US2341346A - High frequency coupling circuit - Google Patents

High frequency coupling circuit Download PDF

Info

Publication number
US2341346A
US2341346A US431767A US43176742A US2341346A US 2341346 A US2341346 A US 2341346A US 431767 A US431767 A US 431767A US 43176742 A US43176742 A US 43176742A US 2341346 A US2341346 A US 2341346A
Authority
US
United States
Prior art keywords
inductance
frequency
electrodes
discharge device
devices
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
Application number
US431767A
Inventor
Jr Harry R Summerhayes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US431767A priority Critical patent/US2341346A/en
Application granted granted Critical
Publication of US2341346A publication Critical patent/US2341346A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03DDEMODULATION OR TRANSFERENCE OF MODULATION FROM ONE CARRIER TO ANOTHER
    • H03D9/00Demodulation or transference of modulation of modulated electromagnetic waves
    • H03D9/06Transference of modulation using distributed inductance and capacitance
    • H03D9/065Transference of modulation using distributed inductance and capacitance by means of discharge tubes having more than two electrodes

Definitions

  • My invention relates to high frequency coupling circuits employed between electron discharge devices and particularly to such circuits operating at frequencies at or approaching the range of frequencies where distributed reactance eiects of the necessarily employed connections are so great as to dictate circuit structure designed to utilize such distributed reactance effects.
  • Such circuit structure may comprise for example, conductors of desired length spaced to operate as standing Wave lines and having connections thereto at points to alford the desired impedance eifects.
  • An object of my invention is to provide an economical interstage circuit for use between electron discharge devices to afford coupling at such frequencies and in which concentrated variable reactance is employed to vary the tuning of the circuit over a wide range including frequencies Where distributed constants are controlling in the design of the circuit.
  • my invention relates to such coupling employed in a converter to couple the output of each of two ampliers to the input of a frequency converter, the amplifiers operating at frequencies variable over a wide range and being different by only a very small percentage of either frequency.
  • An object of my invention is to provide an economical coupling network for such application which is tunable over a wide range by variation of concentrated inductance devices only and in which the upper limit of the range of frequencies is well within the range Where circuit structure commonly employed is that cf the distributed reactance type.
  • Fig. 1 represents the circuit structure of my invention
  • Figs. 2, 3., and 4 represent an inductance device for employment therein
  • Fig. 5 represents in greater detail the mechanical structure of such an inductance device.
  • I have illustrated therein at I, an electron discharge device which operates as a frequency converter. Oscillations of a desired frequency are supplied thereto from a discharge device 2 through a coupling condenser 3 and oscillations of a different desired frequency are supplied thereto from a second discharge device 4 through a coupling condenser 5. These oscillations both appear between the input electrode 6 and cathode 'I of the discharge device I and combine to produce oscillations in the output circuit of discharge device I havinga frequency equal to the difference between the two applied frequencies. These difference, or beat, frequency oscillations may be supplied over conductors 8 to any suitable loa-d circuit.
  • the carrier wave the frequency of which is to .be monitored, is supplied between the grid 9 and cathode I0 of the discharge device 4 through a coupling condenser II.
  • These frequencies may extend, for example, from 260 megacycles to 3'50 megacycles dependent upon the broadcasting station the frequency of which is to be monitored.
  • Such oscillations are amplified by the discharge device 4 and combined between the grid 6 and cathode I of discharge device I with other oscillations of known frequency which are supplied through the discharge device 2.
  • oscillations may have a frequency varying, for example, from 254.6 megacycles to 344.6 megacycles, or, in other words, over a range 5.4 megacycles lower than the range of frequencies supplied through discharge device 4.
  • a frequency of 5.4 megacycles is produced upon the output circuit 8 for any two applied frequencies.
  • the frequency of 350 megacycles is well within the range where careful consideration must be given to the distributed reactance effects and the circuit structure employed may well be that of the distributed reactance type, that is, circuit structure employing parallel spaced conductors operating as standing wave lines, etc., and provided with slidable bridge members, for example, for variation thereof. It is undesirable to employ structure of such character in a frequency monitor contemplated for the applications in which I contemplate my invention to nd its etc.
  • the inductance devices employed in accordance with my invention are indicated conventionally at I2, I3, and I4 in Fig. 1.
  • the inductance device I2 is connected between the anode and cathode of the discharge device 2.
  • the inductance device I 3 is connected between the control electrode 6 and the cathode I of discharge debetween the anode and cathode of discharge device 4. So connected, the upper terminals of the inductance devices I2, I3, I4 are all connected together through the conductors I6 and I1 and the lower terminals of inductances I2, I3, and I4 are connectedtogether through respective condensers 44', 43 and 44 and to ground asindicated at I8. l
  • the condensers 44', 43 and 4.4 in series with the respective inductance devices I2, I3, and I4 are bypass condensers having substantially zero reactance at the frequencies employed. These condensers are of very small physical dimensions thereby avoiding any undesired reactance effects encountered by reason of the lengths of leads,
  • the discharge devices 2 and 4 in the physical embodiment of the equipment, are spaced as close as practicable to the discharge device ⁇ I but in such practical spacing of the discharge devices, the length of each of the conductors IGand I1 may be, for example, 2 inches or more.
