US3105169A - Pulse generator - Google Patents

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US3105169A
US3105169A US789445A US78944559A US3105169A US 3105169 A US3105169 A US 3105169A US 789445 A US789445 A US 789445A US 78944559 A US78944559 A US 78944559A US 3105169 A US3105169 A US 3105169A
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capacitor
discharge
pulse
thyratron
load impedance
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Frithiof B Anderson
Jr Samuel H Pearsall
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AT&T Corp
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Bell Telephone Laboratories Inc
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    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03KPULSE TECHNIQUE
    • H03K3/00Circuits for generating electric pulses; Monostable, bistable or multistable circuits
    • H03K3/02Generators characterised by the type of circuit or by the means used for producing pulses
    • H03K3/53Generators characterised by the type of circuit or by the means used for producing pulses by the use of an energy-accumulating element discharged through the load by a switching device controlled by an external signal and not incorporating positive feedback
    • H03K3/55Generators characterised by the type of circuit or by the means used for producing pulses by the use of an energy-accumulating element discharged through the load by a switching device controlled by an external signal and not incorporating positive feedback the switching device being a gas-filled tube having a control electrode

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  • This invention relates to pulse circuits and, more particularly, to pulse circuits employing gaseous electron discharge devices.
  • vacuum tubes may be so employed but with the limitation that, as the amplitude of the required pulse signal current rises, both the size and heating power requirements of the necessary vacuum tubes may go beyond that which is feasible for a particular application.
  • gaseous electron discharge devices which are exemplified by the well-known thyratron tube.
  • these discharge devices'ionized gas within an envelope serves as a current carrier between cathode and anode electrodes.
  • the initiation of such a current conducting ionized condition may be controlled by an auxiliary grid electrode.
  • heavy current may be conducted by the ionized gas particles Within the envelope without necessitating heavy thermionic electron emission by a cathode.
  • pulse generators of the prior art have required overlarge vacuum tubes and associated power supplies or, on the other hand, have been objectionably inaccurate in either the beginning or the terminating portion of generated pulse wave signals. This latter inaccuracy has often led to a further objectionable delay in the generation of succeeding pulse signals.
  • control discharge devices are advantageously gaseous discharge devices having a control or starter electrode or grid to which the control signal is applied; a thyratron is an example of this type of device. Such devices enable the circuit to provide a large output signal. Circuits in accordance with our invention are so arranged that conduction in the control gaseous discharge devices is terminated by the breakdown of the last of the control devices, conduction in this last device automatically extinguishing the conduction in itself and in any other such devices in the circuit in a high conduction state at that time.
  • the circuit is arranged so that the first control device establishes a series circuit including itself, the storage capacitor, and the load to initiate the output pulse through the load.
  • a second control device upon conduction, bypasses the load and establishes a series path including itself, the storage capacitor, and the first device, to discharge the capacitor and in so doing to extinguish conduction both in itself and in the first device.
  • the first and second control gaseous discharge devices are mutually poled for the flow of current in one direction through the series path including the intermediately connected storage condenser.
  • the first device controls the charging of the storage capacitor and also determines the initiation of the output pulse.
  • the second control gaseous discharge device terminates the output pulse by bypassing the output circuit, and a third gaseous discharge device connected in parallel with the storage condenser upon breakdown discharges the storage condenser and thereby automatically extinguishes the discharge in itself and in both the other control devices.
  • a pulse generator circuit for producing accurately timed large amplitude output pulses includes a pair of control discharge devices series connected with a storage capacitor for passage of current through this series path in a single direction. More specifically in accordance with our invention, the control discharge devices are gaseous discharge devices as of the thyratron type having a control or starter electrode.
  • the storage capacitor be charged independently of the two control gaseous discharge devices set forth above, the two devices being connected so that uponconduction of the second to terminate the output pulse, both devices are initiallycod ducting providing low impedance connections to ground in a series circuit from both plates of the storage capacitor and thereby providing both automatic discharge of the capacitor and extinction of the discharge in both control devices.
  • the charging of the storage condenser may be controlled through another gaseous discharge device having an inductance connected in'series therewith, conduction in this device being selfextinguishing on the charging of the storage condenser.
  • FIG. 1 is a schematic diagramof an illustrative high power pulse generating system in accordance with one embodiment of the invention
  • FIG. 2 is a schematic diagram of another illustrative high power pulse, generating system in accordance-with ing the operations of the embodiments of the invention as shown in FIGS. 1 and 2, respectively.
  • FIG. 1 there is shown a resonantly charged pulse generating circuit to which energy is supplied from a direct energy source 11 which may conveniently be any one of the many direct current power supplies known in the electronic art.
  • Energy from this source serves to charge a storage element, the capacitor 12, through a serially connected charging inductor 14 and a variable impedance isolating element 16 which adv-antageouslymay be a high conductance electron discharge device such as a thyratron electron tube.
  • Completing a serial circuit including the capacitor 12 and the energy source 11 is a rectifying device comprising a diode-connected triode electron tube 18, which is connected across a pair of output terminals 17 and 19 and is poled ior conducting current in a low resistance direction consistent with the polarity of the sourcell.
