US2308523A - Electron discharge device - Google Patents

Electron discharge device Download PDF

Info

Publication number
US2308523A
US2308523A US319414A US31941440A US2308523A US 2308523 A US2308523 A US 2308523A US 319414 A US319414 A US 319414A US 31941440 A US31941440 A US 31941440A US 2308523 A US2308523 A US 2308523A
Authority
US
United States
Prior art keywords
circuit
electron
diode
cathode
high frequency
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
US319414A
Other languages
English (en)
Inventor
Frederick B Llewellyn
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.)
AT&T Corp
Original Assignee
Bell Telephone Laboratories Inc
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
Priority to BE442707D priority Critical patent/BE442707A/xx
Application filed by Bell Telephone Laboratories Inc filed Critical Bell Telephone Laboratories Inc
Priority to US319414A priority patent/US2308523A/en
Priority to FR873500D priority patent/FR873500A/fr
Application granted granted Critical
Publication of US2308523A publication Critical patent/US2308523A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/06Receivers
    • H04B1/16Circuits
    • H04B1/163Special arrangements for the reduction of the damping of resonant circuits of receivers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J17/00Gas-filled discharge tubes with solid cathode
    • H01J17/02Details
    • H01J17/04Electrodes; Screens
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons

Definitions

  • Another object of the invention is to take ad-A vantage in a discharge system having a critical transit time of the increased electron ilow obtainable with an atmosphere of gas or ionizable vapor.
  • An additional object of the invention is to in.A
  • the attainment of the rst of the above-mentioned objects is desirable from the fact that in electrical circuits for the utilization of very high frequencies dimculties are had in maintaining impedances as high as are wanted and in otherwise4 caring adequately for the comparatively large losses which appear as operating frequencies are increased.
  • a rather familiar example of the type of problem involved is that of maintaining the voltage at the grid input of a vacuum tube when the grid losses become large, as they may at high frequencies.
  • Contributing to the diiiiculties as the use of higher frequencies is attempted is the fact that the losses in most physical circuit elements increase rapidly with increase in frequency so that networks and circuit combinations which may be used effectively at low frequencies are often of no value or even a detriment at higher frequencies.
  • a solution to the problems indicated is had according to this invention through using as a circuit component a diode adjusted to a critical electron transit time such that it exhibits a negative resistance which is used to annul a corresponding amount of positive resistance, or loss, in the associated circuit.
  • a triode translating device which may be an amplier, detector or oscillator is provided with a resonant circuit comprising a diode having a. critical electron transit time.
  • the negative resistance property of the diode referred to above is enhanced, when desirable, by the introduction of mercury vapor or other ionizable gas to permit greater electron current to flow.
  • An atmosphere of mercury vapor or other ionizable gas may be introduced either by derivation from a mercury pool serving asa cathode o-in conjunction with a solid cathode of usual type.-
  • the introduction of ionizable gas to permit increased electron current applies generally toapplications of electron discharge tubes where, asl in the above-described use of the diode, the desired effect results from interaction between the electron stream and the high frequency field through which it passes and the magnitude of the effect is proportional to the electron current.
  • ionizable gas in devices having critical electron transit time is distinct from previous uses of mercury vapor or gas in electronic devices where the important feature has been the particular conducting property of an arc or the gaseous atmosphere.
  • the function of the vapor or gas is to neutralize space charge and allow a greater number of electrons to leave the vicinity of the cathode and be employed usefully in the electron stream.
  • Fig. 1 illustrates the use of a diode to control the impedance of a grid in'put circuit
  • Fig. 2 showsvdiagrammatically a triode detector or amplifier circuit in which a diode functions as a tuned circuit component
  • Fig. 2A indicates the modification f'Fig. 2 to e illustrate the use of an ionizable gas in the diode element of Fig. 2 y
  • Fig. 3 indicates the equivalent high frequency circuit corresponding to Fig. 2 and Fig. 2A;
  • Fig. 4 shows a triode oscillator circuit in which a ltiode functions as part of the oscillation circu element of Fig. 6;
