US3051865A - Pulsed beam tube - Google Patents

Pulsed beam tube Download PDF

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US3051865A
US3051865A US765456A US76545658A US3051865A US 3051865 A US3051865 A US 3051865A US 765456 A US765456 A US 765456A US 76545658 A US76545658 A US 76545658A US 3051865 A US3051865 A US 3051865A
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electron
interaction
noise
tube
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Theodore J Marchese
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TDK Micronas GmbH
International Telephone and Telegraph Corp
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Deutsche ITT Industries GmbH
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons
    • H01J25/02Tubes with electron stream modulated in velocity or density in a modulator zone and thereafter giving up energy in an inducing zone, the zones being associated with one or more resonators
    • H01J25/10Klystrons, i.e. tubes having two or more resonators, without reflection of the electron stream, and in which the stream is modulated mainly by velocity in the zone of the input resonator
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/02Electrodes; Magnetic control means; Screens
    • H01J23/11Means for reducing noise

Definitions

  • This invention relates to pulsed lbeam tubes and more particularly to those which are adapted to reduce the noise level during interpulse intervals, including traveling wave and lclystron tube types.
  • Present day radar systems of the pulse type may incorporate either a traveling wave tube or a klystron as the output stage of the transmitter.
  • These electron discharge devices are generally of extremely high power for long range applications. Their range, however, is often limited by the fact that received signals are submerged in noise from various sources.
  • One source of noise is due 'to the environment in which the radiating antenna is placed. This noise may be termed thermal or ambient noise and it exists because all objects in the ordinary environments radiate energy due to their molecular activity, Very little can be done to eliminate this type of noise.
  • Another source of noise exists, however, which contributes greatly to the overall noise being presented to the receiver.
  • This noise which is also thermal in nature, exists in the output tube of the transmitter and is due to three conditions in the region of the electron gun of the output tube.
  • a convenient way to apply pulse modulation to a radio frequency wave is to utilize a modulation anode or grid to turn on and cut-oit the tube electron beam.
  • modulation anodes or grids due to geometrical imperfections are not 100% effective in cutting off the beam during the transmitter oiftime and a small portion of the beam leaks through to enter the interaction region of the electron discharge device where it is amplified and This is one source of noise.
  • the second source of noise in the output tube is the modulating anode or grid.
  • the electron beam in passing through this element heats it up and primary emission due to the heating takes place and continues during the transmitter off-time.
  • a third source of noise, which provides a second order effect is due to secondary emission from the grid.
  • the noise due to incomplete beam cut-off and to primary and secondary emission may be termed l residual noise to distinguish it from. the ambient noise. Since the ambient noise is relatively uncontrollable, one
  • It is another .object of this invention to provide a pulsed electron discharge device system which has an improved signal-to-noise ratio as compared with prior art systems.
  • a feature of this invention is the utilization of an electron discharge device having means for projecting an electron beam along a given path and interaction means for deriving energy from the beam disposed along the electron beam path.
  • the electron discharge device incorporates vdeflection means to deflect the electron beam from the given path when it is desired to preclude interaction with the aforesaid interaction means.
  • Another feature is the utilization of deflection means disposed intermediate the beam generation means and the interaction means, either internally or externally of the vacuum envelope to preclude interaction of the electron beam with the interaction means when desired.
  • a further feature is the utilization of either a split first anode or a split focusing electrode ⁇ coupled to a voltage source to deflect the residual electron beam to preclude interaction of the beam with the interaction means.
  • a still further feature ⁇ of this invention is the utilization of skirt portions on the first anode to collect the deflected residual beam current.
  • FIG. l is a schematic representation of an electron discharge device of the traveling wave tube type which operates in accordance with the principles of this invention',
  • FIG. 2 is a schematic representation of a traveling ywave tube having externally disposed magnetic residual beam deflecting means
  • FIG. 3 is a schematic representation of a traveling wave tube having externally disposed electrostatic residual beam deflecting means
  • FIG. 4 is a schematic representation of a klystron tube which opeates in accordance with the principles of this invention
  • FIG. 5 is a schematic representation of a klystron tube having externally disposed magnetic beam deflection means
  • FIG. 6 is a schematic representation of a klystron tube having externally disposed electrostatic beam deflection means
  • FIG. 7 is a partial longitudinal cross-sectional view of a preferred embodiment which operates in accordance with the principles of this invention and;
  • FIG. 8 is a partial longitudinal cross-sectional view of an alternative preferred embodiment of this invention.
  • Electron discharge device 1 includes means 2 for projecting an electron beam along a given path.
