US2282097A - Nonemitting electrode structure - Google Patents

Nonemitting electrode structure Download PDF

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Publication number
US2282097A
US2282097A US326584A US32658440A US2282097A US 2282097 A US2282097 A US 2282097A US 326584 A US326584 A US 326584A US 32658440 A US32658440 A US 32658440A US 2282097 A US2282097 A US 2282097A
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electrode
grid
thorium
tungsten
molybdenum
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US326584A
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Warren G Taylor
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00Details of vacuum tubes of the types covered by group H01J21/00
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00Details of vacuum tubes of the types covered by group H01J21/00
    • H01J19/28Non-electron-emitting electrodes; Screens
    • H01J19/30Non-electron-emitting electrodes; Screens characterised by the material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00Discharge tubes and lamps
    • H01J2893/0001Electrodes and electrode systems suitable for discharge tubes or lamps
    • H01J2893/0012Constructional arrangements
    • H01J2893/0019Chemical composition and manufacture
    • H01J2893/002Chemical composition and manufacture chemical
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00Discharge tubes and lamps
    • H01J2893/0001Electrodes and electrode systems suitable for discharge tubes or lamps
    • H01J2893/0012Constructional arrangements
    • H01J2893/0019Chemical composition and manufacture
    • H01J2893/0022Manufacture
    • H01J2893/0023Manufacture carbonising and other surface treatments
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9265Special properties
    • Y10S428/929Electrical contact feature
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component

Definitions

  • This invention relates to a non-emitting electrode structure for space discharge devices and more particularly for use in connection with thoriated types of hot cathodes.
  • any cathode material that is, thorium or thorium oxide is evaporated or sputtered from the cathode, some may deposit on one or more of the other hot electrodes which should be normally non-emitting. If the material out of which the hot electrode is made is a suitable base for the thorium, then it is obvious that the deposited thorium will result in emission from what should normally be a non-emitting electrode.
  • a substance should have a high melting point
  • Tungsten as a material for grids is difficult to handle since it is tough and springy. Furthermore, any thorium falling on tungsten will result in emission if the tungsten is hot since tungsten is an excellent base.
  • Tantalum is ordinarily suitable for grid and anode electrodes. It has one serious drawback however in that its gas absorption characteristics under high temperatures are not always suitable to working conditions.
  • tantalum On an extreme overload some absorbed gases may be released with disastrous results to the tubes. If the tantalum is thoroughly cleaned and free of all gas, it provides a rather excellent base in the event that any thorium falls on it.
  • Molybdenum is not as easily handled as tantalum and does not absorb gases as readily as tantalum. However, when thorium falls on it, molybdenum is even a better base material than tantalum so that any electrode operating at an elevated temperature will tend to emit.
  • any one of the above three metals without regard to their characteristics of being a satisfactory base material for thorium.
  • Any one of the metals, that is tungsten, tantalum or molybdenum, when treated as described herein retains its normal properties as previously pointed out, when used as a grid or anode with the exception that substantially all tendency for emission of electrons due to thorium falling thereon is suppressed and eliminated so completely that this is no longer a factor in the choice of metal.
  • this invention contemplates the use of tungsten, tantalum or molybdenum as a material for grids and anodes and subjected to the following treatment.
  • a quantity of any one or more of the metals of group 8 'of the periodic table of elements is applied to any one of the three base materials that is tungsten, tantalum or molybdenum.
  • the application may either be in the form of a plated coating or may be melted into the material to form an alloy.
  • the quantity of such additional metal or metals of group 8 may be very small and in practice the added ingredient is generally driven out by heat to the surface of the base material to form a coating.
  • a base wire of tantalum, tungsten or molybdenum may be plated with platinum, the coating being extremely minute for the sake of cheapness rather than anything else.
  • platinum iridium or osmium may be used. Any one of the three latter elements is particularly desirable for the reason that the melting points are high and vapor pressures are low.
  • This tendency to non-emission may be due to the fact that the thorium does not remain on the material but is driven off. However, irrespective of how this occurs, I have found that this 2 tendency toward non-emission may be enhanced to an even greater degree by the application of carbon to the treated electrode.
  • a molybdenum wire which has been suitably cleaned by heating in 2 a hydrogen atmosphere may have a thin plating of latinum thereon.
  • the hydrogen cleaning of the wire may occur after plating if desired.
  • this wire may be washed in hot water.
  • the wire may then be made up into the 30 form of a grid or other electrode and then sprayed with a mixture of alcohol and aquadag. Thereafter this electrode may be heated in a hydrogen atmosphere until the surface is shiny and clean. This heating may be done during the 35 final evacuation and Kettering steps.
  • the hydrogen atmosphere is not a necessity since the customary evacuation conditions may create a reducing atmosphere around the wire.
  • a grid or anode electrode treated in this manner will have 40 posing one of the normally non-emitting electrodes.
  • a space discharge device may have an envelope l0 or glass or any other suitable material the interior of which is suitably evacuated.
  • a stem H Supported within envelope N as by means of a stem H are a plurality of electrodes consisting of a cathode l2 of the thoriated type adapted to emit when heated.
  • a control grid l3 Surrounding cathode l2 is a control grid l3 and beyond the grid is an anode I4.
  • Anode I may be of metal and if desired and as far as this invention is concerned may be handled in the same way as grid IS.
  • the anode may also consist of graphite.
  • grid l3 as an example of a normally non-emitting electrode which under operating conditions may be hot and upon which thorium may be deposited from cathode I2, is constructed of any one of the metals tantalum, tungsten or molybdenum treated as previously described.
  • a space discharge device having a thoriated incandescible cathode and a non-emitting electrode having a core of the group tungsten and molybdenum, said core having as a cover over its entire surface an intimately bound thin surface layer oi. one or more metals or group eight of the periodic table with the outer surface of.
  • a space discharge device having a thoriated incandescible cathode and a non-emitting electrode having a core of the group tungsten and molybdenum, said core having as a cover over its entire surface an intimately bound thin surface layer of one or more metals of group eight of the periodic table having a melting point of the order of platinum and having the outer surface of said layer carbonized.
  • a space discharge device having a thoriated incandescible cathode and a non-emitting electrode having a core of the group tungsten and molybdenum, said core having as a cover over its entire surface an intimately bound thin surface layer of platinum with the outer surface carbonized.