  • a load impedance 20 is connected in parallel with electron tube 18.
  • This load impedance 20 is shown for convenience of illustration as a resistor. It may as well be any pulse utilization circuit as, for example, a radar magnetron pulsing circuit.
  • Two circuit controlling electron discharge devices 22 and 24 are connected in serial relation with the storage capacitor 12, each for conducting current flowing through that capacitor in a like direction.
  • These discharge devices may advantageously also be thyratron'tubes.
  • tubes are connected anode to cathode.
  • Thyratron 22 is further connected, as shown, in serial relation with the energy source 11, the inductor 14, and the isolating thyratron 16.
  • thyratron 24 is further connected in parallel with the load impedance 20.
  • control grids of the three thyratrons 16, 22, and 24 are respectively connected through resistors 26, 27, and 28 to a source of Off-biasing potential 30.
  • Each has a 7 direct connection of its shield grid to its cathode electrode supplied to the control grid of thyratron 16 by a direct connection, to the control grid of the thyratron 22 through a delay line 34, and to the control grid of the thyratron 24 through both the delay line 34 and an additional delay line 36.
  • These delay lines may be any one or the many such delay lines well known in the art. They may,
  • the Oft biasing potential source 30 renders each of the thyratrons 16, 22, and 24 in .a non-conducting, deionized state,
  • the circuit stands in a quiescent state, and no signal appears across the load impedance 20; accordingly, as indicated in FIG. 3, the output signal voltage E is zero.
  • a positive pulsesignal of suitable amplitude is generated by the timing pulse source 32 Hit a time designated t
  • This positive pulse drives the control grid electrode of the isolating thyratron 16 to ionize the gas particles within that discharge device.
  • an electrical circuit is completed through the electron tube 18, which acts to bypass the loadim-pedance, the capacitor 12, the
  • the inductor voltage E meanwhile decays sinusoidally to a negative value at the instant t
  • the capacitor potential E correspondingly increases sinusoidally to a value substantially above the energy source potential at this same instant 1 Indeed, by well-known circuit analysis it may be shown that if the charging path, including the electron tube 18, the capacitor 12, the thyratron 16 and the inductor 14 are all of zero resistance, the capacitor voltage E rises to a value just twice the potential of the energy source 11. At this instant the thyratron 16 is deionized by the current through it reducing to zero, and the energy source 11 is thus isolated from the capacitor and its associated elements.
  • the time interval required for the capacitor 12 to rise to this maximum potential that is, the interval t t is given by half the period of the natural resonant one of these three tubes at a different time, which times are designatedt t and 1 in FIG. 3.
  • the pulses are frequency of the'inductor 14 and the capacitor 12. Denoting the inductance and capacitance values of these two elements as L and C, respectively, it is readily ap parent that in this preferred illustrative embodiment of the invention the time t .t is given by the expression Accordingly, delay line 34 is constructed to delay pulse signals applied thereto from the pulse source 32 by just this interval -4 as given above.
  • a pulse signal delayed by delay line 34 is applied to the Off-biasing control electrode of the thyratron 22 at this advantageous instant t the pulse may, however, be app-lied at any reasonable time thereafter as the capacitor tends to maintain its charge.
  • the Off-biasing potential applied to this latter thyratron 22 by the biasing source 30 is thus overcome and the thyratron is enabled as an ionized current conducting condition is established. Ion supported discharge current now flows from the storage capacitor 12 through the low impedance path presented by this thyratron 22.
  • the thyratron 16 is deionized and disabled by the equality of the capacitor potential E with the sum of the inductor potential E and the energy source potential E
  • the biasing potential source 30, acting through the resistor 26, re-establishes its Oil-biasing control of the isolating thyratron 16.
  • the now isolated capacitor begins discharging through the thyratron 22, its potential drops and current tends to flow through the load resistor 20 to support the discharge in the thyratron 22.
  • This discharge current in the load impedance 20 appears as a sharp negative-going pulse indicated by the heavy curve designated B in FIG. 3.
  • the output signal appearing across the load impedance 20 tends to have a substantial value for an indefinite period. This follows from the fact that the discharge thyratron tends to remain ionized as long as the capacitor is capable of supplying substantial current thereto.
  • the third thyratron 24 provides for the termination of the output signal.
  • This third thyratron tube 24 is connected in serial relation with the discharge thyratron 22 and the storage capacitor 12 to provide a complete series path for the flow of the capacitor discharge current.
  • This third thyratron is also, as shown, connected in parallel with the load impedance 20.
  • the pulse from the timing source 3-2 is applied through the delay lines 34 and 36 to overcome the Cit-biasing potential supplied by the source 30 through the resistor 28.
  • the third thyratron 24 is enabled and discharge current for the capacitor flows through the very low impedance path provided by the two ionized thyratrons 22 and 24.
  • the load impedance 20 is efiectively shont-oircuited to terminate the output pulse and the capacitor is rapidly discharged through a near zero impedance path provided by the two ionized thyratrons 22 and 24.