  • the length of the connections between discharge devices 2 and I and between discharge devices 4 andy I comprise a substantial part of a quarter of a wave length and hence these connections afford a very substantial impedance to the transmission of these high frequency oscillations.
  • these inductances I2, ⁇ I3,iand I4 all operate'in parallel ,as a single inductance to resonate with the sum of the capacities existing across the circuit, and that the shunt combination of the three inductances reduces the total inductance across the circuit to a sufficiently low value to produce the required resonance at the highest frequencies in the range. Since the different inductances are spaced apart suiiiciently to avoid substantial mutual coupling therebetween such reduction in inductance is readily possible. Such considerationv might suggest that the three inductances be all connected together across a single pair ofv points on the circuit. However, three such inductances spaced closely together would have suflicient mutual to prevent reduction to the required low value at the high frequencies.
  • inductance devices I2, I3, and4 I4 are of the type described and claimed in copending application S. N. 363,016 of Lewis I-I. Van Billiard, filed October 26, 1940, entitled Tuning system, and which is assigned to the same assignee as my present application.
  • Fig. 2 represents a plan view of one of these inductance devices. It comprises a plate '20, which may be an ordinary sheet metal punching as is ordinarily used in the stator section of a variable condenser. This plate 20 has a large -aperture 2
  • a pair of rotor plates 25 are provided, mounted upon a shaft 26 about which it is rotatable. These plates may each be in the form of a half of a disk rotatable from the position shown in Fig. 2 to a position in proximity to the plateEIl, ⁇ one on either side of that plate, whereby they prac# tically cover the aperture 2I in the plate 20 and since they are conducting members they reduce the inductance between terminals 23 and 24 substantially to zero. As the members 25 are rotated from such position to the position shown the inductance between terminals 23 and 24 changes from substantially zero value to one of very substantial value at the frequencies employed.
  • Fig. 3 represents, in a perspective view, such an inductance device in which two stator meinbers 20 are arranged in parallel space .relation and connected in series as indicated at 21.
  • This device also comprises three of the rotor members 25 positioned for rotation into interleaved relationship with the stator plates 26.
  • the inductance of this device varies substantially from zero to values which may be approximately twice as great, or even more than that obtained with but a single stator plate.
  • Fig. 4 represents the arrangement in which two stator plates 20 are connected as indicated at 26 for parallel operation to reduce the inductance obtainable. It will, of course, be understood that in such an inductance device more stator plates may be utilized and that the stator plates may be connected in parallel relation, series relation, or series-parallel relation, as may be required.
  • Fig. 5 is a sectional View with parts in elevation taken on the line 5-5 of Fig. 2.
  • the stator plates 23 are shown broken away but positioned in parallel relation, in interleaved relation with the rotor plates 25.
  • the stator plates are mounted in insulating material 28, bolted in any suitable way to the form member 28.
  • the rotor plates are likewise mounted together in parallel space relation between the bushings 33 which may be either conducting or nonconducting but which are mounted upon a nonconducting shaft 25 arranged in a bearing member 32, for rotation, as by means of a screwdriver applied to a notch 33 in the end of the shaft.
  • any suitable handie or knob may be provided as desired.
  • inductance devices employed is very important in the operation of the circuit described and in addition aiords the ad- A vantage that they are economical to build.
  • These inductance devices may comprise the frame structure of any ordinary standard variable condenser.
  • the stator plates of such a condenser may be removed and suitable punchings, as indicated,
  • the shaft may also be removed and replaced by the nonconducting shaft indicated in Fig. 5.
  • stator plates being of sheet metal and of suiiicient strength to be rigid and self-supporting, may have holes punched therein to permit mounting in close parallel space relation so that the rotor plates may move freely therebetween without contact therewith, and also with a minimum of space between the different plates.
  • These stator plates may also be shaped so that the terminals 23 and 24 thereof may be spaced as close together as possible to reduce the length of thc path between the terminals to as little as possible. In this way, a minimum of inductance is obtainable when the rotor plates are in full interleaved relation with the stator plates.
  • inductances of concentrated, readily variable form and of sufficiently low value to operate at the highest frequencies in the ranges mentioned and over the ranges mentioned are readily obtainable.
  • I have found in the operation of the system that in the upper portion of the range extending, for example, from 300 to 350 megacycles, all three of the inductances, I2, I3, and I4 are necessarily in the circuit.
  • I nd it necessary to remove one of these inductances, preferably the inductance I 3. This may be effected by breaking the circuit at the points near adjacent terminals of this inductance which are marked X on Fig. 1 of the drawing.
  • the discharge device 4 is one employing a screen grid 35 and a suppressor grid 36, the screen grid being connected through a resistance 39 to a source of operating potential which may be connected between conductors 4D.
  • the suppressor grid is connected to the cathode of the discharge device.
  • the screen grid is grounded at the frequencies in question through a condenser 4I.
  • Voltage is also supplied to the anode of discharge device 4 through a suitable isolation filter comprising resistance 42 and condenser 44. Similar circuits are of course employed in connection with the other discharge devices, that in connection with discharge device 2 being indicated at 42 and 44'.
