US2647216A - Dispenser cathode - Google Patents
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- US2647216A US2647216A US153383A US15338350A US2647216A US 2647216 A US2647216 A US 2647216A US 153383 A US153383 A US 153383A US 15338350 A US15338350 A US 15338350A US 2647216 A US2647216 A US 2647216A
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- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 33
- 239000000463 material Substances 0.000 description 15
- 229910052751 metal Inorganic materials 0.000 description 13
- 239000002184 metal Substances 0.000 description 13
- 238000010438 heat treatment Methods 0.000 description 8
- 239000000203 mixture Substances 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 5
- 229910052721 tungsten Inorganic materials 0.000 description 5
- 239000010937 tungsten Substances 0.000 description 5
- 230000005012 migration Effects 0.000 description 4
- 238000013508 migration Methods 0.000 description 4
- 239000003870 refractory metal Substances 0.000 description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 229910052715 tantalum Inorganic materials 0.000 description 3
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 208000027418 Wounds and injury Diseases 0.000 description 2
- 239000011149 active material Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000001994 activation Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000010408 sweeping Methods 0.000 description 1
- WEQHQGJDZLDFID-UHFFFAOYSA-J thorium(iv) chloride Chemical compound Cl[Th](Cl)(Cl)Cl WEQHQGJDZLDFID-UHFFFAOYSA-J 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J1/00—Details of electrodes, of magnetic control means, of screens, or of the mounting or spacing thereof, common to two or more basic types of discharge tubes or lamps
- H01J1/02—Main electrodes
- H01J1/13—Solid thermionic cathodes
- H01J1/20—Cathodes heated indirectly by an electric current; Cathodes heated by electron or ion bombardment
- H01J1/28—Dispenser-type cathodes, e.g. L-cathode
-
- 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
- H01J23/02—Electrodes; Magnetic control means; Screens
- H01J23/04—Cathodes
- H01J23/05—Cathodes having a cylindrical emissive surface, e.g. cathodes for magnetrons
Definitions
- a thermionic cylindrical cathode In a conventional magnetron, a thermionic cylindrical cathode, usually indirectly-heated, is axially mounted within a hollow multi-segment anode.
- the anode segments In the multi-cavity type magnetron the anode segments rare separated by recesses or cavities which provide internal cavity resonator circuits coupled between adjacent segments.
- the anode In operation, the anode is maintained at a suitable positive potential relative to the cathode, and a constant magnetic eld is maintained parallel to the cathode in the space between the cathode and the anode. Electrons emitted by the cathode and attracted toward the anode are deflected by the transverse magnetic eld so that they traverse circular paths.
- the magnetic field strength is adjusted below cut-off, so that most of the deflected electrons miss the anode and return to the vicinity of the cathode.
- the electron space charge sweeping pastthe anode gaps induce voltages between thefanode segments and excite high frequency elds in the cavity resonators.
- the anode voltages inturn produce velocity modulation in the space charge, thus changing the trajectories of the electrons.
- a large number of electrons return to and bombard the cathode, producing secondary electrons and also heating up the cathode. Magnetron cathodes, therefore,
- a good magnetron cathode should:
- cathodes in use in other types of electron dis-charge devices, not having a magnetic eld, have not been found satisfactory in magnetrons.
- Some cathodes which have been used in magnetrons with varying success are those having: a thoriated tungsten surface, a wire-wound oxide coating; a woven nickel mesh welded or sintered to a nichelv base and packed with oxides; a sintered matrix of coarse nickel powder mixed with oxides on a nickel base; and a matrix of sintered thoria with an embedded heater.
- a thoriated tungsten surface a wire-wound oxide coating
- a woven nickel mesh welded or sintered to a nichelv base and packed with oxides a sintered matrix of coarse nickel powder mixed with oxides on a nickel base
- a matrix of sintered thoria with an embedded heater a matrix of sintered thoria with an embedded heater.
- the present invention is concerned primarily with cathodes utilizing sintered thoria.
- sintered thoria type cathodes in continuous wave (C. W.) magnetrons the following difculties have been observed:
- the principal object of the present invention is to provide an improved cathode, especially suited for use in magnetrons.
