US2412315A - Radio transmitter-receiver automatic switching system - Google Patents
Radio transmitter-receiver automatic switching system Download PDFInfo
- Publication number
- US2412315A US2412315A US491963A US49196343A US2412315A US 2412315 A US2412315 A US 2412315A US 491963 A US491963 A US 491963A US 49196343 A US49196343 A US 49196343A US 2412315 A US2412315 A US 2412315A
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- US
- United States
- Prior art keywords
- line
- point
- receiver
- transmitter
- switching system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/03—Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
- G01S7/034—Duplexers
Definitions
- the invention covered herein may be manufactured and used by or for the Government of the United States for governmental, military, naval and national defense purposes without payment to me or assigns of any royalty thereon.
- This invention relates to radio frequency distribution systems, and more particularly to networks for operating a radio transmitter and a receiver with a common antenna system.
- signals comprising short pulses are radiated, reflected by a remote object and picked up at or near the location of the transmitter, it is desirable to use a single antenna system rather than provide separate antennas" for reception and transmission.
- Another object is to provide an improved network of the described type which incorporates no moving parts and provides substantially instantaneous switching of the antenna from transmitter to receiver.
- a further object is to provide an improved network of the described type which is efficient, not critical of adjustment, and capable of providing substantially complete isolation of the receiver from the transmitter without absorbing appreciable power.
- a typical automatic transmit-receive switching system involves the use of a parallel-resonant transmission line connected to the input of the receiver.
- the line is short circuited at one end, and a glow discharge tube is connected across the other end.
- the parallel resonant impedance of the line has no effect on the flow of signal energy .to the receiver.
- the tube discharges, sub-'- st'antially'short circuiting the open end of the line, so that the inductive reactance of the line is effectively connected across the receiver input.
- an intermediate point on the line, rather than the open end is connected to the receiver.
- a radio transmitter l is connected through a coaxial line 3 to an antenna system 4.
- a receiver 5 is connected through a coaxial line 1 to a point 9.
- a section I of coaxial line is connected to the receiver line 1 at a point l3, A wave length distant from the junction point 9.
- the line H is A.; wave length long.
- a short circuited stub line I5 is also connected to the point l3.
- a line H, /4 wave length long, is connected to the transmitter line 3 at a point IS, A; wave length nearer the transmitter than the point 9.
- is connected to the end of the line IT.
- a short circuited stub 23 is also connected to the end of the line H.
- Non-linear impedance devices such as gaseous discharge tubes 25 and 21, are connected across the open circuited ends of the lines H and 2
- the transmitter I When the transmitter I is operating, relatively high peak voltages are impressed on the gas tubes 25 and 21, causing the gas to ionize so that the tubes present relatively low impedances across the open ends of the lines I I and 2
- is reflected through the half wave line H as substantially a short circuit across the line at the point I3.
- the low impedance at the point I3 is reflected through the quarter wave section on the line 1 as a high impedance at the point 9.
- the major portion of the energy reaching the point 9 from the transmitter l flows past the point 9 to the antenna.
- the low impedance presented 3 by the tube 21 is reflected as an open circuit to the point l9.
- the tubes 25 and 21 are nonconductive, presenting very high impedances at the open ends of the lines H and 2
- the stubs I5 and :23 are adjusted to parallel resonate the reactances presented'by the tubes 25 and 2''! through the lines H and 2
- is reflected as a short circuit at the point I9 through the quarter wave line I1. .
- the short circuit atthe point I9 is reflected as an open circuit at the point 9.
- Energy traveling down the line 3 from the antenna flows into the line 1 to the receiver- 5.
- the open circuit presented by the line II at the point l3 has no effect upon the flow of energy through the line 1.
- the lengths of the various line sections are not unduly critical and adjustments may be made by actual measurements of length, without causing substantial departure from ideal performance;
- Gaseous discharge tubes are connected through line sections of resonant lengths to lines connecting the antenna j with the receiver and the transmitter.
- the gas in the tubes is ionized, rendering the tubes conductive and thereby providing relatively low impedances which are reflected inthe transmission line circuit to divert the flow of energy from the receiver to the transmitter.
- the gas tubes are non-conductive, presenting relatively high impedances which are reflected to the transmission line circuit to efiectiv'ely connect the receiver to the antenna system and disconnect the transmitter.
- second transmission line connected to a pointintermediate the ends of said first transmission line for connection to a receiver, a third transmission line Ay'wave length long 'connected to said first transmission line at a point A; wave. length distant from the point of connection ofsaid second transmission line thereto, a fourth transmission line wave length long connected to the end of said third transmission line, a fifth transmission line wave lengthlong connected to said second transmission line at a point A wave length distant from the point of connection betweensaid first and second lines,,and gaseous discharge tubes connected to the ends of said fourth and fifth transmission lines.
