US3292239A - Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules - Google Patents

Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules Download PDF

Info

Publication number
US3292239A
US3292239A US287310A US28731063A US3292239A US 3292239 A US3292239 A US 3292239A US 287310 A US287310 A US 287310A US 28731063 A US28731063 A US 28731063A US 3292239 A US3292239 A US 3292239A
Authority
US
United States
Prior art keywords
tube
cavity
electron beam
members
multicavity
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US287310A
Inventor
James T Sadler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sperry Corp
Original Assignee
Sperry Rand Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sperry Rand Corp filed Critical Sperry Rand Corp
Priority to US287310A priority Critical patent/US3292239A/en
Priority to NL6406552A priority patent/NL6406552A/xx
Priority to DE19641491421 priority patent/DE1491421A1/en
Priority to FR978037A priority patent/FR1417142A/en
Priority to GB24459/64A priority patent/GB1070966A/en
Application granted granted Critical
Publication of US3292239A publication Critical patent/US3292239A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons
    • H01J25/34Travelling-wave tubes; Tubes in which a travelling wave is simulated at spaced gaps
    • H01J25/36Tubes in which an electron stream interacts with a wave travelling along a delay line or equivalent sequence of impedance elements, and without magnet system producing an H-field crossing the E-field
    • H01J25/38Tubes in which an electron stream interacts with a wave travelling along a delay line or equivalent sequence of impedance elements, and without magnet system producing an H-field crossing the E-field the forward travelling wave being utilised
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/005Cooling methods or arrangements
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/16Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
    • H01J23/24Slow-wave structures, e.g. delay systems
    • 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
    • H01J25/12Klystrons, 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 with pencil-like electron stream in the axis of the resonators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49016Antenna or wave energy "plumbing" making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49764Method of mechanical manufacture with testing or indicating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49764Method of mechanical manufacture with testing or indicating
    • Y10T29/49771Quantitative measuring or gauging