  • Interaction means 3 in the form of a helical slow wave structure 4 is disposed along the given path and supports a radio frequency electromagnetic wave which derives energy from the electron beam through the agency of said interaction means 3.
  • Defiection means 5 which may be either electrostatic or electromagnetic is shown disposed either internally or externally of vacuum envelope 6 adjacent beam projecting means 2 to deflect the electron beam from the given path to preclude interaction of the electron beam with the interaction means 3 during a given interval.
  • deliection means 5 consists of two electrodes 7, 8 suitable for applying a difference of potential thereto.
  • electrodes 7, 8 are disposed internally of vacuum envelope 6 and between beam projection means 2 and interaction means 3.
  • Vacuum envelope 6 may be of metal, glass or ceramic.
  • Terminals 9, 10 which penetrate vacuum envelope 6 are used to apply a difference of potential from voltage source 11 to defiect the residual beam during a given interval.
  • the beam projection means 2 includes a cathode 12, a grid 13 and a first anode 14 which cooperatively act to project an electron beam along a given path to collector 15.
  • a pulsed source of voltage 16 coupled to grid 13 applies pulses of the proper polarity to turn on and cut off the beam current so that a radio frequency wave introduced on input terminal 17 of interaction means 3 may be pulse modulated and delivered to output terminal 18 as an amplified pulsed radio frequency wave.
  • deflection means 5 consists of an electromagnetic deflection coil 19 which acts to deflect the residual electron beam from the given path.
  • Coil 19 is disposed between electron projecting means 2 and interaction means 3 and a difference of potential from voltage source 11 is applied to coil 19 across terminals 20, 21.
  • FIG. 3 shows an electron discharge device 1 which is similar in every way to the device of FIG. 1 with the exception that defiection means 5 is disposed externally of vacuum envelope 6. Further, Vacuum envelope 6, for this type of defiection should be glass or ceramic and not metal. A metal envelope, in this application, would shield the beam from the action of the electric field.
  • the electron discharge device 1 includes means 2 for projecting an electron beam along a given path.
  • Interaction means 3 in the form of a plurality of resonant radio frequency cavities 22 are disposed along the given path and are adapted to support a radio frequency electromagnetic wave which derives energy from the electron beam through the agency of resonant cavities 22.
  • Deection means 5 in FIGS. 4, 5, 6 as in FIGS. 1, 2, 3 may be either electrostatic or electromagnetic and may be disposed either internally or externally of Vacuum envelope 6 adjacent beam projection means 2 to deect the electron beam from the given path to preclude interaction of the electron beam with interaction means 3.
  • FIG. 4 is similar in every way to the device of FIG. 1 with the exceptions that the interaction means 3 in FIG. 4 consists of resonant cavities 22 as opposed to a helical slow wave structure 4 in FIG. 3. Input and output terminals 17, 18 in FIG. 4 couple to coupling loops disposed within the cavities 22.
  • FIG. 5 as far as the type of deflection means 5 used, is similar in every way to the embodiment of FIG. 2, and
  • FIG. 6 employs the same type of deflection as shown in connection with the embodiment of FIG. 3.
  • the vacuum envelope should be limited to either glass or ceramic material, so that the beam will not be shielded as it would be if a metallic envelope were used.
  • FIGS. 1 through 6 The operations of the embodiments of FIGS. 1 through 6 are alike; the only ⁇ differences being the type of deflection means used and the position of the deection means 5 with respect to vacuum envelope 6.
  • the grids or modulating anodes 13 of electron discharge devices are energized from a pulse source 16 which is coupled to grids 13.
  • the potential on grids 13 is pulsed from some negative voltage with respect to the cathode which substantially cuts off the beam current to a value which permits the electrons to enter the tube interaction region where the beam interacts with the radio frequency energy present in the interaction means 3.
  • FIGS. 1 to 3 operate in a manner Well known in the traveling wave tube art and FIGS.
  • radio frequency energy is then passed to the output 18 as an amplified pulse of radio frequency energy.
  • the beam is cut-off and no further action is intended in the interaction means 3 until the start of the next pulse.
  • grid 13 does not provide complete cut-off of the electron beam and due to the fact that primary emission due to heating of grid 13 and some secondary emission exists, a residual beam is present during the interpulse interval which can be amplified in the interaction means 3, if it is allowed to enter interaction means 3.
  • a potential difference applied from voltage source 11 to defiection means S of the various embodiments precludes the above-described action from taking place.
  • a potential from voltage source 11 is applied, at the end of the pulse from pulsed source 16, to deflection means 5 to ydeect the residual beam away from interaction means 3 and onto first anode 14.
  • a trigger pulse from pulse source 16r over lead 11' may be used to indicate the instant at which pulse source 16 is de-energized and the instant at which voltage source 11 should be energized.