- a radio system including a transmitter, a receiver and an antenna system, a main transmission line connected between said transmitter and said antenna system, a branch transmission line connected between said receiver and a point on said main transmission line, a quarter wave transmission line connected to a Point on' said main line A wave length nearer said transmitter than the point of connection of said branch line thereto, half wave open-ended line sections connected to the end of said quarter wave line and to a point on said branch line wave length distant from the point of connectionrof said branch line to said main line respectively, and gaseous discharge tubes connected to the open ends of said half wave line.
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Emergency Protection Circuit Devices (AREA)
Description
G. H. BROWN Dec. 10, 1946.
RADIO TRANSMITTER-RECEIVER AUTOMATIC SWITCHING SYSTEM Filed June 23, 1943 mam 0 I i i i v l (Ittorneg I Patented Dec. 10, 1946 RADIO TRANSMITTER-RECEIVER AUTO- MATIC SWITCHING SYSTEM George H.- Brown, Princeton, N. J., as sig'nor t Radio Corporation of America, a corporation of Delaware Application June 23, 1943, Serial No. 491,963
3 Claims.
The invention covered herein may be manufactured and used by or for the Government of the United States for governmental, military, naval and national defense purposes without payment to me or assigns of any royalty thereon.
This invention relates to radio frequency distribution systems, and more particularly to networks for operating a radio transmitter and a receiver with a common antenna system. In certain applications, particularly those in which signals comprising short pulses are radiated, reflected by a remote object and picked up at or near the location of the transmitter, it is desirable to use a single antenna system rather than provide separate antennas" for reception and transmission. In order to prevent damage to the receiver during the periods of transmission, as well as dissipation of power, it is necessary to provide means for isolating electrically 'the receiver from the transmitter.
Prior art systems for this purpose have been somewhat uncertain in operation, extremely critical of adjustment, and relatively inefiicient in that a compromise must be effected between the degree of isolation of the receiver and the amount of transmitter power dissipated in the network.
It is the principal object of the present invention to provide an improved radio frequency network for operating a transmitter and a receiver with a common antenna system.
Another object is to provide an improved network of the described type which incorporates no moving parts and provides substantially instantaneous switching of the antenna from transmitter to receiver.
A further object is to provide an improved network of the described type which is efficient, not critical of adjustment, and capable of providing substantially complete isolation of the receiver from the transmitter without absorbing appreciable power.
These and other objects will become apparent to those skilled in the art upon consideration of the following description, with reference to the accompanying drawing, which is a schematic diagram of a transmission network embodying the invention.
A typical automatic transmit-receive switching system according to prior practice involves the use of a parallel-resonant transmission line connected to the input of the receiver. The line is short circuited at one end, and a glow discharge tube is connected across the other end. When the tube is not discharging, the parallel resonant impedance of the line has no effect on the flow of signal energy .to the receiver. When the transmitter is operating, the tube discharges, sub-'- st'antially'short circuiting the open end of the line, so that the inductive reactance of the line is effectively connected across the receiver input. In order to present a sufiici'ently low impedance at this point, an intermediate point on the line, rather than the open end, is connected to the receiver. Thus, by tapping down on the line, the minimum impedance is lowered, at the expense' of loweringthe' maximum impedanceby the same ratio. This in itself is not a particularly serious defect. Howeven th'e adjustment of the line length becomes more and more critical as the tapping point is moved toward the short circuited end. In a typical installation, an error of one percent in the adjustment may render the system inoperative, owing to failure to pro test the receiver or because of improper loading of the transmitter, or both.
According to the present invention, a radio transmitter l is connected through a coaxial line 3 to an antenna system 4. A receiver 5 is connected through a coaxial line 1 to a point 9.
on the transmitter line 3. A section I of coaxial line is connected to the receiver line 1 at a point l3, A wave length distant from the junction point 9. The line H is A.; wave length long. A short circuited stub line I5 is also connected to the point l3. A line H, /4 wave length long, is connected to the transmitter line 3 at a point IS, A; wave length nearer the transmitter than the point 9. A half wave open-circuited line 2| is connected to the end of the line IT. A short circuited stub 23 is also connected to the end of the line H. Non-linear impedance devices, such as gaseous discharge tubes 25 and 21, are connected across the open circuited ends of the lines H and 2| respectively.
