Traffic switching in communications satellites
First Claim
1. In a transponder useful in a satellite for transmitting signals in three different r-f frequency band channels via two antennas to two regions on earth, the combination ofan input triplexer having outputs for three different band channels,two output triplexers each having three inputs for said three different frequency band channels, and each having one output for coupling to a respective antenna feed,two signal paths from two outputs of said input triplexer to corresponding inputs of respective ones of said two output triplexers, each of said paths including, in the order named, a first circulator, an amplifier, a second circulator, and a single-pole, double-throw switch,a third switch for connecting a third output of the input triplexer to the first circulator in a selected one of said two signal paths, whereby to couple therein signals of a third frequency band channel, andmeans coupling second outputs of the second circulators in said two signal paths to third inputs of respective output triplexers.
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Accused Products
Abstract
A channel switching system useful in a satellite for amplifying some or all of three different RF frequency-band channel signals in two traveling wave tube amplifiers and transmitting the signals via two spot antennas to two regions on earth. Two signals are normally amplified in the two amplifiers and directed to the two regions on earth. A third frequency channel signal can be simultaneously applied through one or the other of the two paths. If an amplifier fails, the third frequency channel can be directed through the remaining operative amplifier to either one of the two regions on earth.
27 Citations
8 Claims
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1. In a transponder useful in a satellite for transmitting signals in three different r-f frequency band channels via two antennas to two regions on earth, the combination of
an input triplexer having outputs for three different band channels, two output triplexers each having three inputs for said three different frequency band channels, and each having one output for coupling to a respective antenna feed, two signal paths from two outputs of said input triplexer to corresponding inputs of respective ones of said two output triplexers, each of said paths including, in the order named, a first circulator, an amplifier, a second circulator, and a single-pole, double-throw switch, a third switch for connecting a third output of the input triplexer to the first circulator in a selected one of said two signal paths, whereby to couple therein signals of a third frequency band channel, and means coupling second outputs of the second circulators in said two signal paths to third inputs of respective output triplexers.
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4. The combination of
a first triplexer having outputs for three different r-f frequency channels, second and third triplexers each having inputs for said three different frequency channels, first and second signal paths from two outputs of the first triplexer to corresponding inputs, respectively, of said second and third triplexers, each of said paths including a first circulator having three ports, an amplifier and first and second ports of a second circulator having three ports, a switch coupling a third output of said first triplexer to a port of the first circulator in a selected one of said signal paths, whereby to couple therein signals of a third frequency channel, means coupling a third port of the second circulator in the first signal path to the third input of the second triplexer, and means coupling a third port of the second circulator in the second signal path to the third input of the third triplexer.
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6. In combination,
a first signal path including a first input band-pass filter for signals in a first frequency band, an input circulator, an amplifier, an output circulator and a first output band-pass filter for signals in said first frequency band, a second signal path including a second input band-pass filter for signals in a second frequency band, an input circulator, an ampifier, an output circulator and a second output band-pass filter for signals in said second frequency band, a third input band-pass filter for signals in a third frequency band selectably connectable to the input circulator in said first or second paths, and two additional output band-pass filters for signals in said third frequency band, each coupled to an output circulator in a respective one of said first and second signal paths.
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8. In a transponder useful in a satellite for transmitting signals in three different r-f frequency band channels via two antennas to two regions on earth, the combination of
an input triplexer having outputs for three different frequency band channels, two output triplexers each having three inputs for said three different frequency band channels, and each having one output for coupling to a respective antenna feed, two signal paths from two outputs of said input triplexer to said two output triplexers, each of said paths including, in the order named, a first circulator, an amplifier, a second circulator having first and second outputs, and a switch having one input connected to the first output of the circulator and first and second outputs, the second output of the second circulator in one path connecting to the input to the third channel in one output triplexer, and the first and second outputs of the switch in said one path connecting to the input to the first channel of said two output triplexers, respectively, the second output of the second circulator in the other path connecting to the input to the third channel in the other output triplexer, and the first and second outputs of the switch in said other path connecting to the input to the second channel in said two output triplexers, respectively, and a third switch for connecting a third output of the input triplexer to the first circulator in a selected one of said two signal paths, whereby to couple therein signals of a third frequency band channel.
Specification
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- Resources
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Current AssigneeLockheed Martin Corporation (Martin Marietta Corporation)
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Original AssigneeRCA Corporation
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InventorsKudsia, Chandra Mohan, Moody, Harry John, Keyes, Lorne Allan
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Primary Examiner(s)Gensler, Paul L.
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Application NumberUS05/783,656Time in Patent Office508 DaysField of Search333/1.1, 333/6, 325/1-3, 325/4, 325/9, 325/11, 179/15 FEUS Class Current455/17CPC Class CodesH04B 1/74 for increasing reliability,...H04B 7/2045 SS-FDMA, FDMA satellite swi...