Definitions

  • the present invention relates to multi cavity electron beam tubes and more particularly to a simple and economical manner of constructing such a tube.
  • multicavity electron beam tubes such as klystron tubes depends upon the accuracy with which the individual cavities of a completely assembled tube can exhibit their desired electrical characteristics such as Q values and resonant frequencies.
  • Most tubes of these types are constructed i'rom a great many component parts, and as a result of the cumulative effects of dimension variations in various component parts and dimensional errors arising during assembly of the tube, the completed tube may operate with electrical characteristics so different from the desired characteristics that expensive and difiicult reworking of the assembled tube may be required, or the tube may have to be discarded completely.
  • Extreme caution and attention to dimensional tolerances in the component parts and in the assembly procedure of the tube greatly adds to the cost of the tube and cannot always be permitted.
  • the addition of cavity tuners having an appreciable frequency tuning range to help compensate for the above difliculties is not always possible because of mechanical and electrical limitations.
  • a further object of this invention is to provide a multicavity electron beam tube constructed in such a manner as to permit the preassembly and pretuning of individual cavities of the tube.
  • Another object of this invention is to provide a multicavity electron beam tube that is constructed in a manner to permit a plurality of preassembled and pretuned cavities to be finally assembled into the tube body in a single operation that does not disturb the tuning of the cavities.
  • a further object of the invention is to provide a simple and economical manner of constructing a multi-cavity electron beam tube.
  • Another object of this invention is to provide a rugged and reliable klystron tube that is easily constructed from a stock of standard and interchangeable parts.
  • a tube body structure comprised of a plurality of pairs of first and second solid, longitudinallycxtending end members that are coaxially positioned along the tube :axis.
  • the adjacent faces of each pair of first and second end members are disposed in spaced-apart relationship and an annular enclosing member is secured in a vacuum-tight manner about the peripheries of the adjacent faces of each pair, thereby fonming an electromagnetic wave cavity therebetween.
  • the adjacent faces of successive pairs of end members are secured in abutting relationship to complete the vacuumtight seal for the body portion of the tube and to form beam drift tubebetween successive cavities.
  • FIG. 1 is a partial sectional view showing a completely assembled multi-cavity :klystron amplifier tube constructed in accordance with the present invention
  • FIG. 2 is a sectional view of an individual cavity unit constructed in accordance with this invention, and further illustrates a means flol pretuning the cavity unit;
  • FIG. 3 is a transverse sectional view taken at section 33 of FIG. 1 and showing an arrangement of a trim tuner, cut away in the sectional view of FIG. 1, for slightly tuning a cavity of the tube;
  • FIG. 4 is a sectional view of an alternative embodiment of an individual cavity unit constructed in accordance with the teachings of this invention.
  • a multi-cavity klystron tube amplifier is illustrated in FIG. 1 and is comprised of a conventional electron gun .12 that forms and directs a beam of electrons along the longitudinal axis of the tube.
  • An electron beam collector 13 which also may be of conventional design, is located at the opposite end of the tube to terminate the electron beam.
  • the body portion of the tube is comprised of a plurality of individual cavity units 15-21 which are assembled in a vacuum-tight manner along the length of the tube.
  • the cavity units include the respective reentrant cavity resonators 25-31 that are disposed in spaced apart relationship throughout the length of the body portion of the tube.
  • Electromagnetic wave energy to be amplified may be coupled into the first cavity 15 by means of input waveguide 32, and the amplified electromagnetic waves may be coupled from the last cavity 31 by means of output waveguide 33.