  • the action of electrostatic and electromagnetic fields on electrons is well known to lchose skilled in the electron ballistic art and occurs in each of the above embodiments in this known manner.
  • the magnitude of the defiecting potential is relatively small because the density of the residual beam is small.
  • the residual beam for the same reason, may be collected on the first anode 14 or the vacuum envelope walls with the generation of only a ⁇ small amount of heat.
  • the potential from voltage source 11 is removed from defection means 5 at the beginning of the next pulse from pulsed source 16. In this manner, therefore, the residual beam is precluded from entering the interaction means and the noise due to the amplification in the interaction means 3 is substantially eliminated.
  • FIG. 7 there is shown therein a preferred embodiment which operates in accordance with the principles of this invention. Since the novelty of [this invention resides principally in the region of the elec- 'tron gun, only the electron gun and the deiiection structure are shown. The portions of the traveling wave tube or klystron not shown can be of a design well knovm to those skilled in the art.
  • Electron ygun 23 consists of a cathode 24 for projecting an electron beam along a given path; a heater 25 for energizing cathode 24, a grid 26 disposed adjacent cathode to apply pulse modulation from pulsed source 16 to the electron beam; a focusing electrode 27 toI focus the electron beam to a given cross- -sectional area, and a first anode 28 to accelerate the electron beam toward interaction structure shown generally at 29.
  • Interaction structure 29 may be any slow wave structure used in conventional traveling wave tubes or may be a series of cavities such as used in conventional klystrons.
  • focusing electrode 27 has at least two portions 30, 31 separated one from the other by a narrow gap 32 and oppositely disposed to act as d'eilection electrodes during the interpulse interval.
  • the narrow gap 32 has no eiect whatsoever on the operation of electrode 27 when it is functioning as a yfocusing electrode during pulsed operation provided the gap 32 is kept quite narrow.
  • FIG. 8 is an alternative to the embodiment of FIG. 7.
  • the focusing electr-ode 27 is no longer split, but appears as a conventional focusing electrode.
  • Like elements in FIG. 8 are numbered the same ias in FIG. 7.
  • each of the portions 33, 34 ' has exten- :sions or skirts 35, 36 which extend in the direction of the electron beam flow to act as collectors for the residual beam current which is deflected by the first anode.
  • the skirts 35, 36 could be used in the embodiment of FIG. 7 in the same manner. Since a potential is to be applied to at least one of the two portions 33, 34 of anode 28, one of the portions or both may be insulated from the tube shell by a semi-circular insulator 37 disposed between anode 2S and tube shell 38. In this manner, the Ideilecting voltage is prevented from shorting to ground.
  • the deflection voltage is applied to anode 28 by means of terminal 39 and lead 40 which is passed through the vacuum envelope by a conventional vacuum seal.
  • the embodiment of FIG. 8, like the embodiment of FIG. 7, may be used with both traveling wave tubes and with Iklystrons.
  • An electron discharge ⁇ device system comprising an electron discharge device, means to project discrete electron beam segments along a given path, said electron beam segments having undesired electrons therebetween, interaction means for deriving energy from said beam segments disposed .along said given path, electron deiiection means kdisposed adjacent sai-d beam segment projecting means to deflect said undesired electro-ns from 6 said path, and means coupled to said electron deliection means to energize sai-d electron detiection means during the interval between each of said beam segments to prelclude interaction of said undesired electrons with said interaction means.
  • An electron discharge device system comprising an electron discharge device, means to project discrete electron beam segments along Ia given path, said electron beam segments having undesired electrons therebetween, interaction means 'for deriving energy from said seg'- ments disposed along said given path, electron deection means disposed adjacent said beam segment projecting means to detlect said undesired electrons from said path, means coupled to said electron deiiection means to energize said electron deflection means during the interval between each of said beam segments to preclude interaction of said undesired electrons with said interaction means, ⁇ and an electron absorption electrode mounted be tween said interaction means and said electron deection means for ⁇ absorbing said undesired electrons during the intervals between each of said beam segments.
  • An electron discharge device system comprising :an electron discharge device, a source of pulses, means responsive to said pulses for projecting a plurality of discrete beam segments Ialong a given path, said electron beam segments having undesired electrons therebetween, interaction means for deriving energy from said beam segments disposed along said given path, electron deflection means disposed adjacent said beam segment projecting means to deflect said undesired electrons from said path, means coupled to said electron deiiection means land said source of pulses to energize said electron deection means during the interval between each ot said pulses to preclude interaction of said undesired electrons with said interaction means, and an electron absorption electrode mounted between said interaction means .and said electron deflection means for yabsorbing said undesired electrons be tween each of sai-d pulses.