  • the capacitor being discharged rapidly, the ionizing potential for these thyratrons is rapidly removed and they both are returned to a nonconducting condition in expeditious fashion to await a repetition of the above described operation to generate a new high current pulse in the load impedance 20.
  • FIG. 2 there is seen another illustrative embodiment of the principles of the invention.
  • elements corresponding to those of FIG. 1 are correspondingly numbered.
  • a first gaseous electron discharge device 46 which may advantageously be a thyratron, is serially connected with the storage capacitor 12 and a load impedance 20*.
  • a second gaseous electron discharge device 54 again advantageously a thyratron, is connected in serial arrangement with the first discharge device 46 and the capacitor 12.
  • This capacitor is of a 'value to have, in conjunction with the load impedance 20, a charging time constant which is large compared with the desired pulse signal duration.
  • a third gaseous discharge device, thyratron 52 is connected in parallel with the storage capacitor and in serial relation with the first and second discharge devices 46 and 54.
  • a control grid electrode of each of these three thyratrons '46, 52, and 54 is connected through resistors 26, 27, and 28, respectively, to a source of Off-biasing potential 30.
  • Energy source 41 is connected as shown with a polarity to supply energy to the capacitor 12 in a direction consistent with a high conductance condition of the serially connected discharge devices 46, 52, and 54.
  • a timing pulse source 32 supplies intermittent positive enabling pulses to the control electrodes of the thyratrons 46, '52, and 54 at successive instants of time t t and t;, by virtue of the operation of delay lines 34 and 36 as shown.
  • this embodiment of the invention can readily be understood with reference to the wave forms of FIG. 4.
  • the Off-biasing potential applied to the thyratron 46 is overcome. Accordingly, this thyratron is conditioned for heavy discharge conduction and the capacitor 12 is charged by the energy source 41 through the load impedance 20 connected between a pair of output terminals 17 and 19. Accordingly, an output pulse signal B immediately appears across this load impedance.
  • This output signal as indicated in FIG. 4. has a value substantially corresponding to the potential E in view of the large capacitance of the capacitor 12 and the virtually zero impedance of the conducting thyratron 46.
  • the second of the serially connected discharge devices the thyratron 54
  • the thyratron 54 is driven into an ionized discharge condition by the arrival of the positive pulse from the source 32.
  • This thyratron by virtue of its parallel connection with the load impedance 20, acts to bypass the load impedance and to terminate the output pulse E
  • the capacitor 12 now is almost immediately charged to the full potential of the energy source 41 and the two discharge devices 46 and 54 are mutually driven by the heavy conduction of the second discharge device to a deionized condition.
  • the pulse from the source 32 arrives at the control grid of the third thyratron 52 to condition this thyratron for discharge conduction.
  • the energy stored in the capacitor 12 is dissipated rapidly and the pulse generator is restored to a quiescent condition awaiting the generation of a new enabling pulse from the source 32.
  • Pulse generating apparatus comprising a storage capacitor, electrical energy source means for charging said capacitor, a pair of terminals for connection of a load impedance, said capacitor, said source means, and said load impedance terminals being connected in serial arrangement, first and second gaseous discharge devices connected in serial arrangement for current conduction in a like circuit direction, said first discharge device being connected to one side of said capacitor and being pole-d for current conduction in a direction consistent with the polarity of said source, said second discharge device being connected to the other side of said capacitor and across said terminal pair, means for normally biasing said first and second discharge devices in a non-conducting condition, means for applying an enabling trigger signal to said first discharge device to establish a current conduction condition therein to alter the charge state of said capacitor through said load impedance, and means for thereafter applying said trigger signal to said second device for establishing a conduction condition therein for bypassing said load impedance terminals and for accelerating the re-establishment of a non-conducting condition in said first device.
  • a pulse generator which comprises an electrical energy storage element, first and second gaseous electron discharge devices, a distinct series circuit comprising said storage element and said first and second discharge devices being mutually poled for current conduction in a like circuit direction through said storage element, a load impedance, an energy source connected for charging said storage element with a polarity to drive current through at least one of said discharge devices, biasing means for maintaining said discharge devices in a normally nonconducting condition, means for applying a trigger pulse signal to said first device forestablishing'a discharge condition therein for altering a current flow condition in said load impedance, and means for thereafter applying said trigger pulse signal to said second device to-establish a discharge condition therein for accelerating the dis establishment of the discharge condition in said first device.
  • said first and second discharge devices are connected in parallel with said load impedance.
  • Apparatus for applying electrical energy from a source as an energy pulse to a load comprising a storagetcapacitor having one terminal connected to a first gaseous electron discharge device and the other terminal connected to a second gaseous electron discharge device, said first and second discharge devices being connected in shunt with the load, a distinct series circuit including said storage element and said first and second discharge devices mutually poled in a like direction, biasing means for maintaining said discharge devices in a normally deionized or nonconducting condition, means for applying an ionizing trigger signal to said first de-- vice for establishing a discharge condition therein to initiate a current pulse in the load, and means for thereafter applying said ionizing trigger signal to said second device for establishinga discharge condition therein to terminate the pulse in said load and to accelerate the disestablishment of the discharge conditionsin said first and second devices.