- Anothery object of the invention is to provide a magnetron cathode which is capable of supplying the desired amount of primary and secondary 'emission without becoming overheated or damaged by back-bombardment.
- Still another object is to provide an improved cathode of the dispenser or reservoir type having satisfactory and consistent life.
- Another object is to provide a magnetron-cathode requiring low heating current and power.
- a perforated s leeve of refractory metal is packed with powdered thoria, or a mixture of thoria and other refractory oxides or some metal powders.
- the enclosure is then heated to ybond and sinter .the ⁇
- Fig. 1 is a transverse sectional view, taken on line I-I of Fig. 2, of a cylindrical magnetron embodying ⁇ the present invention
- Fig. 3 is a longitudinal sectional View of a mod-- ification of the invention.
- Fig. 4 is a fragmentary detail View showing another modification.
- Fig. 5 is a longitudinal sectional view of Still another modication.
- anode 3 comprises a hollow cylindrical shell 5 in which are mounted a number, eight as shown, of radial anode vanes '1. lIhe inner edges of varies 'I constitute electronfreceiving anode elements or segments 3. Each pair of adjacent vanes together with the portion of the shell 5 therebetween constitute a cavity resonator circuit l coupled between adjacent, anode elements 9- The elements 9 comprisee a cylindrical cathode space I I in whicha cylindrical cathode I3 is axially mounted.
- Conventional electrostatic shields or hats i may be provided at each end of the cathode to minimize loss of electrons to the end spaces of the magnetron.
- the envelope of the device is completed by end plates il' and IS cio..- ing the ends of the shell 5.
- extend through an aperture 23 in end'plate Il, being supported therein by insulation 25.
- Suitable means such as magnets schematically shown as pole pieces 2,1 and 29 in Fig. 2, are provided to establish an axial magnetic field Within the cathode space.
- the cathode i3 comprises an apertured or perforated sleeve 3
- the sleeve may be constructed by boring or punching the desired pattern of holes or apertures 33 in a rectangular sheet of the metal, forming the sheet into a hollow cylinder and welding the edges together.
- One such cathode sleeve was constructed with a pattern of nine axial rows of eight holes each bored with a #80 drill. As shown in the drawing, the size and spacing of the holes S3 in the sleeve 3i are such that the total area of the holes is an appreciable fraction, considerably less than one-half, of the total sleeve area.
- is packed with powdered thoria of the type used for sintered cathodes.
- thoria powdered thoria of the type used for sintered cathodes.
- a. mixture of thoria and other refractory oxides, carbides, nitrides or borides of metals such as thorium, zirconium, ⁇ titanium and tantalum, or of thoria and some refractory metal powders, 'such as molybdenum, tantalum or tungsten, may be used.
- a preferred method of preparing the cathode is to: (l) make a paste of 20() mesh thoria and a solution of thorium chloride (l g. in 5 ml. of H2O); (2) pack the paste into the apertured sleeve; (3) wipe oiT the outside, avoiding any contact with lint; and inspect for clean, smoothl metal surface, absence of any foreign matter or any bulge in the sleeve.
- a refractory conducting rod 31 of tungsten, molybdenum or tantalum is mounted coaxially within the sleeve 3
- heating current issupplied to ytherod 3l, ring- 39 and sleeve 3
- the thoria, or thoria mixture is packed into the annular space between the sleeve 3
- double-helical, non-inductive heater 4I is embedded in the thoria material 35.
- is closed by a plug 43, and the thoria mixture is packed into the sleeve from the other end while the heater coil lll is held in position by suitable means.
- the heater is separately energized, so that the sleeve 3
- Fig., i shows a modiication of Figs. 1 and 2 wherein the conducting ring 33 is replaced by anV insulating ring d5.
- the thoria material 35 is made conductive, so that it takes the place ofA the conducting ring 39 in the heater circuit of Figs. 1 and 2.