  • the cathode of discharge device I is grounded through a condenser 46 at the frequencies of currents supplied to the input of the discharge device, this condenser being one of small capacity arranged as close as is practicable to the cathode of the discharge device. It is also grounded for currents of the 5.4 megacycle frequency through a larger condenser 41 which is connected across a cathode bias resistance 48.
  • a pair of amplifiers operating at frequencies differing from each other by a small percentage and varying over a wide range, each of said amplifiers having a pair of output electrodes, a discharge device having a pair of input electrodes, all of said pairs of electrodes being connected in parallel, the frequencies at which said amplifiers operate being so high that the length of the connections from said pairs of output electrodes to the input electrodes of said discharge device is a substantial part of a quarter of a wave length of the waves at which the respective ampliers operate, and a pair of inductances, each inductance being connected between said electrodes of a respective one of said amplifiers and spaced close thereto so that said length of said connections extends from said inductance to said discharge device, said inductance being variable to resonate with the interelectrode capacity between the respective electrodes at any frequency in a wide range.
  • a pair of electron discharge amplifiers each of said amplifiers having an anode and a cathode, an electron discharge device operating as a frequency converter having a cathode, a control electrode, and an output circuit, all of said cathodes being connected together and each of said anodes being connected to said control electrode through a respective conductor having a length equal to a substantial portion of a quarter of a wave length of the wave at which the respective amplifier operates, said amplifiers operating at short wave lengths varying over a vwiderange, theV frequency at which one amplifier operates being different.
  • each inductance ldevice being connected between said anode and rtrodes.
  • a pair of electron discharge amplifiers each of said amplifiers having an anode and a cathode, an electron discharge device operating as a frequency converter comprising a cathode, a control electrode, and an output circuit, said anodes being connected to said control electrode through respective conductors having a length equal to a substantial portion of a quarter of a wave length of the wave at which the respective amplifier operates, said ampliers oper- ⁇ ating at short wave lengths varying over a wide range, the frequency at which one amplifier operates being different from that of the other by a small percentage, thereby producing a low frequency in said output circuit of said converter, a plurality of inductance devices, each inductance device being connected between said electrodes of a respective one of said amplifiers and converter, and proportioned to resonate with the interelectrode capacity between the respective electrodes, said inductances being spaced adjacent said respective electrodes.
  • a pair of'electron discharge devices operating at high frequency, one of said devices having a pair' of input electrodes andthe other of said devices having a pair of output electrodes, said pairs of electrodes being connected in parallel whereby oscillations from said output electrodes are supplied to said input electrodes, said devices being mounted as close together as practicable but the frequency of said oscillations being so great that the short interconnections between said pairs of electrodes have a length equal to a substantial part of a quarter of a wave length of said oscillations, a pair of inductances, each inductance' being .connected between a respective pair of said electrodes and resonating with the capacity therebetween, and being spaced apart by said substantial part of a quarter of a wave length.
  • a high frequency electron rdischarge amplifier having a pair of outputl electrodes, a second electron discharge device having a pair of input electrodes, capacitive coupling between said pairs of electrodes through connections having a length such that substantial inherent impedance produced by reason of distributed reactance exists in said connections at the frequency at which said amplifier operates, a pair of inductance devices, each inductance device comprising a conductor shaped about the periphery of an enclosure, said periphery being broken at one point, the points of said conductor adjacent said break being connected to opposite electrodes of a respective one of said pairs, and a conducting member parallel with said plane of said conductor and movable into proximity thereto to reduce the inductance of saidL conductor,
  • said inductance being substantially zero on one extreme of movement of said member and of substantial value at the other extreme of movement vof said member, said inductance of each of said inductance devices being variable to resonate with the capacity between the respective electrodes to which itis connected at any frequency in a wide range.
  • a pair of electron discharge devices operating at high frequency, each of said devices having a pair of output electrodes, athird ⁇ electron discharge device having a pair-of input electrodes, a plurality of conducting plates, each conducting plate being shaped to form an enclosure and having inductance between two closely spaced points thereof, said points of each plate being connected to opposite electrodes of a respective one of said pairs, said plates being spaced apart suiciently to have little mutual inductance, connections between said different pairs of electrodes, and a plurality of movable plates, each movable plate being spaced in parallel relation with a respective one of said rst plates and movable to close spaced relation thereto whereby the inductance of said plates may be reduced to resonate with the capaci'ty between the respective' electrodes at a frequency so high that the length of the conductors comprising said connections is a substantial part of a quarter of the operating wave length, and efficient transfer of energy from said pair of discharge devices to said third discharge device is produced.