  • Each of the individual cavities 1521 is similar in construction, and taking cavity unit 16 as an example, it may be seen that the cavity unit is tormed as an assembly of first and second solid axially-extending spacing members 34 and 35 which are secured in spacedapart relationship by means of an annular enclosing member 36 that fits within shoulders 37 and 38 that extend around the peripheries of spacing members 34 and 35. The adjacent faces of spacing members.
  • Spacing members 34, 35 and annular enclosing member 36 have centrally positioned extensions 4% and 41 that provide reentrant nibs in the cavity that is formed in the enclosed region between spacing members 34, 35 and annular enclosing member 36.
  • Spacing members 34, 35 and annular enclosing member 36 are secured together in a vacuum-tight manner, as by brazing.
  • Each of the members 34, 35 and 36 are circularly symmetrical about the beam axis and may be machined from blocks of a suitable material such as copper.
  • Spacing member 35 of cavity unit 16 is provided with a centrally positioned stud 45 and spacing member 42 of the adjacent cavity unit 17 is provided with a registering recess 46 to assure the correct alignment of the individual cavity units during final assembly.
  • Spacing members 34 and 35 are axially apertured throughout their lengths to provide a path tor the electron beam through each of the cavity units 1521. It may be seen that the axial apertures in the spacing members 3S and 42 that are in abutting contact form a beam drift tube between cavities 26 and 27.
  • thin cylinders 51-55 are sealed in a fluid-tight manner between the successive annular enclosing members so as to provide a fluid-tight envelope about the tube.
  • Each of the annular enclosing members, such as member 36, is provided with longitudinallycxtending fluid passages 57 and 58 to perm-i-t the flow of a fluid coolant in the regions between the outermost envelope formed by thin cylinders 51-55 and the outer circumferences of the spacing members such as 34 and 35. Additional means not illustrated are provided for passing the fluid to an external heat exchanger and pump.
  • a primary advantage of constructing a multi-cavity klystron tube in the manner illustrated in FIG. 1 is that each of the cavity units 15-21 may be individually preassembled and pretuned to their desired resonant frequency prior to final assembly into the tube body.
  • FIG. 2 One means for pretuning the individual cavity units prior to final assembly is illustrated in FIG. 2.
  • a closely-fitting rigid and non-deformable metallic rod 61 is inserted through the axial apertures in spacing members 34 and 35.
  • Short cylinders 62 and 63 formed of a rigid, non-yielding material such as steel, is inserted over the two ends of rod 61 and contact the outer faces of spacing members 34 and 35 only in the respective regions immediately surrounding their axial apertures.
  • the members 34-36 are dimensioned to assure that the axial spacing between the reentrant nibs 40 and 41 is slightly greater than ultimately desired to assure that the resonant frequency of the cavity is slightly higher than desired.
  • inwardly directed forces F are applied to the short cylinders 62 and 63 to slightly deform the spacing members in the regions of the nibs 40 and 41 so as to bring the nibs closer together.
  • the resonant frequency of the cavity is then tested until the desired resonant frequency is obtained.
  • the solid rod 61 extending through the axial apertures prevents the material of spacing members 34 and 35 firom collapsing to deform the apertures during the application of forces to cylinders 62 and 63. This avoids beam intercept problems during operation of the tube.
  • each of the individual cavity units After each of the individual cavity units has been tested to assure that it meets electrical and mechanical requirements, all of the cavity units then are stacked together and brazed in a single brazing operation to form the completed body portion of the tube.
  • This assembly of the cavity units to form the assembled tube is accomplished by inserting brazing material between the end faces of adjacent cavity untis, such as the adjacent faces of spacing members 35, and 42, FIG. 1, and adding further brazing material within the annular notch 60 provided in one of the members.