The operation of the above described system is as follows:
When the transmitter I is operating, relatively high peak voltages are impressed on the gas tubes 25 and 21, causing the gas to ionize so that the tubes present relatively low impedances across the open ends of the lines I I and 2|. The low impedance of the tube 2| is reflected through the half wave line H as substantially a short circuit across the line at the point I3. The low impedance at the point I3 is reflected through the quarter wave section on the line 1 as a high impedance at the point 9. Thus the major portion of the energy reaching the point 9 from the transmitter l flows past the point 9 to the antenna. Similarly, the low impedance presented 3 by the tube 21 is reflected as an open circuit to the point l9.
During the periods when the transmitter I is not operating, the tubes 25 and 21 are nonconductive, presenting very high impedances at the open ends of the lines H and 2|. The stubs I5 and :23 are adjusted to parallel resonate the reactances presented'by the tubes 25 and 2''! through the lines H and 2| at the points l3 and 3|. The open circuit point 3| is reflected as a short circuit at the point I9 through the quarter wave line I1. .The short circuit atthe point I9 is reflected as an open circuit at the point 9. Energy traveling down the line 3 from the antenna flows into the line 1 to the receiver- 5. The open circuit presented by the line II at the point l3 has no effect upon the flow of energy through the line 1. The lengths of the various line sections are not unduly critical and adjustments may be made by actual measurements of length, without causing substantial departure from ideal performance;
Thus the invention has been described as an improved distribution network for radio frequency systems employing a common antenna fortransmission and reception. Gaseous discharge tubes are connected through line sections of resonant lengths to lines connecting the antenna j with the receiver and the transmitter. During transmission, the gas in the tubes is ionized, rendering the tubes conductive and thereby providing relatively low impedances which are reflected inthe transmission line circuit to divert the flow of energy from the receiver to the transmitter. During reception, the gas tubes are non-conductive, presenting relatively high impedances which are reflected to the transmission line circuit to efiectiv'ely connect the receiver to the antenna system and disconnect the transmitter.
second transmission line connected to a pointintermediate the ends of said first transmission line for connection to a receiver, a third transmission line Ay'wave length long 'connected to said first transmission line at a point A; wave. length distant from the point of connection ofsaid second transmission line thereto, a fourth transmission line wave length long connected to the end of said third transmission line, a fifth transmission line wave lengthlong connected to said second transmission line at a point A wave length distant from the point of connection betweensaid first and second lines,,and gaseous discharge tubes connected to the ends of said fourth and fifth transmission lines.
2. A radio system including a transmitter, a receiver and an antenna system, a main transmission line connected between said transmitter and said antenna system, a branch transmission line connected between said receiver and a point on said main transmission line, a quarter wave transmission line connected to a Point on' said main line A wave length nearer said transmitter than the point of connection of said branch line thereto, half wave open-ended line sections connected to the end of said quarter wave line and to a point on said branch line wave length distant from the point of connectionrof said branch line to said main line respectively, and gaseous discharge tubes connected to the open ends of said half wave line. I
3. The invention as s'et forth in claim 2, including short-circuited stub lines connected to the points of connection of said half wave lines to said branch line and said quarter wave line; GEORGE H. BROWN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US491963A US2412315A (en) | 1943-06-23 | 1943-06-23 | Radio transmitter-receiver automatic switching system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US491963A US2412315A (en) | 1943-06-23 | 1943-06-23 | Radio transmitter-receiver automatic switching system |
Publications (1)
Publication Number | Publication Date |
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US2412315A true US2412315A (en) | 1946-12-10 |
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Application Number | Title | Priority Date | Filing Date |
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US491963A Expired - Lifetime US2412315A (en) | 1943-06-23 | 1943-06-23 | Radio transmitter-receiver automatic switching system |