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Ac-Ac Conversion (AREA)

Description

Feb. 8, 1944. H. R. sUMMERHAYEs,.JR
HIGH FREQUENCY COUPLING CIRCUITS Filed Feb. 20, 1942 y l I T? la 47 v Inventor: Harry F?. Summerhayes Jr.
by His Attorney.
Patented Feb. 8, 1944 UNITED STATES PATENT OFFICE HIGH FREQUENCY COUPLING CIRCUIT Harry R. Summerhayes, Jr., Schenectady, N. Y.,
assignor to General Electric Company, a corporation cf New York 6 Claims.
My invention relates to high frequency coupling circuits employed between electron discharge devices and particularly to such circuits operating at frequencies at or approaching the range of frequencies where distributed reactance eiects of the necessarily employed connections are so great as to dictate circuit structure designed to utilize such distributed reactance effects. Such circuit structure may comprise for example, conductors of desired length spaced to operate as standing Wave lines and having connections thereto at points to alford the desired impedance eifects.
Such structure is ordinarily expensive to build, is bulky, imposes undesired space requirements, and in general, is to be avoided in cases where circuit structure having concentrated reactance constants can be employed. This is especially true if the frequency at which the system operates is to be variable to any substantial extent.
An object of my invention is to provide an economical interstage circuit for use between electron discharge devices to afford coupling at such frequencies and in which concentrated variable reactance is employed to vary the tuning of the circuit over a wide range including frequencies Where distributed constants are controlling in the design of the circuit.
More particularly, my invention relates to such coupling employed in a converter to couple the output of each of two ampliers to the input of a frequency converter, the amplifiers operating at frequencies variable over a wide range and being different by only a very small percentage of either frequency.
An object of my invention is to provide an economical coupling network for such application which is tunable over a wide range by variation of concentrated inductance devices only and in which the upper limit of the range of frequencies is well within the range Where circuit structure commonly employed is that cf the distributed reactance type.
The novel features which I believe to be characteristic of my invention are set forth with particularity in the appended claims. My invention itself, however, both as to its organization and method of operation, together with further objects and advantages thereof may best be understood .by reference to the following description taken in connection with the drawing in which Fig. 1 represents the circuit structure of my invention; Figs. 2, 3., and 4 represent an inductance device for employment therein, and Fig. 5 represents in greater detail the mechanical structure of such an inductance device.
Referring to Fig. 1 of the drawing, I have illustrated therein at I, an electron discharge device which operates as a frequency converter. Oscillations of a desired frequency are supplied thereto from a discharge device 2 through a coupling condenser 3 and oscillations of a different desired frequency are supplied thereto from a second discharge device 4 through a coupling condenser 5. These oscillations both appear between the input electrode 6 and cathode 'I of the discharge device I and combine to produce oscillations in the output circuit of discharge device I havinga frequency equal to the difference between the two applied frequencies. These difference, or beat, frequency oscillations may be supplied over conductors 8 to any suitable loa-d circuit.
I contemplate my invention for use more particularly in connection with frequency monitors for broadcast stations which operate by frequency modulation of the transmitted carrier wave. The carrier wave, the frequency of which is to .be monitored, is supplied between the grid 9 and cathode I0 of the discharge device 4 through a coupling condenser II. These frequencies may extend, for example, from 260 megacycles to 3'50 megacycles dependent upon the broadcasting station the frequency of which is to be monitored. Such oscillations are amplified by the discharge device 4 and combined between the grid 6 and cathode I of discharge device I with other oscillations of known frequency which are supplied through the discharge device 2. These other oscillations may have a frequency varying, for example, from 254.6 megacycles to 344.6 megacycles, or, in other words, over a range 5.4 megacycles lower than the range of frequencies supplied through discharge device 4. Thus a frequency of 5.4 megacycles is produced upon the output circuit 8 for any two applied frequencies.
The frequency of 350 megacycles is well within the range where careful consideration must be given to the distributed reactance effects and the circuit structure employed may well be that of the distributed reactance type, that is, circuit structure employing parallel spaced conductors operating as standing wave lines, etc., and provided with slidable bridge members, for example, for variation thereof. It is undesirable to employ structure of such character in a frequency monitor contemplated for the applications in which I contemplate my invention to nd its etc.
greatest utility, not only because of the expense of the apparatus and its cumbersomeness but also because the frequency must be variable over such a broad range as to render coupling circuits of that type difficult to build. I have found, however, that by the employment of the system presently to be described, such structure may be avoided and that the lcircuit may be tuned for operation at any frequency in the desired range solely by variation of vconcentrated inductance devices.