  • Fig. 7 indicates the equivalent high frequency circuit corresponding to Fig. 6 and Fig. 6A;
  • Fig. 8 shows a diode employing mercury vapor connected in an oscillator circuit wherein oscil- Fig. 4A indicates the modification of Fig. 4 to illustrate the use of an ionizable gas in the diode lations are generated by virtue of a critical relation between the transit time of the electrons in the diode and the period of the high frequency oscillations;
  • Fig. 9 shows an alternate form of diode structure employing mercury vapor in an oscillator circuit which is similar to that of Fig. 8 except that the resonant circuit is in the form of a cavity resonator which is the envelope of the diode;
  • Fig. 10 shows a section of wave guide used as a cavity resonator in which oscillations are pro- Y cuted by an electron gun containing an ionizable gas
  • Fig. 1l shows the production of oscillations in a resonant wave guide by projecting electrons transversely through it by means of an electron gun containing an ionizable gas;
  • Fig. 2 shows a high frequency amplifier arrangement employing cavity resonators and an electron stream produced by an electron gun containing an ionizable gas
  • Fig. 13 shows a modification of the arrangement of Fig. 12 to produce self-oscillation.
  • Cavity resonators may take various shapes and one is that of a section of wave guide which is made short or is partitioned off from the balance of a long guide so that it has resonant properties.
  • the more general term cavity resonator is often applied to cavity type structures not obviously in the form of a portion of wave guide or other distinctively named device.
  • a resonant wave guide may not necessarily appear to be of the cavity type. This is exemplied by a relatively short wave guide with open ends.
  • any resonant circuit whether it be a cavity type termed cavity resonator, a resonant wave guide, a tunedLecher system, a tuned coaxial line or a combination of lumped inductance and capacity may function similarly in an electric circuit.
  • the Wave guide or cavity type of structure possesses several advantages over other forms of resonant circuit, among which are: that radiation is more readily controlled or prevented and that the conducting material is more favorably distributed to minimize circuit resistance.
  • Fig. 1 illustrates a type of circuit problem frequently encountered in the use of very high frequencies and a solution therefor by use of a diode as a circuit element to improve impedance conditions according to a feature of this invention.
  • a detector or amplifier circuit a three-element vacuum tube Ill with conventional input blocking condenser I I, grid input resistance I2 and grid bias battery I3 to which may be connected, by means of switch I6, the tuned input circuit consisting of inductance 1 and capacitance 8. It is assumed that the tuned input circuit is energized from an external source indicated symbolically at 9.
  • the diode I4 utilizing the source of direct current power supply, battery 5 and limiting resistance 6, and bypass capacitance 4 may be connected across the tuned input circuit by closure of the two-pole switch I5, I5. With a given amount of energy delivered to the tuned circuit from source 9 a certain voltage is developed between the points A and B, opposing terminals of the tuned input cirmay be connected to the tuned circuit at A and B by the closure of switch Il. At low frequencies the grid losses in the tube would ordinarily be so low that the voltage developed between A and B by the source 3 would not be greatly affected by the connection.
  • the grid loss may be so high that 'when switch I6 is closed the load imposed on the tuned circuit so lowers the effective impedance between points A and B that the energy available from source ⁇ 9 does not develop sufficient voltage between those points to effectively drive the grid of tube IU.
  • This situation is bettered according to the invention by connection also between the points A and B, through closure of switch I5, of the diode Il which is adjusted to have a critical electron transit time as will be explained later.
  • the diode I4 consists of the anode 2 and cathode 3 enclosed in the envelope I together with the necessary lead-in conductors.
  • the cathode 3 is shown as a mercury pool which is a source of vapor employed to increase the effectiveness of the electron discharge, which feature of the invention will be described in more detail later.
  • the advantage of vapor or other lonizable gas may not always be required for satisfactory results, in which cases any suitable cathode may be employed and the vapor or gas omitted.
  • the anode of the diode I4 is positively charged by source 5 through limiting resistor i and inductance 1.
  • Capacitance 4 serves as a high l frequency by-pass around source 5 and resistor vacuum tube and for such purpose the tube I D G.
