[go: up one dir, main page]

US3325671A - Klystron device having fluid cooled tunable cavities and output window mode suppression means - Google Patents

Klystron device having fluid cooled tunable cavities and output window mode suppression means Download PDF

Info

Publication number
US3325671A
US3325671A US15641661A US3325671A US 3325671 A US3325671 A US 3325671A US 15641661 A US15641661 A US 15641661A US 3325671 A US3325671 A US 3325671A
Authority
US
United States
Prior art keywords
tuner
waveguide
cup
window
cavity
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
Other languages
English (en)
Inventor
Charles S Biechler
Maurice J Sharpe
Robert S Symons
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.)
Varian Medical Systems Inc
Original Assignee
Varian Associates Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to NL285748D priority Critical patent/NL285748A/xx
Application filed by Varian Associates Inc filed Critical Varian Associates Inc
Priority to US15641661 priority patent/US3325671A/en
Priority to GB4425962A priority patent/GB998592A/en
Priority to GB701864A priority patent/GB998595A/en
Priority to GB701764A priority patent/GB998594A/en
Priority to GB701664A priority patent/GB998593A/en
Priority to JP38021322A priority patent/JPS4929778B1/ja
Priority to DEV29239A priority patent/DE1298169B/de
Priority to FR917235A priority patent/FR1345258A/fr
Priority to DE19651466578 priority patent/DE1466578B2/de
Priority to SE303966A priority patent/SE318018B/xx
Application granted granted Critical
Publication of US3325671A publication Critical patent/US3325671A/en
Priority to NL7210685A priority patent/NL7210685A/xx
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00—Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/16—Circuit elements, having distributed capacitance and inductance, structurally associated with the tube and interacting with the discharge
    • H01J23/18—Resonators
    • H01J23/20—Cavity resonators; Adjustment or tuning thereof
    • H01J23/207—Tuning of single resonator
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00—Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons
    • H01J25/02—Tubes 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
    • H01J25/10—Klystrons, 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
    • H01J25/12—Klystrons, 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
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00—Auxiliary devices
    • H01P1/08—Dielectric windows
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00—Auxiliary devices
    • H01P1/16—Auxiliary devices for mode selection, e.g. mode suppression or mode promotion; for mode conversion
    • H01P1/162—Auxiliary devices for mode selection, e.g. mode suppression or mode promotion; for mode conversion absorbing spurious or unwanted modes of propagation
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01P—WAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P7/00—Resonators of the waveguide type
    • H01P7/06—Cavity resonators