  • a traveling wave tube system comprising ⁇ a traveling wave tube, a source of pulses, means responsive to said -pulses for projecting la plurality of discrete electron beam segments along a given path, said electron beam segments having undesired electrons therebetween, a slow wave interaction structure for deriving energy from said beam segments disposed along said given path, electron deilection means disposed intermediate said beam segment projecting means and said slow wave structure to deilect said undesired electron trom said path, and means coupled to said electron deflection means and said source of pulses to energize said electron deection means during the interval between each of said pulses to preclude interaction of said undesired electrons with said slow wave structure.
  • a klystron tube system comprising a klystron tube, a source of pulses, means responsive to said pulses for projecting la plurality of discrete electron beam segments along a given path, said electron beam segments having undesired electrons therebetween, radio frequency resonant structure for deriving energy from said beam segments disposed along said given path, electron deflection means disposed lintermediate said beam generating means and said resonant structures to deflect said undesired electrons from said path, tand means coupled to said electron deflection means and said source of pulses to energize said electron detiection means during the interval between each of said pulses to preclude interaction of said undesired electrons with said resonant structures.
  • An electron discharge device system comprising an electron ⁇ discharge device having an input means for projecting an electron beam along a given path, means for applying beam switching pulses to said beam projecting means to produce a plurality of discrete beam segments having undesired electrons therebetween, electron deection means ladjacent said beam projecting means and adapted to deiiect said undesired electrons from said path,

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Description

Aug- 28, 1962 T. J. MARCHESE 3,051,865
PULSED BEAM TUBE Filed Oct. 6, 1958 2 Sheets-Sheet 2 "l L0 z 3i 2 s "o, a C N u; i
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` www Attorney Apresented to the receiver as noise.
nite.v States ice 3,051,865 PULSED BEAM TUBE Theodore I. Marchese, Nutley, NJ., assigner to International Telephone and Telegraph Corporation, Nutley, NJ., a corporation of Maryland Filed Oct. 6, 1958, Ser. No. 765,456 6 Claims. (Cl. 315-3) This invention relates to pulsed lbeam tubes and more particularly to those which are adapted to reduce the noise level during interpulse intervals, including traveling wave and lclystron tube types.
It is well known in the prior art that the existence of noise in electronic systems from any source is undesirable. This is true particularly in systems which obtain information from reflected signals which are only a minute portion of the transmitted power. Much time and energy has been spent in discovering and eliminating sources of noise from both transmitters and receivers used in the above type systems. Because of the requirements for the detection of small targets at long ranges in present day and future systems, much time and energy will be spent to provide for further noise reductions. It has been noticed, however, that recent advances in noise reduction techniques have been rather complex and expensive and, in some cases, only desirable because of the extreme necessity for reducing noise levels.
Present day radar systems of the pulse type may incorporate either a traveling wave tube or a klystron as the output stage of the transmitter. These electron discharge devices are generally of extremely high power for long range applications. Their range, however, is often limited by the fact that received signals are submerged in noise from various sources. One source of noise is due 'to the environment in which the radiating antenna is placed. This noise may be termed thermal or ambient noise and it exists because all objects in the ordinary environments radiate energy due to their molecular activity, Very little can be done to eliminate this type of noise. Another source of noise exists, however, which contributes greatly to the overall noise being presented to the receiver. This noise, which is also thermal in nature, exists in the output tube of the transmitter and is due to three conditions in the region of the electron gun of the output tube. In pulsed output tubes, a convenient way to apply pulse modulation to a radio frequency wave is to utilize a modulation anode or grid to turn on and cut-oit the tube electron beam. These modulation anodes or grids, however, due to geometrical imperfections are not 100% effective in cutting off the beam during the transmitter oiftime and a small portion of the beam leaks through to enter the interaction region of the electron discharge device where it is amplified and This is one source of noise. The second source of noise in the output tube is the modulating anode or grid. The electron beam in passing through this element heats it up and primary emission due to the heating takes place and continues during the transmitter off-time. A third source of noise, which provides a second order effect is due to secondary emission from the grid. The noise due to incomplete beam cut-off and to primary and secondary emission may be termed l residual noise to distinguish it from. the ambient noise. Since the ambient noise is relatively uncontrollable, one
approach in the reduction of the overall noise figure, not shown heretofore in the prior art, would be to reduce the residual noise due to incomplete beam cut-off and primary and secondary emission during the off-time of radar transmitters.
It is therefore an object of this invention to provide a pulsed electron discharge device in which residual noise during the interpulse interval is substantially reduced.
