US2404413A - Electrical gaseous discharge device - Google Patents

Electrical gaseous discharge device Download PDF

Info

Publication number
US2404413A
US2404413A US426892A US42689242A US2404413A US 2404413 A US2404413 A US 2404413A US 426892 A US426892 A US 426892A US 42689242 A US42689242 A US 42689242A US 2404413 A US2404413 A US 2404413A
Authority
US
United States
Prior art keywords
shield
discharge
anode
atmosphere
electrical
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
US426892A
Inventor
Paul W Stutsman
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.)
Raytheon Co
Original Assignee
Raytheon Manufacturing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Raytheon Manufacturing Co filed Critical Raytheon Manufacturing Co
Priority to US426892A priority Critical patent/US2404413A/en
Application granted granted Critical
Publication of US2404413A publication Critical patent/US2404413A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J17/00Gas-filled discharge tubes with solid cathode
    • H01J17/02Details
    • H01J17/04Electrodes; Screens

Definitions

  • An object of this invention is-th provision of means for shielding the electrodes of devices of the character described so as to prevent undesirable arcing.
  • Another object of the present invention is the provision of means in said devices for permitting the employment of higher voltages therein.
  • Fig. 1 is a front elevational view of a tube embodying my invention.
  • Fig. 2 is a fragmentary view taken along the line 2-2 of Fig. 1 and is partly in section.
  • the tube which I have shown by way of exemplification' is a thermionic gaseous rectifier having a self-heating cathode and two anodes.
  • Tube I consists of a glass envelope 2 having a reentrant stem 3 with a press 4 at the upper end thereof, said press carrying a cathode 5 and a plurality of anode structures 6.
  • Each anode structure 6 consists of a short rod of graphite I carried within a nickel sleeve 8, the graphite rod extending partially outside of the sleeve.
  • a nickel rod .9 is also arranged within said nickel sleeve 8 and is spaced a'distance from-said graphite rod.
  • the lower end I0 of the nickel rod 9 may be tapered and a dumet wire II is butt-Welded thereto.
  • Thedumet wire ll passes through the pres 4 and is'welded to a heavy copper'lead-in [2, said lead-in serving to conduct heat from said nickel rod.
  • the lower end l0'of the rod 9 is sealed in the press 4.
  • the nickel sleeve 8 is sealed therein, the glass from the press being forced upwardsinto the space betweenthe. tapered lower-end of the nickel rod and the nickel sleeve 8.
  • the ' Rod 9 serves as a relatively low-resistance conductor of the anode current-g RodgQ: conducts current from the lead-in l2 anddumet wire ll to a point on the nickel sleeve 8 which is adjacent the lower 'end of the space separating the top of rod 9 from the bottom of graphite rod 1.
  • the graphite rod 1 serves as the active anode element;
  • the 'aforedesoribed anode structure has several advantages.
  • the separation of the active anode element 1 from the rod 9 reduces heat transference between them since this heat transference takes place substantially entirely through the comparatively small cross-sectional area of the material of sleeve 8. Consequently .rod 9 and the dumet wire I l are maintained at a lower temperature, heat being transferred away from them through the heavy lead-in wire l2, and. damage becauseof'heat is less likely to occur to the stem press-4' in which these members are sealed.
  • the. anode element 1 is-also maintained ata substantially higher temperature than it would ordinarily have. It has been found that such higher anode temperature is desirable in certaintypes of operation.
  • I surround the anode structure by a conducting shield l3 which may be made of any suitable material such as nickel.
  • the shield I3. is cylindrical in configuration and extends to a point above the top of the nickel sleeve 8 and below the top of the graphite 'rod 1.
  • the maximum distance between the exterior of the sleeve 8 and the interior of the shield 13 is sufficiently small so that a discharge cannot occur in the space between these elements. This distance is of the order of, or less than, the mean free pathof the electrons. in the gas
  • the lower end of the shield 13 is likewise sealed in the press by having glass from the press forced upwards on both the interior and exterior-sidesof thebottom thereof.
  • the insulating member [4 madeof .steatite is cylindrical in outline and has an opening 1:5 therein so that it may be arranged over the Shield [3 in contact therewith.
  • An annularring of glass It may be formed at the top of the press 4 and an annular opening corresponding thereto formed at the bottom of the member I 4 so that member l4 may be arranged 'on said rin and positioned thereby,
  • The. member J 4 extends asubstantial distance a bov'e the top "of the graphite rod 1.
  • Inrorder to insulate theshield I3 from any material sputtered off the graphite rod 1, which sputtered material 'may cling to the walls of the membe'r ld, I prefer to provide an insulating space "between the upper portion of ,the shield 13 and the interior 'wall of theinsulating member M.
  • This space is comparatively narrow and the distance between ⁇ the exterior of the shield l3 and the interior wall of the insulating member measured transversely across said space is of the order of the mean free path of the electrons in the gas enclosed-within thetube or less.
  • This'insulating space I! may be formedby cutting away a portion of the Walls of the insulating member M at the place designated.
  • the shield l3' is' thereby arranged ina restricted chamber which serves to prevent flashing to said shield.
  • the-.upper'end of said standard l9 loops of wire .20 having getter 'material therein may be arranged and are adapted to be flashed in ⁇ the usual manner.
  • the cathode is aspiral wire supported by suitable. standards and connected tolead-in wires in a manner well known inthe art and which therefore will not-be hereinafter described.