The inductance devices employed in accordance with my invention are indicated conventionally at I2, I3, and I4 in Fig. 1. The inductance device I2 is connected between the anode and cathode of the discharge device 2. The inductance device I 3 is connected between the control electrode 6 and the cathode I of discharge debetween the anode and cathode of discharge device 4. So connected, the upper terminals of the inductance devices I2, I3, I4 are all connected together through the conductors I6 and I1 and the lower terminals of inductances I2, I3, and I4 are connectedtogether through respective condensers 44', 43 and 44 and to ground asindicated at I8. l
The condensers 44', 43 and 4.4 in series with the respective inductance devices I2, I3, and I4 are bypass condensers having substantially zero reactance at the frequencies employed. These condensers are of very small physical dimensions thereby avoiding any undesired reactance effects encountered by reason of the lengths of leads, The discharge devices 2 and 4, in the physical embodiment of the equipment, are spaced as close as practicable to the discharge device `I but in such practical spacing of the discharge devices, the length of each of the conductors IGand I1 may be, for example, 2 inches or more. At a frequency of 350 megacycles the length of the connections between discharge devices 2 and I and between discharge devices 4 andy I comprise a substantial part of a quarter of a wave length and hence these connections afford a very substantial impedance to the transmission of these high frequency oscillations. I have found, however, that very satisfactory vtransmission of oscillations of desired frequency from the discharge devices 2 and 4 to the conf rproperly adjusted, resonates with the interelectrode capacity between the input electrodes of the discharge device I 'and that the inductance device I4 resonates with the interelectrode capacity between the output electrodes of dis- `charge device 4, all of these resonances'occurring .at some frequency between the two applied frequencies Since'these inductances so resonate, they' produce high impedances between these different pairs of. electrodes at that frequency. The two vapplied Vfrequencies differ by such a `small percentage, less than two per cent, that this :high impedance exists for both of the applied frequencies. That is the Q of the circuit or the ratio of inductive reactance to resistance,
:is not so great" but that these frequencies may 4vice I and the inductance device I4 is connected both fall near the top of the resonance curve. This impedance between the different electrodes of the different pairs of electrodes is so high that the impedance of the interconnecting conductors comprising conductors I6, II and the cathode return conductors is small in comparison therewith.
It may be, however, that these inductances I2,`I3,iand I4 all operate'in parallel ,as a single inductance to resonate with the sum of the capacities existing across the circuit, and that the shunt combination of the three inductances reduces the total inductance across the circuit to a sufficiently low value to produce the required resonance at the highest frequencies in the range. Since the different inductances are spaced apart suiiiciently to avoid substantial mutual coupling therebetween such reduction in inductance is readily possible. Such considerationv might suggest that the three inductances be all connected together across a single pair ofv points on the circuit. However, three such inductances spaced closely together would have suflicient mutual to prevent reduction to the required low value at the high frequencies. This is true even though the different inductances be positioned in planes mutually at right angles to each other. It might also suggest a single inductance device with morestator plates connected in parallel and more rotor plates. However, the addition of more stator and rotor plates is not likely to afford the required reduction` in inductance because of the mutual between the different stator plates. Accordingly, I believe that my invention operates according to the theory first above explained, particularly at the upper end of the range.
Whatever may be the theory of the operatic of the circuit, however, I have found that very satisfactory transmission takes place with the equipment arranged as thus explained and that such efficient transmission may be had at any frequency in the range of from 260 to 350 megacycles by variation only of the concentrated inductance devices I2, I 3, and I4.'
These inductance devices I2, I3, and4 I4 are of the type described and claimed in copending application S. N. 363,016 of Lewis I-I. Van Billiard, filed October 26, 1940, entitled Tuning system, and which is assigned to the same assignee as my present application.
Fig. 2 represents a plan view of one of these inductance devices. It comprises a plate '20, which may be an ordinary sheet metal punching as is ordinarily used in the stator section of a variable condenser. This plate 20 has a large -aperture 2| punched therein, leaving a portion ,of the plate formed about the periphery of the aperture, this periphery being broken at 22. The two terminals of the inductance are taken from points adjacent this break 22 in the periphery, such points being indicated at 23 and 24. These points, or terminals, may be connected through the bypass condensers as shown in Fig. l, with connecting leads as short as possible, tothe re. spective electrodes of the discharge device to which the inductance is to be connected.
In order that the inductance be variable, a pair of rotor plates 25 are provided, mounted upon a shaft 26 about which it is rotatable. These plates may each be in the form of a half of a disk rotatable from the position shown in Fig. 2 to a position in proximity to the plateEIl,` one on either side of that plate, whereby they prac# tically cover the aperture 2I in the plate 20 and since they are conducting members they reduce the inductance between terminals 23 and 24 substantially to zero. As the members 25 are rotated from such position to the position shown the inductance between terminals 23 and 24 changes from substantially zero value to one of very substantial value at the frequencies employed.