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Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2460755A (en) * | 1945-06-30 | 1949-02-01 | Bell Telephone Labor Inc | Receiver protective circuit for pulse transmission systems |
US2484798A (en) * | 1945-12-29 | 1949-10-11 | Philco Corp | Signal transmission system |
US2485606A (en) * | 1944-06-27 | 1949-10-25 | Standard Telephones Cables Ltd | Protective coupling circuit |
US2491971A (en) * | 1945-07-13 | 1949-12-20 | Raytheon Mfg Co | Switch tube device for wave guides |
US2531122A (en) * | 1944-06-02 | 1950-11-21 | Gen Electric | Frequency responsive protective arrangement for ultra high frequency systems |
US2547539A (en) * | 1946-06-27 | 1951-04-03 | Bell Telephone Labor Inc | Signal wave duplexing system |
US2549639A (en) * | 1945-06-23 | 1951-04-17 | Rca Corp | Antenna switching system |
US2582205A (en) * | 1943-09-07 | 1952-01-08 | Longacre Andrew | Compound protective device for radio detection system |
US2605356A (en) * | 1945-05-09 | 1952-07-29 | George L Ragan | Radio-frequency power divider circuit |
US2623207A (en) * | 1945-02-07 | 1952-12-23 | Csf | Radio obstacle detector |
US2627020A (en) * | 1949-05-28 | 1953-01-27 | William S Parnell | Two-feed "x" band antenna |
US2640916A (en) * | 1948-07-27 | 1953-06-02 | Gen Electric Co Ltd | Filter arrangement for combined radio receiving and transmitting systems |
US2640915A (en) * | 1950-12-28 | 1953-06-02 | Int Standard Electric Corp | Circularly polarized antenna arrangement for radar |
US2644926A (en) * | 1948-01-09 | 1953-07-07 | Arthur A Varela | Electronic switch for highfrequency power |
US2646550A (en) * | 1948-01-09 | 1953-07-21 | Arthur A Varela | Controlled impedance gas discharge device for mechanical transmission mediums |
US2656534A (en) * | 1950-01-14 | 1953-10-20 | Westinghouse Electric Corp | Tune-up system for radar |
US2658991A (en) * | 1946-05-08 | 1953-11-10 | Richard S O'brien | Antijamming radar system |
US2691105A (en) * | 1951-07-26 | 1954-10-05 | Rca Corp | Tuning system |
US2738502A (en) * | 1947-12-30 | 1956-03-13 | Esther M Armstrong | Radio detection and ranging systems |
US2867800A (en) * | 1948-09-18 | 1959-01-06 | Gen Precision Lab Inc | Microwave phasing system |
US2981946A (en) * | 1947-09-30 | 1961-04-25 | Rca Corp | Antenna feed system |
-
1943
- 1943-06-23 US US491963A patent/US2412315A/en not_active Expired - Lifetime
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2582205A (en) * | 1943-09-07 | 1952-01-08 | Longacre Andrew | Compound protective device for radio detection system |
US2531122A (en) * | 1944-06-02 | 1950-11-21 | Gen Electric | Frequency responsive protective arrangement for ultra high frequency systems |
US2485606A (en) * | 1944-06-27 | 1949-10-25 | Standard Telephones Cables Ltd | Protective coupling circuit |
US2623207A (en) * | 1945-02-07 | 1952-12-23 | Csf | Radio obstacle detector |
US2605356A (en) * | 1945-05-09 | 1952-07-29 | George L Ragan | Radio-frequency power divider circuit |
US2549639A (en) * | 1945-06-23 | 1951-04-17 | Rca Corp | Antenna switching system |
US2460755A (en) * | 1945-06-30 | 1949-02-01 | Bell Telephone Labor Inc | Receiver protective circuit for pulse transmission systems |
US2491971A (en) * | 1945-07-13 | 1949-12-20 | Raytheon Mfg Co | Switch tube device for wave guides |
US2484798A (en) * | 1945-12-29 | 1949-10-11 | Philco Corp | Signal transmission system |
US2658991A (en) * | 1946-05-08 | 1953-11-10 | Richard S O'brien | Antijamming radar system |
US2547539A (en) * | 1946-06-27 | 1951-04-03 | Bell Telephone Labor Inc | Signal wave duplexing system |
US2981946A (en) * | 1947-09-30 | 1961-04-25 | Rca Corp | Antenna feed system |
US2738502A (en) * | 1947-12-30 | 1956-03-13 | Esther M Armstrong | Radio detection and ranging systems |
US2644926A (en) * | 1948-01-09 | 1953-07-07 | Arthur A Varela | Electronic switch for highfrequency power |
US2646550A (en) * | 1948-01-09 | 1953-07-21 | Arthur A Varela | Controlled impedance gas discharge device for mechanical transmission mediums |
US2640916A (en) * | 1948-07-27 | 1953-06-02 | Gen Electric Co Ltd | Filter arrangement for combined radio receiving and transmitting systems |
US2867800A (en) * | 1948-09-18 | 1959-01-06 | Gen Precision Lab Inc | Microwave phasing system |
US2627020A (en) * | 1949-05-28 | 1953-01-27 | William S Parnell | Two-feed "x" band antenna |
US2656534A (en) * | 1950-01-14 | 1953-10-20 | Westinghouse Electric Corp | Tune-up system for radar |
US2640915A (en) * | 1950-12-28 | 1953-06-02 | Int Standard Electric Corp | Circularly polarized antenna arrangement for radar |
US2691105A (en) * | 1951-07-26 | 1954-10-05 | Rca Corp | Tuning system |
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