Definitions

  • the present invention relates in general to high frequency tubes and more particularly to a novel rugged, high power, continuous wave, UHF, broadband amplifier useful, for example, in applications such as navigation and communication systems, as a driver for a linear accelerator, and the like.
  • a high frequency, high power, broadband amplifier which is easily constructed, is rigid, and is broadband.
  • the teachings of the present invention contemplate a high frequency tube wherein the body of the tube is made up of a number of punch press cups which can be joined together to form a cavity subassembly and then a plurality of cavity subassemblies can be joined together to form the body assembly.
  • a removable water-cooled tuning mechanism is provided for the tube whereby no critical parts of the tuner mechanism are processed with the tube.
  • a tapered section is provided in the output waveguide which produces a frequency-dependent impedance at the waveguide side i the output iris of the tube which compensates for the ir pedance changes in the output cavity as the tuner is tun to vary the output frequency of the tube over the enti band of the tube.
  • Conduction means are provided at tl output iris to conduct heat to cooling means for preven ing overheating of the structure around the output ir:
  • the broadband output window is provided by p05 tioning a circular dielectric window within a circular se tion of guide positioned between two partially circular ar partially rectangular high impedance guide sections.
  • Als undesired modes in the region of the output window i the tube are perturbed by positioning mode suppressic means in the region around the output window.
  • a typical UHF broadband amplifier klystron tube a cording to the present invention is on the order of 5 fe long and about 250 pounds in weight and can supply mo: than 100 kilowatts of continuous wave power over mo: than a 26% frequency band between 755 and 985 meg. cycles.
  • the object of the present invention is to provide an in proved high frequency klystron amplifier tube apparatl which is relatively simple of construction, relatively rig: and which will have long operating life while deliverir high average RF. power over a wide frequency range.
  • One feature of the present invention is the provision a punch press cup cavity construction wherein individu: cavities can be formed in subassembly form and the cavit subassemblies can be secured together to form the bot assembly.
  • Another feature of the present invention is the provisic of a removable fluid-cooled tuner mechanism the parts which are cooled by a flowing fluid and which is easiI removable from the rest of the tube apparatus so that ti tube can be processed without the tuner mechanism.
  • Another feature of the present invention is the prov sion of an output waveguide section provided with tapered portion on the waveguide to produce a frequenc dependent impedance for the output cavity so that tt optimum impedance is maintained at the output gap the tube over the frequency range of the tube.
  • Another feature of the present invention is the prov sion of conduction means at the output iris of an electro tube for conducing heat from the output iris to C00ll1. means for reducing the temperature of the structui around the output iris.
  • Still another feature of the present invention is the pri vision of a novel broadband output window assembl which does not support spurious resonant modes in th frequency band of interest wherein a circular dielectri window is positioned between two semicircular and sem rectangular waveguide portions in a rectangular way: guide transmission line.
  • Still another feature of the present invention is the prt vision of a novel waveguide window assembly wherein dielectric window is positioned in a resonance structur which will support desired and undesired resonant mode and conduction means are provided orthogonal to the elec tric field lines of the desired resonant mode whereby ur desired resonant modes are suppressed.
  • Still another feature of the present invention is th provision of a novel waveguide window assembly wherei current attenuating means are provided in the paths the currents of undesired modes without substantially a tenuating the currents of the desired mode whereby undc sired modes will be suppressed.
  • FIG. 1 is a longitudinal view showing the multicavit klystron amplifier apparatus of the present invention
  • FIG. 2 is an enlarged cross sectional view of a portion E the structure of FIG. 1 delineated by the line 22,
  • FIG. 3 is a cross sectional view of a portion of the ructure of FIG. 2 taken along the line 3-3 in the di- :ction of the arrows,
  • FIG. 4 is an enlarged cross sectional view of a portion E the structure of FIG. 3 taken along line 4-4 in the lrection of the arrows,
  • FIG. 5 is a reduced cross sectional view of a portion E the structure shown in FIG. 2 taken along line 55 in re direction of the arrows,
  • FIG. 6 is a cross sectional view of a portion of the ructure shown in FIG. 5 taken along line 66 in the irection of the arrows,
  • FIG. 7 is an end view, partially broken away, of a poron of the structure shown in FIG. 1 taken along line 7 in the direction of the arrows,
  • FIG. 8 is an enlarged cross sectional view of a portion E the structure shown in FIG. 7 taken along line 8-8 l the direction of the arrows,
  • FIG. 9 is a side view of an alternative output window :sign.
  • FIG. 10 is a fragmentary view of FIG. 8 delineated y lines 10-10 depicting the septum mode suppression nbodiment.
  • a segmented tbular cathode assembly 11 provides a source of elecons which are formed into a pencil-like beam and procted longitudinally of the tube apparatus.
  • a plurality E circular cavity resonators including an input cavity 2, second, third, and fourth buncher cavities 13, 14, and 5 and an output cavity 16 are centrally apertured to al- IW the passage of the pencil-like beam of electrons theretrough.
  • Each of the cavity resonators 12-16 is tunable over wide range via a novel tuner assembly 17 which will 3 more fully described below.
  • the beam after passing trough the output cavity resonator 16 is collected in a )llector assembly 18.
  • The-thermal energy generated by re impinging electrons within the collector 18 is carried way by a fluid coolant circulated through the collector Ssembly 18.
  • RF signal energy which it is desired to amplify, is :d to the input cavity 12 via a vacuum sealed coaxial annector 19.
  • the signal energy velocity modulates the earn as it passes through the input cavity 12.
  • the velocity iodulation of the beam is transformed into current denty modulation in the drift space between the input cavity 2 and the first buncher cavity 13.
  • Buncher cavity resona- )rs 13, 14, and further velocity modulate the beam produce greater current density modulation of the beam t the output cavity 16.
  • the output cavity 16 extracts R.F. Jergy from the current density modulated beam.
  • the output R.F. energy is coupled outwardly of the utput cavity 16 via a rectangular waveguide 21 and fed a suit-able load, not shown, such as, for example, an ntenna.
  • the waveguide 21 is sealed in a vacuum-tight tanner by a novel vacuum window assembly 22 which is escribed in greater detail below.