Description

y 1942. w. G. TAYLOR 2,282,097
NON-EMITTING ELECTRODE STRUCTURE Filed March 29, 1940 Coating of mefa/ of group 8 Carbon/zed l surface (2/7192? Zf/Of Patented May 5, 1942 UNITED STATES PATENT OFFICE NONEMITTING ELECTRODE STRUCTURE Warren G. Taylor, Chicago, Ill.
Application March 29, 1940, Serial No. 326,584
3 Claims.
This invention relates to a non-emitting electrode structure for space discharge devices and more particularly for use in connection with thoriated types of hot cathodes.
In order to obtain certain characteristics in a space discharge device it is frequently necessary to dispose grids and even anodes quite close to cathodes. Since the thoriated type of cathode operates at a high temperature, it is evident that the physical proximity to the cathode of normally non-emitting electrodes will result in heating of these latter electrodes. This is particularly true of grid electrodes.
In addition thereto, electron bombardment will elevate the electrode temperature. Reflection and radiation from an anode or solid plate will also tend to heat grids. The net result is that a so-called cold electrode is in reality an electrode which is normally operating at an elevated temperature.
In the event that any cathode material, that is, thorium or thorium oxide is evaporated or sputtered from the cathode, some may deposit on one or more of the other hot electrodes which should be normally non-emitting. If the material out of which the hot electrode is made is a suitable base for the thorium, then it is obvious that the deposited thorium will result in emission from what should normally be a non-emitting electrode.
The closer a grid electrode is to the cathode, the hotter it is likely to be, the more likely it is to have thorium deposited on it, and the greater the efiect of the emission, since a grid in this position exercises an extremely delicate control.
In order to be satisfactory as a'grid material, a substance should have a high melting point,
low vapor pressure, should surrender substantially all absorbed gases when hot during the evacuation process, should not itself sensibly emit electrons under all operating conditions, and in addition have the usual normal commercial requirements of cheapness and workability. f the metals generally available, iron and nickel would be satisfactory except that they melt and vaporize too easily. Thus, in tubes having carbon or graphite anodes it is necessary to heat the electrode to extremely high temperatures for relatively long times during processing and this usually results in an overheating of the metallic electrodes. Furthermore, during operation many tubes are subjected to extreme overloads where the grid and anode electrodes are operated at a temperature corresponding to red heat or higher.
Under such conditions, iron or nickel would not stand up.
Tungsten as a material for grids is difficult to handle since it is tough and springy. Furthermore, any thorium falling on tungsten will result in emission if the tungsten is hot since tungsten is an excellent base.
Tantalum is ordinarily suitable for grid and anode electrodes. It has one serious drawback however in that its gas absorption characteristics under high temperatures are not always suitable to working conditions.
On an extreme overload some absorbed gases may be released with disastrous results to the tubes. If the tantalum is thoroughly cleaned and free of all gas, it provides a rather excellent base in the event that any thorium falls on it.
Molybdenum is not as easily handled as tantalum and does not absorb gases as readily as tantalum. However, when thorium falls on it, molybdenum is even a better base material than tantalum so that any electrode operating at an elevated temperature will tend to emit.
By the invention herein disclosed it is possible to utilize as a grid or anode material any one of the above three metals without regard to their characteristics of being a satisfactory base material for thorium. Any one of the metals, that is tungsten, tantalum or molybdenum, when treated as described herein retains its normal properties as previously pointed out, when used as a grid or anode with the exception that substantially all tendency for emission of electrons due to thorium falling thereon is suppressed and eliminated so completely that this is no longer a factor in the choice of metal.