- the cathode is processed as follows. After the thoria material has been packed into the sleeve Si, the cathode assembly is mounted in the magnetron which then undergoes normal processing. After the tube is exhausted and baked, thek oathode is degassed by slowly raising the heater current to about 35 amperes,A or to produce. a cathode brightness ofl 1600 to 1700" C. Upon lowering of the temperature to operatingt value, full emission is obtained with no apparent activation process occurring. By this normal processing and heating of the cathode, the contained thoria material is fully bonded and sintered within theA cathode sleeve. rIfhe thoria material may ll the holes 33 as well as the space within the sleeve 3
- the holes 33 in the cathode sleeve preferably do notextend to the hats I5 but, instead,1 are spaced substantially therefrom as shown in Figs. 2-4. ⁇ As shown in Fig. 2, the outermost holes 33 arespaced inwardly from the ends o the anode 3.
- a central region of the cathode sleeve l may be left imperforate between two perforated regions, because this is the region where maximum back-bombardment power is dissipated.
- the operating temperature of a cathode so constructed has been of the order of 1200 to 1300 C. brightness, which is 300 to 400 C. lower than usually encountered in thoriated tungsten and sintered thoria matrix type cathodes under the same test conditions;
- the thoria material is not required to provide structural support for the cathode assembly and, moreover, is mechanically protected by the metal sleeve;
- Cut-off characteristics are equal to or better than that of any other type of cathodes tested in C. W. magnetrons.
- the improved dispensertype cathode is not limited to such use.
- the cathode is especially suitable for use in electron tubes employing a magnetic eld, such as magnetrons, because of its ability to withstand backbombardment caused by the magnetic eld.
- a magnetic eld such as magnetrons
- it may also be used in high frequency power triodes or other tubes in which radio frequency currents occur in the cathode.
- a dispenser-type cathode comprising a sleeve of refractory sheet metal having a smooth bare exterior surface and a plurality of apertures therethrough, said sleeve containing a compact mass of electron-emissive material ⁇ including thoria in contact with its interior surface, and electrostatic shield elements mounted on and surrounding the ends of said sleeve, the perforations of said sleeve being spaced substantially from said shields to prevent migration of thoria to said shields during operation of said cathode.
- An electron discharge device of the magnetron type including a hollow anode structure defining a cylindrical cathode space, an elongated dispenser-type cathode axially mounted within said space, and means for producing a constant magnetic field in said space axial to said cathode,
- said cathode comprising a sleeve of refractory sheet metal having a smooth bare exterior surface and containing a compact mass of electronemissive material including thoria in contact with its interior surface, a substantial part of said sleeve having apertures therethrough to permit direct emission from said material through said sleeve.
- An electron discharge device of the magnetron type including a hollow anode structure dening a cylindrical cathode space, an elongated dispenser-type cathode axially mounted within said space, and means for producing a constant magnetic field in said space axialto said cathode, said cathode comprising a sleeve of refractory sheet metal having a smooth bare exterior surface and containing a compact mass of electronemissive material including thoria in contact with its interior surface, the central portion of said sleeve having apertures therethrough to permit direct emission from said material through said sleeve, a substantial portion of said sleeve within each end of said space being imperforate to restrict primary emission to said central portion and facilitate dissipation of heat generated by back-bombardment of the cathode.
- An electron discharge device wherein said mass of electron-emissive material is a sintered mixture of thoria powder and another refractory oxide.
- An electron discharge device wherein said mass of electron-emissive material is a sintered mixture of thoria powder and a metal powder.
- An electron discharge device including a refractory metal rod positioned within said sleeve and y electrically connected thereto to form a return References Cited in the le of this patent UNITED STATES PATENTS Number Name Date 2,107,945 Hull et al Feb. 8, 1938i 2,147,447 Kolligs Feb. 14, 1939 2,175,345 Gaides et al. Oct. 10, 1939 2,201,731 Hull May 21, 1940 2,416,899 Brown Mar. 4, 1947 2,473,550 Spencer June 21, 1949
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Description
July. 28, 1953 B. B. BROWN DISPENSER CATHODE Filed April 1, 195o J5 ll 4.5 31 5.5
INVENTOR Brregll Ivmwu i I ATTORNEY` Patented July 28,-- 1953 DISPENSER CATHODE Barremore B. Brown, Lancaster, Pa., assignor to Radio Corporation of of Delaware America, a corporation Application Apri11`, 195o, semi No. 153,383 a claims. (Crais- 157) This invention relates to improvements in cathodes for electron discharge devices, and particularly, to a dispenser cathode especially useful in magnetrons.