  • a pulse generator which comprises an electrical energy storage element, a load impedance, means including an energy source for charging said storage element, a firs-t gaseous discharge device series connected between said charging means and said storage element, means for triggering said first gaseous discharge device to inio tiate said charging of said storage element, a second gaseous discharge device connected to said storage ele: ment so as to define a series fpath therewith and with said load impedance, and means for triggering said second References Cited in the file of this patent V UNITED STATES PATENTS 2,470,895 Marlowe May 24, 1949 2,596,142 GerWin May 13, 1952 2,677,053 Nirns Apr.

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wuosQm Sept. 24, 1963 F. B. ANDERSON ETAL PULSE GENERATOR Filed Jan. 27, 1959 MUQSOW suw/ QSSR B. ANDERSON WVENTORSs H PEARSALL, JR.
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ATTORNEY United States Patent 3,105,169 PULSE GENERATGR Frithiof B. Anderson, Winston-Salem, N.C., and Samuel H. Pearsall, In, Donelson, Tenm, assignors to Bell Telephone Laboratories, Incorporated, New York,
N.Y., a corporation of New York Filed Jan. 27, 1959, Ser. No. 789,445 5 (Ilaims. (Cl. 315-166) This invention relates to pulse circuits and, more particularly, to pulse circuits employing gaseous electron discharge devices.
In a wide variety of electronic equipments, for both operating and testing purposes, there is a need for accurately timed pulse signals of precise duration and of substantial magnitude. This widespread need has given rise to a large number of difierent generators for such pulse signals. In a broad group of these generators, energy has been passed through one path for storage at a high level in a suitable reservoir. Thereafter, at a desired instant this stored energy is released through a different path. conventionally, one of these paths includes a utilization apparatus, and the shift between storage and release circuit states marks the beginning and ending, though not necessarily in that order, of a desired pulse signal.
Advantageously in this type of apparatus, electron tubes have been employed as accurately timed switching devices tor shitting storage energy between a charging path and a discharge path. Commonly, vacuum tubes may be so employed but with the limitation that, as the amplitude of the required pulse signal current rises, both the size and heating power requirements of the necessary vacuum tubes may go beyond that which is feasible for a particular application.
In such circumstances advantageous resort may be made to gaseous electron discharge devices which are exemplified by the well-known thyratron tube. In these discharge devices'ionized gas within an envelope serves as a current carrier between cathode and anode electrodes. As is well known in the art, the initiation of such a current conducting ionized condition may be controlled by an auxiliary grid electrode. Thereafter, heavy current may be conducted by the ionized gas particles Within the envelope without necessitating heavy thermionic electron emission by a cathode.
Utilization of such gaseous electron discharge devices in the past, however, has been limited to pulse signal generators in which the timing of one portion of the pulse signal, for example, the terminating portion, is of relative unimportance. This limitation has resulted from the fact that, once an appropriate conduction condition has been established within these gaseous devices, the electrostatic effect of auxiliary grids becames insignificant compared to that of the current conducting ionized particles. Hence, termination of a current conducting electron discharge through such ionized devices becomes de pendent upon external circuit phenomena almost entirely, and the discharge conduction current 'alone has, to a great extent, governed its own termination.
Accordingly, pulse generators of the prior art, on the one hand, have required overlarge vacuum tubes and associated power supplies or, on the other hand, have been objectionably inaccurate in either the beginning or the terminating portion of generated pulse wave signals. This latter inaccuracy has often led to a further objectionable delay in the generation of succeeding pulse signals.
It is a principal object of the present invention to generate accurately timed pulse signals of well-defined wave form, of substantial amplitude, and of rapid recurrence rate.
hid-5J5? Patented Sept. 24, 1963 It is a further object of the present invention to simplify and to reduce the cost of pulse generating structures.
In accordance with the present invention these and other objects are achieved with a structure in which two gas-filled electron discharge devices are arranged in serial connection with each other and with an energy storing reservoir. A control signal applied to one of these devices establishes heavy current conducting discharge conditions therein to initiate an abrupt change of substantial magnitude in an output signal. This control signal, applied at a later time, establishes a like discharge condition within the other device to accelerate the termination of the conducting discharge in both devices by their deionization and to terminate an output pulse signal by bypassing the parallel connected load circuit in Which the output signal appears.
The control discharge devices are advantageously gaseous discharge devices having a control or starter electrode or grid to which the control signal is applied; a thyratron is an example of this type of device. Such devices enable the circuit to provide a large output signal. Circuits in accordance with our invention are so arranged that conduction in the control gaseous discharge devices is terminated by the breakdown of the last of the control devices, conduction in this last device automatically extinguishing the conduction in itself and in any other such devices in the circuit in a high conduction state at that time.