  • the function of the diode when con nected between A and B is to provide a negative resistance to neutralize the positive resistance introduced into the tuned input circuit 1, 8 by the grid loss in tube I0, and also part of that inherent in 'I and 8 if that is desired.
  • This counteracts the lowering of the eective impedance between A and B when the grid of tube I0 is connected and permits source 9 to maintain an effective grid driving voltage.
  • the reactance and resistance characteristics of the diode enable it to function in this desired manner when the electron transit time is adjusted to approximate the period of 1%, 21A, 31A, etc., cycles of the high frequency employed.
  • the essentials, in any case, are that the electron stream traverse a space occupied by the alternating electromagnetic lfield associated with a circuit which is resonant at the desired frequency and that the time required for the electrons to traverse the space is approximately the period of 11/4, 21/4, 31/4, etc., cycles.
  • Factors affecting the diode resistance are shown in the theory presented in the above-mentioned copending application, Serial No. 156,647, illed July 31, 1937,
  • Patent No. 2,190,668, dated February 20, 1940, and Fig. 3 of that application and patent shows graphically the variation of the diode resistance with variation of the electron transit time. It will be noted from this curve that the resistance varies cyclically between positive and negative values, the maximum negative values occurring at transit angles in radians corresponding to the periods of 11/4, 21A and 31A cycles mentioned above.
  • the transit time is determined by the spacing of the gap between the surfaces of the cathode and anode, which determines the distance through the field traversed by the electrons, by the anode or accelerating voltage used to propel the electrons throughthe gap space, and to a lesser extent by the space charge density within the gap. It will be noted in the discussion in the above-mentioned copending application, Serial No. 156,647, led July 31, 1937, Patent No. 2,190,668, dated February 20, 1940, that the magnitude of the negative resistance effect is dependent upon the electron stream current. To quote:
  • Equation 6 the negative resistance, and hence the driving power for the oscillations, is proportional to the density In of the directelectron current.
  • a feature of this invention is to employ for that purpose in the electron discharge tube mercury vapor or other ionizable gas to neutralize space charge and allow electrons to leave more readily the vicinity of the cathode.
  • the density of the gas must be kept sufliciently low that there are relatively few collisions between electrons and gas ions. This condition is maintained by control of temperature and pressure of the gas and is one commonly met in the operation of rectifiers of the hot cathode mercury vapor type.
  • a diode may be used as a circuit component regardless of the type of cathode employed and either with or without the gaseous atmosphere.
  • the cathode may be cold or of the heated type, and the purpose of the gas is to increase the effective- ⁇ ness of the diode.
  • Fig. 1 for illustrative purposes shows conventional forms of inductance and capacitance whereas at very high frequencies, as in the range where this invention is particularly applicable, tube elements and connecting leads though short may be the principal reactance elements of the circuit. For that reason the essentials of Fig. 1 are shownsomewhat differently in Figs. 2 and 3. In Fig. 2 and the figures following 4through Fig. 7, which are schematic diagrams, the triode and diode elements, and the other circuit elements shown, are indicated by conventional symbols therefor. In practice these elements may take various mechanical forms.
  • Fig. 2 shows an ampliiier or detector circuit, typical for high frequency operation, which includes a diode as a circuit component for the purpose of improving the performance. The triode ampliiier or.
  • Fig. 3 is a schematic of the high frequency circuit shown in Fig. 2 with direct current paths omitted and the reactances and resistances effective under high frequency Cil operation indicated.
  • the brackets I0 and I4 in these and following figures are to assist in identifying the elements in the equivalent circuit schematics. For instance, the various circuit elements, capacitance, resistance, inductance, included by bracket I4 in equivalent circuits Figs.
  • the resonant input circuit to the triode now includes all these elements I9, 20, 2
  • a diode adjusted for critical transit time operation may be used to avoid serious depression of the impedance of a grid input circuit due to high frequency grid losses.
  • Fig. 4 shows a triode oscillator circuit employing a diode as a circuit component. Designations correspond to those of Fig. 2.
  • the direct current plate potential source 26 supplies both diode I4 and triode I0 through choke 21.
