 2^n-1 hybrid couplers;

said input multiport coupler system having N input terminals for receiving the N input signals and N output terminals where N is equal to 2ⁿ, said N output terminals being connected to N amplifiers, said N amplifiers having outputs connected to an output multiport hybrid system including n stages, each stage including 2^n-1 hybrid couplers, wherein the N input signals may be of arbitrary amplitude.

2. The system of claim 1 wherein said N amplifiers are divided into groups, with each group including the same number of amplifiers, and each group dissipating substantially the same thermal energy.

3. The system of claim 2 wherein each of the amplifier groups is positioned adjacent to a separate radiator panel to dissipate, through each panel, substantially the sam thermal energy.

4. The system of claim 3 wherein each of said radiator panels is positioned on the walls of a three-axis spacecraft that receives signals from a multiple beam antenna.

5. The system of claim 4 wherein each of said radiator panels is of substantially the same size and has substantially the same capacity to dissipate thermal energy.

6. The system of claim 1 wherein said N input terminals of said input multiport hybrid coupler system are coupled to outputs of corresponding N signal transmission lines of a feed network of an antenna means.

7. The system of claim 6 wherein said output multiport hybrid coupler system includes N output terminals coupled to corresponding N input ports of said antenna means.

8. The system of claim 6 wherein at least two of said N signal transmission lines of said antenna feed network convey beam-forming RF signals of unequal amplitude.

9. The system of claim 8 further comprising at least one phase shifter in said input coupler system and at least one phase shifter in said output coupler system.

10. The system of claim 1 further comprising at least one phase shifter in said input coupler system and at least one phase shifter in said output coupler system.

11. The system of claim 6 wherein said antenna means is carried by a spacecraft.

12. The system of claim 1 wherein said N amplifiers are each of substantially the same design.

13. The system of claim 3 wherein said amplifiers are of substantially the same size and of substantially the same design.

14. A system comprising N signal transmission lines of a beam-forming network of an antenna means, said N signal transmission lines having N outputs coupled to N input terminals of an input multiport hybrid coupler system adapted to receive N input signals, said input multiport hybrid coupler system comprising n×

2^n-1 hybrid couplers divided into n stages where n is an integer equal to or greater than 2 and where each stage includes 2^n-1 hybrid couplers;

said input multiport coupler system having N output terminals where N is equal to 2ⁿ, said N output terminals being connected to N amplifiers, said N amplifiers having outputs connected to an output multiport hybrid system including n stages, each stage including 2^n-1 hybrid couplers, wherein the N input signals may be of arbitrary amplitude.

15. The system of claim 14 wherein said output multiport hybrid coupler system further includes N output terminals coupled to corresponding N input ports of said antenna means.

16. The system of claim 14 wherein at least of two of said N signal transmission lines of said antenna feed network convey beam-forming RF signals of unequal amplitude.

17. The system of claim 16 further comprising at least one phase shifter in said input coupler system and at least one phase shifter in said output coupler system.

18. The system of claim 14 further comprising at least one phase shifter in said input coupler system and at least one phase shifter in said output coupler system.

19. The system of claim 14 wherein said antenna means is carried by a spacecraft.

20. The system of claim 14 wherein said N amplifiers are of substantially the same size and design.

21. The system of claim 14 wherein said N amplifiers are divided into two groups, each of said groups including the same number of amplifiers, and each of said groups dissipating substantially the same thermal energy.