  • the envelope '2 ' is'filled with any suitable ionizable gas such as argon preferably at a pressure of 2.5+; millimeters .offmercury'.
  • the tube may be provided with a suitable base and contact prongs.
  • An electrical space discharge device compris- "ing an envelope containing an ionizable atmos- "phere at a pressure sufiiciently high to produce,
  • electrodes adapted to support ;an ionizing discharge through said atmosphere, a shield arranged about at least one of said electrodes, and a member having the characteristic phere at a pressure sufliciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing dischargethrough said atmosphere, a conducting shield arranged about at least one of 7 said electrodes, and a steatite insulating member arranged about said shield, said' shield and mem her being provided with openings therein topermit the passage of the discharge therethrough.
  • An electrical space discharge device comprising an envelope containing an ionizable atmos-' phere at a pressure sufiiciently high to produce substantial ionization upon the occurrence of a a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere.
  • a conducting shield arranged about at least one of said electrodes and spaced therefrom a distance of the order of the mean free path of the electrons in said atmosphere or less, and an insulating member arranged about said shield, -said shield and member being provided with openings therein to permit the "passage of the discharge therethrough.
  • said electrodes including an anode, aconduct'ingv shield arranged about said anode, and a nonconducting member arranged about said shield;
  • said shield terminating in a plane spaced closely to a plane including the end of said anode, said shield and member being provided with openings therein to permit the passage of the discharge therethrough.
  • An electrical space discharge device com-prising an envelope containing an ionizable atmosphere at a pressure sufficiently high'to produce substantial ionization upon the occurrence of a I discharge therein, electrodes adaptedto support an ionizing. discharge through said atmosphere, said electrodes including a plurality of'ano'des', conducting'shields arranged about said anodes. each of said shields terminating in substantially the same plane-as the end of the corresponding.
  • An electrical space discharge device comprising an nvelope containing an ionizable atmosphere at a pressure sufliciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, said electrodes including a cylindrical anode, a hollow cylindrical conducting shield arranged around said anode and spaced therefrom, said anode projecting beyond the end of said shield, and'a hollow cylindrical insulating member arranged about said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough.
  • An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufficiently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a shield arranged about one of said electrodes, and an insulating member arranged about said shield, said shield and member having openings therein for the passage of the discharge therethrough, said anode having a portion projecting beyond said shield, the portion of said member adjacent said opening projecting beyond said shield to thereby form a restricted chamber to thereby prevent fiashing to said shield.
  • An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufficiently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a conducting shield arranged about and terminating adjacent the end of at least one of said electrodes, and an insulating member arranged about said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough, said member and said shield being constructed and arranged to provide an insulating space therebetween.
  • an electrical space discharge device a conducting sleeve, an anode element arranged at least partially within said conducting sleeve in electrical contact therewith, and an electrical conducting member arranged at least partially within the conducting sleeve and spaced from said anode element, said conducting member being in electrical contact with said sleeve at a point on said member nearest said anode element.
  • an electrical space discharge device a hollow cylindrical conductor, an anode element arranged within one end thereof in electrical contact therewith, and an electrical conducting member projecting at least partially within said conductor from the other end thereof, and being spaced from said anode element, said member 'makin electrical contact with said conductor at a point on said member nearest said anode element.
  • an electrical space discharge device a conducting sleeve, an anode element arranged within said conducting sleeve in electrical contact therewith, and an electrical conducting member having at least a portion thereof arranged within said sleeve, the portion of said conducting member arranged within said sleeve being in electrical contact throughout its length with said sleeve, said conducting member being spaced from said anode element.
  • An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufficiently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a conducting shield arranged about at least one of said electrodes, and an insulating member arranged about said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough, said member and said shield being constructed and arranged to provide an insulating space therebetween, the distance between said shield and member across said space being of the order of the mean free path of the electrons in said atmosphere or less.
  • An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufiiciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a conducting shield arranged about at least one of said electrodes and spaced therefrom a distance of the order of the mean free path of the electrons in said atmosphere or less, and an insulating member arrangedabout said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough, the distance between said shield and member across said space being of the order of the mean free path of the electrons in said atmosphere, or less.