Fig. 3 represents, in a perspective view, such an inductance device in which two stator meinbers 20 are arranged in parallel space .relation and connected in series as indicated at 21. This device also comprises three of the rotor members 25 positioned for rotation into interleaved relationship with the stator plates 26. Thus it will be seen that the inductance of this device varies substantially from zero to values which may be approximately twice as great, or even more than that obtained with but a single stator plate.
Fig. 4 represents the arrangement in which two stator plates 20 are connected as indicated at 26 for parallel operation to reduce the inductance obtainable. It will, of course, be understood that in such an inductance device more stator plates may be utilized and that the stator plates may be connected in parallel relation, series relation, or series-parallel relation, as may be required.
Fig. 5 is a sectional View with parts in elevation taken on the line 5-5 of Fig. 2. The stator plates 23 are shown broken away but positioned in parallel relation, in interleaved relation with the rotor plates 25. The stator plates are mounted in insulating material 28, bolted in any suitable way to the form member 28. The rotor plates are likewise mounted together in parallel space relation between the bushings 33 which may be either conducting or nonconducting but which are mounted upon a nonconducting shaft 25 arranged in a bearing member 32, for rotation, as by means of a screwdriver applied to a notch 33 in the end of the shaft. Of course, any suitable handie or knob may be provided as desired.
The structure of the inductance devices employed is very important in the operation of the circuit described and in addition aiords the ad- A vantage that they are economical to build. These inductance devices may comprise the frame structure of any ordinary standard variable condenser. The stator plates of such a condenser may be removed and suitable punchings, as indicated,
substituted therefor. The shaft may also be removed and replaced by the nonconducting shaft indicated in Fig. 5.
The stator plates being of sheet metal and of suiiicient strength to be rigid and self-supporting, may have holes punched therein to permit mounting in close parallel space relation so that the rotor plates may move freely therebetween without contact therewith, and also with a minimum of space between the different plates. These stator plates may also be shaped so that the terminals 23 and 24 thereof may be spaced as close together as possible to reduce the length of thc path between the terminals to as little as possible. In this way, a minimum of inductance is obtainable when the rotor plates are in full interleaved relation with the stator plates.
With such a structure, inductances of concentrated, readily variable form and of sufficiently low value to operate at the highest frequencies in the ranges mentioned and over the ranges mentioned are readily obtainable. I have found in the operation of the system that in the upper portion of the range extending, for example, from 300 to 350 megacycles, all three of the inductances, I2, I3, and I4 are necessarily in the circuit. In the range from 260 to 300 megacycles, however, I nd it necessary to remove one of these inductances, preferably the inductance I 3. This may be effected by breaking the circuit at the points near adjacent terminals of this inductance which are marked X on Fig. 1 of the drawing.
Preferably in the equipment thus described, the discharge device 4 is one employing a screen grid 35 and a suppressor grid 36, the screen grid being connected through a resistance 39 to a source of operating potential which may be connected between conductors 4D. The suppressor grid is connected to the cathode of the discharge device. Of course, the screen grid is grounded at the frequencies in question through a condenser 4I. Voltage is also supplied to the anode of discharge device 4 through a suitable isolation filter comprising resistance 42 and condenser 44. Similar circuits are of course employed in connection with the other discharge devices, that in connection with discharge device 2 being indicated at 42 and 44'.
The cathode of discharge device I is grounded through a condenser 46 at the frequencies of currents supplied to the input of the discharge device, this condenser being one of small capacity arranged as close as is practicable to the cathode of the discharge device. It is also grounded for currents of the 5.4 megacycle frequency through a larger condenser 41 which is connected across a cathode bias resistance 48.
While I have shown a particular embodiment of my invention, it will of course be understood that I do not wish to be limited thereto since various modifications both in the circuit elements and in the instrumentalities employed may be made and I contemplate by the appended claims to cover any such modications as fall within the true spirit and scope of my invention.
What I claim as new and desire to secure by Letters Patent of the United States, is:
1. In combination, a pair of amplifiers operating at frequencies differing from each other by a small percentage and varying over a wide range, each of said amplifiers having a pair of output electrodes, a discharge device having a pair of input electrodes, all of said pairs of electrodes being connected in parallel, the frequencies at which said amplifiers operate being so high that the length of the connections from said pairs of output electrodes to the input electrodes of said discharge device is a substantial part of a quarter of a wave length of the waves at which the respective ampliers operate, and a pair of inductances, each inductance being connected between said electrodes of a respective one of said amplifiers and spaced close thereto so that said length of said connections extends from said inductance to said discharge device, said inductance being variable to resonate with the interelectrode capacity between the respective electrodes at any frequency in a wide range.