It is another .object of this invention ,to provide a pulsed electron discharge device system which has an improved signal-to-noise ratio as compared with prior art systems.
It is a further object of this invention to provide a pulsed electron discharge device in which the residual beam current is prevented from entering the interaction region of the electron discharge device.
A feature of this invention is the utilization of an electron discharge device having means for projecting an electron beam along a given path and interaction means for deriving energy from the beam disposed along the electron beam path. In addition, the electron discharge device incorporates vdeflection means to deflect the electron beam from the given path when it is desired to preclude interaction with the aforesaid interaction means.
Another feature is the utilization of deflection means disposed intermediate the beam generation means and the interaction means, either internally or externally of the vacuum envelope to preclude interaction of the electron beam with the interaction means when desired.
A further feature is the utilization of either a split first anode or a split focusing electrode `coupled to a voltage source to deflect the residual electron beam to preclude interaction of the beam with the interaction means.
A still further feature `of this invention is the utilization of skirt portions on the first anode to collect the deflected residual beam current.
The foregoing and other objects and features of this invention will become more apparent by reference to the following description taken in conjunction with the accompanying drawings, wherein:
FIG. l is a schematic representation of an electron discharge device of the traveling wave tube type which operates in accordance with the principles of this invention',
FIG. 2 is a schematic representation of a traveling ywave tube having externally disposed magnetic residual beam deflecting means;
FIG. 3 is a schematic representation of a traveling wave tube having externally disposed electrostatic residual beam deflecting means;
FIG. 4 is a schematic representation of a klystron tube which opeates in accordance with the principles of this invention;
FIG. 5 is a schematic representation of a klystron tube having externally disposed magnetic beam deflection means;
FIG. 6 is a schematic representation of a klystron tube having externally disposed electrostatic beam deflection means;
FIG. 7 is a partial longitudinal cross-sectional view of a preferred embodiment which operates in accordance with the principles of this invention and;
FIG. 8 is a partial longitudinal cross-sectional view of an alternative preferred embodiment of this invention.
Referring to FIGS. 1, 2, 3, there is shown in each of the figures an electron discharge device 1 of the traveling wave tube type. Electron discharge device 1 includes means 2 for projecting an electron beam along a given path. Interaction means 3 in the form of a helical slow wave structure 4 is disposed along the given path and supports a radio frequency electromagnetic wave which derives energy from the electron beam through the agency of said interaction means 3. Defiection means 5 which may be either electrostatic or electromagnetic is shown disposed either internally or externally of vacuum envelope 6 adjacent beam projecting means 2 to deflect the electron beam from the given path to preclude interaction of the electron beam with the interaction means 3 during a given interval.
In FIG. 1, deliection means 5 consists of two electrodes 7, 8 suitable for applying a difference of potential thereto. In this embodiment, electrodes 7, 8 are disposed internally of vacuum envelope 6 and between beam projection means 2 and interaction means 3. Vacuum envelope 6 may be of metal, glass or ceramic. Terminals 9, 10 which penetrate vacuum envelope 6 are used to apply a difference of potential from voltage source 11 to defiect the residual beam during a given interval. The beam projection means 2 includes a cathode 12, a grid 13 and a first anode 14 which cooperatively act to project an electron beam along a given path to collector 15. A pulsed source of voltage 16 coupled to grid 13 applies pulses of the proper polarity to turn on and cut off the beam current so that a radio frequency wave introduced on input terminal 17 of interaction means 3 may be pulse modulated and delivered to output terminal 18 as an amplified pulsed radio frequency wave.
In FIG. 2 an electron discharge device 1 is shown which is similar in every way to the `device of FIG. 1 with the exception that the deiiection means 5 is disposed externally of vacuum envelope 6 and is electromagnetic in nature. All elements in this figure and in those which follow which are similar are indicated with the same number. Thus, in FIG. 2 deflection means 5 consists of an electromagnetic deflection coil 19 which acts to deflect the residual electron beam from the given path. Coil 19 is disposed between electron projecting means 2 and interaction means 3 and a difference of potential from voltage source 11 is applied to coil 19 across terminals 20, 21.
FIG. 3 shows an electron discharge device 1 which is similar in every way to the device of FIG. 1 with the exception that defiection means 5 is disposed externally of vacuum envelope 6. Further, Vacuum envelope 6, for this type of defiection should be glass or ceramic and not metal. A metal envelope, in this application, would shield the beam from the action of the electric field.
