Compact microstrip hybrid coupled input multiplexer
View Patent ↗A multiplexer includes a filter channelizer having at least two output filters, each output filter being coupled with a respective hybrid coupler. The multiplexer channelizes an input radio frequency (RF) band of electromagnetic energy into a set of output ports. Each hybrid coupler includes an input port (port 1), two output ports and an isolated port (port 4). Each output filter is coupled to a first one of the two output ports of a respective hybrid coupler, a second one of the two output ports being connected to an open stub microstrip transmission line. The respective hybrid coupler is coupled in a daisy chain, by way of port 1 and port 4, with one or more of the input of the multiplexer, and at least one other hybrid coupler. Advantageously, each output channel may include no more than one filter and no more than one hybrid coupler.
1. A multiplexer comprising:
an input and a plurality of outputs, and
a filter channelizer comprising at least two output filters, each output filter being coupled with a respective hybrid coupler, each respective hybrid coupler comprising an input port (port 1), two output ports (ports 2 and 3) and an isolated port (port 4); wherein:
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;
each output filter is coupled with a respective one of the plurality of multiplexer outputs;
an input of each output filter is coupled to a first one of the two output ports of the respective hybrid coupler, a second one of the two output ports of the respective hybrid coupler being connected to a reflective open stub transmission line; and
the respective hybrid coupler is coupled in a daisy chain, by way of port 1 and port 4, with one or more of the input of the multiplexer, and at least one other respective hybrid coupler in the daisy chain.
2. The multiplexer of claim 1 , wherein at least one output filter is coupled directly to the respective one of the plurality of multiplexer outputs.
3. The multiplexer of claim 1 , wherein for each of the output channels, the multiplexer includes no more than one filter, and no more than one hybrid coupler.
4. The multiplexer of claim 1 , wherein each reflective open stub transmission line is configured such that the respective hybrid coupler has a balanced reflected signal at the two output ports.
5. The multiplexer of claim 1 , wherein the multiplexer is an input multiplexer of a spacecraft communications payload system.
6. The multiplexer of claim 1 , wherein the RF signal is at a frequency range between three KHz and three hundred GHz.
7. The multiplexer of claim 1 , wherein the multiplexer is a manifold coupled multiplexer, the manifold including microstrip transmission lines configured to receive an input radio frequency (RF) signal at an input port and to distribute the input RF signal to each of the respective hybrid couplers.
8. The multiplexer of claim 7 , wherein the microstrip transmission lines are planar conductive paths disposed on a dielectric substrate.
9. The multiplexer of claim 1 , wherein at least two output channels of the set of output channels are contiguous in frequency.
10. The multiplexer of claim 1 , wherein each of the set of output channels are respectively contiguous in frequency.
11. A spacecraft communications payload system comprising at least one input multiplexer, the at least one input multiplexer comprising:
an input and a plurality of outputs, and
a filter bank comprising at least two output filters, each output filter being coupled with a respective hybrid coupler, each respective hybrid coupler comprising an input port (port 1), two output ports (ports 2 and 3) and an isolated port (port 4); wherein:
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;
each output filter is coupled with a respective one of the plurality of multiplexer outputs;
an input of each output filter is coupled to a first one of the two output ports of the respective hybrid coupler, a second one of the two output ports of the respective hybrid coupler being connected to a reflective open stub transmission line; and
the respective hybrid coupler is coupled in a daisy chain, by way of port 1 and port 4, with one or more of the input of the multiplexer, and at least one other respective hybrid coupler in the daisy chain.
12. The payload system of claim 11 , wherein at least one output filter is coupled directly to the respective one of the plurality of multiplexer outputs.
13. The payload system of claim 11 , wherein for each of the output channels, the multiplexer includes no more than one filter, and no more than one hybrid coupler.
14. The payload system of claim 11 , wherein each reflective open stub transmission lines is configured such that the respective hybrid coupler has a balanced reflected signal at the two output ports.
15. The payload system of claim 11 , wherein the multiplexer is an input multiplexer of a spacecraft communications payload system.
16. The payload system of claim 11 , wherein the RF signal is at a frequency range between three KHz and three hundred GHz.
17. The payload system of claim 11 , wherein the multiplexer is a manifold coupled multiplexer, the manifold including microstrip transmission lines configured to receive an input radio frequency (RF) signal at an input port and to distribute the input RF signal to each of the respective hybrid couplers.
18. The payload system of claim 17 , wherein the microstrip transmission lines are planar conductive paths disposed on a dielectric substrate.
19. The multiplexer of claim 11 , wherein at least two output channels of the set of output channels are contiguous in frequency.
20. The multiplexer of claim 11 , wherein each of the set of output channels are respectively contiguous in frequency.