  • the type of construction illustrated in the tube of FIG. 1 simplifies the assembly process inasmuch as it minimizes the number of component parts, and enables a relatively unskilled worker to assemble the tube.
  • Each one of the different spacing members, or cavity end members such as members 34 and 35, and each one of the annular enclosing members such as member 36 may be individually marked or coded so that the workers who assemble the cavity units and who make the final assembly of the tube need only follow a simple procedure of stacking the correctly coded parts, thus minimizing errors that might otherwise arise in the assembly process.
  • constructing a tube in the manner described is more economical than in other types of known construction.
  • each cavity unit is individually preassembled and tested prior to final assembly, and should any one of the cavities be found to be faulty, only that one cavity need be discarded, or reworked if possible, and it is not necessary that an entirely assembled tube be discarded, as is very commonly required in present manufacturing techniques. Reworking a com pletely assembled tube often is a diflicult and time consuming task and is to be avoided if at all possible.
  • the cavities 29, 30, and 31 (litter in size from each other; and are difierent in size from the cavities 26, 27 and 28.
  • the longitudinal dimensions of cavity resonators 26, 27, 28, 29, 30 and 31 are .755, .718, .664, .772, .658 and .650 inch, respectively. This is to achieve staggered tuning of the cavities so that the tube will operate over a broad range of frequencies.
  • the sizes of the cavities are readily varied by merely changing the thickness of the spacing members and/or the axial depths of the shoulders, such as 37 and 38, and/or the diameters of the shoulders and the annular enclosing member 36.
  • the gap spacings between the 1 reentrant nibs 40 and 41 may be varied by changing nib length, shoulder depth and/ or annular enclosing member length to change either the frequency or the loaded cavity Q.
  • Tubes constructed in accordance with the teachings of this invention lend themselves well to large volume production techniques inasmuch as spacing members of various different sizes may be maintained as stock items and tubes having various different characteristics mayreadily be constructed by choosing appropriate ones of the stocked spacing members so as to assemble cavities and drift tubes of the correct precalculated dimensions that will assure the desired operating characteristics in the tube.
  • rigid rod 70 is secured to the central region of flexible diaphragm 68 and extends through a clearance hole 72 in the top cover plate 73 that encloses the other end of cylinder 67.
  • the outer end of rod 70 is threaded and adjusting nuts 75 and 76 are threaded to rod 70 on opposite sides of cover plate 73 so as to provide means for adjusting the depth of insertion of rod 70, and thus the position of flexible diaphragm 68 Within cavity 26 so as to afiect the tuning of said cavity.
  • the entire tube body is comprised of an assembly of cavity units of the type illustrated in FIG. 4 wherein each cavity unit is comprised of first and second cavity end members, or spacing mem-.
  • bers 84 and 85 which are similar to the members 34 and 35 of FIG. 1 except that the cavity end members of FIG. 1 4 each are in abutting contact so that themembers them-.
  • a method for constructing a plural cavity electron beam tube using pretuned cavity component parts comprising forming each cavity from first and second longitudinab,
  • each said member being apertured longitudinally to permit the passage of an electron beam therethrough, the adjacent faces of said first and second members having respective longitudinally-extending portions in the region immediately surrounding the respective apertures, said lon-. gitudinally-extending portions being spaced to pro-.
  • each said cavity having a trim tuner
  • pretuning each cavity to a predetermined frequency by subjecting said first and second members to forces directed longitudinally inwardly whereby the spacing of the respective gap is permanently reduced and the resonant frequency of the respective cavity is set to a desired value
  • each said trim tuner to closely set the resonant frequency of the respective cavity to the respective desired value.