Description

y 1946- P. w. STUTSMAN ELECTRICAL GASEOUS DISCHARGE DEVIGE Filed Jan; 15, 1942 llll Patented July 23, 1946 2,404,413 ELECTRICAL GASEOUS DISCHARGE DEVICE Paul W. Stutsman, Waltham, Mass, assignor, by
mesne assignments, to Raytheon Manufacturing Company, Newton, Mass, acorporation of Delaware Application January 15, 1942, Serial N 0. 426,892
13 Claims. (01. 250-2715).
In devices of the character described, one of I the major difliculties encountered has been the occurrence of undesired arcing. This difficulty has imposed a serious limit as to the voltage which may be successfully applied to said devices.
I have invented means for shielding electrodes of such devices so as to-:permit higher voltages to be employed without objectionable arcing.
An object of this invention is-th provision of means for shielding the electrodes of devices of the character described so as to prevent undesirable arcing.
Another object of the present invention is the provision of means in said devices for permitting the employment of higher voltages therein.
, Other objects and advantages of my invention will become apparent, and the foregoing. objects will be best understood from the following description of an exemplification thereof, reference being had to the accompanying drawing wherein:
Fig. 1 is a front elevational view of a tube embodying my invention; and
Fig. 2 is a fragmentary view taken along the line 2-2 of Fig. 1 and is partly in section.
The tube which I have shown by way of exemplification' is a thermionic gaseous rectifier having a self-heating cathode and two anodes.
Tube I consists of a glass envelope 2 having a reentrant stem 3 with a press 4 at the upper end thereof, said press carrying a cathode 5 and a plurality of anode structures 6.
Each anode structure 6 consists of a short rod of graphite I carried within a nickel sleeve 8, the graphite rod extending partially outside of the sleeve. A nickel rod .9 is also arranged within said nickel sleeve 8 and is spaced a'distance from-said graphite rod. The lower end I0 of the nickel rod 9 may be tapered and a dumet wire II is butt-Welded thereto. Thedumet wire ll passes through the pres 4 and is'welded to a heavy copper'lead-in [2, said lead-in serving to conduct heat from said nickel rod. The lower end l0'of the rod 9 is sealed in the press 4. Similarly, the nickel sleeve 8 is sealed therein, the glass from the press being forced upwardsinto the space betweenthe. tapered lower-end of the nickel rod and the nickel sleeve 8.
' Rod 9;serves as a relatively low-resistance conductor of the anode current-g RodgQ: conducts current from the lead-in l2 anddumet wire ll to a point on the nickel sleeve 8 which is adjacent the lower 'end of the space separating the top of rod 9 from the bottom of graphite rod 1. The nickel sleeve 8, which has greater resistance'than rod 9, then conducts the current to the graphite rod l. The graphite rod 1 serves as the active anode element;
The 'aforedesoribed anode structure has several advantages. The separation of the active anode element 1 from the rod 9 reduces heat transference between them since this heat transference takes place substantially entirely through the comparatively small cross-sectional area of the material of sleeve 8. Consequently .rod 9 and the dumet wire I l are maintained at a lower temperature, heat being transferred away from them through the heavy lead-in wire l2, and. damage becauseof'heat is less likely to occur to the stem press-4' in which these members are sealed. By this arrangement the. anode element 1 is-also maintained ata substantially higher temperature than it would ordinarily have. It has been found that such higher anode temperature is desirable in certaintypes of operation.
In order to confinethe active area of the anode to the upper end thereof, I surround the anode structure by a conducting shield l3 which may be made of any suitable material such as nickel. The shield I3. is cylindrical in configuration and extends to a point above the top of the nickel sleeve 8 and below the top of the graphite 'rod 1. The maximum distance between the exterior of the sleeve 8 and the interior of the shield 13 is sufficiently small so that a discharge cannot occur in the space between these elements. This distance is of the order of, or less than, the mean free pathof the electrons. in the gas The lower end of the shield 13 is likewise sealed in the press by having glass from the press forced upwards on both the interior and exterior-sidesof thebottom thereof.
In arrangements of this general type, difficulties 7 have been encountered'in discharges oc'curring between the lower. end of the shieldl3 and the In order to prevent the undesired arcing men-v tioned heretofore, I prefer to arrange an insulating material about the anode and its shield. For this purpose materials having relatively high dielectric strength are required. Furthermore such material should not give off excessive vapor atthe made by the American Lava Corporation, a dense steatite consisting chiefly of clinoenstatite crystals (MgO-SiOz) has been used and found satisfactory for this purpose.