  • a segmented magnetic )lenoid 23 shown in phantom circumscribes the central art of the tube apparatus, containing the cavity resonaars, for providing a strong axial magnetic field longiidinally of the tube from an anode pole piece 24 adjaent the cathode assembly 11 to a collector pole piece 5 adjacent the collector assembly for confining the penil-like beam of electrons.
  • a capacitive tuner plate 31 as of, for example, :ainless steel and in the form of the top and sides of a fapezoid is supported on one closed end of a flexible ietallic bellows 32 as of, for example, stainless steel.
  • a nut 33 as of, for example, stainless steel for attaching the novel tuner actuating means described in detail below.
  • the bellows 32 is secured in a vacuum-tight manner to one end of apunched (hydroformed) bellows support cup 34 as of, for example, stainless steel, which surrounds the portion of the bellows 32 extending outside the cavity resonator.
  • the opposite end of the bellows support cup 34 is flared and cut to conform to the cylindrical outside surface of a flanged open ended, punched, main cavity cup' 35 as of, for example, stainless steel the axis of which is aligned with the axis of the electron tube.
  • the bellows support cup 34 is secured to the main cavity cup 35 in a vacuumtight manner such as by brazing.
  • the main cavity cup 35 is apertured within the bellows support cup 34 to receive the bellows 32 in the cavity resonator.
  • a mounting ring 36 as of, for example, stainless steel, is secured to the base of the bellows support cup 34 for securing the tuner actuating mechanism onto the bellows support cup 34.
  • the bottom end of the main cavity cup 35 is apertured, and the flanged top open end of the cup 35 is closed by an apertured cavity header disc 37 as of, for example, stainless steel.
  • Drift tubes 38 such as copper, project into the cavity through the apertures in the main cavity cup 35 and the header disc 37 to provide an interaction gap substantially midway of the cavity.
  • a flanged open ended, punched, coolant cavity cup 39 as of, for example, stainless steel, apertured in its base has its base secured such as by brazing to the base of the main cavity cup 35 surrounding the drift tube 38 and its flanged open end secured, such as by brazing, to the header disc 37 of the next adjacent cavity.
  • the coolant cavity cup 39 is divided along a diameter by a septum 41 as of, for example, stainless steel, and is provided with inlet and outlet coolant fluid fittings 42 and 43, respectivcly, for passing a coolant fluid therethrough.
  • the septum 41 is made up by a segment on each side of the drift tube 38.
  • Each segment is made up of two partially overlapping pieces 41' and 41" which are initially secured to the coolant cavity cup 39 and the heater disc 37, respectively, during fabrication of the tube.
  • the segment pieces 41 and 41" are then joined together, as by brazing, during construction of the cavity subassembly and allow for different tolerances in the parts of the cavity subassembly.
  • each drift tube 38 longitudinal grooves 44 are cut extending from adjacent one end of the drift tube 38 to adjacent the other end thereof.
  • An annular groove 45 is provided adjacent each end of the drift tubes 38 connecting all of the longitudinal grooves 44.
  • a sleeve 46 of the same material as the drift tubes 38 is slid over each end of the drift tubes 38 which project into one of the cavities, and the sleeves 46 are secured to the drift tubes 38 in a vacuum-tight manner thereby defining fluid coolant channels in the grooves 44 and 45.
  • a radial projecting ridge 47 is provided at one end of each drift tube 38 so that one of the two sleeves 46 for each drift tube can be slid over the drift tube 38 and seated against the ridge 47 before the drift tube 38 is inserted into the apertures in the main cavity cup 35, the coolant cavity cup 39, and the cavity header disc 37 at which time the other sleeve 46 is added.
  • cooling fluid directed by the inlet fitting 42 into the coolant cavity cup 39 which is divided into two separated sides by the septum 41, passes through the longitudinal grooves 44 to the ends of the drift tube 38, passes around the ends of the drift tube 38 by means of the annular grooves 45, and passes down the other side of the drift tube 38 through the longitudinal grooves 44 to the other side of the coolant cavity cup 39 and out the outlet fitting 43.
  • the mutually opposing free end portions of the drift tubes 38 within the cavities are provided with serrations 48 to prevent occurrence of multipactor which would adversely effect the power output of the tube apparatus.
  • the novel cavity construction permits easy assembly of rugged individual cavity subassem'blies in the manner set forth below, and then these cavity subassemblies are joined together to form the rugged integral body assembly.
  • the individual cavity subassemblies are formed by first joining, as by spot welding, the septum pieces 41 and the water fittings 42 and 43 to the coolant cavity cup 39.
  • the coolant cavity cup 39 is then joined, as by spot welding, to the main cavity cup 35 which has joined thereto, as by spot welds, the bellows support cup 34 with the mounting ring 36 secured thereto.
  • the cavity header disc 37 with the septum pieces 41 secured thereto as by spot welds is secured, as by spot welding, over the open end of the coolant cavity cup 39.
  • This entire assembled structure is then sealed together in a vacuum-tight manner as by brazing in a furnace.
  • the drift tube 38 with one sleeve 46 positioned thereon abutting the ridge 47 is slid through the apertures in the main cavity cup 35, the coolant cavity cup 39, and the header disc 37 and the other sleeve 45 positioned thereon. Then the bellows 32 with the tuner plate 31 and the nut 33 joined thereto, as by spot welds and then brazes, is secured to the bellows support cup 34 as by an RF braze to complete the cavity subassembly. The required number of these cavity subassemblies are secured together to form the body assembly of the tube.
  • the tuner actuating mechanism includes a cup-shaped tuner support 51 as of, for example, cast bronze, which is fixedly secured at its open end in a water-tight manner to the mounting ring 36 by a plurality of bolts 52 and an O-ring 53.
  • the tuner support 51 is provided with a re-entrant opening 54) adapted to slideably receive therein the bellows 32 and the bellows support cup 34, and the tuner support 51 also includes a hollow cylindrical tuner bearing support portion 54- axially thereof which extends within the bellows 32.
  • the re-entrant opening 50 is enlarged outside the bellows support cup 34, inside the bellows 32, and at the outer end of the bellows support cup 34 and the bellows 32 (see FIGS. 3 and 4).
  • Inlet and outlet coolant fluid fittings 55 and 56, respectively, are provided on the tuner support 51 and communicate with these enlarged portions of the opening 50.
  • a stepped diameter bore is provided within the tuner bearing support portion 54 of the tuner support 51, and a hollow tuner bearing member 57 as of, for example, bronze, with a threaded bore therethrough and with a stepped diameter exterior surface is inserted within the bore of the tuner support 51.
  • One end of the tuner bearing member 57 is screwed into the nut 33 on the closed end of the bellows 32.