Description

J. T. SADLER Filed June 12, 1963 METHOD OF MANUFACTURING A MULTI-CAVITY ELECTRON BEAM TUBE, THE TUBE COMPRISING MULTIPLE RESONATOR MODULES 1 5 4 1 y, Z6 2% m Dec. 20, 1966 r mm mm wm J fy/v P E r 2 w O D A i mm 6 mm mm Km 6 0 D R wm v ffil l m l ha United States Patent METHOD OF MANUFACTURING A MULTI- CAVITY ELECTRON BEAM TUBE, THE TUBE COMPRISING M U L T I P L E RESONATOR MODULES James T. Sadler, Garden City, N.Y., assignor to Sperry Rand Corporation, Great Neck, N.Y., a corporation of Delaware Filed June 12, 1963, Ser. No. 287,310 1 Claim. (Cl. 29155.5)
The present invention relates to multi cavity electron beam tubes and more particularly to a simple and economical manner of constructing such a tube.
The successful and economical manufacture of multicavity electron beam tubes such as klystron tubes depends upon the accuracy with which the individual cavities of a completely assembled tube can exhibit their desired electrical characteristics such as Q values and resonant frequencies. Most tubes of these types are constructed i'rom a great many component parts, and as a result of the cumulative effects of dimension variations in various component parts and dimensional errors arising during assembly of the tube, the completed tube may operate with electrical characteristics so different from the desired characteristics that expensive and difiicult reworking of the assembled tube may be required, or the tube may have to be discarded completely. Extreme caution and attention to dimensional tolerances in the component parts and in the assembly procedure of the tube greatly adds to the cost of the tube and cannot always be permitted. The addition of cavity tuners having an appreciable frequency tuning range to help compensate for the above difliculties is not always possible because of mechanical and electrical limitations.
It therefore is an object of the present invention to provide a multi-cavity electron beam tube constructed in such a manner as to permit accurate pretuning of individual cavities.
A further object of this invention is to provide a multicavity electron beam tube constructed in such a manner as to permit the preassembly and pretuning of individual cavities of the tube.
Another object of this invention is to provide a multicavity electron beam tube that is constructed in a manner to permit a plurality of preassembled and pretuned cavities to be finally assembled into the tube body in a single operation that does not disturb the tuning of the cavities.
A further object of the invention is to provide a simple and economical manner of constructing a multi-cavity electron beam tube.
Another object of this invention is to provide a rugged and reliable klystron tube that is easily constructed from a stock of standard and interchangeable parts.-
These and other objects and advantages of the present invention are achieved by providing a tube body structure comprised of a plurality of pairs of first and second solid, longitudinallycxtending end members that are coaxially positioned along the tube :axis. The adjacent faces of each pair of first and second end members are disposed in spaced-apart relationship and an annular enclosing member is secured in a vacuum-tight manner about the peripheries of the adjacent faces of each pair, thereby fonming an electromagnetic wave cavity therebetween. The adjacent faces of successive pairs of end members are secured in abutting relationship to complete the vacuumtight seal for the body portion of the tube and to form beam drift tubebetween successive cavities.
The invention will be described by referring to the accompanying drawings wherein:
FIG. 1 is a partial sectional view showing a completely assembled multi-cavity :klystron amplifier tube constructed in accordance with the present invention;
FIG. 2 is a sectional view of an individual cavity unit constructed in accordance with this invention, and further illustrates a means flol pretuning the cavity unit;
FIG. 3 is a transverse sectional view taken at section 33 of FIG. 1 and showing an arrangement of a trim tuner, cut away in the sectional view of FIG. 1, for slightly tuning a cavity of the tube; and
FIG. 4 is a sectional view of an alternative embodiment of an individual cavity unit constructed in accordance with the teachings of this invention.
Referring in detail to the drawings, a multi-cavity klystron tube amplifier is illustrated in FIG. 1 and is comprised of a conventional electron gun .12 that forms and directs a beam of electrons along the longitudinal axis of the tube. An electron beam collector 13, which also may be of conventional design, is located at the opposite end of the tube to terminate the electron beam. The body portion of the tube is comprised of a plurality of individual cavity units 15-21 which are assembled in a vacuum-tight manner along the length of the tube. The cavity units include the respective reentrant cavity resonators 25-31 that are disposed in spaced apart relationship throughout the length of the body portion of the tube. Electromagnetic wave energy to be amplified may be coupled into the first cavity 15 by means of input waveguide 32, and the amplified electromagnetic waves may be coupled from the last cavity 31 by means of output waveguide 33. Each of the individual cavities 1521 is similar in construction, and taking cavity unit 16 as an example, it may be seen that the cavity unit is tormed as an assembly of first and second solid axially-extending spacing members 34 and 35 which are secured in spacedapart relationship by means of an annular enclosing member 36 that fits within shoulders 37 and 38 that extend around the peripheries of spacing members 34 and 35. The adjacent faces of spacing members. 