In a conventional magnetron, a thermionic cylindrical cathode, usually indirectly-heated, is axially mounted within a hollow multi-segment anode. In the multi-cavity type magnetron the anode segments rare separated by recesses or cavities which provide internal cavity resonator circuits coupled between adjacent segments. In operation, the anode is maintained at a suitable positive potential relative to the cathode, and a constant magnetic eld is maintained parallel to the cathode in the space between the cathode and the anode. Electrons emitted by the cathode and attracted toward the anode are deflected by the transverse magnetic eld so that they traverse circular paths. The magnetic field strength is adjusted below cut-off, so that most of the deflected electrons miss the anode and return to the vicinity of the cathode. The electron space charge sweeping pastthe anode gaps induce voltages between thefanode segments and excite high frequency elds in the cavity resonators. The anode voltages inturn produce velocity modulation in the space charge, thus changing the trajectories of the electrons. A large number of electrons return to and bombard the cathode, producing secondary electrons and also heating up the cathode. Magnetron cathodes, therefore,
must be designed to withstand such bombardment without injury.
A good magnetron cathode should:
' 1. Provide sufficient primary emission for starting and for supplying a part of operating current; 2. Provide 'suiiicient secondary emission to supply the remainder of the operating current; 3. Include suicient active material to permit satisfactory life;
4. Have means for holding the active material on the cathode surface;
5. I-Iave consistent life;
6. Have suciently low electrical resistance to permit large currents without undue local heatmg:
7. Not exhibit tendency to excessive or repeated sparking;
8. Have the ability to withstand backbombardment without damage;
9. Have satisfactory heat dissipation characteristics;
10. Require low heating current and power and consequent low evaporation;
11. Have low noise; and
l2. Be easy to manufacture.
Conventional oxide-coated cathodes in use in other types of electron dis-charge devices, not having a magnetic eld, have not been found satisfactory in magnetrons. Some cathodes which have been used in magnetrons with varying success are those having: a thoriated tungsten surface, a wire-wound oxide coating; a woven nickel mesh welded or sintered to a nichelv base and packed with oxides; a sintered matrix of coarse nickel powder mixed with oxides on a nickel base; and a matrix of sintered thoria with an embedded heater. However, insofar as applicant is aware, none of the cathodes used heretofore has proven ideal for magnetron use.
The present invention is concerned primarily with cathodes utilizing sintered thoria. In the course of tests on known sintered thoria type cathodes in continuous wave (C. W.) magnetrons, the following difculties have been observed:
(a) The constructional difliculties of such cathodes are great, and mechanica1 strength is low, particularly in small size cathodes;v
(b) The thermalconductivity of the sintered thoria is so low that relatively low back-bombardment power will raise the cathode surface tooperating temperature, even though the thermal conductivity of cathodes can be made sufficiently high when pure metal emitters are used;
(c) The cut-01T characteristics of magnetrons with such cathodes have been poor, indicating diode emission even in the presence of the magnetic eld. There is evidence that this arises from the hats or end shields of the cathode which are initially uncoated, leading to the assumption that there is migration ofthoria to the hats.
The principal object of the present invention, therefore, is to provide an improved cathode, especially suited for use in magnetrons.
Anothery object of the invention is to provide a magnetron cathode which is capable of supplying the desired amount of primary and secondary 'emission without becoming overheated or damaged by back-bombardment.
Still another object is to provide an improved cathode of the dispenser or reservoir type having satisfactory and consistent life.
. Another object is to provide a magnetron-cathode requiring low heating current and power.
In :accordance with the invention, a perforated s leeve of refractory metal is packed with powdered thoria, or a mixture of thoria and other refractory oxides or some metal powders. The enclosure is then heated to ybond and sinter .the`
thoria or thoriavmixture within the sleeve,
'drical magnetron of the multi-cavity type.