  • the oscillator load is connected through blocking condenser 28.
  • Fig. 5, in the same manner as Fig. 3, shows the important elements of the equivalent high frequency circuit of Fig. 4.
  • elements 22 and 23 representing the capacitance and resistance of the grid-cathode circuit and 29 representing the inductance of the external gridto-cathode lead.
  • These elements constitute a resonant input circuit which may in practice be supplemented, if necessary, by an adjustable tuning element.
  • Such an element may consist oi a variable inductance in series with the grid-tocathode lead represented by inductance 29, a variable capacitance in shunt with that lead or any other desired arrangement.
  • 24 represents the grid-to-plate capacitance and 25 the plate-tocathode capacitance of triode I0.
  • I9, 20 and'ZI represent lead inductance, anode-cathode capacitance and negative resistance, respectively, of the diode I4 making up the resonant output circuit.
  • Fig. 5 the complete circuit as indicated schematically in Fig. 5 constitutes an oscillator of the commonly termed tuned-plate tuned-grid type in which the feedback voltage is impressed upon the input circuit through the grid-to-plate capacitance 24.
  • the diode enhances the strength of oscillation by compensating with its negative resistance for positive resistance in the oscillator or load circuit.
  • Fig. 6 shows a triode oscillator circuit in which.
  • a diode is used to provide a stiif frequency control circuit in much the same manner as a piezoelectric crystal is employed.
  • the diode I4 is connected to the grid of triode I0 through blocking condenser I I and is energized from source 5 through choke 28.
  • the plate potential of triode I0 is supplied from source I1 through inductance 30.
  • the load I8 is connected through blocking condenser 28.
  • Fig. 7 shows the important elements of the equivalent high frequency circuit of Fig. 6. It will be observed that this is an oscillator circuit of the tuned-plate tuned-grid type similar to that of Fig. 4 and Fig. 5.
  • I 3, 20 and 2l represent, respectively.
  • the lead inductance, the anode-cathode capacitance and the negative resistance of the diode I4. 22 and 23 represent, respectively, the grid-cathode capacitance and remstance of the triode i0.
  • the resonant output circuit which is tuned to substantially the same frequency as the control circuit, is composed of the plate cathode capacitance 25 of triode i0 and the inductance 30.
  • Figs. 2, 4 and 6 the diodes are shown in diagrammatic form indicating a simple hot thermionic cathode.
  • Other forms of cathode may be used, and in accordance with a feature of the invention previously mentioned an ionizable gas may be introduced into the tube for the purpose of increasing the direct electron current.
  • Fig. 8 illustrates the use of a diode having mercury vapor and a mercury pool cathode in an oscillator circuit wherein oscillations are produced by virtue of critical electron transit time in the diode.
  • the diode comprising the envelope I, anode 2 and cathode 3 is connected through by-pass condenser 4 to the resonant circuit consisting of induotance 1 and capacitance 8.
  • the anode potential source 5 is connected to the diode through the limiting resistor 6 and inductance l.
  • oscillations will occur in a circuit of this type when the power generated in the negative resistance of the diode by virtue of critical electron transit time exceeds the losses in the circuit.
  • ionizable gas By the use of ionizable gas in the diode the negative resistance power is increased and oscillationsmay be had under more adverse conditions or the strength of oscillations may be increased.
  • the gas may be derived in the form of mercury vapor from a. mercury pool cathode, as shown in Figs. 8 and 9, from a mercury pool in combination with a hot cathode emitter, as indicated in Figs. 10, 11, 12 and 13, or the proper amount of some other form of ionizable gas, such as argon, may be placed in the diode envelope.
  • Fig. 9 is shown an alternative form of diode oscillator arrangement.
  • the circuit is similar to that of Fig. 8 but here the diode envelope l is in the form of a conducting resonant cavity which serves also as the oscillatory circuit.
  • the gure shows an axial section of the cavity which is cylindrical in shape.
  • the disc-shaped anode 2 is insulated for direct current from the rest of the cavity at 3
  • a load circuit may be connected to the output coupling coil 32.
  • the mercury pool at 3 directly opposite the anode serves as a cathode and a source of mercury vapor to increase the electron current.
  • another form of cathode may be employed in combination with a mercury pool or with another type of ionizable gas eliminating the mercury.
  • Fig. 9 illustrates only one of many possible forms a cavity diode may take and only one embodiment of the eectiveness of critical electron transit time opera on.