Referring to FIGS. 4, 5, 6, there is shown in each of these figures an electron discharge `device 1 of the klystron tube type. As in FIGS. l, 2, 3 the electron discharge device 1 includes means 2 for projecting an electron beam along a given path. Interaction means 3 in the form of a plurality of resonant radio frequency cavities 22 are disposed along the given path and are adapted to support a radio frequency electromagnetic wave which derives energy from the electron beam through the agency of resonant cavities 22. Deection means 5 in FIGS. 4, 5, 6 as in FIGS. 1, 2, 3 may be either electrostatic or electromagnetic and may be disposed either internally or externally of Vacuum envelope 6 adjacent beam projection means 2 to deect the electron beam from the given path to preclude interaction of the electron beam with interaction means 3.
FIG. 4, then, is similar in every way to the device of FIG. 1 with the exceptions that the interaction means 3 in FIG. 4 consists of resonant cavities 22 as opposed to a helical slow wave structure 4 in FIG. 3. Input and output terminals 17, 18 in FIG. 4 couple to coupling loops disposed within the cavities 22.
FIG. 5, as far as the type of deflection means 5 used, is similar in every way to the embodiment of FIG. 2, and
FIG. 6 employs the same type of deflection as shown in connection with the embodiment of FIG. 3. In the externally disposed electrostatic defiection application of FIG. 6, the vacuum envelope should be limited to either glass or ceramic material, so that the beam will not be shielded as it would be if a metallic envelope were used.
The operations of the embodiments of FIGS. 1 through 6 are alike; the only `differences being the type of deflection means used and the position of the deection means 5 with respect to vacuum envelope 6. Thus, in FIGS. l through 6, the grids or modulating anodes 13 of electron discharge devices are energized from a pulse source 16 which is coupled to grids 13. The potential on grids 13 is pulsed from some negative voltage with respect to the cathode which substantially cuts off the beam current to a value which permits the electrons to enter the tube interaction region where the beam interacts with the radio frequency energy present in the interaction means 3. FIGS. 1 to 3 operate in a manner Well known in the traveling wave tube art and FIGS. 4 to 6 operate in a manner well known in the klystron art in their respective interaction regions. The radio frequency energy is then passed to the output 18 as an amplified pulse of radio frequency energy. At the end of the pulse applied to grid 13 from source 16, the beam is cut-off and no further action is intended in the interaction means 3 until the start of the next pulse. However, due to the fact that grid 13 does not provide complete cut-off of the electron beam and due to the fact that primary emission due to heating of grid 13 and some secondary emission exists, a residual beam is present during the interpulse interval which can be amplified in the interaction means 3, if it is allowed to enter interaction means 3. A potential difference applied from voltage source 11 to defiection means S of the various embodiments precludes the above-described action from taking place. By means well known to those skilled in the electronics art, a potential from voltage source 11 is applied, at the end of the pulse from pulsed source 16, to deflection means 5 to ydeect the residual beam away from interaction means 3 and onto first anode 14. A trigger pulse from pulse source 16r over lead 11', for instance, may be used to indicate the instant at which pulse source 16 is de-energized and the instant at which voltage source 11 should be energized.
The action of electrostatic and electromagnetic fields on electrons is well known to lchose skilled in the electron ballistic art and occurs in each of the above embodiments in this known manner. The magnitude of the defiecting potential is relatively small because the density of the residual beam is small. The residual beam, for the same reason, may be collected on the first anode 14 or the vacuum envelope walls with the generation of only a `small amount of heat. The potential from voltage source 11 is removed from defection means 5 at the beginning of the next pulse from pulsed source 16. In this manner, therefore, the residual beam is precluded from entering the interaction means and the noise due to the amplification in the interaction means 3 is substantially eliminated.
Referring now to FIG. 7, there is shown therein a preferred embodiment which operates in accordance with the principles of this invention. Since the novelty of [this invention resides principally in the region of the elec- 'tron gun, only the electron gun and the deiiection structure are shown. The portions of the traveling wave tube or klystron not shown can be of a design well knovm to those skilled in the art. Electron ygun 23 consists of a cathode 24 for projecting an electron beam along a given path; a heater 25 for energizing cathode 24, a grid 26 disposed adjacent cathode to apply pulse modulation from pulsed source 16 to the electron beam; a focusing electrode 27 toI focus the electron beam to a given cross- -sectional area, and a first anode 28 to accelerate the electron beam toward interaction structure shown generally at 29. Interaction structure 29 may be any slow wave structure used in conventional traveling wave tubes or may be a series of cavities such as used in conventional klystrons. All of the above-mentioned elements are con- Venti'onal and operate in the conventional manner with the exception of the focusing electrode 27 which differs from the ordinary electrode both as to structure and function. Structurally, focusing electrode 27 has at least two portions 30, 31 separated one from the other by a narrow gap 32 and oppositely disposed to act as d'eilection electrodes during the interpulse interval. The narrow gap 32 has no eiect whatsoever on the operation of electrode 27 when it is functioning as a yfocusing electrode during pulsed operation provided the gap 32 is kept quite narrow. By applying a diiierence of potenti-al trom voltage source 11 between the two portions 30, 31 of electrode 27, it is possible to electrostatically deflect lthe residual electron beam such that it is intercepted by ffirst anode 28 and dissipated as heat thereon. The deflection of the beam may be accomplished, in a practical way, by simply reducing the voltage on existing connections applied to one of the portions 30, 31 during the interpulse interval from the equal negative voltages with respect to the cathode which exist when the tube is operating as a pulsed ampliiier. Focusing electrode 27 may be divided into a plurality of opposed portions any pair of which may be energized to cause deflection of the residual beam without affecting operation of the tube as a pulsed amplifier.
