Microstrip manifold coupled multiplexer

• US 9,030,271 B2
• Filed: 12/29/2011
• Issued: 05/12/2015
• Est. Priority Date: 12/29/2011
• Status: Expired due to Fees

• Current Assignee: Space Systems/Loral LLC A Delaware Limited Liability Company
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Holme, Stephen C., Berry, Stephen D., Carastro, Lawrence Alan
• Primary Examiner(s): Pascal, Robert
• Assistant Examiner(s): GLENN, KIMBERLY E
• Application Number:
  US13/340,095
• Publication Number:
  US 20130169379A1
• Time in Patent Office: 1,230 Days
• Field of Search: 333/110, 333/115, 333/116, 333126-129, 333/132, 333/134
• US Class Current: 333/134
• CPC Class Codes: H01P 5/12 Coupling devices having more than two ports H01P5/04 takes precedence

Abstract

A multiplexer includes a microstrip manifold, and a filter bank having at least two output filters. The multiplexer channelizes an input radio frequency (RF) band of electromagnetic energy into a set of output channels by way of the filter bank. The microstrip manifold has an input port that receives an input RF signal, and at least two output ports. The microstrip manifold distributes the input RF signal to each output port, each said output port being coupled to a respective one of the at least two output filters. The multiplexer may be an input multiplexer for a spacecraft communications payload system.

Claims

1. A multiplexer comprising:

a microstrip manifold, the microstrip manifold including at least one planar conductive strip disposed on a non-conductive or dielectric substrate; and

a filter bank, external to the microstrip manifold, comprising at least two output filters, wherein;

at least one of the two output filters is a cavity or dielectric resonator filter;

the multiplexer is configured to channelize an input radio frequency (RF) band of electromagnetic energy into a set of output channels by way of the filter bank; and

the microstrip manifold has an input port configured to receive an input RF signal, and at least two output ports, the microstrip manifold being configured to distribute, by way of the at least one planar conductive strip, said input RF signal to each of said output ports, each said output port being coupled to a respective input of the at least two output filters.

2. The multiplexer of claim 1, wherein each of the at least two output filters is a high Q bandpass filter.

3. The multiplexer of claim 1, wherein the multiplexer is adjustable by way of a tuning screw coupled to a conductive or dielectric pad.

4. The multiplexer of claim 1, wherein the multiplexer is an input multiplexer of a spacecraft communications payload system.

5. The multiplexer of claim 1, wherein the RF signal is at a frequency range between one and one hundred GHz.

6. A manifold coupled multiplexer, wherein the manifold is a microstrip including at least one planar conductive strip disposed on a non-conductive or dielectric substrate, and is configured to receive an input radio frequency (RF) signal at an input port and to distribute, by way of the at least one planar conductive strip, the input RF signal to each of at least two output ports, each said output port being coupled to a respective input of at least two output filters, at least one of the two output filters being a cavity or dielectric resonator filter.

7. The manifold coupled multiplexer of claim 6, wherein each of the at least two output filters is a high Q bandpass filter.

8. The manifold coupled multiplexer of claim 7, wherein the RF signal is at a frequency range between one and one hundred GHz.

9. The manifold coupled multiplexer of claim 6, wherein the manifold coupled multiplexer is adjustable by way of a tuning screw coupled to a conductive or dielectric pad.

10. The manifold coupled multiplexer of claim 6, wherein the multiplexer is an input multiplexer of a spacecraft communications payload system.

11. A spacecraft communications payload system comprising at least one input multiplexer, the at least one input multiplexer comprising:

a microstrip manifold, the microstrip manifold including at least one planar conductive strip disposed on a non-conductive or dielectric substrate; and

a filter bank, external to the microstrip manifold, comprising at least two output filters, wherein;

at least one of the two output filters is a cavity or dielectric resonator filter;

the multiplexer is configured to channelize an input radio frequency (RF) band of electromagnetic energy into a set of output channels by way of the filter bank; and

the microstrip manifold has an input port configured to receive an input RF signal, and at least two output ports, the microstrip manifold being configured to distribute, by way of the at least one planar conductive strip, said input RF signal to each of said output ports, each said output port being coupled to a respective input of the at least two output filters.

12. The spacecraft communications payload system of claim 11, wherein each of the at least two output filters is a high Q bandpass filter.

13. The spacecraft communications payload system of claim 11, wherein the multiplexer is adjustable by way of a tuning screw coupled to a conductive or dielectric pad.

14. The spacecraft communications payload system of claim 11, wherein the multiplexer is an input multiplexer of a spacecraft communications payload system.

15. The spacecraft communications payload system of claim 11, wherein the RF signal is at a frequency range between one and one hundred GHz.