  • a sealing plug 58 such as Teflon is inserted within the tuner bearing member 57 and a metallic set screw 59 is screwed within the threaded bore in the tuner bearing member 57 to compress the plug 53 thereby locking the tuner bearing member 57 to the nut 33 and creating a water-tight seal.
  • a hollow cylindrical bushing 61 such as Teflon, is contained within the end of the tuner bearing support portion 54 of the tuner support 51 by means of a metallic snap ring 62 thereby providing a sliding bearing surface for the tuner bearing member 57 within the tuner support 51.
  • a tuner drive screw 63 as of, for example, stainless steel, threadably engages the threads in the bore through the tuner bearing member 57 for moving the tuner plate 31 in and out of the cavity.
  • the outer end of the tuner drive screw 63 is captured against rectilinear translation by a shoulder in the here through the tuner support 51 and by a metallic snap ring 64.
  • the dummy is removed and the tuner actua in mechanism can be secured thereto by bolting tl tuner support 51 to the mounting ring 36, screwing tl tuner bearing member 57 into the nut 33, locking tl tuner bearing member with the nut 33 by means of tl sealing plug 58, and then screwing the tuner drive scre 63 into the tuner bearing member 57 and locking tl drive screw 63 in place with the snap ring 64.
  • the cooling fluid wi cool the entire tuner mechanism without coming in CO1 tact with the critical moving parts.
  • a removable tunabi mechanism can also be provided by threading the of the tuner bearing member 57 immediately adjacei the closed end of the bellows 32 and providing an on wardly threaded stub instead of the nut 33 for screwin and locking the tuner bearing member 57 to the bac side of the closed end of the bellows 32.
  • coolant fl-uid suc as water
  • the inlet fitting 55 around th bellows support cup 34 and the bellows 32, down th bellows 32 to the closed end of the bellOWs where passes to the other side of the bellows and out the on let fitting 56.
  • Some of the coolant fluid will travel aroun the convolutions of the bellows so that the entire bellow 32 is in direct contact with the coolant fluid.
  • the output drift tube 38' tapers outwardly in the direction of the collectc assembly 18 to decrease interception of the divergin electron beam and is fluid-cooled by means of longi tudinal and annular grooves 44 and 45, respectively similar to those on the drift tubes 38 of the other cavities
  • the tuner plate 31 in the output cavity 16 is semicircula in cross section better to conform to the field pattern within the cavity.
  • the bellows 32' is in the form of a open ended, hollow cylinder and the base end of th cylinder is connected directly to the drift tube 31' 0 providing direct cooling of the tuner plate 31.
  • the nu 33 is secured directly on the back of the tuner plat 31.
  • the output cavity cup 35' is open ended and reverse. in direction from those of the other cavities of the tub whereby the output cavity 16 and collector pole piec 25 can be assembled together in one subassembly. Thi subassembly can then be mounted on the stack of othe cavity assemblies and then the collector assembly 1: mounted thereon.
  • an iris opening 71 is milled in the side of the output cavity cup 35 ad jacent the collector pole piece 25 for coupling electro magnetic energy out of the output cavity 16.
  • the sidi walls 72 of the output rectangular waveguide 21 art connected to the output main cavity cup 35' via taperet wall sections '73 which make an angle A with the wave guide side walls 72 and along with flat end walls 71 reduce the wide dimension of the waveguide 21 to tht size of the output cavity 15.
  • the waveguide 21 is ZllSt provided with a step transformer 74 between the outpu cavity 16 and the window assembly 22 (see FIGS. j and 2).
  • the shunt impedance of the output cavity drif tube gap and the coupling of the iris 71 vary across the tuning range of the electron tube.
  • a certain fixed outpu gap impedance is required over the tuning range of the tube for optimum power transfer from the output cavit3 16 to the output waveguide 21.
  • the tapered walls 73 provide a frequency-dependent impedance at the waveguide side of the iris slot 71 which compensates for the tfect of the tuner and maintains the output gap imedance substantially constant over the frequency range f the tube.
  • the height of this waveguide with the tapered alls 73 is then matched to regular waveguide sizes with re step transformer 74.
  • Changing the angle of the tapered wall sections 73 hanges their characteristic frequency-dependent impednce, and, thus, there is an optimum angle for any given lb. This angle can be determined by cut and try methds.
  • the taper of these walls 73 effects the shunt reactive omponent presented to the iris 71 and also effects the :ngth of the first section of the step transformer 74. or the type of tube illustrated here which operates at center frequency of 870 me. with more than 26% andwidth and power output greater than 100 kc.
  • CW 1e tapered wall sections 73 make an angle A of approxi lately 145 with the waveguide side walls '72.
  • the solenoid 23 is able to come closer o the output pole piece 25 so that more uniform mag- .etic field strength is maintained in the output gap region or better beam focusing, and also a direct line is preented between the output cavity drift tube gap and the vindow assembly 22 to protect the window assembly rom electron bombardment.
  • cooling members 75 of ligh heat conductive materials such as copper are posiioned along the side of the iris opening 71 to conduct he beat to the base of the output waveguide 21.
  • Coolingizid channels 76 are positioned around the output cavity .6 adjacent the pole piece 25 and in direct contact with he base of the waveguide 21 for conducting heat from he output cavity cup and the cooling members 75.
  • the cooling fluid for the body cooling of the tube ncluding the drift tube cooling, the tuner cooling and the ris cooling is supplied to the tube apparatus at the contector 77 (see FIG. 1) which directs the fluid to a maniold 78. From the manifold 78 fluid is piped to the inlet itting 42 of the coolant cavity cup 39 for the input cavity .2, to the inlet fitting 55 of the tuner assembly 17 for avity 14, and to the inlet fitting (not shown) of the :ooling fluid channels 76. The cooling fluid from the nput cavity coolant cavity cup 39 is piped on to other .avities and the cooling fluid from the cavity 14 tuner tssembly 17 is piped on to other tuner assemblies.
  • Structural support is provided for the output waveguide 51 by a metallic angle bar 79, as of, for example, steel, vhich extends across the long side of the waveguide 21 see FIG. 1).
  • the novel window tssembly 22 which seals the output waveguide 21 includes t circular, gas-tight, wave permeable window 81 as of, or example, aluminum oxide (A1 0 or quartz or other lielectric and whose diameter is less than the diagonal )I largest dimension of the rectangular waveguide 21.
  • the window 81 is sealed in a vacuum-tight manner to an innular window support cup 82 as of, for example, iovar, which is joined at its periphery as by welding to in annular flange member 83 as of, for example, Kovar.
