US2607019A - Electron discharge device of the cavity resonator type - Google Patents

Electron discharge device of the cavity resonator type Download PDF

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US2607019A
US2607019A US29984A US2998448A US2607019A US 2607019 A US2607019 A US 2607019A US 29984 A US29984 A US 29984A US 2998448 A US2998448 A US 2998448A US 2607019 A US2607019 A US 2607019A
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resonators
ring
magnetron
cavity resonator
cavity
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US29984A
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Wellesley J Dodds
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RCA Corp
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RCA Corp
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    • 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
    • H01J23/18Resonators
    • H01J23/22Connections between resonators, e.g. strapping for connecting resonators of a magnetron
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J25/00Transit-time tubes, e.g. klystrons, travelling-wave tubes, magnetrons
    • H01J25/50Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field
    • H01J25/52Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field with an electron space having a shape that does not prevent any electron from moving completely around the cathode or guide electrode
    • H01J25/58Magnetrons, i.e. tubes with a magnet system producing an H-field crossing the E-field with an electron space having a shape that does not prevent any electron from moving completely around the cathode or guide electrode having a number of resonators; having a composite resonator, e.g. a helix
    • H01J25/587Multi-cavity magnetrons

Definitions

  • the generated frequency is determined largely by the form and dimensions of the cavity resonator structure, as distinguished from earlier magnetrons of the singleor plural anode plate types wherein'the generated frequency is determined by the distributed inductance and capacitance of the anode .circuit.
  • the resonant frequency of the cavity resonator magnetron is necessarily limited-during manufactureto a given value, or atlleast'to a rather limited range .of values.
  • the resonant frequency can be varied within certain limits after manufacture of the magnetron by deforming the cavity resonator structure or moving conducting members toward or away from the cavity resonators.
  • the cavity resonators are usually formed by conducting anode vanes or walls which extend radially inward from a cylindrical anode ring or shell and define a cylindrical cathode space at their inner ends.
  • the outer closed end of each cavity resonator constitutes a'predominantly inductive region and the inner open end constitutes-apredominantly capacitative region. 7
  • I prove adjacent either the inductive or capacitative regions one or more conducting elements movable a predetermined amount into or out of these regions in order to pre-tune the cavity magnetron to a desired frequency, either during or after manufacture thereof.
  • Fig. 1 is a transverse section, taken along the line l-l 'of Fig. 2, of a cavity resonator magnetron embodyin my invention
  • Fig. 2 is a longitudinal section taken along the line'22 of 'Fig. l
  • Figs. 3'and 4 are sections similar to Figs. 1 and 2, respectively, of a modification.
  • a cylindrical .vanetype cavity resonator-magnetron is shown in to high frequency electron discharge devices "employing cavity resonators-and particularly to such devices of the 'ma'gnetron type, although not limited .to the latter.
  • An elongated thermionic cathode” lp which may be indirectly'heated; is centrally'mounted; in insulated relation to "the anode structure, "in the cathode space "by suitable means, not "shown.
  • the cathode "4" is adapted when-heated to-supply electrons in the cathode space for-exciting the "cavity'resonators in a manner to be described.
  • the anode vanes may -be-strapped together, in order to favor operation of the magnetron in the so-called 1r mode in-which-adjacent cavityresonators oscillate at'1-80 phasediiference, by means of conductingstrapping-rings 6 and' '1.
  • the cylinder l 1 is recessed at each end as shown at 'B and er-id plates 8- are sealedto the ends of the cylinder by-suitable meanssuch as brazing.
  • the resonant frequency of the magnetron is the same for all of the resonators even though the resonators may difier slightly in shape or size.
  • a metallic tuning member or ring it is fixedly mounted in the recessed portion 9 at each end of the shell I adjacentthe lateral edges of thevanes 2, as shown. in the drawing.
  • the rings l are provided with deformable tuning elements in the form of inwardly-projecting integral lugs or tabs H each of which is disposed adjacent the rear end of a cavity resonator 3.
  • Each of the lugs H is bendable out of the plane of the ring ⁇ 0 toward or away from the corresponding cavity resonator 3. In'the drawing only one of the lugs, Ha, is shown bent into the corresponding cavity resonator 3.
  • lugs li would be bent an equal amount either toward or away from the cavity resonators, depending upon whether it is desired to increase or decrease the resonant frequency. Since the lugs H in Figs. 1 and 2 are disposed adjacent the outer ends of the cavity resonators, the change is made in the apparent inductance of the cavity resonators. Whenthe lug is bent into the cavity resonator, the apparent inductance is decreased which causes anincrease in the resonant frequency of the cavity resonator. Bending the lug out of the cavity resonator increases the apparent inductance and decreases the resonant frequency.
  • High frequency energy may be extracted from the anode cavity resonator structure by any suitable means, such :as a coupling loop 12 formin a part of a coaxial transmission line H. 4
  • the apparent capacitance of the cavity resonator may be changed by locating a tuning member or ring adjacent the inner, predominantly capacitative region of the cavity resonators.
  • This modification of the invention is shown in Figs. 3 and 4 wherein the same reference numerals are applied to the parts identical with the corresponding parts illustrated in Figs. 1 and 2. In this form,
  • bendable tuning lugs ll are provided integral with the outer strapping ring I which serves also as the tuning member.
  • the lugs Il may have th same thickness as the ring I, but preferably are made thinner, as shown in Fig. 4, to render them more flexibla
  • the cavity resonator is tuned by bending the lugs l l into or out of the cavity resonators.
  • the lugs H are bent into the cavity resonators, the apparent capacitance of the cavity resonators is increased, resulting in a decrease in the resonant frequency.
  • the lugs I I could be provided on the inner strapping ring 6 if desired.
  • the tuning ring may be incorporated in a conventional magnetron of the type shown. This may be done at the time of manufacture and assembly of the parts of the magnetron, to pre-tune the magnetron, and also to provide means for tuning the magnetron to a desired frequency after manufacture.
  • the ring may be incorporated in a magnetron of the type shown after manufacture. In either case, this structure provides a simple means for tuning the magnetron cavity resonator structure without deforming the cavity resonator structure itself, as has been done previously.
  • a convenient and easy method of setting the lugs of the tuning ring is to provide a machine having a. horizontal support for the tuning ring, or the magnetron block with the tuning ring attached, and a vertically-movable carriage having a circular series of projections arranged to engage the bendable lugs H of the tuning ring I.
  • By moving the carriage a predetermined amount it is thus possible to bend all of the lugs I l the same amount out of the plane of the ring, to pre-tune the cavity resonator structure to a predetermined desired frequency.
  • a large number of magnetrons may be tuned to the same frequency in a mass production manner'and the frequency may be changed to a different desired frequency merely by changing the limit of travel of the carriage.
  • An electron discharge device comprising a cavity resonator having predominantly inductive and capacitative regions therein determining its normal resonant frequency, and means for changing said resonant frequency comprising a conducting member rigidly mounted adjacent but outside of said resonator and having a deformable tab disposed adjacent one of said regions and bendable into or out of said one of said regions to change the reactance thereof.
  • a magnetron anode structure comprising a plurality of similar radially-extending cavity resonators closed at their outer ends and opening into a central cathode space, the closed and open ends of said resonators constituting predominantly inductive and capacitative regions, respectively, determining the normal resonant frequency of said resonators, and means for changing said resonant frequency comprising a conducting ring mounted adjacent one end of said resonators and-having deformable tabs bendable into or out of said resonators to change the reactance thereof.