34 and 35 have centrally positioned extensions 4% and 41 that provide reentrant nibs in the cavity that is formed in the enclosed region between spacing members 34, 35 and annular enclosing member 36. Spacing members 34, 35 and annular enclosing member 36 are secured together in a vacuum-tight manner, as by brazing. Each of the members 34, 35 and 36 are circularly symmetrical about the beam axis and may be machined from blocks of a suitable material such as copper. Spacing member 35 of cavity unit 16 is provided with a centrally positioned stud 45 and spacing member 42 of the adjacent cavity unit 17 is provided with a registering recess 46 to assure the correct alignment of the individual cavity units during final assembly.
Spacing members 34 and 35 are axially apertured throughout their lengths to provide a path tor the electron beam through each of the cavity units 1521. It may be seen that the axial apertures in the spacing members 3S and 42 that are in abutting contact form a beam drift tube between cavities 26 and 27.
In the assembled tube shown in FIG. 1, thin cylinders 51-55 are sealed in a fluid-tight manner between the successive annular enclosing members so as to provide a fluid-tight envelope about the tube. Each of the annular enclosing members, such as member 36, is provided with longitudinallycxtending fluid passages 57 and 58 to perm-i-t the flow of a fluid coolant in the regions between the outermost envelope formed by thin cylinders 51-55 and the outer circumferences of the spacing members such as 34 and 35. Additional means not illustrated are provided for passing the fluid to an external heat exchanger and pump.
A primary advantage of constructing a multi-cavity klystron tube in the manner illustrated in FIG. 1 is that each of the cavity units 15-21 may be individually preassembled and pretuned to their desired resonant frequency prior to final assembly into the tube body.
One means for pretuning the individual cavity units prior to final assembly is illustrated in FIG. 2. After the solid spacing members, or cavity end members 34 and 35 have been brazed to annular enclosing member 36 and the assembled cavity unit has been tested for vacuum tightness, a closely-fitting rigid and non-deformable metallic rod 61 is inserted through the axial apertures in spacing members 34 and 35. Short cylinders 62 and 63, formed of a rigid, non-yielding material such as steel, is inserted over the two ends of rod 61 and contact the outer faces of spacing members 34 and 35 only in the respective regions immediately surrounding their axial apertures. In the initial assembly of the cavity unit, the members 34-36 are dimensioned to assure that the axial spacing between the reentrant nibs 40 and 41 is slightly greater than ultimately desired to assure that the resonant frequency of the cavity is slightly higher than desired. To reduce the gap width and thus reduce the frequency to the desired value, inwardly directed forces F are applied to the short cylinders 62 and 63 to slightly deform the spacing members in the regions of the nibs 40 and 41 so as to bring the nibs closer together. The resonant frequency of the cavity is then tested until the desired resonant frequency is obtained.
The solid rod 61 extending through the axial apertures prevents the material of spacing members 34 and 35 firom collapsing to deform the apertures during the application of forces to cylinders 62 and 63. This avoids beam intercept problems during operation of the tube.
After each of the individual cavity units has been tested to assure that it meets electrical and mechanical requirements, all of the cavity units then are stacked together and brazed in a single brazing operation to form the completed body portion of the tube. This assembly of the cavity units to form the assembled tube is accomplished by inserting brazing material between the end faces of adjacent cavity untis, such as the adjacent faces of spacing members 35, and 42, FIG. 1, and adding further brazing material within the annular notch 60 provided in one of the members.
The type of construction illustrated in the tube of FIG. 1 simplifies the assembly process inasmuch as it minimizes the number of component parts, and enables a relatively unskilled worker to assemble the tube. Each one of the different spacing members, or cavity end members such as members 34 and 35, and each one of the annular enclosing members such as member 36 may be individually marked or coded so that the workers who assemble the cavity units and who make the final assembly of the tube need only follow a simple procedure of stacking the correctly coded parts, thus minimizing errors that might otherwise arise in the assembly process. Additionally, constructing a tube in the manner described is more economical than in other types of known construction. This results from the fact that each cavity unit is individually preassembled and tested prior to final assembly, and should any one of the cavities be found to be faulty, only that one cavity need be discarded, or reworked if possible, and it is not necessary that an entirely assembled tube be discarded, as is very commonly required in present manufacturing techniques. Reworking a com pletely assembled tube often is a diflicult and time consuming task and is to be avoided if at all possible.