The foregoing and other objects, features and advantages of the invention will be understood from the following detailed description referring to the accompanying drawing, in which:
Fig. 1 is a transverse sectional view, taken on line I-I of Fig. 2, of a cylindrical magnetron embodying `the present invention; e
Fig. 2'Vis a longitudinal sectional view on `line 2-2 of Fig. 1;
Fig. 3 is a longitudinal sectional View of a mod-- ification of the invention;
Fig. 4 is a fragmentary detail View showing another modification; and
Fig. 5 is a longitudinal sectional view of Still another modication.
Referring to Figs. 1 and 2, the invention is illustrated, for example, as embodied in a cylin- An anode 3 comprises a hollow cylindrical shell 5 in which are mounted a number, eight as shown, of radial anode vanes '1. lIhe inner edges of varies 'I constitute electronfreceiving anode elements or segments 3. Each pair of adjacent vanes together with the portion of the shell 5 therebetween constitute a cavity resonator circuit l coupled between adjacent, anode elements 9- The elements 9 denne a cylindrical cathode space I I in whicha cylindrical cathode I3 is axially mounted. Conventional electrostatic shields or hats i may be provided at each end of the cathode to minimize loss of electrons to the end spaces of the magnetron. The envelope of the device is completed by end plates il' and IS cio..- ing the ends of the shell 5. The cathode I3 and its support 2| extend through an aperture 23 in end'plate Il, being supported therein by insulation 25. Suitable means, such as magnets schematically shown as pole pieces 2,1 and 29 in Fig. 2, are provided to establish an axial magnetic field Within the cathode space.
lIn accordance with the present invention, the cathode i3 comprises an apertured or perforated sleeve 3| of a refractory metal such as molybdenum, tantalurn or tungsten.Y The sleeve may be constructed by boring or punching the desired pattern of holes or apertures 33 in a rectangular sheet of the metal, forming the sheet into a hollow cylinder and welding the edges together. One such cathode sleeve was constructed with a pattern of nine axial rows of eight holes each bored with a #80 drill. As shown in the drawing, the size and spacing of the holes S3 in the sleeve 3i are such that the total area of the holes is an appreciable fraction, considerably less than one-half, of the total sleeve area.
To provide a reservoir of refractory emissive material 35 beneath the holes 33, the sleeve 3| is packed with powdered thoria of the type used for sintered cathodes. Alternatively, a. mixture of thoria and other refractory oxides, carbides, nitrides or borides of metals such as thorium, zirconium,` titanium and tantalum, or of thoria and some refractory metal powders, 'such as molybdenum, tantalum or tungsten, may be used.
A preferred method of preparing the cathode is to: (l) make a paste of 20() mesh thoria and a solution of thorium chloride (l g. in 5 ml. of H2O); (2) pack the paste into the apertured sleeve; (3) wipe oiT the outside, avoiding any contact with lint; and inspect for clean, smoothl metal surface, absence of any foreign matter or any bulge in the sleeve.
Some means must be provided for heating the cathode I 3 to maintain it at the desired operating temperature. Three alternative heating means CII are illustrated in Figs. 2, 3 and 4, respectively. In Fig. 1, a refractory conducting rod 31 of tungsten, molybdenum or tantalum is mounted coaxially within the sleeve 3| and electrically connected at its inner end to the sleeve 3| by a conducting ring 39 (Fig. 2). In operation, heating currentissupplied to ytherod 3l, ring- 39 and sleeve 3| in series, heating the enclosure to the desired temperature. In this form of the invention the thoria, or thoria mixture, is packed into the annular space between the sleeve 3| and rod 31.
In Fig. 3 a, double-helical, non-inductive heater 4I is embedded in the thoria material 35. Preferably, the inner end of the sleeve 3| is closed by a plug 43, and the thoria mixture is packed into the sleeve from the other end while the heater coil lll is held in position by suitable means. In operation, the heater is separately energized, so that the sleeve 3| does not iorm a part of thev heater circuit.
Fig., i shows a modiication of Figs. 1 and 2 wherein the conducting ring 33 is replaced by anV insulating ring d5. In, this form the thoria material 35 is made conductive, so that it takes the place ofA the conducting ring 39 in the heater circuit of Figs. 1 and 2.