The insulating member [4 madeof .steatite is cylindrical in outline and has an opening 1:5 therein so that it may be arranged over the Shield [3 in contact therewith.
An annularring of glass It may be formed at the top of the press 4 and an annular opening corresponding thereto formed at the bottom of the member I 4 so that member l4 may be arranged 'on said rin and positioned thereby,
. The. member J 4 extends asubstantial distance a bov'e the top "of the graphite rod 1. Inrorder to insulate theshield I3 from any material sputtered off the graphite rod 1, which sputtered material 'may cling to the walls of the membe'r ld, I prefer ,to provide an insulating space "between the upper portion of ,the shield 13 and the interior 'wall of theinsulating member M. This space is comparatively narrow and the distance between {the exterior of the shield l3 and the interior wall of the insulating member measured transversely across said space is of the order of the mean free path of the electrons in the gas enclosed-within thetube or less. This'insulating space I! may be formedby cutting away a portion of the Walls of the insulating member M at the place designated.
' The shield l3' is' thereby arranged ina restricted chamber which serves to prevent flashing to said shield.
h In-the ,tubegl two such anodestructures are provided and arranged at opposite ends of the press -4. A "metallic band l8'ymay be arranged about eachofthe-anodestructures 6 to hold them in position, the bandsjbeing connected together and t a' standard l9 secured in the press 4. At
the-.upper'end of said standard l9 loops of wire .20 having getter 'material therein may be arranged and are adapted to be flashed in} the usual manner.
.The cathode is aspiral wire supported by suitable. standards and connected tolead-in wires in a manner well known inthe art and which therefore will not-be hereinafter described. The envelope '2 'is'filled with any suitable ionizable gas such as argon preferably at a pressure of 2.5+; millimeters .offmercury'. The tube may be provided with a suitable base and contact prongs.
'In actual tests of .a tube of the general type hereinabove described it was found that without the insulating members I4 it was incapable of delivering anoutput of 250 volts D. C. because of .the flashing and arcing within the tube. When, however, insulating members 14 of steatite (Al-Si Mag .35) were arranged as hereinabove described, such tube readily delivered an output or arcing therein.
this "embodiment of my invention it will beapof '55 0volts D; C. without any sign of breakdown parentitthat-these details may be varied-without departingfromthe spirit thereof. For example,
, other materials besides steatite having thedesired 'characteristicsmay be employed. The specific,
shape oftheinsulating member and the various elements of the tube may bealtered without departing from this invention. Other variations within the scope of this invention Will readily occur to one versed in the art. It is accordingly desired that the appended claims be given a broad interpretation commensurate with the scope of the invention within the art.
What is claimed is:
1. An electrical space discharge device compris- "ing an envelope containing an ionizable atmos- "phere at a pressure sufiiciently high to produce,
substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support ;an ionizing discharge through said atmosphere, a shield arranged about at least one of said electrodes, and a member having the characteristic phere at a pressure sufliciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing dischargethrough said atmosphere, a conducting shield arranged about at least one of 7 said electrodes, and a steatite insulating member arranged about said shield, said' shield and mem her being provided with openings therein topermit the passage of the discharge therethrough.
3. An electrical space discharge device comprising an envelope containing an ionizable atmos-' phere at a pressure sufiiciently high to produce substantial ionization upon the occurrence of a a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere.
a conducting shield arranged about at least one of said electrodes and spaced therefrom a distance of the order of the mean free path of the electrons in said atmosphere or less, and an insulating member arranged about said shield, -said shield and member being provided with openings therein to permit the "passage of the discharge therethrough. I
4. An electrical space discharge'devicecomprise ing an envelope containing an ionizable atmosphere at a "pressure'sufiiciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an. ionizing discharge through said'atmosphere,
said electrodes including an anode, aconduct'ingv shield arranged about said anode, and a nonconducting member arranged about said shield;
said shield terminating in a plane spaced closely to a plane including the end of said anode, said shield and member being provided with openings therein to permit the passage of the discharge therethrough.