In one specific illustrative embodiment wherein the storage capacitor is priorly changed, as through a gaseous discharge device of the thyratron type, the circuit is arranged so that the first control device establishes a series circuit including itself, the storage capacitor, and the load to initiate the output pulse through the load. A second control device, upon conduction, bypasses the load and establishes a series path including itself, the storage capacitor, and the first device, to discharge the capacitor and in so doing to extinguish conduction both in itself and in the first device. Accordingly, the first and second control gaseous discharge devices are mutually poled for the flow of current in one direction through the series path including the intermediately connected storage condenser.
In a second illustrative embodiment the first device controls the charging of the storage capacitor and also determines the initiation of the output pulse. The second control gaseous discharge device terminates the output pulse by bypassing the output circuit, and a third gaseous discharge device connected in parallel with the storage condenser upon breakdown discharges the storage condenser and thereby automatically extinguishes the discharge in itself and in both the other control devices.
It is a feature of this invention that a pulse generator circuit for producing accurately timed large amplitude output pulses includes a pair of control discharge devices series connected with a storage capacitor for passage of current through this series path in a single direction. More specifically in accordance with our invention, the control discharge devices are gaseous discharge devices as of the thyratron type having a control or starter electrode.
It is another feature of our invention that the breakdown of one such control discharge device both discharges the storage capacitor and in so doing extinguishes or disables both itself and any other conducting control discharge device.
It is a further feature of one specific illustrative embodiment of our invention that the storage capacitor be charged independently of the two control gaseous discharge devices set forth above, the two devices being connected so that uponconduction of the second to terminate the output pulse, both devices are initiallycod ducting providing low impedance connections to ground in a series circuit from both plates of the storage capacitor and thereby providing both automatic discharge of the capacitor and extinction of the discharge in both control devices. Further in accordance with our invention,'in this specific embodiment thereof the charging of the storage condenser may be controlled through another gaseous discharge device having an inductance connected in'series therewith, conduction in this device being selfextinguishing on the charging of the storage condenser.
A complete understanding of this'invention and of these and other features thereof may be gained from con. sideration of the following detailed description together with the accompanying drawing, in which:
FIG. 1 is a schematic diagramof an illustrative high power pulse generating system in accordance with one embodiment of the invention;
FIG. 2 is a schematic diagram of another illustrative high power pulse, generating system in accordance-with ing the operations of the embodiments of the invention as shown in FIGS. 1 and 2, respectively.
7 Referring now more particularly to the drawing, in FIG. 1 there is shown a resonantly charged pulse generating circuit to which energy is supplied from a direct energy source 11 which may conveniently be any one of the many direct current power supplies known in the electronic art. Energy from this source serves to charge a storage element, the capacitor 12, through a serially connected charging inductor 14 and a variable impedance isolating element 16 which adv-antageouslymay be a high conductance electron discharge device such as a thyratron electron tube. Completing a serial circuit including the capacitor 12 and the energy source 11 is a rectifying device comprising a diode-connected triode electron tube 18, which is connected across a pair of output terminals 17 and 19 and is poled ior conducting current in a low resistance direction consistent with the polarity of the sourcell.
A load impedance 20 is connected in parallel with electron tube 18. This load impedance 20 is shown for convenience of illustration as a resistor. It may as well be any pulse utilization circuit as, for example, a radar magnetron pulsing circuit. I
Two circuit controlling electron discharge devices 22 and 24 are connected in serial relation with the storage capacitor 12, each for conducting current flowing through that capacitor in a like direction. These discharge devices may advantageously also be thyratron'tubes. In accordance with the above-noted serial connection these thyratron, tubes are connected anode to cathode.
to promote heavy current conduction. Thyratron 22 is further connected, as shown, in serial relation with the energy source 11, the inductor 14, and the isolating thyratron 16. The other circuit controlling discharge device,
thyratron 24, is further connected in parallel with the load impedance 20.
As shown, the control grids of the three thyratrons 16, 22, and 24 are respectively connected through resistors 26, 27, and 28 to a source of Off-biasing potential 30.
Each has a 7 direct connection of its shield grid to its cathode electrode supplied to the control grid of thyratron 16 by a direct connection, to the control grid of the thyratron 22 through a delay line 34, and to the control grid of the thyratron 24 through both the delay line 34 and an additional delay line 36. These delay lines may be any one or the many such delay lines well known in the art. They may,
for example, be serially connected 1r sections of inductors and capacitors having values chosen to yield delay times corresponding to the intervals t -t and t t The magnitude of these intervals can best be considered together with a discussion of the operation of the pulse generator of FIG. 1 which may be understood more clearly Iby a consideration of the wave forms shown in FIG. 3.
Assuming the capacitor 12 to be initially discharged, the Oft biasing potential source 30 renders each of the thyratrons 16, 22, and 24 in .a non-conducting, deionized state, The circuit stands in a quiescent state, and no signal appears across the load impedance 20; accordingly, as indicated in FIG. 3, the output signal voltage E is zero.