In each of the forms shown in Figs. 2,` 3 and 4 the cathode is processed as follows. After the thoria material has been packed into the sleeve Si, the cathode assembly is mounted in the magnetron which then undergoes normal processing. After the tube is exhausted and baked, thek oathode is degassed by slowly raising the heater current to about 35 amperes,A or to produce. a cathode brightness ofl 1600 to 1700" C. Upon lowering of the temperature to operatingt value, full emission is obtained with no apparent activation process occurring. By this normal processing and heating of the cathode, the contained thoria material is fully bonded and sintered within theA cathode sleeve. rIfhe thoria material may ll the holes 33 as well as the space within the sleeve 3|, as` shown in Fig. 4.
In operation, electronv emissionV apparently occurs fromV the thoria beneath the holes and also from the adjacent surfaces of the metal enclosure dueto migration' of the thoria thereon. It is desirable to prevent migration of thoria to the hats I5, and also to limit direct emission from the parts of* the cathode I3 immediately opposite the ends or the anode 3. Therefore, the holes 33 in the cathode sleeve preferably do notextend to the hats I5 but, instead,1 are spaced substantially therefrom as shown in Figs. 2-4.` As shown in Fig. 2, the outermost holes 33 arespaced inwardly from the ends o the anode 3. This leaves a substantial solidor imperforate portion 46 ofthe cathode sleeve 3i at each end thereof, which restricts primary emission t0 the central portion of the cathode and also facilitates dissipation of heat generated by bach-bombardment of the cathode.
It is also possible to provide other patterns of holes or perforated` areas for the purpose of con,- trolling the thermal and electrical conductivity of various portions'of the cathode surface. For example, as shown in Fig. 5, a central region of the cathode sleeve l may be left imperforate between two perforated regions, because this is the region where maximum back-bombardment power is dissipated. l
Tests on the dispenser-type cathodes disclosed herein in C. W. magnetrons yhave shownA them. to be far superior to sinteredv thoria and other cathodes tested. The following advantages have been noted:
(l) Because of the bare metal sleeve, the thermal conductivity of the cathode can be made as great as necessary to dissipate back-bombardment power;
(2) 'Ihe cathode has low sparking characteristics due to the use of the bare metal sleeve;
(3) The operating temperature of a cathode so constructed has been of the order of 1200 to 1300 C. brightness, which is 300 to 400 C. lower than usually encountered in thoriated tungsten and sintered thoria matrix type cathodes under the same test conditions;
(4) The supply of thoria is so great relative to other cathode constructions that emission life is observed to be many times as long as for such other constructions;
(5) 'I'he fabrication of cathodes constructed in this manneris very simple as compared to other methods, since it merely involves packing the thoria material into a receptacle, followed by normal tube processing operations;
(6) The thoria material is not required to provide structural support for the cathode assembly and, moreover, is mechanically protected by the metal sleeve;
(7) Emission from the hats is practically nonexistent; and
(8) Cut-off characteristics are equal to or better than that of any other type of cathodes tested in C. W. magnetrons.
Although the invention has been described particularly with reference to magnetron use, it will be understood that the improved dispensertype cathode is not limited to such use. The cathode is especially suitable for use in electron tubes employing a magnetic eld, such as magnetrons, because of its ability to withstand backbombardment caused by the magnetic eld. However, it may also be used in high frequency power triodes or other tubes in which radio frequency currents occur in the cathode.
What is claimed is:
1. A dispenser-type cathode comprising a sleeve of refractory sheet metal having a smooth bare exterior surface and a plurality of apertures therethrough, said sleeve containing a compact mass of electron-emissive material `including thoria in contact with its interior surface, and electrostatic shield elements mounted on and surrounding the ends of said sleeve, the perforations of said sleeve being spaced substantially from said shields to prevent migration of thoria to said shields during operation of said cathode.
2. An electron discharge device of the magnetron type including a hollow anode structure defining a cylindrical cathode space, an elongated dispenser-type cathode axially mounted within said space, and means for producing a constant magnetic field in said space axial to said cathode,
said cathode comprising a sleeve of refractory sheet metal having a smooth bare exterior surface and containing a compact mass of electronemissive material including thoria in contact with its interior surface, a substantial part of said sleeve having apertures therethrough to permit direct emission from said material through said sleeve.