As may be seen in FIG. 1, the cavities 29, 30, and 31 (litter in size from each other; and are difierent in size from the cavities 26, 27 and 28. For example, in one typical embodiment of the present invention, the longitudinal dimensions of cavity resonators 26, 27, 28, 29, 30 and 31 are .755, .718, .664, .772, .658 and .650 inch, respectively. This is to achieve staggered tuning of the cavities so that the tube will operate over a broad range of frequencies. The sizes of the cavities are readily varied by merely changing the thickness of the spacing members and/or the axial depths of the shoulders, such as 37 and 38, and/or the diameters of the shoulders and the annular enclosing member 36. .The gap spacings between the 1 reentrant nibs 40 and 41 may be varied by changing nib length, shoulder depth and/ or annular enclosing member length to change either the frequency or the loaded cavity Q. Tubes constructed in accordance with the teachings of this invention lend themselves well to large volume production techniques inasmuch as spacing members of various different sizes may be maintained as stock items and tubes having various different characteristics mayreadily be constructed by choosing appropriate ones of the stocked spacing members so as to assemble cavities and drift tubes of the correct precalculated dimensions that will assure the desired operating characteristics in the tube.
It is virtually impossible to build a number of electron guns that have identical beam characteristics, and because the electron beam passing through a klystron cavity loads the cavity and affects its frequency of operation, it is desirable to have some type of tuning means in each cavity of the conductive boundary of reentrant cavity 26.. A
rigid rod 70 is secured to the central region of flexible diaphragm 68 and extends through a clearance hole 72 in the top cover plate 73 that encloses the other end of cylinder 67. The outer end of rod 70 is threaded and adjusting nuts 75 and 76 are threaded to rod 70 on opposite sides of cover plate 73 so as to provide means for adjusting the depth of insertion of rod 70, and thus the position of flexible diaphragm 68 Within cavity 26 so as to afiect the tuning of said cavity. A notch 80 may be providedon the outer periphery of annular enclosing member 36 to as-= sist in aligning the various parts during assembly.
It will be obvious that the various modifications may be made to the type of tube construction illustrated in FIG. 1. In one alternative embodiment, the entire tube body is comprised of an assembly of cavity units of the type illustrated in FIG. 4 wherein each cavity unit is comprised of first and second cavity end members, or spacing mem-. bers 84 and 85 which are similar to the members 34 and 35 of FIG. 1 except that the cavity end members of FIG. 1 4 each are in abutting contact so that themembers them-.
selves provide the cavity enclosing means, thus eliminating the requirement for additional annular enclosing means such as the member 36 of FIG. 1.. It has been found,l
however, that it is more diflicult and costly to incorporate a trim tuner mechanism into the structure of thi embodiment of the invention. Other obvious modifications willi be apparent to those skilled in the art.
While the invention has been described in its preferred embodiments, it is to be understood that the Words which have been used are words of description rather than limitation and that changes within the purview of the appended.
claim may be made without departing from the true scope and spirit of the invention in its broader aspects.
What is claimed is:
A method for constructing a plural cavity electron beam tube using pretuned cavity component parts comprising forming each cavity from first and second longitudinab,
ly-extending cavity end members, each said member being apertured longitudinally to permit the passage of an electron beam therethrough, the adjacent faces of said first and second members having respective longitudinally-extending portions in the region immediately surrounding the respective apertures, said lon-. gitudinally-extending portions being spaced to pro-.
vide a gap therebetween, each said cavity having a trim tuner,
pretuning each cavity to a predetermined frequency by subjecting said first and second members to forces directed longitudinally inwardly whereby the spacing of the respective gap is permanently reduced and the resonant frequency of the respective cavity is set to a desired value,
joining the pretuned cavities to form a composite plural cavity electron beam tube, and
adjusting each said trim tuner to closely set the resonant frequency of the respective cavity to the respective desired value.
References Cited by the Examiner 5 UNITED STATES PATENTS 2,463,267 3/ 1949 Hahn 3155.43 X 2,582,186 1/1952 WillshaW 315---5.43 X 2,852,715 9/1958 Rich 3l55.48 2,994,009 7/ 1961 Schmidt et al 3l55.48
10 HERMAN KARL SAALBACH, Primary Examiner.
R. D. COHN, Assistant Examiner.
US287310A 1963-06-12 1963-06-12 Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules Expired - Lifetime US3292239A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US287310A US3292239A (en) 1963-06-12 1963-06-12 Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules
NL6406552A NL6406552A (en) 1963-06-12 1964-06-10
DE19641491421 DE1491421A1 (en) 1963-06-12 1964-06-11 Electron beam tubes with multiple resonance cavities and method for making same
FR978037A FR1417142A (en) 1963-06-12 1964-06-12 Multiple cavity electron beam tube
GB24459/64A GB1070966A (en) 1963-06-12 1964-06-12 Electron beam tube and method of making same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US287310A US3292239A (en) 1963-06-12 1963-06-12 Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules

Publications (1)

Publication Number Publication Date
US3292239A true US3292239A (en) 1966-12-20

Family

ID=23102341

Family Applications (1)

Application Number Title Priority Date Filing Date
US287310A Expired - Lifetime US3292239A (en) 1963-06-12 1963-06-12 Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules

Country Status (4)

Country Link
US (1) US3292239A (en)
DE (1) DE1491421A1 (en)
GB (1) GB1070966A (en)
NL (1) NL6406552A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3573680A (en) * 1969-04-24 1971-04-06 Raytheon Co Temperature compensation of microwave cavity
US4038602A (en) * 1976-02-25 1977-07-26 The United States Of America As Represented By The Secretary Of The Navy Automodulated realtivistic electron beam microwave source
US4542581A (en) * 1982-04-30 1985-09-24 Siemens Aktiengesellschaft Method for manufacturing a tubular part for generating a spatially alternating magnetic field within a magnet system for guiding the electron beam of travelling-wave tubes
US5281894A (en) * 1990-09-28 1994-01-25 The United States Of America As Represented By The Secretary Of The Navy Dual cavity for a dual frequency gyrotron
US5959406A (en) * 1995-08-23 1999-09-28 Hughes Electronics Corporation Traveling wave tube with expanding resilient support elements

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463267A (en) * 1941-04-26 1949-03-01 Gen Electric High-frequency apparatus
US2582186A (en) * 1945-11-14 1952-01-08 Gen Electric Co Ltd Apparatus for accelerating charged particles, especially electrons, to very high-velocity
US2852715A (en) * 1949-09-22 1958-09-16 Sperry Rand Corp High frequency structure
US2994009A (en) * 1958-07-17 1961-07-25 Varian Associates High frequency tube apparatus

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463267A (en) * 1941-04-26 1949-03-01 Gen Electric High-frequency apparatus
US2582186A (en) * 1945-11-14 1952-01-08 Gen Electric Co Ltd Apparatus for accelerating charged particles, especially electrons, to very high-velocity
US2852715A (en) * 1949-09-22 1958-09-16 Sperry Rand Corp High frequency structure
US2994009A (en) * 1958-07-17 1961-07-25 Varian Associates High frequency tube apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3573680A (en) * 1969-04-24 1971-04-06 Raytheon Co Temperature compensation of microwave cavity
US4038602A (en) * 1976-02-25 1977-07-26 The United States Of America As Represented By The Secretary Of The Navy Automodulated realtivistic electron beam microwave source
US4542581A (en) * 1982-04-30 1985-09-24 Siemens Aktiengesellschaft Method for manufacturing a tubular part for generating a spatially alternating magnetic field within a magnet system for guiding the electron beam of travelling-wave tubes
US5281894A (en) * 1990-09-28 1994-01-25 The United States Of America As Represented By The Secretary Of The Navy Dual cavity for a dual frequency gyrotron
US5959406A (en) * 1995-08-23 1999-09-28 Hughes Electronics Corporation Traveling wave tube with expanding resilient support elements

Also Published As

Publication number Publication date
NL6406552A (en) 1964-12-14
DE1491421A1 (en) 1969-02-20
GB1070966A (en) 1967-06-07

Similar Documents

Publication Publication Date Title
US3297905A (en) Electron discharge device of particular materials for stabilizing frequency and reducing magnetic field problems
US3668459A (en) Coupled cavity slow wave circuit and tube using same
USRE25329E (en) Periodically focused traveling wave tube
US3906300A (en) Multiperiodic accelerator structures for linear particle accelerators
US3310704A (en) Output coupling circuit for microwave tube apparatus
US3292239A (en) Method of manufacturing a multicavity electron beam tube, the tube comprising multiple resonator modules
US3412279A (en) Electromagnetic wave energy absorbing elements for use in high frequency electron discharge devices having traveling wave tube sections
US3453483A (en) Microwave linear beam tube employing an extended interaction resonator operating on an odd pi mode
US4237402A (en) Slow-wave circuit for traveling-wave tubes
US3471738A (en) Periodic slow wave structure
US2871397A (en) Electron tube of the klystron type
US3423632A (en) Electron discharge device construction
James et al. A ladder circuit coupled-cavity TWT at 80-100 GHz
US3205398A (en) Long-slot coupled wave propagating circuit
US3466576A (en) Impedance matched periodic slow wave structure
US3668460A (en) Coalesced mode coupled cavity slow wave tube
US2548808A (en) Continuous-strip anode for magnetrons
US2824289A (en) Drift tube for klystron
US3032681A (en) Magnetron device
US3594605A (en) Mode suppression means for a clover-leaf slow wave circuit
US5239235A (en) Multiple-beam microwave tube with coaxial output and coaxial collector
US3573680A (en) Temperature compensation of microwave cavity
US4866343A (en) Re-entrant double-staggered ladder circuit
US4724408A (en) Waveguide filter
US4578620A (en) Slow wave circuit for a traveling wave tube