  • Figs. 10, 11, 12 and 13 show other embodiments of the principle of using an ionizable gas to increase the electron current and therefore the energy available from an electron stream which is caused to react with an alternating electromagnetic fleld for the purpose of transferring energy from the electron stream to the field.
  • Fig. 10 shows an electron gun, employing mercury vapor as an example of ionizable-gas. arranged to excite a short section of wave guide and a method of transferring the high frequency energy generated therein for transmission through a wave guide.
  • axial cross-sectional views of cylindrical wave guides are shown at 36 and 40.
  • the length of the short section 36 is limited by the end closures to form a resonant cavity of the desired dimensions while 40 is indefinite in length, serving only to transmit the high frequency energy generated in 36.
  • the electron gun comprising envelope I, anode 2, cathode 3 and hollow cylindrical accelerating electrode 34 is inserted along the axis through the short section of wave guide 36 which constitutes a resonant cavity as described in applicants copending application Serial No.
  • FIG. 10 corresponds to 36 of the present Fig. 10.
  • 33 in the patent corresponds to the openings at the inner ends of 31, 31 in the present Fig. 10.
  • F, 36 and 34 in the patent correspond to 3, 34 and 2, respectively, in the present Fig. l0.
  • the utilization circuit, 38, 39 and 40 of the present Fig. 10, is not included in the Fig. 10 of the patent.
  • the electron stream is shown to traverse the axis of the resonant chamber and high frequency energy is generated by virtue of the critical relation between the electron transit time across the chamber and the high frequency period.
  • the equivalent diode surfaces between which the electron transit time is measured are the intersecting surfaces of the electron stream and the boundaries of the resonant chamber. These are, the inner edges of the holes 33 in Fig. 10 of the Patent 2,190,668 and the inner edges of the cylinders 31, 31 in the present Fig. 10.
  • the stream of electrons will react with the type of electric field within the section of guide which is associated with the type of wave designated type Eo by G. C. Southworth on page 287 of the Bell System Technical Journal, vol. 15 (April 1936) and consists of lines of electric force passing along the principle of using an ionizable gas to increase the axis, then radially to terminate on the enclosing conductor of the guide and this type of field will be produced by the electrons passing along the axis when their transit time is approximately equal to the period of 11A, 2%. 3%, etc., cycles of the high frequency, as explained in the abovementioned copending application.
  • the coaxial line consisting of the outer conductor 38 and the inner conductor 39 is arranged to transfer the highfrequency energy of such a wave in 36 to the wave guide 40 by virtue of the inner conductor 39 projecting into both sections of guide in a manner -to couple with the electric fields.
  • the small projecting cylinders 31, 31 at the openings through which the electron gun is inserted are to prevent loss by radiation through those openings.
  • the accelerating electrode 34 is energized positively with respect to the cathode 3 by potential source 5.
  • the collecting anode 2 is energized positively with respect to 3 by potential source 35.
  • a small amount of mercury is shown at 33 as a source of mercury vapor to serve as the ionizable gas to facilitate the passage of electrons from the cathode to the anode.
  • the increase in electron flow due to the use of an ionizable gas in a device of this kind is beneficial since, as has been previously indicated, the output and eiciency are directly dependent upon the amount of electron current.
  • FIG. 1l A slightly different arrangement of an electron l gun, using an ionizable gas, for producing high frequency waves in a wave guide is shown in Fig. 1l.
  • the electron gun is shown passing transversely through the cylindrical wave guide 4
  • Other designations are the same as in Fig. 10.
  • the stream of electrons passing transversely through the guide will react with a type of electric field therein which is associated with the type of wave designated by G. C. Southworth as type Hi, page 287 of the Bell System Technical Journal, vol. 15 (April 1936) and consists of lines of electric force passing transverse to the axis substantially parallel to a diameter and this type of field will be produced by the electrons when their transit time is as indicated above in connection with Fig. 10.
  • Fig. 11 like that of Fig. 14 in applicants copending application Serial No. 156,647, filed July 31, 1937, Patent No. 2,190,668, dated February 20, 1940, previously referred to, requires that the portion of the wave guide immediatelysurrounding the electron gun be closed oi to the proper length with a plunger, as indicated at in Fig. 11, and an apertured diaphragm, 5I, to determine the frequency and the coupling to the transmitting portion of the wave guide as indicated in that application and shown in the associated Fig. 14.