3. An electron discharge device of the magnetron type including a hollow anode structure dening a cylindrical cathode space, an elongated dispenser-type cathode axially mounted within said space, and means for producing a constant magnetic field in said space axialto said cathode, said cathode comprising a sleeve of refractory sheet metal having a smooth bare exterior surface and containing a compact mass of electronemissive material including thoria in contact with its interior surface, the central portion of said sleeve having apertures therethrough to permit direct emission from said material through said sleeve, a substantial portion of said sleeve within each end of said space being imperforate to restrict primary emission to said central portion and facilitate dissipation of heat generated by back-bombardment of the cathode.
4. An electron discharge device according to claim 2, wherein the total area of said apertures is an appreciable fraction considerably less than one-half of the total area of said surface.
5. An electron discharge device according to claim 2, wherein said mass of electron-emissive material is a sintered mixture of thoria powder and another refractory oxide.
6. An electron discharge device according to claim 2, wherein said mass of electron-emissive material is a sintered mixture of thoria powder and a metal powder.
7. An electron discharge device according to claim 2, wherein said cathode includes a refractory metal rod positioned within said sleeve and y electrically connected thereto to form a return References Cited in the le of this patent UNITED STATES PATENTS Number Name Date 2,107,945 Hull et al Feb. 8, 1938i 2,147,447 Kolligs Feb. 14, 1939 2,175,345 Gaides et al. Oct. 10, 1939 2,201,731 Hull May 21, 1940 2,416,899 Brown Mar. 4, 1947 2,473,550 Spencer June 21, 1949
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US153383A US2647216A (en) | 1950-04-01 | 1950-04-01 | Dispenser cathode |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US153383A US2647216A (en) | 1950-04-01 | 1950-04-01 | Dispenser cathode |
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US2647216A true US2647216A (en) | 1953-07-28 |
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Application Number | Title | Priority Date | Filing Date |
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US153383A Expired - Lifetime US2647216A (en) | 1950-04-01 | 1950-04-01 | Dispenser cathode |
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US (1) | US2647216A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2737607A (en) * | 1951-07-17 | 1956-03-06 | Hartford Nat Bank & Trust Co | Incandescible cathode |
US2798180A (en) * | 1953-11-05 | 1957-07-02 | Egyesuelt Izzolampa | Cathode-ray tubes for use in television receivers |
US2808531A (en) * | 1952-03-24 | 1957-10-01 | Siemens Ag | Cathode for electrical discharge tubes |
US2848644A (en) * | 1953-01-19 | 1958-08-19 | Philips Corp | Thermionic cathode |
US2860275A (en) * | 1955-02-09 | 1958-11-11 | Philips Corp | Indirectly heated cathode |
US2864028A (en) * | 1955-08-15 | 1958-12-09 | Philips Corp | Thermionic dispenser cathode |
US3027480A (en) * | 1958-12-15 | 1962-03-27 | Raytheon Co | Electron discharge device cathodes |
US3251641A (en) * | 1962-03-27 | 1966-05-17 | Rca Corp | Electron tube and method of making the same |
US3258636A (en) * | 1961-09-01 | 1966-06-28 | Electron emitter with activator of sill cide, boride or carbide of solid solu- tion of barium and at least one other alkaline earth metal | |
US3298096A (en) * | 1963-12-30 | 1967-01-17 | Varian Associates | Method of forming distortion resistant tubular elements |
US3308329A (en) * | 1962-11-23 | 1967-03-07 | Litton Industries Inc | Thermionic emissive cathode with end structure for emissive suppression |