  • lhe flange member 83 is mounted as by brazing on an txially projecting annular shoulder portion 84 of a first vide, annular, waveguide mounting flange 85 as of, for :xample, stainless steel.
  • This first mounting flange 85 is iolted to a second wide, annular, waveguide mounting iange 86 as of, for example, aluminum, with the window 51, its support cup 82 and the flange member 83 supported inder compression therebetween.
  • each of the waveguide mounting flanges 35 and 8d opposite from the window 81 are respectively mounted, as by brazing, one end of high impedance waveguide sections 87 and 88 as of, for example, stainless steel and aluminum, respectively.
  • These waveguiding sections 87 and 88 have a higher characteristic impedance than the waveguide 21.
  • the other end of waveguide section 87 is joined as by brazing to the rectangular waveguide 21 while the other end of waveguide section 88 is joined as by brazing to an output waveguide flange 89 as of, for example, aluminum.
  • These high impedance waveguide sections 87 and 88 are shaped in cross section to conform to at least the largest portions of both the rectangular waveguide 21 and the inner surfaces of the output waveguide flange 89 and the waveguide mounting flanges and 86. Therefore, the cross section of these high impedance waveguide sections 87 and 88 is a rectangle 91 with circular portions 92 centered in and extending outwardly from the long sides thereof.
  • the window 81 its supporting structure including the mounting flanges 85 and 86, and the high impedance waveguide sections 87 and 88 form a resonant structure which will support undesired resonant modes as well as transmitting the desired mode.
  • Mode suppression means are provided in the region adjacent the window 81 to prevent the existence of undesired resonant modes which will cause leaks in the window assembly or cause the window to crack.
  • a round metallic conducting bar 95 as of, for example, aluminum, is positioned in the middle of the rectangular portion 91 of the high impedance waveguide 87 across the long dimension thereof. This bar is orthogonal to the electric field lines of the dominant mode propagated by the circular window, i.e., the TE mode.
  • the window assembly undesired resonant modes which have electric field lines that have components tangent to the bar 95 will be perturbed and thereby displaced in frequency by the bar 95.
  • the bar 95 is positioned as near to the center of the window 81 as possible but the bar 95 can be placed anywhere in the region of the window to be effective.
  • the bar 95 is positioned in the waveguide section 87 outside the vacuum envelope of the tube so that it can be adjusted or plated with material without effecting the vacuum within the tube.
  • the bar 95 could take the form of a wide septum extending in the direction of wave propagation in waveguide section 87 as shown in FIG. 10.
  • a window assembly 22 constructed in the manner shown in FIGS. 7 and 8 will pass high powers over a 36% mode-free frequency band centered on a frequency of 865 me.
  • bar 95 being a metallic conductor it could be made of lossy material or coated with lossy material such as Kanthal to attenuate rather than to perturb undesired modes. Such attenuation means could also be positioned elsewhere in the path of the electric currents of undesired modes but so as not to attenuate the currents of the desired mode.
  • This mode suppression means could also take other forms such as metallic wires, strips, or a layer of metal particles 95' positioned directly on or plated on the window 81 as shown in FIG. 9. Such mode suppression means would also serve the purpose of conducting away from the window surface charges which might have a tendency to puncture the window.
  • the mode suppression means could take the form of attenuation means such as lossy strips (not shown) positioned so as to absorb wall currents of undesired modes or coupling means such as slots 97 (see FIG. 9) to couple the energy of undesired modes out of the region of the Waveguide window.
  • the attenuation and coupling means should be positioned so as to reduce the power in the desired dominant mode as little as possible.
  • the window assembly described above provides several advantages over prior art high power, broadband, circular waveguide windows of this general type constructed according to the teachings of the U.S. Patent 2,958,834.
  • certain waveguide resonant modes can be perturbed or attenuated by mode suppression means in the form of electric conductors or attenuators positioned orthogonal to the electric field lines of the dominant mode.
  • mode suppression means in the form of electric conductors or attenuators positioned orthogonal to the electric field lines of the dominant mode.
  • the reduction of the diameter of the circular window 81 below the length of the diagonal of the rectangular waveguide shifts the frequency of certain resonant modes in the window assembly.
  • a typical resonant mode shifted in frequency in this manner is the mode similar to the TE mode in a circular cylindrical resonator.
  • a pair of capacitive bars 101 and 132 are provided along the long side of the waveguide 21 and are machined in the output waveguide flange 89 at the junctions between the waveguide 21 and the flange 89 and the high impedance waveguides 87 and 88, respectively, to provide the net capacitive discontinuity as taught in U.S. Patent 2,958,834 referred to above.
  • High frequency tube apparatus including,
  • (c) means spatially disposed apart along said beam path for producing successive electromagnetic interaction with said beam and for extracting high frequency energy from said beam
  • a tuner mechanism for accurately adjusting the pos tion of a movable tuner means mounted on a flexibI wall of a cavity resonator comprising, in combinatiol (a) an externally threaded tuner drive screw,
  • tuner support means for supporting said tune drive screw and said bearing member, said SHPPO] means adapted to be supported on said cavity resonz tor and to retain said tuning screw against rectilinea motion, and
  • means for securing and locking said bearing merr her to said flexible wall including threaded mean for screwing said tuner bearing member to sai flexible Wall, a deformable member slideably in serted within said bearing member to the end thereo adjacent the flexible wall and means for applyin pressure to said deformable member to lock sail tuner bearing member to said flexible wall such that a fluid tight seal is created between said tuner bear ing member and said flexible wall.
  • a fluid cooled tuner mechanism for accurately ad justing the position of a movable tuner means of a cavit resonator comprising, in combination,
  • tuner actuating means positioned within said bear ing support portion for providing motion to sait bellows and thus said tuner means
  • (g) means for introducing a cooling fluid in one side of said chamber region and extracting said cooling fluid from another side thereof, said cooling fluid coming in contact with said bellows.
  • High frequency tube apparatus including (a) means for producing and directing a beam of charged particles over a predetermined path longitudinally of the tube,
  • (0) means spatially disposed apart along said beam path for producing successive electromagnetic inter action with said beam and for extracting high frequency energy from said beam including,