A positive pulsesignal of suitable amplitude is generated by the timing pulse source 32 Hit a time designated t This positive pulse drives the control grid electrode of the isolating thyratron 16 to ionize the gas particles within that discharge device. Thus, an electrical circuit is completed through the electron tube 18, which acts to bypass the loadim-pedance, the capacitor 12, the
thyratron 16, and the inductor 14 to the energy source 11. At this instant 1 a voltage E appears across the inductor with a polarity as indicated by the arrow and I in magnitude almost equal to and opposing the energy source potential E This situation is shown in FIG. 3 at time t by referring to the curve designated in this figure as E a r l 7 Immediately afiter the instant t the storage capacitor 12 potential E rises as the capacitor is charged through the electron tube 18. 'The inductor voltage E meanwhile decays sinusoidally to a negative value at the instant t The capacitor potential E correspondingly increases sinusoidally to a value substantially above the energy source potential at this same instant 1 Indeed, by well-known circuit analysis it may be shown that if the charging path, including the electron tube 18, the capacitor 12, the thyratron 16 and the inductor 14 are all of zero resistance, the capacitor voltage E rises to a value just twice the potential of the energy source 11. At this instant the thyratron 16 is deionized by the current through it reducing to zero, and the energy source 11 is thus isolated from the capacitor and its associated elements.
The time interval required for the capacitor 12 to rise to this maximum potential, that is, the interval t t is given by half the period of the natural resonant one of these three tubes at a different time, which times are designatedt t and 1 in FIG. 3. The pulses are frequency of the'inductor 14 and the capacitor 12. Denoting the inductance and capacitance values of these two elements as L and C, respectively, it is readily ap parent that in this preferred illustrative embodiment of the invention the time t .t is given by the expression Accordingly, delay line 34 is constructed to delay pulse signals applied thereto from the pulse source 32 by just this interval -4 as given above.
As shown in FIG. 1, a pulse signal delayed by delay line 34 is applied to the Off-biasing control electrode of the thyratron 22 at this advantageous instant t the pulse may, however, be app-lied at any reasonable time thereafter as the capacitor tends to maintain its charge. The Off-biasing potential applied to this latter thyratron 22 by the biasing source 30 is thus overcome and the thyratron is enabled as an ionized current conducting condition is established. Ion supported discharge current now flows from the storage capacitor 12 through the low impedance path presented by this thyratron 22. Meanwhile the thyratron 16 is deionized and disabled by the equality of the capacitor potential E with the sum of the inductor potential E and the energy source potential E Thus, the biasing potential source 30, acting through the resistor 26, re-establishes its Oil-biasing control of the isolating thyratron 16. As the now isolated capacitor begins discharging through the thyratron 22, its potential drops and current tends to flow through the load resistor 20 to support the discharge in the thyratron 22. This discharge current in the load impedance 20 appears as a sharp negative-going pulse indicated by the heavy curve designated B in FIG. 3.
As the energy stored in the capacitor 12 decays at an exponentially decreasing rate, the output signal appearing across the load impedance 20 tends to have a substantial value for an indefinite period. This follows from the fact that the discharge thyratron tends to remain ionized as long as the capacitor is capable of supplying substantial current thereto.
In accordance with an aspect of our invention, the third thyratron 24 provides for the termination of the output signal. This third thyratron tube 24 is connected in serial relation with the discharge thyratron 22 and the storage capacitor 12 to provide a complete series path for the flow of the capacitor discharge current. This third thyratron is also, as shown, connected in parallel with the load impedance 20. At a desired pulse termination time t the pulse from the timing source 3-2 is applied through the delay lines 34 and 36 to overcome the Cit-biasing potential supplied by the source 30 through the resistor 28. Thus, the third thyratron 24 is enabled and discharge current for the capacitor flows through the very low impedance path provided by the two ionized thyratrons 22 and 24. Immediately the thy ratron 24 is ionized, the load impedance 20 is efiectively shont-oircuited to terminate the output pulse and the capacitor is rapidly discharged through a near zero impedance path provided by the two ionized thyratrons 22 and 24. The capacitor being discharged rapidly, the ionizing potential for these thyratrons is rapidly removed and they both are returned to a nonconducting condition in expeditious fashion to await a repetition of the above described operation to generate a new high current pulse in the load impedance 20.
Turning attention now to the pulse generator delineated in FIG. 2, there is seen another illustrative embodiment of the principles of the invention. In this embodiment, shown in FIG. 2, elements corresponding to those of FIG. 1 are correspondingly numbered.
In this generator a first gaseous electron discharge device 46, which may advantageously be a thyratron, is serially connected with the storage capacitor 12 and a load impedance 20*. A second gaseous electron discharge device 54, again advantageously a thyratron, is connected in serial arrangement with the first discharge device 46 and the capacitor 12. This capacitor is of a 'value to have, in conjunction with the load impedance 20, a charging time constant which is large compared with the desired pulse signal duration. Still a third gaseous discharge device, thyratron 52, is connected in parallel with the storage capacitor and in serial relation with the first and second discharge devices 46 and 54.