US3896332A (en) * | 1973-06-04 | 1975-07-22 | M O Valve Co Ltd | High power quick starting magnetron |
EP0245982A2 (en) * | 1986-05-16 | 1987-11-19 | English Electric Valve Company Limited | Directly heated cathodes |
WO2014134595A3 (en) * | 2013-03-01 | 2015-02-19 | Soo Yong Park | Magnetron |
WO2020041377A1 (en) * | 2018-08-22 | 2020-02-27 | Modern Electron, LLC | Cathodes with conformal cathode surfaces for vacuum electronic devices |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2107945A (en) * | 1934-11-20 | 1938-02-08 | Gen Electric | Cathode structure |
US2147447A (en) * | 1936-09-21 | 1939-02-14 | Siemens Ag | Glow cathode |
US2175345A (en) * | 1935-07-12 | 1939-10-10 | Gen Electric | Electric gaseous discharge device |
US2201731A (en) * | 1938-11-30 | 1940-05-21 | Gen Electric | Discharge tube electrode assembly |
US2416899A (en) * | 1943-09-24 | 1947-03-04 | Raytheon Mfg Co | Electronic discharge device of the magnetron type |
US2473550A (en) * | 1947-08-19 | 1949-06-21 | Raytheon Mfg Co | Directly heated cathode |
-
1950
- 1950-04-01 US US153383A patent/US2647216A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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US2107945A (en) * | 1934-11-20 | 1938-02-08 | Gen Electric | Cathode structure |
US2175345A (en) * | 1935-07-12 | 1939-10-10 | Gen Electric | Electric gaseous discharge device |
US2147447A (en) * | 1936-09-21 | 1939-02-14 | Siemens Ag | Glow cathode |
US2201731A (en) * | 1938-11-30 | 1940-05-21 | Gen Electric | Discharge tube electrode assembly |
US2416899A (en) * | 1943-09-24 | 1947-03-04 | Raytheon Mfg Co | Electronic discharge device of the magnetron type |
US2473550A (en) * | 1947-08-19 | 1949-06-21 | Raytheon Mfg Co | Directly heated cathode |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2737607A (en) * | 1951-07-17 | 1956-03-06 | Hartford Nat Bank & Trust Co | Incandescible cathode |
US2808531A (en) * | 1952-03-24 | 1957-10-01 | Siemens Ag | Cathode for electrical discharge tubes |
US2848644A (en) * | 1953-01-19 | 1958-08-19 | Philips Corp | Thermionic cathode |
US2798180A (en) * | 1953-11-05 | 1957-07-02 | Egyesuelt Izzolampa | Cathode-ray tubes for use in television receivers |
US2860275A (en) * | 1955-02-09 | 1958-11-11 | Philips Corp | Indirectly heated cathode |
US2864028A (en) * | 1955-08-15 | 1958-12-09 | Philips Corp | Thermionic dispenser cathode |
US3027480A (en) * | 1958-12-15 | 1962-03-27 | Raytheon Co | Electron discharge device cathodes |
US3258636A (en) * | 1961-09-01 | 1966-06-28 | Electron emitter with activator of sill cide, boride or carbide of solid solu- tion of barium and at least one other alkaline earth metal | |
US3251641A (en) * | 1962-03-27 | 1966-05-17 | Rca Corp | Electron tube and method of making the same |
US3308329A (en) * | 1962-11-23 | 1967-03-07 | Litton Industries Inc | Thermionic emissive cathode with end structure for emissive suppression |
US3298096A (en) * | 1963-12-30 | 1967-01-17 | Varian Associates | Method of forming distortion resistant tubular elements |
US3896332A (en) * | 1973-06-04 | 1975-07-22 | M O Valve Co Ltd | High power quick starting magnetron |
EP0245982A2 (en) * | 1986-05-16 | 1987-11-19 | English Electric Valve Company Limited | Directly heated cathodes |
EP0245982A3 (en) * | 1986-05-16 | 1989-06-14 | English Electric Valve Company Limited | Directly heated cathodes |
WO2014134595A3 (en) * | 2013-03-01 | 2015-02-19 | Soo Yong Park | Magnetron |
CN105190822A (en) * | 2013-03-01 | 2015-12-23 | 朴秀用 | Magnetron |
CN108962704A (en) * | 2013-03-01 | 2018-12-07 | 朴秀用 | Magnetron |
US11011339B2 (en) | 2013-03-01 | 2021-05-18 | Soo Yong Park | Magnetron |
WO2020041377A1 (en) * | 2018-08-22 | 2020-02-27 | Modern Electron, LLC | Cathodes with conformal cathode surfaces for vacuum electronic devices |
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