  • a tunable output cavity resonator provided with an interaction gap therein and an output iris in a wall thereof for extracting radio frequency energy therefrom
  • a gas tight wave permeable window assembly diiensioned for passing wave energy therethrough over a ertain passband of frequencies including,
  • selective mode suppression means positioned within said resonant waveguide structure in the immediate vicinity of said wave permeable dielectric window member for suppressing undesired modes within the passband of frequencies of said window member, which modes have maximum field strengths at said window.
  • a high frequency tube apparatus including (a) means for producing and directing a beam of charged particles over a predetermined path longitudinally of the tube,
  • (c) means spatially disposed apart along said beam path for producing successive electromagnetic interaction with said beam and for extracting high frequency energy from said beam
  • said means for extracting wave energy from the beam including an electromagnetic wave permeable window positioned in a resonant structure which supports desired and undesired modes, and mode suppression means positioned orthogonal to the field lines of the desired mode whereby undesired modes will be suppressed within the frequency band of the tube apparatus, said mode suppression means being disposed in the immediate vicinity of said window for suppressing undesired resonant modes within the passband of said window which modes have maximum field strengths at said window.
  • the mode suppression means includes conduction means positioned orthogonal to the electric field lines of the desired mode of propagation through said wave permeable window assembly for suppressing undesired modes within the passband of frequencies of the window assembly.
  • the mode suppression means includes attenuating means for attenuating the currents of undesired modes without substantially attenuating currents of the desired mode of propagation through said wave permeable window assembly whereby undesired modes are suppressed within the passband of frequencies of the window assembly.
  • the mode suppression means includes coupling means for coupling energy out of undesired modes without coupling substantial energy out of the desired mode of propagation through said wave permeable window assembly whereby undesired modes are suppressed within the passband of frequencies of the window assembly.
  • High frequency tube apparatus comprising, in combination,
  • waveguide means for directing energy from said means for producing interaction with and extracting energy from said beam including:
  • second and third tubular waveguiding means positioned on either side of said first means forming a portion of a waveguide
  • said gas tight wave permeable window having a major dimension less than the greatest dimension of said fourth waveguiding means
  • said second and third tubular waveguiding means having a cross section conforming to at least the largest portions of both said first means forming a portion of a waveguide and said fourth waveguiding means.
  • a gas tight wave permeable window assembly dimensioned for passing wave energy therethrough over a certain passband of frequencies, comprising in combination,
  • said third waveguiding means adapted to be joined to a fifth waveguiding means similar to said fourth waveguiding means
  • said second and third waveguiding means having a cross section conforming to at least the largest portions of both said first waveguiding means and said fourth waveguiding means.
  • said first means forming a portion of a waveguide, second, and third waveguiding means comprise a resonant structure which supports desired and undesired modes and including mode suppression means positioned within said resonant waveguide structure for suppressing undesired modes within the passband of frequencies of the window assembly.
  • first means forming a portion of a waveguide, second, and third waveguiding means comprise a resonant structure which supports desired and undesired modes and including mode suppression conducting means positioned orthogonal to the electric field lines of the desired mode of propagation through said wave permeable window assembly for suppressing undesired modes within the passband of frequencies of the window assembly.
  • said first means forming a portion of a waveguide, second, and third waveguiding means comprise a resonant structure which supports desired and undesired modes and including mode suppression attenuating means for attenuating the cur- 13 rents of undesired modes without substantialy attenuating currents of the desired mode of propagation through said wave permeable window assembly whereby undesired modes are suppressed within the passband of frequencies of the window assembly.
  • High frequency tube apparatus including (A) means for producing and directing a beam of charged particles over a predetermined path longitudinally of the tube;
  • (B) means for collecting the beam at the terminating end of the beam path
  • a vacuum tight envelope enclosing the beam path including (1) a plurality of metallic cup members, said members of said plurality of metallic cup members having bases on the one end thereof and having outwardly directed flanges,
  • (D) means spatially disposed apart along with said beam path for producing successive electromagnetic interaction with said .beam and for extracting high frequency energy from said beam including 1) tunable cavity resonator means including (a) a flexible cavity resonator wall,
  • output waveguide means communicating with said cavity resonator through said output iris and including (a) tapered wall portions having a frequency dependent characteristic which compensates for changes occurring due to tuning of the output cavity resonator in order to keep the gap impedance in the output cavity resonator constant over the tuning band of the tube,
  • said first, second and third waveguiding means comprising a resonant Stl'llCtllI't which supports desired and undesirer modes
  • mode supression means positioned Withir said resonant waveguide structure for sup pressing undesired modes within the pass band of frequencies of the window assem bly.
  • sair drift tubes have a plurality of cooling channels extending along the length thereof and said cooling channels being adapted and arranged such that cooling fluid will flov bidirectionally along the length of said cooling channels 17.
  • a waveguide window structure including a sectior of circular waveguide and means for establishing a broad band, strong hermetic seal across said section of circulai waveguide, said window structure further comprising,
  • a disc of dielectric material disposed transversely acros: said circular waveguide section and sealed along it: periphery to said waveguide section,
  • said disc being permeable to electromagnetic waves ant impervious to fluids
  • a longitudinally extending septum extending within sait circular waveguide along a diametral plane of saic circular waveguide and said dielectric disc, saic septum disposed in the immediate vicinity of saiC dielectric disc such that undesired modes in the pass band of said window are suppressed
  • HERMAN KARL SAALBACH Primary Examiner.
  • GEORGE N. WESTBY Examiner. S. CHATMON, JR., Assistant Examiner.