A control grid electrode of each of these three thyratrons '46, 52, and 54 is connected through resistors 26, 27, and 28, respectively, to a source of Off-biasing potential 30. Energy source 41 is connected as shown with a polarity to supply energy to the capacitor 12 in a direction consistent with a high conductance condition of the serially connected discharge devices 46, 52, and 54. A timing pulse source 32 supplies intermittent positive enabling pulses to the control electrodes of the thyratrons 46, '52, and 54 at successive instants of time t t and t;, by virtue of the operation of delay lines 34 and 36 as shown.
The operation of this embodiment of the invention can readily be understood with reference to the wave forms of FIG. 4. Upon generation of a timing pulse from the source 32 at a time t the Off-biasing potential applied to the thyratron 46 is overcome. Accordingly, this thyratron is conditioned for heavy discharge conduction and the capacitor 12 is charged by the energy source 41 through the load impedance 20 connected between a pair of output terminals 17 and 19. Accordingly, an output pulse signal B immediately appears across this load impedance. This output signal, as indicated in FIG. 4. has a value substantially corresponding to the potential E in view of the large capacitance of the capacitor 12 and the virtually zero impedance of the conducting thyratron 46.
At the instant t later than t by an interval which is governed by the delay line 34, the second of the serially connected discharge devices, the thyratron 54, is driven into an ionized discharge condition by the arrival of the positive pulse from the source 32. This thyratron, by virtue of its parallel connection with the load impedance 20, acts to bypass the load impedance and to terminate the output pulse E The capacitor 12 now is almost immediately charged to the full potential of the energy source 41 and the two discharge devices 46 and 54 are mutually driven by the heavy conduction of the second discharge device to a deionized condition.
At a still later instant t later than t by an interval governed by the delay line 36, the pulse from the source 32 arrives at the control grid of the third thyratron 52 to condition this thyratron for discharge conduction. Hence, the energy stored in the capacitor 12 is dissipated rapidly and the pulse generator is restored to a quiescent condition awaiting the generation of a new enabling pulse from the source 32.
While specific illustrative embodiments of this invention have been described herein, it is, of course, to be understood that the above-described arrangements are merely illustrative of the application of the principles of the invention. Thus, numerous other arrangements may be devised by those skilled in the art without departing from the spirit and scope of the invention.
What is claimed is:
1. Pulse generating apparatus comprising a storage capacitor, electrical energy source means for charging said capacitor, a pair of terminals for connection of a load impedance, said capacitor, said source means, and said load impedance terminals being connected in serial arrangement, first and second gaseous discharge devices connected in serial arrangement for current conduction in a like circuit direction, said first discharge device being connected to one side of said capacitor and being pole-d for current conduction in a direction consistent with the polarity of said source, said second discharge device being connected to the other side of said capacitor and across said terminal pair, means for normally biasing said first and second discharge devices in a non-conducting condition, means for applying an enabling trigger signal to said first discharge device to establish a current conduction condition therein to alter the charge state of said capacitor through said load impedance, and means for thereafter applying said trigger signal to said second device for establishing a conduction condition therein for bypassing said load impedance terminals and for accelerating the re-establishment of a non-conducting condition in said first device.
-2. A pulse generator which comprises an electrical energy storage element, first and second gaseous electron discharge devices, a distinct series circuit comprising said storage element and said first and second discharge devices being mutually poled for current conduction in a like circuit direction through said storage element, a load impedance, an energy source connected for charging said storage element with a polarity to drive current through at least one of said discharge devices, biasing means for maintaining said discharge devices in a normally nonconducting condition, means for applying a trigger pulse signal to said first device forestablishing'a discharge condition therein for altering a current flow condition in said load impedance, and means for thereafter applying said trigger pulse signal to said second device to-establish a discharge condition therein for accelerating the dis establishment of the discharge condition in said first device. 3. Apparatus as set forth in claim 2 wherein said first and second discharge devices are connected in parallel with said load impedance.
4. Apparatus for applying electrical energy from a source as an energy pulse to a load,'said apparatus comprising a storagetcapacitor having one terminal connected to a first gaseous electron discharge device and the other terminal connected to a second gaseous electron discharge device, said first and second discharge devices being connected in shunt with the load, a distinct series circuit including said storage element and said first and second discharge devices mutually poled in a like direction, biasing means for maintaining said discharge devices in a normally deionized or nonconducting condition, means for applying an ionizing trigger signal to said first de-- vice for establishing a discharge condition therein to initiate a current pulse in the load, and means for thereafter applying said ionizing trigger signal to said second device for establishinga discharge condition therein to terminate the pulse in said load and to accelerate the disestablishment of the discharge conditionsin said first and second devices.