In general this invention contemplates the use of tungsten, tantalum or molybdenum as a material for grids and anodes and subjected to the following treatment. A quantity of any one or more of the metals of group 8 'of the periodic table of elements is applied to any one of the three base materials that is tungsten, tantalum or molybdenum. The application may either be in the form of a plated coating or may be melted into the material to form an alloy. The quantity of such additional metal or metals of group 8 may be very small and in practice the added ingredient is generally driven out by heat to the surface of the base material to form a coating.
Thus, for example, a base wire of tantalum, tungsten or molybdenum may be plated with platinum, the coating being extremely minute for the sake of cheapness rather than anything else. Instead of platinum, iridium or osmium may be used. Any one of the three latter elements is particularly desirable for the reason that the melting points are high and vapor pressures are low.
Thus, if a grid must withstand a high tem- 5 metals will withstand extremely high temperal0 tures and will be easily driven oif. However, as long as any one of these metals remains on the surface of the base material, there will be practically no tendency for emission to occur even at an elevated temperature in case any thorium 1o settles on the electrode.
This tendency to non-emission may be due to the fact that the thorium does not remain on the material but is driven off. However, irrespective of how this occurs, I have found that this 2 tendency toward non-emission may be enhanced to an even greater degree by the application of carbon to the treated electrode.
' Thus, as an example, a molybdenum wire which has been suitably cleaned by heating in 2 a hydrogen atmosphere may have a thin plating of latinum thereon. The hydrogen cleaning of the wire may occur after plating if desired. Thereafter this wire may be washed in hot water. The wire may then be made up into the 30 form of a grid or other electrode and then sprayed with a mixture of alcohol and aquadag. Thereafter this electrode may be heated in a hydrogen atmosphere until the surface is shiny and clean. This heating may be done during the 35 final evacuation and Kettering steps. The hydrogen atmosphere is not a necessity since the customary evacuation conditions may create a reducing atmosphere around the wire. A grid or anode electrode treated in this manner will have 40 posing one of the normally non-emitting electrodes.
Referring to the drawing a space discharge device may have an envelope l0 or glass or any other suitable material the interior of which is suitably evacuated. Supported within envelope N as by means of a stem H are a plurality of electrodes consisting of a cathode l2 of the thoriated type adapted to emit when heated. Surrounding cathode l2 is a control grid l3 and beyond the grid is an anode I4. Anode I may be of metal and if desired and as far as this invention is concerned may be handled in the same way as grid IS. The anode may also consist of graphite. In any event, grid l3, as an example of a normally non-emitting electrode which under operating conditions may be hot and upon which thorium may be deposited from cathode I2, is constructed of any one of the metals tantalum, tungsten or molybdenum treated as previously described.
What is claimed is:
l. A space discharge device having a thoriated incandescible cathode and a non-emitting electrode having a core of the group tungsten and molybdenum, said core having as a cover over its entire surface an intimately bound thin surface layer oi. one or more metals or group eight of the periodic table with the outer surface of.
said layer carbonized.
2. A space discharge device having a thoriated incandescible cathode and a non-emitting electrode having a core of the group tungsten and molybdenum, said core having as a cover over its entire surface an intimately bound thin surface layer of one or more metals of group eight of the periodic table having a melting point of the order of platinum and having the outer surface of said layer carbonized.
3. A space discharge device having a thoriated incandescible cathode and a non-emitting electrode having a core of the group tungsten and molybdenum, said core having as a cover over its entire surface an intimately bound thin surface layer of platinum with the outer surface carbonized.
WARREN. G. TAYLOR.
US326584A 1940-03-29 1940-03-29 Nonemitting electrode structure Expired - Lifetime US2282097A (en)