Landscapes

  • Microwave Tubes (AREA)
  • Particle Accelerators (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)
  • Discharge Lamps And Accessories Thereof (AREA)
  • Waveguide Connection Structure (AREA)
US15641661 1961-12-01 1961-12-01 Klystron device having fluid cooled tunable cavities and output window mode suppression means Expired - Lifetime US3325671A (en)

Priority Applications (12)

Application Number Priority Date Filing Date Title
NL285748D NL285748A (xx) 1961-12-01
US15641661 US3325671A (en) 1961-12-01 1961-12-01 Klystron device having fluid cooled tunable cavities and output window mode suppression means
GB701864A GB998595A (en) 1961-12-01 1962-11-22 Window assembly for microwave devices
GB701764A GB998594A (en) 1961-12-01 1962-11-22 Window for microwave devices
GB701664A GB998593A (en) 1961-12-01 1962-11-22 Tuner mechanisms for cavity resonators
GB4425962A GB998592A (en) 1961-12-01 1962-11-22 Electron discharge device
JP38021322A JPS4929778B1 (xx) 1961-12-01 1962-11-27
DEV29239A DE1298169B (de) 1961-12-01 1962-11-30 Gasdichte wellendurchlaessige Fensteranordnung fuer Hochfrequenz-Hohlleiter
FR917235A FR1345258A (fr) 1961-12-01 1962-11-30 Dispositif à décharge électronique du type klystron
DE19651466578 DE1466578B2 (de) 1961-12-01 1965-07-28 Kuehlmitteldurchstroemte abstimmvorrichtung zum einstellen einer im hohlraumresonator eines klystrons angeordneten abstimmplatte
SE303966A SE318018B (xx) 1961-12-01 1966-03-08
NL7210685A NL7210685A (xx) 1961-12-01 1972-08-03

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15641661 US3325671A (en) 1961-12-01 1961-12-01 Klystron device having fluid cooled tunable cavities and output window mode suppression means

Publications (1)

Publication Number Publication Date
US3325671A true US3325671A (en) 1967-06-13

Family

ID=22559484

Family Applications (1)

Application Number Title Priority Date Filing Date
US15641661 Expired - Lifetime US3325671A (en) 1961-12-01 1961-12-01 Klystron device having fluid cooled tunable cavities and output window mode suppression means

Country Status (7)

Country Link
US (1) US3325671A (xx)
JP (1) JPS4929778B1 (xx)
DE (2) DE1298169B (xx)
FR (1) FR1345258A (xx)
GB (4) GB998594A (xx)
NL (2) NL7210685A (xx)
SE (1) SE318018B (xx)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3412283A (en) * 1965-10-15 1968-11-19 Westinghouse Electric Corp Coaxial magnetron in which the anode is welded to the body
US4216409A (en) * 1977-11-25 1980-08-05 Nippon Electric Co., Ltd. Multi-cavity klystron device
US20070080762A1 (en) * 2004-11-04 2007-04-12 Communications & Power Industries, Inc. L-band inductive output tube
US20090261760A1 (en) * 2005-09-26 2009-10-22 National Institute Of Radiological Sciences H-mode drift-tube linac and design method therefor

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1541027C2 (de) * 1966-12-24 1970-08-20 Philips Patentverwaltung Mehrkammerklystron
JPS515336U (xx) * 1974-06-27 1976-01-16
JPS5313048U (xx) * 1976-07-15 1978-02-03
RU2150766C1 (ru) * 1999-07-19 2000-06-10 Петров Дмитрий Михайлович Многолучевой регенеративный усилитель электромагнитных колебаний

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2218331A (en) * 1938-01-28 1940-10-15 Fides Gmbh Grid-controlled discharge tube
US2263184A (en) * 1940-10-09 1941-11-18 Westinghouse Electric & Mfg Co Tuning device
US2806976A (en) * 1952-11-26 1957-09-17 Karl G Hernqvist Impedance matching device
US2817823A (en) * 1953-12-11 1957-12-24 Ernest C Okress Circular waveguide output for magnetrons
US2820924A (en) * 1954-01-28 1958-01-21 Litton Industries Inc Magnetron output coupler
US2849644A (en) * 1953-05-15 1958-08-26 Bell Telephone Labor Inc Electron discharge devices
US2892986A (en) * 1953-06-11 1959-06-30 Ernest C Okress Waveguide polarization locking device
US2947908A (en) * 1958-04-15 1960-08-02 Litton Ind Of California Output structure for electron discharge devices employing cavity resonators
US2949559A (en) * 1958-01-31 1960-08-16 Eitel Mccullough Inc Klystron tube
US2963616A (en) * 1955-07-08 1960-12-06 Varian Associates Thermionic tube apparatus
US3028519A (en) * 1959-01-02 1962-04-03 Varian Associates High frequency tube apparatus and coupled cavity output circuit therefor
US3078385A (en) * 1954-07-20 1963-02-19 Eitel Mccullough Inc Klystron