5. An electrical space discharge device com-prising an envelope containing an ionizable atmosphere at a pressure sufficiently high'to produce substantial ionization upon the occurrence of a I discharge therein, electrodes adaptedto support an ionizing. discharge through said atmosphere, said electrodes including a plurality of'ano'des', conducting'shields arranged about said anodes. each of said shields terminating in substantially the same plane-as the end of the corresponding.
, anode, and aninsul'ating member arranged about each of said shields, i said shields and-members being provided'with openings therein to. permit the passage of the discharge therethroughfi V 6. An electrical space discharge device comprising an nvelope containing an ionizable atmosphere at a pressure sufliciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, said electrodes including a cylindrical anode, a hollow cylindrical conducting shield arranged around said anode and spaced therefrom, said anode projecting beyond the end of said shield, and'a hollow cylindrical insulating member arranged about said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough.
'7. An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufficiently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a shield arranged about one of said electrodes, and an insulating member arranged about said shield, said shield and member having openings therein for the passage of the discharge therethrough, said anode having a portion projecting beyond said shield, the portion of said member adjacent said opening projecting beyond said shield to thereby form a restricted chamber to thereby prevent fiashing to said shield.
8. An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufficiently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a conducting shield arranged about and terminating adjacent the end of at least one of said electrodes, and an insulating member arranged about said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough, said member and said shield being constructed and arranged to provide an insulating space therebetween.
9. In an electrical space discharge device a conducting sleeve, an anode element arranged at least partially within said conducting sleeve in electrical contact therewith, and an electrical conducting member arranged at least partially within the conducting sleeve and spaced from said anode element, said conducting member being in electrical contact with said sleeve at a point on said member nearest said anode element.
10. In an electrical space discharge device a hollow cylindrical conductor, an anode element arranged within one end thereof in electrical contact therewith, and an electrical conducting member projecting at least partially within said conductor from the other end thereof, and being spaced from said anode element, said member 'makin electrical contact with said conductor at a point on said member nearest said anode element.
11. In an electrical space discharge device a conducting sleeve, an anode element arranged within said conducting sleeve in electrical contact therewith, and an electrical conducting member having at least a portion thereof arranged within said sleeve, the portion of said conducting member arranged within said sleeve being in electrical contact throughout its length with said sleeve, said conducting member being spaced from said anode element.
12. An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufficiently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a conducting shield arranged about at least one of said electrodes, and an insulating member arranged about said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough, said member and said shield being constructed and arranged to provide an insulating space therebetween, the distance between said shield and member across said space being of the order of the mean free path of the electrons in said atmosphere or less.
13. An electrical space discharge device comprising an envelope containing an ionizable atmosphere at a pressure sufiiciently high to produce substantial ionization upon the occurrence of a discharge therein, electrodes adapted to support an ionizing discharge through said atmosphere, a conducting shield arranged about at least one of said electrodes and spaced therefrom a distance of the order of the mean free path of the electrons in said atmosphere or less, and an insulating member arrangedabout said shield, said shield and member being provided with openings therein to permit the passage of the discharge therethrough, the distance between said shield and member across said space being of the order of the mean free path of the electrons in said atmosphere, or less.
PAUL W. STUTSMAN.
US426892A 1942-01-15 1942-01-15 Electrical gaseous discharge device Expired - Lifetime US2404413A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US426892A US2404413A (en) 1942-01-15 1942-01-15 Electrical gaseous discharge device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US426892A US2404413A (en) 1942-01-15 1942-01-15 Electrical gaseous discharge device