FIG. 8 is an alternative to the embodiment of FIG. 7. In the embodiment of FIG. 8, the focusing electr-ode 27 is no longer split, but appears as a conventional focusing electrode. Like elements in FIG. 8 are numbered the same ias in FIG. 7. First anode 28, however, diiiers from the anode of FIG. 7 in that it has at least two portions 33, 34 to which a potential ydiiierence is applied from voltage source 11 to cause electrostatic deflection of the residual beam current during the transmitter off- 'time Further, each of the portions 33, 34 'has exten- :sions or skirts 35, 36 which extend in the direction of the electron beam flow to act as collectors for the residual beam current which is deflected by the first anode. The skirts 35, 36, of course, could be used in the embodiment of FIG. 7 in the same manner. Since a potential is to be applied to at least one of the two portions 33, 34 of anode 28, one of the portions or both may be insulated from the tube shell by a semi-circular insulator 37 disposed between anode 2S and tube shell 38. In this manner, the Ideilecting voltage is prevented from shorting to ground. The deflection voltage is applied to anode 28 by means of terminal 39 and lead 40 which is passed through the vacuum envelope by a conventional vacuum seal. The embodiment of FIG. 8, like the embodiment of FIG. 7, may be used with both traveling wave tubes and with Iklystrons.
Experiments conducted on the above-described deflection technique have produced significant reductions in the noise due to residual beam current during the interpulse interval. The results are significant in that i-t is possible to provide bulit-in no-ise reduction means in pulse tubes such as shown in FIGS. 7 and 8 without seriously altering the structure of lthe electron discharge device.
While I have described above the principles of my invention in connecti-on with specific apparatus, it is to be clearly understood that this description is ina-de only by way of example and not as a limitation to the scope of my invention as set forth in the objects thereof and in the accompanying claims.
I claim:
1. An electron discharge `device system comprising an electron discharge device, means to project discrete electron beam segments along a given path, said electron beam segments having undesired electrons therebetween, interaction means for deriving energy from said beam segments disposed .along said given path, electron deiiection means kdisposed adjacent sai-d beam segment projecting means to deflect said undesired electro-ns from 6 said path, and means coupled to said electron deliection means to energize sai-d electron detiection means during the interval between each of said beam segments to prelclude interaction of said undesired electrons with said interaction means.
2. An electron discharge device system comprising an electron discharge device, means to project discrete electron beam segments along Ia given path, said electron beam segments having undesired electrons therebetween, interaction means 'for deriving energy from said seg'- ments disposed along said given path, electron deection means disposed adjacent said beam segment projecting means to detlect said undesired electrons from said path, means coupled to said electron deiiection means to energize said electron deflection means during the interval between each of said beam segments to preclude interaction of said undesired electrons with said interaction means, `and an electron absorption electrode mounted be tween said interaction means and said electron deection means for `absorbing said undesired electrons during the intervals between each of said beam segments.
3. An electron discharge device system comprising :an electron discharge device, a source of pulses, means responsive to said pulses for projecting a plurality of discrete beam segments Ialong a given path, said electron beam segments having undesired electrons therebetween, interaction means for deriving energy from said beam segments disposed along said given path, electron deflection means disposed adjacent said beam segment projecting means to deflect said undesired electrons from said path, means coupled to said electron deiiection means land said source of pulses to energize said electron deection means during the interval between each ot said pulses to preclude interaction of said undesired electrons with said interaction means, and an electron absorption electrode mounted between said interaction means .and said electron deflection means for yabsorbing said undesired electrons be tween each of sai-d pulses.
4. A traveling wave tube system comprising `a traveling wave tube, a source of pulses, means responsive to said -pulses for projecting la plurality of discrete electron beam segments along a given path, said electron beam segments having undesired electrons therebetween, a slow wave interaction structure for deriving energy from said beam segments disposed along said given path, electron deilection means disposed intermediate said beam segment projecting means and said slow wave structure to deilect said undesired electron trom said path, and means coupled to said electron deflection means and said source of pulses to energize said electron deection means during the interval between each of said pulses to preclude interaction of said undesired electrons with said slow wave structure.