2. In combination, a pair of electron discharge amplifiers, each of said amplifiers having an anode and a cathode, an electron discharge device operating as a frequency converter having a cathode, a control electrode, and an output circuit, all of said cathodes being connected together and each of said anodes being connected to said control electrode through a respective conductor having a length equal to a substantial portion of a quarter of a wave length of the wave at which the respective amplifier operates, said amplifiers operating at short wave lengths varying over a vwiderange, theV frequency at which one amplifier operates being different. from that of the other by `a small percentage thereby producing a W fre'- quency in said output circuit of said converter, and apair of inductance devices, each inductance ldevice being connected between said anode and rtrodes.
3. In combination, a pair of electron discharge amplifiers, each of said amplifiers having an anode and a cathode, an electron discharge device operating as a frequency converter comprising a cathode, a control electrode, and an output circuit, said anodes being connected to said control electrode through respective conductors having a length equal to a substantial portion of a quarter of a wave length of the wave at which the respective amplifier operates, said ampliers oper- `ating at short wave lengths varying over a wide range, the frequency at which one amplifier operates being different from that of the other by a small percentage, thereby producing a low frequency in said output circuit of said converter, a plurality of inductance devices, each inductance device being connected between said electrodes of a respective one of said amplifiers and converter, and proportioned to resonate with the interelectrode capacity between the respective electrodes, said inductances being spaced adjacent said respective electrodes.
4. In combination, a pair of'electron discharge devices operating at high frequency, one of said devices having a pair' of input electrodes andthe other of said devices having a pair of output electrodes, said pairs of electrodes being connected in parallel whereby oscillations from said output electrodes are supplied to said input electrodes, said devices being mounted as close together as practicable but the frequency of said oscillations being so great that the short interconnections between said pairs of electrodes have a length equal to a substantial part of a quarter of a wave length of said oscillations, a pair of inductances, each inductance' being .connected between a respective pair of said electrodes and resonating with the capacity therebetween, and being spaced apart by said substantial part of a quarter of a wave length.
5. In combination, a high frequency electron rdischarge amplifier having a pair of outputl electrodes, a second electron discharge device having a pair of input electrodes, capacitive coupling between said pairs of electrodes through connections having a length such that substantial inherent impedance produced by reason of distributed reactance exists in said connections at the frequency at which said amplifier operates, a pair of inductance devices, each inductance device comprising a conductor shaped about the periphery of an enclosure, said periphery being broken at one point, the points of said conductor adjacent said break being connected to opposite electrodes of a respective one of said pairs, and a conducting member parallel with said plane of said conductor and movable into proximity thereto to reduce the inductance of saidL conductor,
said inductance being substantially zero on one extreme of movement of said member and of substantial value at the other extreme of movement vof said member, said inductance of each of said inductance devices being variable to resonate with the capacity between the respective electrodes to which itis connected at any frequency in a wide range.
6. In combination, a pair of electron discharge devices operating at high frequency, each of said devices having a pair of output electrodes, athird `electron discharge device having a pair-of input electrodes, a plurality of conducting plates, each conducting plate being shaped to form an enclosure and having inductance between two closely spaced points thereof, said points of each plate being connected to opposite electrodes of a respective one of said pairs, said plates being spaced apart suiciently to have little mutual inductance, connections between said different pairs of electrodes, and a plurality of movable plates, each movable plate being spaced in parallel relation with a respective one of said rst plates and movable to close spaced relation thereto whereby the inductance of said plates may be reduced to resonate with the capaci'ty between the respective' electrodes at a frequency so high that the length of the conductors comprising said connections is a substantial part of a quarter of the operating wave length, and efficient transfer of energy from said pair of discharge devices to said third discharge device is produced.
HARRY R. SUMMERHAYES, JR.
US431767A 1942-02-20 1942-02-20 High frequency coupling circuit Expired - Lifetime US2341346A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US431767A US2341346A (en) 1942-02-20 1942-02-20 High frequency coupling circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US431767A US2341346A (en) 1942-02-20 1942-02-20 High frequency coupling circuit