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1025515A (fr) * 1950-10-05 1953-04-16 Csf Perfectionnements aux filtres pour ultra-hautes fréquences
GB807557A (en) * 1956-01-04 1959-01-14 Gen Electric Co Ltd Improvements in or relating to apparatus of the kind including a waveguide
DE1048301B (xx) * 1956-06-13
US2958834A (en) * 1956-06-13 1960-11-01 Varian Associates Sealed wave guide window
FR1212051A (fr) * 1958-03-18 1960-03-22 Thomson Houston Comp Francaise Perfectionnements aux fenêtres étanches pour guide d'ondes

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2218331A (en) * 1938-01-28 1940-10-15 Fides Gmbh Grid-controlled discharge tube
US2263184A (en) * 1940-10-09 1941-11-18 Westinghouse Electric & Mfg Co Tuning device
US2806976A (en) * 1952-11-26 1957-09-17 Karl G Hernqvist Impedance matching device
US2849644A (en) * 1953-05-15 1958-08-26 Bell Telephone Labor Inc Electron discharge devices
US2892986A (en) * 1953-06-11 1959-06-30 Ernest C Okress Waveguide polarization locking device
US2817823A (en) * 1953-12-11 1957-12-24 Ernest C Okress Circular waveguide output for magnetrons
US2820924A (en) * 1954-01-28 1958-01-21 Litton Industries Inc Magnetron output coupler
US3078385A (en) * 1954-07-20 1963-02-19 Eitel Mccullough Inc Klystron
US2963616A (en) * 1955-07-08 1960-12-06 Varian Associates Thermionic tube apparatus
US2949559A (en) * 1958-01-31 1960-08-16 Eitel Mccullough Inc Klystron tube
US2947908A (en) * 1958-04-15 1960-08-02 Litton Ind Of California Output structure for electron discharge devices employing cavity resonators
US3028519A (en) * 1959-01-02 1962-04-03 Varian Associates High frequency tube apparatus and coupled cavity output circuit therefor

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3412283A (en) * 1965-10-15 1968-11-19 Westinghouse Electric Corp Coaxial magnetron in which the anode is welded to the body
US4216409A (en) * 1977-11-25 1980-08-05 Nippon Electric Co., Ltd. Multi-cavity klystron device
US20070080762A1 (en) * 2004-11-04 2007-04-12 Communications & Power Industries, Inc. L-band inductive output tube
US20090261760A1 (en) * 2005-09-26 2009-10-22 National Institute Of Radiological Sciences H-mode drift-tube linac and design method therefor
US7868564B2 (en) * 2005-09-26 2011-01-11 National Institute Of Radiological Sciences H-mode drift-tube linac and design method therefor

Also Published As

Publication number Publication date
DE1466578B2 (de) 1971-07-22
DE1298169B (de) 1969-06-26
GB998594A (en) 1965-07-14
NL7210685A (xx) 1972-10-25
GB998592A (en) 1965-07-14
JPS4929778B1 (xx) 1974-08-07
SE318018B (xx) 1969-12-01
GB998593A (en) 1965-07-14
FR1345258A (fr) 1963-12-06
DE1466578A1 (de) 1969-02-27
GB998595A (en) 1965-07-14
NL285748A (xx) 1900-01-01

Similar Documents

Publication Publication Date Title
US4480210A (en) Gridded electron power tube
US2994009A (en) High frequency tube apparatus
US5767625A (en) High frequency vacuum tube with closely spaced cathode and non-emissive grid
RU2160943C2 (ru) Электронно-лучевая трубка с линейным выходом
EP0181214B1 (en) Beam tube with density plus velocity modulation
US3310704A (en) Output coupling circuit for microwave tube apparatus
US3325671A (en) Klystron device having fluid cooled tunable cavities and output window mode suppression means
US3876901A (en) Microwave beam tube having an improved fluid cooled main body
US5691667A (en) RF radiation absorbing material disposed between the cathode and anode of an electron beam tube
US3227915A (en) Fluid cooling of hollow tuner and radio frequency probe in klystron
US3028519A (en) High frequency tube apparatus and coupled cavity output circuit therefor
US3614518A (en) Microwave tuner having sliding contactors
US3070725A (en) Travelling wave amplifier
US3305742A (en) High frequency electron discharge device and cooling means therefor
EP0883152B1 (en) Coaxial inductive output tube
EP0753878A1 (en) Linear electron beam tubes arrangements
US3436588A (en) Electrostatically focused klystron having cavities with common wall structures and reentrant focusing lens housings
US3231781A (en) Reverse magnetron with slot mode absorber
US3394283A (en) High frequency electron discharge device
US2994800A (en) High-power, high-frequency amplifier klystron tube
US3227916A (en) Tuning mechanism for electron discharge devices
US2929955A (en) Cavity resonator for klystron tube
US2915670A (en) Klystron amplifier
US3400295A (en) Matched transmission line coupling for electron discharge tube
Broadway et al. Velocity-modulation valves