Publications (1)

Publication Number Publication Date
US2404413A true US2404413A (en) 1946-07-23

Family

ID=23692634

Family Applications (1)

Application Number Title Priority Date Filing Date
US426892A Expired - Lifetime US2404413A (en) 1942-01-15 1942-01-15 Electrical gaseous discharge device

Country Status (1)

Country Link
US (1) US2404413A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472865A (en) * 1946-02-26 1949-06-14 Raytheon Mfg Co Gaseous discharge device
US2644101A (en) * 1950-12-29 1953-06-30 Chatham Electronics Corp Anode insulating structure
US2745988A (en) * 1950-04-13 1956-05-15 Hartford Nat Bank & Trust Co Glow discharge tube and circuit therefor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472865A (en) * 1946-02-26 1949-06-14 Raytheon Mfg Co Gaseous discharge device
US2745988A (en) * 1950-04-13 1956-05-15 Hartford Nat Bank & Trust Co Glow discharge tube and circuit therefor
US2644101A (en) * 1950-12-29 1953-06-30 Chatham Electronics Corp Anode insulating structure

Similar Documents

Publication Publication Date Title
US2331398A (en) Electronic discharge device
US2018071A (en) Short wave tube
US2692350A (en) Discharge lamp and electrode
US2399003A (en) Electric discharge device
US1353976A (en) Vacuum-tube device
US2184756A (en) Electric discharge device
US2295569A (en) Gaseous electron discharge device
US2416661A (en) Dispenser type cathode electric discharge device
US2870366A (en) Electric discharge tube of the kind comprising a cathode of the indirectly heated type
US2797348A (en) Grid system for gaseous discharge device
US1874753A (en) Controlled arc discharge apparatus
US2404413A (en) Electrical gaseous discharge device
US2435246A (en) Gaseous discharge device containing perforated starting electrodes
US2492666A (en) Hydrogen-filled thyratron
US2481365A (en) Gaseous discharge device
US2451556A (en) Electrode structure for gaseous discharge devices
US2556855A (en) Gaseous discharge device
US2292081A (en) Electric discharge device
US2381632A (en) Electron discharge device
US2195913A (en) Electric discharge tube
US2281878A (en) Valve tube and casing therefor
US2396807A (en) Discharge device and cathode therefor
US2069814A (en) Electric discharge device
US2541335A (en) Glow discharge device
US2473358A (en) Cathode coating for electron discharge devices