5. A klystron tube system comprising a klystron tube, a source of pulses, means responsive to said pulses for projecting la plurality of discrete electron beam segments along a given path, said electron beam segments having undesired electrons therebetween, radio frequency resonant structure for deriving energy from said beam segments disposed along said given path, electron deflection means disposed lintermediate said beam generating means and said resonant structures to deflect said undesired electrons from said path, tand means coupled to said electron deflection means and said source of pulses to energize said electron detiection means during the interval between each of said pulses to preclude interaction of said undesired electrons with said resonant structures.
l6. An electron discharge device system comprising an electron `discharge device having an input means for projecting an electron beam along a given path, means for applying beam switching pulses to said beam projecting means to produce a plurality of discrete beam segments having undesired electrons therebetween, electron deection means ladjacent said beam projecting means and adapted to deiiect said undesired electrons from said path,
References Cited in the file of this patent UNITED STATES PATENTS Prinz Aug. 11, 1936 Ardenne Nov. 30, 1937 Varian etal Feb. 3, 1942 Linder Apr. 17, 1945 Kilgore Sept. 24, 1946 Strutt et al Apr. 8, 1947 Tomlin June 29, 1948 Norton Aug. 7, 1956
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US3210594A (en) * 1961-09-18 1965-10-05 Gen Electric Gating device for microwave signals
US3295066A (en) * 1962-07-05 1966-12-27 Continental Electronics Mfg Multiple modulating anode beam type electron tube and modulating circuit
US3394284A (en) * 1966-03-07 1968-07-23 Sanders Associates Inc Capacitive loads and circuits for providing pulsed operation thereof
DE3316609A1 (en) * 1982-05-12 1983-11-17 Varian Associates, Inc., 94303 Palo Alto, Calif. GRID CONTROLLED POWER ELECTRON TUBES
US4629937A (en) * 1984-02-02 1986-12-16 California Institute Of Technology Compact electron gun for emitting high current short duration pulses
US20120187832A1 (en) * 2007-02-21 2012-07-26 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator

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US2100704A (en) * 1930-12-23 1937-11-30 Loewe Opta Gmbh Television reception arrangement with braun tubes
US2272165A (en) * 1938-03-01 1942-02-03 Univ Leland Stanford Junior High frequency electrical apparatus
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US2418735A (en) * 1940-07-11 1947-04-08 Hartford Nat Bank & Trust Co Oscillation generator including a cathode-ray tube
US2444073A (en) * 1941-05-02 1948-06-29 Standard Telephones Cables Ltd Electron beam tube for ultra high frequencies
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US2100704A (en) * 1930-12-23 1937-11-30 Loewe Opta Gmbh Television reception arrangement with braun tubes
US2050628A (en) * 1931-03-02 1936-08-11 Telefunken Gmbh Cathode ray television system
US2272165A (en) * 1938-03-01 1942-02-03 Univ Leland Stanford Junior High frequency electrical apparatus
US2418735A (en) * 1940-07-11 1947-04-08 Hartford Nat Bank & Trust Co Oscillation generator including a cathode-ray tube
US2444073A (en) * 1941-05-02 1948-06-29 Standard Telephones Cables Ltd Electron beam tube for ultra high frequencies
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3210594A (en) * 1961-09-18 1965-10-05 Gen Electric Gating device for microwave signals
US3295066A (en) * 1962-07-05 1966-12-27 Continental Electronics Mfg Multiple modulating anode beam type electron tube and modulating circuit
US3394284A (en) * 1966-03-07 1968-07-23 Sanders Associates Inc Capacitive loads and circuits for providing pulsed operation thereof
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US4480210A (en) * 1982-05-12 1984-10-30 Varian Associates, Inc. Gridded electron power tube
US4629937A (en) * 1984-02-02 1986-12-16 California Institute Of Technology Compact electron gun for emitting high current short duration pulses
US20120187832A1 (en) * 2007-02-21 2012-07-26 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator
US8618736B2 (en) 2007-02-21 2013-12-31 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator
US8624494B2 (en) * 2007-02-21 2014-01-07 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator
US8624495B2 (en) 2007-02-21 2014-01-07 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator
US8847490B2 (en) 2007-02-21 2014-09-30 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator
US8884519B2 (en) 2007-02-21 2014-11-11 Manhattan Technologies Ltd. High frequency helical amplifier and oscillator

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