  • FIGs. l2 and 13 representing, respectively, a high frequency amplifier and an oscillator circuit utilizing the principle of velocity modulation, where the'electron stream is subjected to different electric field conditions in different parts of its path as shown in applicants prior Patent No. 2,096,460, issued October 19, 1937.
  • Other applications of the velocity modulation principle are to be found in articles by Messrs. Hahn and Metcalf in the Proceedings of the Institute of Radio Engineers, vol. 27, February 1939, pages to 116. and by Messrs. R. H.y Varian and S. F. Varian in the Journal of Applied Physics, vol. 10, February 1939, page 140.
  • Fig. 12 the electron gun and sources of operating potentials are designated the same as in Figs. 10 and 11.
  • 42 and 43 represent resonant cavities of the circular reentrant type, with axial openings through which the electron gun is passed at 45 and 46.
  • Cavity 42 serves as the input circuitand is coupled to an input line at 44.
  • Cavity 43 serves as the output circuit and is coupled to an output line at 32.
  • the electron stream from cathode 3 to collector 2 passes through the electric ileld of cavity 42 for a short distance-at 45 and through the eld of cavity'43 for a short distance at 46.
  • the alternating eld at 45 resulting from the input to the amplifier at 44, reacts upon the electron stream to speed up those electrons which enter the field during one half of each cycle and to retard those which enter during the other half cycles. After leavingthe region of the field at 45 the electrons which have had their velocity increased tend to overtake .those which have had their velocityreduced, so that by the time the region of 46 is reached a rearrangement of electrons along the path has taken place andthe stream is no longer of uniform density. Regions of greater and less electron density alternate in accordance with the effect of the field at 45. In other words, the electron stream has been density modulated in accordance with the input to the amplifier.
  • Fig. 13 shows how the amplifier circuit of Fig. 12 may be modified to act as an oscillator.
  • an electron discharge device containing an ionizable gaseous atmosphere and electrodes including at least a cathode and an anode, means including electric potential means for causing a stream of electrons to traverse a path from the cathode to the anode, and means for'impressing a high frequency electric field upon the electron stream over at least a portion of the path and between two substantially parallel planes transverse to .the path, the magnitude of the said electric potential means and the distance between the said transverse planes being such that ,the electron transit time through the high frequency eld substantially equals the period of any whole number of cycles plus one-quarter cycle of the high frequency field.
  • a high frequency system comprising an electron discharge device having an ionizable medium, a pair of substantially parallel electrodes between which a high frequency electric field may be impressed, electric potential means for producing an electron discharge over a path including the space between the said electrodes, the distance between the electrodes and the magnitude of the electric potential means having such relationship as to cause the electron transit time between the electrodes to be a period between that of any whole number of cycles of the operating frequency of the system and that number increased by one-half cycle.
  • a high frequency system comprising an electron discharge device containing an ionizable medium having as electrodes at least a cathode and an anode, means including electric potential means for producing an electron discharge over a path between the cathode and anode, means for impressing a high frequency field upon the electron stream over at least a portion of the path and between two planes substantially parallel and transverse to the path, the path of the electron discharge and the magnitude of the electric potential means being such that the electron transit time through the high frequency electric field between the transverse planes is a period between the period of any whole number of cycles of the high frequency field and the period of that number increased by one-half cycle.