Description

W. J. DODDS Aug. T12, l52
ELECTRON DISCHARGE DEVICE OF THE. CAVITY RESONATOR TYPE Filed May 29, 1948 3nventor WELLESLEY T. Dumas Gttorneg Patented Aug. 12, 1952 UN-[TED j STAT-ES "PA- 1;ENT 1 :oF F- eEi 2,607,019" v M ELECTRON DI SGHARGEiD EVICE OF-THE GAVITYRESONATQR TYPE Wellesley 3. Dodds', 'Cranbury, N. J.,*assignr"t0 Radio Corporation of America, a corporation Application May 29, 1948, SerialNo.'291,984
invention relates Itjis'the object of my invention to provide means forpre-tuningcavity resonators during or after manufacture thereof.
In magnetron oscillators of the cavity resonator type, .the generated frequency is determined largely by the form and dimensions of the cavity resonator structure, as distinguished from earlier magnetrons of the singleor plural anode plate types wherein'the generated frequency is determined by the distributed inductance and capacitance of the anode .circuit.
' Hence, the resonant frequency of the cavity resonator magnetron is necessarily limited-during manufactureto a given value, or atlleast'to a rather limited range .of values. TI-Iowever, the resonant frequency can be varied within certain limits after manufacture of the magnetron by deforming the cavity resonator structure or moving conducting members toward or away from the cavity resonators. In conventional cavity'type magnetrons the cavity resonators are usually formed by conducting anode vanes or walls which extend radially inward from a cylindrical anode ring or shell and define a cylindrical cathode space at their inner ends. The outer closed end of each cavity resonator constitutes a'predominantly inductive region and the inner open end constitutes-apredominantly capacitative region. 7
In accordance with my invention, I, prove adjacent either the inductive or capacitative regions one or more conducting elements movable a predetermined amount into or out of these regions in order to pre-tune the cavity magnetron to a desired frequency, either during or after manufacture thereof.
The novel features which I believe to' be characteristic of my invention are set forth with particularity in the appendedclaims, but the invention itself will best be understood by reference to the following description taken in con- "nection with the accompanying drawing in which Fig. 1 isa transverse section, taken along the line l-l 'of Fig. 2, of a cavity resonator magnetron embodyin my invention; Fig. 2 is a longitudinal section taken along the line'22 of 'Fig. l; and Figs. 3'and 4 are sections similar to Figs. 1 and 2, respectively, of a modification.
Referring'to Figs. 1 and 2, a cylindrical .vanetype cavity resonator-magnetron is shown in to high frequency electron discharge devices "employing cavity resonators-and particularly to such devices of the 'ma'gnetron type, although not limited .to the latter.
Claims. (Cl. 315-39) which r is a cylindricalmetarshell. providedfwith a cylindrical aperture therethrough. A series'of evenly spaced metal vanes '2 is 'atta'ched'to the shell I within said aperture toextend radially'inwardly. with the inner ends spaced from the axis of the shell *to form 'a'cylindrical" central cathode space. The vanes 2, t ogether"with the inner wall of the shell" I provide'cavityresonators 3 uniformly disposed around the": cathodespace and opening thereinto. The inner ends of the vanes -2 constitute equally 'spaced"parallel anode segments. 1
An elongated thermionic cathode" lpwhich may be indirectly'heated; is centrally'mounted; in insulated relation to "the anode structure, "in the cathode space "by suitable means, not "shown.
' End plates or hats' 'o-are provided at the ends of the cathode to serve as electrostatic shields for the ends ofthe cathode space. The cathode "4" is adapted when-heated to-supply electrons in the cathode space for-exciting the "cavity'resonators in a manner to be described.
The anode vanes may -be-strapped together, in order to favor operation of the magnetron in the so-called 1r mode in-which-adjacent cavityresonators oscillate at'1-80 phasediiference, by means of conductingstrapping-rings 6 and' '1. The ring '5, located near'theinner-en'ds or' the vanes 2'is attached to alternate vanes "and I passes freely through notches in theother alternate vanes.
Similarly, thering "I is attached to the other alternate vanes outside of the ring-"6- andpasses freely through notches in the vanes to 'which the ring 6 is attached.
In order to complete a-vacuum enclosure for the magnetron, the cylinder l 1 is recessed at each end as shown at 'B and er-id plates 8- are sealedto the ends of the cylinder by-suitable meanssuch as brazing. I
--Means for producinga magnetic iieldin I the cathode-space axially thereof 'is provided. Such the potential of the anode and the strength of the magnetic field are suitably chosen, the cloud of electrons sweeps past the anode segments at the inner end of the vanes 2 and induces radio frequency voltages in the anode segments, and an oscillatory electromagnetic field is set up in each of the cavity resonators, at a frequency determined by the apparent inductance and capacitance of the anode resonator structure. Since the resonators are coupled together through the cathode space and around the lateral edges of the vanes through the end spaces of the magnetron the resonant frequency of the magnetron is the same for all of the resonators even though the resonators may difier slightly in shape or size.