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Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417459A (en) * 1945-05-21 1947-03-18 Eitel Mccullough Inc Electron tube and electrode for the same
US2425090A (en) * 1942-08-24 1947-08-05 Eitel Mccullough Inc Method of making cathodes
US2450007A (en) * 1942-11-23 1948-09-28 Standard Telephones Cables Ltd Carburized filament and method for treating the same
US2497111A (en) * 1947-07-25 1950-02-14 Eitel Mccullough Inc Electron tube having carburized thoriated cathode
US2497109A (en) * 1946-02-04 1950-02-14 Eitel Mccullough Inc Electrode for electron tubes
US2497110A (en) * 1946-02-04 1950-02-14 Eitel Mccullough Inc Method of making electrodes
US2497090A (en) * 1947-12-13 1950-02-14 Eitel Mccullough Inc Electrode and method of making the same
US2682101A (en) * 1946-06-01 1954-06-29 Whitfield & Sheshunoff Inc Oxidation protected tungsten and molybdenum bodies and method of producing same
US2719797A (en) * 1950-05-23 1955-10-04 Baker & Co Inc Platinizing tantalum
US2720494A (en) * 1950-01-09 1955-10-11 Harold R Suter Process of preparing catalytic elements
US2771666A (en) * 1950-03-18 1956-11-27 Fansteel Metallurgical Corp Refractory bodies
US2788460A (en) * 1951-05-23 1957-04-09 Itt Electrodes for electron discharge devices and methods of making same
US2788289A (en) * 1951-06-29 1957-04-09 Climax Molybdenum Co Method of forming protective coatings for molybdenum and molybdenum-base alloys
US2844868A (en) * 1954-06-01 1958-07-29 Sylvania Electric Prod Method of joining refractory metals
US2864026A (en) * 1953-03-20 1958-12-09 Philips Corp Electric discharge tube
US2876400A (en) * 1953-02-27 1959-03-03 Siemens Ag Composite electrodes for directional crystal devices
US3024522A (en) * 1959-07-24 1962-03-13 Gen Electric Rhenium bonded composite material and method
US3045333A (en) * 1951-10-18 1962-07-24 Rem Cru Titanium Inc Titanium coated article
US3092749A (en) * 1960-04-15 1963-06-04 Gen Electric Electron discharge device
US3096421A (en) * 1958-04-16 1963-07-02 Walter G Finch Superconducting contact devices
US3188720A (en) * 1965-06-15 Method of sealing and joining and articles made thereby
US3259782A (en) * 1961-11-08 1966-07-05 Csf Electron-emissive structure
US3458408A (en) * 1962-11-16 1969-07-29 Monsanto Co Method for making an inductive heating element for zone refining apparatus
US3489602A (en) * 1965-05-25 1970-01-13 Hughes Aircraft Co Method of impregnating porous tungsten and resulting article
US3544285A (en) * 1966-11-16 1970-12-01 Imp Metal Ind Kynoch Ltd Oxidation-resistant coatings
US5343126A (en) * 1992-10-26 1994-08-30 General Electric Company Excitation coil for an electrodeless fluorescent lamp