  • a resonant circuit means for predetermining the terminal impedance of the circuit comprising an electron discharge tube containing an ionizable gaseous atmosphere, having a cathode and anode and being electrically coupled to the circuit, means including electric potential means for causing a iiow of electrons over a path between the cathode and anode, and means independent of the said electron discharge tube for energizing the said circuit at a frequency substantially equal to its resonant frequency, the coupling between the discharge tube and the circuit including means for impressing upon the electron stream, over at least a portion of the said path and between two substantially parallel planes transverse to the path, a high frequency electric field derived from the high frequency energy in the circuit, .the magnitude of the said electric potential means and the distance between the two said transverse planes being such that the electron transit .time through the high frequency electric field is a period between that of any whole number of cycles of the high frequency ileld and that number increased by one-half cycle
  • a resonant circuit energy transfer leads connected thereto, the damping factor of the circuit being dependent upon the losses within the circuit and those imposed by the energy transfer leads and any devices connected to the leads, means for reducing the damping of the circuit to a small magnitude comprising a diode containing an ionizable gaseous atmosphere and having its cathode and anode terminals connected to the circuit, means independent of the said diode for energizing the circuit at substantially its resonant frequency, and means including electric potential means for causing a flow of electrons between substan-f tially parallel surfaces of the cathode and anode', the magnitude of the electric potential means and the distance between the cathode and anode being such that the electron transit time therebetween ls a period between that of any whole number of cycles of the high frequency and that number increased by one-half cycle.
  • a wave translating device having input and output terminals and a resonant circuit. of which the damping is to be reduced. connected with said device comprising a diode containing an ionizable gaseous atmosphere, means external to the resonant circuit for energizing it at substan tially its resonant frequency, the diode having substantially parallel electrode surfaces and means including electric potential means for causing a ow of electrons therebetween, the length of the electron path between the two said surfaces and the magnitude of the electric potential means being such that the electron transit time between the two surfaces is sub stantially the period of any Whole number of cycles plus one-quarter cycle of the operating frequency of the device.
  • a thermionic triode translating device having input and output terminals and a resonant circuit for said device comprising a diode containing an ionizable gaseous atmosphere connected between two of said terminals, means external to the resonant circuit for energizing it at substantially its resonant frequency, the diode having substantially parallel electrode surfaces and means including electric potential means for causing a flow of electrons therebetween, the length of the electron path between the said surfaces and the magnitude of the electric potential means being such that the electron transit time between the two surfaces is a period between that of any whole number of cycles of the operating frequency of the device and that number increased by one-half cycle.
  • a device for producing electric oscillations of a desired high frequency comprising a thermionic amplifier with tuned grid and plate circuits coupled to produce electrical oscillations,
  • At least one of the tuned circuits serving as a frequency determining circuit and comprising a diode containing an ionizable gaseous amplifier and having a cathode and an anode, means including electric potential means for causing a stream of electrons to traverse a path between the said cathode and anode, and means for impressing a high frequency electric field produced from the electric oscillations upon the electron stream over at least a portion of the path and between two substantially parallel planes transverse to the path, the magnitude of the said electric potential means and the distance between the said transverse planes being such that the electron transit time through the high frequency field is between the period of any whole number of cycles of the high frequency and that number increas'eriday onehalf cycle, the diode being electrically connected to the amplifier to function in the frequency determining circuit therefor.
  • An electron discharge device for producing electric oscillations comprising a thermionic amplifier, a diode containing an ionizable gaseous atmosphere electrically connected to the ampliiier to function in a frequency determining circuit therefor, and means including electric potential means for causing a flow of electrons over a path between the cathode and anode of and the distance between the two said transverse planes being such that the electron transit time through the high frequency eld is a period between that of any whole number of cycles of the high frequency eld and that number increased by one-half cycle.