Publications (1)

Publication Number Publication Date
US2341346A true US2341346A (en) 1944-02-08

Family

ID=23713334

Family Applications (1)

Application Number Title Priority Date Filing Date
US431767A Expired - Lifetime US2341346A (en) 1942-02-20 1942-02-20 High frequency coupling circuit

Country Status (1)

Country Link
US (1) US2341346A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2448642A (en) * 1947-03-03 1948-09-07 Wilburn Frank Tuner
US2475636A (en) * 1946-09-20 1949-07-12 Gen Electric Tuning device
US2475637A (en) * 1946-09-20 1949-07-12 Gen Electric Variable inductance tuning system
US2492773A (en) * 1946-09-20 1949-12-27 Gen Electric Tuning unit
US2557178A (en) * 1948-04-21 1951-06-19 Hartford Nat Bank & Trust Co Input damping compensated amplifier
US2631241A (en) * 1949-04-23 1953-03-10 Du Mont Allen B Lab Inc Tuning device for high-frequency electrical energy
US2646500A (en) * 1947-03-15 1953-07-21 Rca Corp High-frequency tuner
US2849602A (en) * 1952-03-01 1958-08-26 Du Mont Allen B Lab Inc Heterodyne circuit
US2957124A (en) * 1956-11-26 1960-10-18 Aeronautical Comm Equipment In High frequency choke coil
US4777436A (en) * 1985-02-11 1988-10-11 Sensor Technologies, Inc. Inductance coil sensor
US5402096A (en) * 1992-03-27 1995-03-28 Penny & Giles Position Sensors Limited Transducers
US20050253576A1 (en) * 2004-05-17 2005-11-17 Nyce David S Simplified inductive position sensor and circuit configuration

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2475636A (en) * 1946-09-20 1949-07-12 Gen Electric Tuning device
US2475637A (en) * 1946-09-20 1949-07-12 Gen Electric Variable inductance tuning system
US2492773A (en) * 1946-09-20 1949-12-27 Gen Electric Tuning unit
US2448642A (en) * 1947-03-03 1948-09-07 Wilburn Frank Tuner
US2646500A (en) * 1947-03-15 1953-07-21 Rca Corp High-frequency tuner
US2557178A (en) * 1948-04-21 1951-06-19 Hartford Nat Bank & Trust Co Input damping compensated amplifier
US2631241A (en) * 1949-04-23 1953-03-10 Du Mont Allen B Lab Inc Tuning device for high-frequency electrical energy
US2849602A (en) * 1952-03-01 1958-08-26 Du Mont Allen B Lab Inc Heterodyne circuit
US2957124A (en) * 1956-11-26 1960-10-18 Aeronautical Comm Equipment In High frequency choke coil
US4777436A (en) * 1985-02-11 1988-10-11 Sensor Technologies, Inc. Inductance coil sensor
US5402096A (en) * 1992-03-27 1995-03-28 Penny & Giles Position Sensors Limited Transducers
US20050253576A1 (en) * 2004-05-17 2005-11-17 Nyce David S Simplified inductive position sensor and circuit configuration
US7135855B2 (en) * 2004-05-17 2006-11-14 David Scott Nyce Simplified inductive position sensor and circuit configuration

Similar Documents

Publication Publication Date Title
US2341345A (en) Tuning system
US2410656A (en) Tuned ultra high frequency transformer
US2341346A (en) High frequency coupling circuit
GB541634A (en) Improvements in or relating to electric wave transmission networks
US1998322A (en) High frequency circuit
US3223947A (en) Broadband single pole multi-throw diode switch with filter providing matched path between input and on port
US2342896A (en) Electron discharge device and circuit
USRE20189E (en) Oscillation circuit for electric
US2143671A (en) Ultra short wave circuit
US2153205A (en) Tuning arrangement
US2135672A (en) Ultra short wave system
US2954468A (en) Microwave filter and detector
US3621367A (en) Frequency multiplier employing input and output strip transmission lines without spatially coupling therebetween
US2715211A (en) Ultra high frequency tuning systems
US2426185A (en) Translation of microwaves
US2892163A (en) Band-pass filters
US3267352A (en) Harmonic generators utilizing a basic multiplying element resonant at both the input and output frequencies
US2201326A (en) Electrical wave filter
US3969681A (en) Fast electronic tuning of high power circuits for VHF-UHF power amplifier at high-efficiency
US4823400A (en) Radio frequency mixer
US2401634A (en) Ultra high frequency coupling device
US2141242A (en) Ultra short wave system
US2522370A (en) High-frequency coupling device
US2163247A (en) Electron discharge apparatus
US2344689A (en) Variable capacitor