In accordance with the invention, in order to provide means for changing the resonant frequency of the cavity resonators after manufacture, a metallic tuning member or ring it is fixedly mounted in the recessed portion 9 at each end of the shell I adjacentthe lateral edges of thevanes 2, as shown. in the drawing. The rings l are provided with deformable tuning elements in the form of inwardly-projecting integral lugs or tabs H each of which is disposed adjacent the rear end of a cavity resonator 3. Each of the lugs H is bendable out of the plane of the ring {0 toward or away from the corresponding cavity resonator 3. In'the drawing only one of the lugs, Ha, is shown bent into the corresponding cavity resonator 3. However, it is understood that preferably all of the lugs li would be bent an equal amount either toward or away from the cavity resonators, depending upon whether it is desired to increase or decrease the resonant frequency. Since the lugs H in Figs. 1 and 2 are disposed adjacent the outer ends of the cavity resonators, the change is made in the apparent inductance of the cavity resonators. Whenthe lug is bent into the cavity resonator, the apparent inductance is decreased which causes anincrease in the resonant frequency of the cavity resonator. Bending the lug out of the cavity resonator increases the apparent inductance and decreases the resonant frequency.
High frequency energy may be extracted from the anode cavity resonator structure by any suitable means, such :as a coupling loop 12 formin a part of a coaxial transmission line H. 4
Instead of changing the apparent inductance, the apparent capacitance of the cavity resonator may be changed by locating a tuning member or ring adjacent the inner, predominantly capacitative region of the cavity resonators. This modification of the invention is shown in Figs. 3 and 4 wherein the same reference numerals are applied to the parts identical with the corresponding parts illustrated in Figs. 1 and 2. In this form,
bendable tuning lugs ll are provided integral with the outer strapping ring I which serves also as the tuning member. The lugs Il may have th same thickness as the ring I, but preferably are made thinner, as shown in Fig. 4, to render them more flexibla As in Fig. 1, the cavity resonator is tuned by bending the lugs l l into or out of the cavity resonators. When the lugs H are bent into the cavity resonators, the apparent capacitance of the cavity resonators is increased, resulting in a decrease in the resonant frequency. It is of course understood that the lugs I I could be provided on the inner strapping ring 6 if desired.
In either of the modifications shown the tuning ring may be incorporated in a conventional magnetron of the type shown. This may be done at the time of manufacture and assembly of the parts of the magnetron, to pre-tune the magnetron, and also to provide means for tuning the magnetron to a desired frequency after manufacture. Instead, the ring may be incorporated in a magnetron of the type shown after manufacture. In either case, this structure provides a simple means for tuning the magnetron cavity resonator structure without deforming the cavity resonator structure itself, as has been done previously.
A convenient and easy method of setting the lugs of the tuning ring is to provide a machine having a. horizontal support for the tuning ring, or the magnetron block with the tuning ring attached, and a vertically-movable carriage having a circular series of projections arranged to engage the bendable lugs H of the tuning ring I. By moving the carriage a predetermined amount it is thus possible to bend all of the lugs I l the same amount out of the plane of the ring, to pre-tune the cavity resonator structure to a predetermined desired frequency. In this way a large number of magnetrons may be tuned to the same frequency in a mass production manner'and the frequency may be changed to a different desired frequency merely by changing the limit of travel of the carriage.
While the invention has been described as applied to a cavity resonator magnetron for the purpose of illustration, the principles thereof have wider application. The invention can be applied to other electron discharge devices employing cavity resonators, for examplato velocity i modulation tubes.
Hence, it will be understood that various changes and modifications may be made Without departing from the spirit and scope of the invention as set forth in the following claims.
What I claim as new is:
1. An electron discharge device comprising a cavity resonator having predominantly inductive and capacitative regions therein determining its normal resonant frequency, and means for changing said resonant frequency comprising a conducting member rigidly mounted adjacent but outside of said resonator and having a deformable tab disposed adjacent one of said regions and bendable into or out of said one of said regions to change the reactance thereof.
2. An electron discharge device according to claim 1, wherein said deformable tab is adjacent and bendable into or out of said predominantly inductive region.
3. An electron discharge device according to claim 1, wherein said deformable tab is adjacent and bendable into or out of said predominantly capacitative region.
4 An electron discharge device comprising a series of similar adjacent cavity resonators open at one end and closed at the other, said open and closed ends constituting predominantly capacitative and inductive regions, respectively, determining the normal resonant frequency of the resonators, and means for changing said resonant frequency comprising a conducting strip mounted adjacent but outside of one end of said resonators and having a deformable tab bendable into or out of said resonators tochange the reactance thereof.
5 An electron discharge device according to claim 4, wherein said strip is mounted adjacent the closed ends of said resonators to change the effective inductance thereof.
6. An electron discharge device according to claim 4, wherein said strip is mounted adjacent the open ends of said resonators to change the efiective capacitance thereof.
'7. A magnetron anode structure comprising a plurality of similar radially-extending cavity resonators closed at their outer ends and opening into a central cathode space, the closed and open ends of said resonators constituting predominantly inductive and capacitative regions, respectively, determining the normal resonant frequency of said resonators, and means for changing said resonant frequency comprising a conducting ring mounted adjacent one end of said resonators and-having deformable tabs bendable into or out of said resonators to change the reactance thereof.
8. A magnetron anode structure according to claim 7, wherein said ring is mounted adjacent the closed ends of said resonators to change the effective inductance thereof.
9. A magnetron anode structure according to claim 7, wherein said ring is mounted adjacent the open ends of said resonators to change the effective capacitance thereof.
10. A magnetron anode structure comprising a cylindrical block having a central aperture, a plurality of spaced, radially extending anode vanes mounted in said aperture and spaced from the central axis of said block and forming an annular series of similar cavity resonators closed at their outer end and opening into a central space, the closed and open ends of said resonators constituting predominantly inductive and capacitative regions, respectively, determining the normal resonant frequency of said resonators, means comprising a conducting ring mounted adjacent one end of said resonators, and means for charging said resonant frequency comprising radially-extending deformable tabs integral with said ring and bendable into or out of said resonators to change the reactance thereof.
11. A magnetron anode structure according to claim 10, wherein said ring is connected to the lateral edges of alternate ones of said anode vanes adjacent the inner ends thereof, whereby said ring serves also as a strapping ring for favoring operation of said magnetron in the 1r-mode wherein adjacent resonators oscillate out of phase.
12. A tuning member for a cavity magnetron comprising a conducting ring having a plurality of evenly spaced integral tabs normally lying in the plane of said ring, said tabs being bendable to a position partially out of said plane.
13. A magnetron tuning member according to claim 12, wherein said tabs project inwardly from said ring.
14. A magnetron tuning member according to claim 12, wherein said tabs project outwardly from said ring.
15. A magnetros anode structuse according to claim 10, wherein said ring is mounted on said cylindrical block adjacent but outside of said closed ends of said resonators and said tabs are movable into or out of said predominantly inductive regions to change the effective inductance thereof.
WELLESLEY J. DODDS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US29984A 1948-05-29 1948-05-29 Electron discharge device of the cavity resonator type Expired - Lifetime US2607019A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2887615A (en) * 1956-01-16 1959-05-19 M O Valve Co Ltd Magnetrons
US2931943A (en) * 1954-09-01 1960-04-05 Jakobsbergs Elektrotekniska Fa Magnetron with variable resonance frequency
US3045147A (en) * 1959-11-16 1962-07-17 Raytheon Co Magnetron electrode structures
US3176188A (en) * 1960-10-28 1965-03-30 Gen Electric Mixed lines crossed fields oscillator or amplifier
EP3244438A1 (en) * 2016-05-13 2017-11-15 Hitachi Power Solutions Co., Ltd. Magnetron and method of adjusting resonance frequency of magnetron