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Amplifiers (AREA)
US319414A 1940-02-17 1940-02-17 Electron discharge device Expired - Lifetime US2308523A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
BE442707D BE442707A (me) 1940-02-17
US319414A US2308523A (en) 1940-02-17 1940-02-17 Electron discharge device
FR873500D FR873500A (fr) 1940-02-17 1941-06-27 Systèmes à fréquences élevées utilisant des dispositifs à décharge électronique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US319414A US2308523A (en) 1940-02-17 1940-02-17 Electron discharge device

Publications (1)

Publication Number Publication Date
US2308523A true US2308523A (en) 1943-01-19

Family

ID=23242152

Family Applications (1)

Application Number Title Priority Date Filing Date
US319414A Expired - Lifetime US2308523A (en) 1940-02-17 1940-02-17 Electron discharge device

Country Status (3)

Country Link
US (1) US2308523A (me)
BE (1) BE442707A (me)
FR (1) FR873500A (me)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2466136A (en) * 1943-11-16 1949-04-05 Raytheon Mfg Co Electrical protective device
US2475652A (en) * 1942-08-03 1949-07-12 Sperry Corp High-frequency tube structure
US2505534A (en) * 1943-04-27 1950-04-25 Gen Electric Device for controlling the propagation of energy in a wave guide
US2511106A (en) * 1942-05-07 1950-06-13 Fredholm Johan Olof Helge Gas-filled cavity resonator
US2532796A (en) * 1940-12-18 1950-12-05 Csf Velocity modulation electronic valve
US2540148A (en) * 1945-03-22 1951-02-06 Sperry Corp Ultra high frequency powerselective protective device
US2557180A (en) * 1943-04-27 1951-06-19 Gen Electric Apparatus for coupling ultra high frequency systems
US2625605A (en) * 1948-04-14 1953-01-13 Rca Corp Resonator
US2644908A (en) * 1949-03-26 1953-07-07 Sperry Corp Microwave frequency cavity resonator structure
US2656484A (en) * 1945-12-27 1953-10-20 Bruce B Cork Tunable cavity
US2706782A (en) * 1949-06-11 1955-04-19 Bell Telephone Labor Inc Broad band microwave noise source
US2725531A (en) * 1943-04-27 1955-11-29 Gen Electric Gas discharge coupling device for waveguides
US2848649A (en) * 1952-01-24 1958-08-19 Itt Electromagnetic wave generator
US2962677A (en) * 1945-10-04 1960-11-29 Bell Telephone Labor Inc Wave guide joint
US3411109A (en) * 1966-09-06 1968-11-12 Union Carbide Corp Thermionic diode oscillator

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2532796A (en) * 1940-12-18 1950-12-05 Csf Velocity modulation electronic valve
US2511106A (en) * 1942-05-07 1950-06-13 Fredholm Johan Olof Helge Gas-filled cavity resonator
US2475652A (en) * 1942-08-03 1949-07-12 Sperry Corp High-frequency tube structure
US2557180A (en) * 1943-04-27 1951-06-19 Gen Electric Apparatus for coupling ultra high frequency systems
US2505534A (en) * 1943-04-27 1950-04-25 Gen Electric Device for controlling the propagation of energy in a wave guide
US2725531A (en) * 1943-04-27 1955-11-29 Gen Electric Gas discharge coupling device for waveguides
US2466136A (en) * 1943-11-16 1949-04-05 Raytheon Mfg Co Electrical protective device
US2540148A (en) * 1945-03-22 1951-02-06 Sperry Corp Ultra high frequency powerselective protective device
US2962677A (en) * 1945-10-04 1960-11-29 Bell Telephone Labor Inc Wave guide joint
US2656484A (en) * 1945-12-27 1953-10-20 Bruce B Cork Tunable cavity
US2625605A (en) * 1948-04-14 1953-01-13 Rca Corp Resonator
US2644908A (en) * 1949-03-26 1953-07-07 Sperry Corp Microwave frequency cavity resonator structure
US2706782A (en) * 1949-06-11 1955-04-19 Bell Telephone Labor Inc Broad band microwave noise source
US2848649A (en) * 1952-01-24 1958-08-19 Itt Electromagnetic wave generator
US3411109A (en) * 1966-09-06 1968-11-12 Union Carbide Corp Thermionic diode oscillator

Also Published As

Publication number Publication date
FR873500A (fr) 1942-07-09
BE442707A (me)

Similar Documents

Publication Publication Date Title
US2368031A (en) Electron discharge device
US2308523A (en) Electron discharge device
US2425748A (en) Electron discharge device
US2404261A (en) Ultra high frequency system
US2222902A (en) High frequency apparatus
US2312919A (en) Modulation system for velocity modulation tubes
US2314794A (en) Microwave device
US2235414A (en) Thermionic valve circuits
US2422695A (en) Suppression of parasitic oscillations in high-frequency devices
US2482769A (en) High-frequency apparatus
US2436397A (en) Ultra high frequency oscillator
US2237878A (en) Electron discharge device
US2267520A (en) Oscillation generator system
US2372213A (en) Ultra-high-frequency tube
US2329780A (en) Electron discharge device
US2462137A (en) Electron discharge device
US1853632A (en) Multiunit tube
US2487656A (en) Electron discharge device of the beam deflection type
US2404226A (en) High-frequency discharge device
US2153131A (en) High frequency oscillator
US2515998A (en) Electron discharge device
US2293387A (en) Electron discharge device
US1982916A (en) Transmitter
US2433634A (en) Electron discharge device of the cavity resonator type
US2027919A (en) Short wave signaling