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3188720A (en) * 1965-06-15 Method of sealing and joining and articles made thereby
US2425090A (en) * 1942-08-24 1947-08-05 Eitel Mccullough Inc Method of making cathodes
US2450007A (en) * 1942-11-23 1948-09-28 Standard Telephones Cables Ltd Carburized filament and method for treating the same
US2417459A (en) * 1945-05-21 1947-03-18 Eitel Mccullough Inc Electron tube and electrode for the same
US2497109A (en) * 1946-02-04 1950-02-14 Eitel Mccullough Inc Electrode for electron tubes
US2497110A (en) * 1946-02-04 1950-02-14 Eitel Mccullough Inc Method of making electrodes
US2682101A (en) * 1946-06-01 1954-06-29 Whitfield & Sheshunoff Inc Oxidation protected tungsten and molybdenum bodies and method of producing same
US2497111A (en) * 1947-07-25 1950-02-14 Eitel Mccullough Inc Electron tube having carburized thoriated cathode
US2497090A (en) * 1947-12-13 1950-02-14 Eitel Mccullough Inc Electrode and method of making the same
US2720494A (en) * 1950-01-09 1955-10-11 Harold R Suter Process of preparing catalytic elements
US2771666A (en) * 1950-03-18 1956-11-27 Fansteel Metallurgical Corp Refractory bodies
US2719797A (en) * 1950-05-23 1955-10-04 Baker & Co Inc Platinizing tantalum
US2788460A (en) * 1951-05-23 1957-04-09 Itt Electrodes for electron discharge devices and methods of making same
US2788289A (en) * 1951-06-29 1957-04-09 Climax Molybdenum Co Method of forming protective coatings for molybdenum and molybdenum-base alloys
US3045333A (en) * 1951-10-18 1962-07-24 Rem Cru Titanium Inc Titanium coated article
US2876400A (en) * 1953-02-27 1959-03-03 Siemens Ag Composite electrodes for directional crystal devices
US2864026A (en) * 1953-03-20 1958-12-09 Philips Corp Electric discharge tube
US2844868A (en) * 1954-06-01 1958-07-29 Sylvania Electric Prod Method of joining refractory metals
US3096421A (en) * 1958-04-16 1963-07-02 Walter G Finch Superconducting contact devices
US3024522A (en) * 1959-07-24 1962-03-13 Gen Electric Rhenium bonded composite material and method
US3092749A (en) * 1960-04-15 1963-06-04 Gen Electric Electron discharge device
US3259782A (en) * 1961-11-08 1966-07-05 Csf Electron-emissive structure
US3458408A (en) * 1962-11-16 1969-07-29 Monsanto Co Method for making an inductive heating element for zone refining apparatus
US3489602A (en) * 1965-05-25 1970-01-13 Hughes Aircraft Co Method of impregnating porous tungsten and resulting article
US3544285A (en) * 1966-11-16 1970-12-01 Imp Metal Ind Kynoch Ltd Oxidation-resistant coatings
US5343126A (en) * 1992-10-26 1994-08-30 General Electric Company Excitation coil for an electrodeless fluorescent lamp

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