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2356414A (en) * 1941-02-26 1944-08-22 Rca Corp Tunable resonant cavity device
US2408903A (en) * 1943-06-12 1946-10-08 Sylvania Electric Prod Ultra high frequency generator
US2444418A (en) * 1942-10-15 1948-07-06 Gen Electric High-frequency electronic device
US2448573A (en) * 1946-02-28 1948-09-07 Bell Telephone Labor Inc Cathode structure for electron discharge devices

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2356414A (en) * 1941-02-26 1944-08-22 Rca Corp Tunable resonant cavity device
US2444418A (en) * 1942-10-15 1948-07-06 Gen Electric High-frequency electronic device
US2408903A (en) * 1943-06-12 1946-10-08 Sylvania Electric Prod Ultra high frequency generator
US2448573A (en) * 1946-02-28 1948-09-07 Bell Telephone Labor Inc Cathode structure for electron discharge devices

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2931943A (en) * 1954-09-01 1960-04-05 Jakobsbergs Elektrotekniska Fa Magnetron with variable resonance frequency
US2887615A (en) * 1956-01-16 1959-05-19 M O Valve Co Ltd Magnetrons
US3045147A (en) * 1959-11-16 1962-07-17 Raytheon Co Magnetron electrode structures
US3176188A (en) * 1960-10-28 1965-03-30 Gen Electric Mixed lines crossed fields oscillator or amplifier
EP3244438A1 (en) * 2016-05-13 2017-11-15 Hitachi Power Solutions Co., Ltd. Magnetron and method of adjusting resonance frequency of magnetron

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