'5. In a pulse generator which comprises an electrical energy storage element, a load impedance, means including an energy source for charging said storage element, a firs-t gaseous discharge device series connected between said charging means and said storage element, means for triggering said first gaseous discharge device to inio tiate said charging of said storage element, a second gaseous discharge device connected to said storage ele: ment so as to define a series fpath therewith and with said load impedance, and means for triggering said second References Cited in the file of this patent V UNITED STATES PATENTS 2,470,895 Marlowe May 24, 1949 2,596,142 GerWin May 13, 1952 2,677,053 Nirns Apr. 27, 1954 2,709,746 Page May 31, 1955 2,710,351 Lebacqz June 7, 1955 2,752,500 1 Bruyning June 7, 1956 2,793,290 Wagner May 21, 1957 V FOREIGN PATENTS 454,678 Canada Feb. 15, 1949 OTHER REFERENCES Graydon: The Application of Pulse Forming Networks, Proceeding of the National Electronic Conference, vol. XII, 1956, pp. 1071-1075.

Claims (1)

1. PULSE GENERATING APPARATUS COMPRISING A STORAGE CAPACITOR, ELECTRICAL ENERGY SOURCE MEANS FOR CHARGING SAID CAPACITOR, A PAIR OF TERMINALS FOR CONNECTION OF A LOAD IMPEDANCE, SAID CAPACITOR, SAID SOURCE MEANS, AND SAID LOAD IMPEDANCE TERMINALS BEING CONNECTED IN SERIAL ARRANGEMENT, FIRST AND SECOND GASEOUS DISCHARGE DEVICES CONNECTED IN SERIAL ARRANGEMENT FOR CURRENT CONDUCTION IN A LIKE CIRCUIT DIRECTION, SAID FIRST DISCHARGE DEVICE BEING CONNECTED TO ONE SIDE OF SAID CAPACITOR AND BEING POLED FOR CURRENT CONDUCTION IN A DIRECTION CONSISTENT WITH THE POLARITY OF SAID SOURCE, SAID SECOND DISCHARGE DEVICE BEING CONNECTED TO THE OTHER SIDE OF SAID CAPACITOR AND ACROSS SAID TERMINAL PAIR, MEANS FOR NORMALLY BIASING SAID FIRST AND SECOND DISCHARGE DEVICES IN A NON-CONDUCTING CONDITION, MEANS FOR APPLYING AN ENABLING TRIGGER SIGNAL TO SAID FIRST DISCHARGE DEVICE TO ESTABLISH A CURRENT CONDUCTION CONDITION THEREIN TO ALTER THE CHARGE STATE OF SAID CAPACITOR THROUGH SAID LOAD IMPEDANCE, AND MEANS FOR THEREAFTER APPLYING SAID TRIGGER SIGNAL TO SAID SECOND DEVICE FOR ESTABLISHING A CONDUCTION CONDITION THEREIN FOR BYPASSING SAID LOAD IMPEDANCE TERMINALS AND FOR ACCELERATING THE RE-ESTABLISHMENT OF A NON-CONDUCTING CONDITION IN SAID FIRST DEVICE.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3171030A (en) * 1961-03-06 1965-02-23 Zenith Radio Corp System for producing short pulses of x-ray energy
US3673504A (en) * 1967-11-28 1972-06-27 Trw Inc Laser with combined q-switch and synchronized cavity dump circuit
US5563457A (en) * 1993-08-27 1996-10-08 The Regents Of The University Of California Charge line quad pulser

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA454678A (en) * 1949-02-15 Shockley William Pulse generator
US2470895A (en) * 1945-12-13 1949-05-24 Elbert W Marlowe Impulse type power supply
US2596142A (en) * 1946-02-21 1952-05-13 Harry L Gerwin Signal generator
US2677053A (en) * 1949-06-29 1954-04-27 Westinghouse Electric Corp Pulse generator
US2709746A (en) * 1948-11-02 1955-05-31 Westinghouse Electric Corp Pulse generator
US2710351A (en) * 1946-04-16 1955-06-07 Jean V Lebacqz Pulse generator
US2752500A (en) * 1952-12-24 1956-06-26 Hartford Nat Bank & Trust Co Pulse generator
US2793290A (en) * 1953-05-04 1957-05-21 Herbert M Wagner Rectangular pulse generator

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA454678A (en) * 1949-02-15 Shockley William Pulse generator
US2470895A (en) * 1945-12-13 1949-05-24 Elbert W Marlowe Impulse type power supply
US2596142A (en) * 1946-02-21 1952-05-13 Harry L Gerwin Signal generator
US2710351A (en) * 1946-04-16 1955-06-07 Jean V Lebacqz Pulse generator
US2709746A (en) * 1948-11-02 1955-05-31 Westinghouse Electric Corp Pulse generator
US2677053A (en) * 1949-06-29 1954-04-27 Westinghouse Electric Corp Pulse generator
US2752500A (en) * 1952-12-24 1956-06-26 Hartford Nat Bank & Trust Co Pulse generator
US2793290A (en) * 1953-05-04 1957-05-21 Herbert M Wagner Rectangular pulse generator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3171030A (en) * 1961-03-06 1965-02-23 Zenith Radio Corp System for producing short pulses of x-ray energy
US3673504A (en) * 1967-11-28 1972-06-27 Trw Inc Laser with combined q-switch and synchronized cavity dump circuit
US5563457A (en) * 1993-08-27 1996-10-08 The Regents Of The University Of California Charge line quad pulser

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