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US1765605A - Space-current device - Google Patents

Space-current device Download PDF

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Publication number
US1765605A
US1765605A US26339A US2633925A US1765605A US 1765605 A US1765605 A US 1765605A US 26339 A US26339 A US 26339A US 2633925 A US2633925 A US 2633925A US 1765605 A US1765605 A US 1765605A
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US
United States
Prior art keywords
grid
space
electrode
current device
triode
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
US26339A
Inventor
Ilia E Mouromtseff
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.)
Westinghouse Electric Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to US26339A priority Critical patent/US1765605A/en
Application granted granted Critical
Publication of US1765605A publication Critical patent/US1765605A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • H01J19/32Anodes
    • H01J19/34Anodes forming part of the envelope
    • 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
    • H01J2893/0002Construction arrangements of electrode systems
    • H01J2893/0003Anodes forming part of vessel walls
    • H01J2893/0004Anodes formed in central part

Definitions

  • My invention relates to space-current devices and particularly to triode vacuum-tube devices.
  • An object of my invention is to provide, in
  • a triode device auxiliary supporting means for a grid electrode.
  • Another object of my invention is to provide, in a triode device, a more conveniently assembled grid lead.
  • Another object of my invention is to simplify the problems of manufacture of a highpower triode.
  • My invention provides means whereby a lower-resistance lead to the grid and a greater lateral stiflness thereof are obtained, and whereby inspection means are provided for the positioning of the grid electrode.
  • the single figure is a view, partially in elevation and partially in section, of an embodiment of my invention.
  • a cylindrical metallic anode 1 has thinned edges to which glass members 2 and 3 are sealed.
  • the glass member 2 has an integral re-entrant portion 4 to which is attached a jacket tube 5 and on which is formed a press 6, through which cathode leadwires 7, Sand 9. are inserted.
  • the jacket tube5 has mounted, near its free end, a grid-supporting band to which are attached. the grid foundation wires 12 and 14 ⁇ .
  • the structure so far described is, in general, similar to thestructure of the prior art except that no grid lead is provided through the glass closure member 2 in the device of my invention.
  • the glass closure member 3 similarly has a re-entrant portion 15 havinga press lfi formed thereon.
  • the press 16 is in serted a grid lead seal wire 17;
  • Theupper ends of the longitudinal grid foundation Wires 12 and 1d are attached to a lead wire 18 which is connected to the seal wires 17 by a flexible member 19.
  • the member 19 is formed of a flat sheet of metal having a pinrality of longitudinal slits defining a plurality of bars 20 and rolled around a small cylinder of substantially the size of the wires 17 and 18. The ends are then pressed toward each other to expand the middle section into a flexible portion intermediate a plurality of hub portions 21, which has a considerable lengthwise elasticity, but is relatively stiff laterally.
  • the seal wire 17, the flexible member 19 and the foundation wire 18 constitute a grid lead which is substantially straight and which is of a minimum length, having a minimum ohmic resistance and a minimum inductance.
  • the low impedance values ensure a minimum energy loss and enable the structure to carry a larger current without undue heating or other difficulty.
  • the presence of the glass closure 3 at the upper end of the anode structure -1 permits inspection of the upper end of the grid structure and accurate positioning centrally with much less difficulty than occurs when the end of the anode 1 is closed by an opaque portion.
  • a space-current device having an envelope and an electrode and means for sup porting said electrode from opposite ends of said envelope including a hollow spheroid having co-directional slits in its walls.
  • a space-current device having a tubular electrode, another electrode therein, and means, attached to the opposite ends of said first electrode, for supporting and positioning said other electrode, including two endhubs connected by curvedbars of sheet metal evenly spaced around their peripheries.
  • an electrode In a vacuum tube, an electrode, supports therefor at each end of the tube, one of said supports including a yieldable connection comprising a cage-like member having bars co-directional with said supports.

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  • Electrolytic Production Of Metals (AREA)

Description

SPACE CURRENT DEVICE Filed April 28, 1925 h m Rf H m W. E m I I WITNESSES: 5, #44602.
Patented June 24, 1930 UNITED STATES PATENT ILIA E. MOUROMTSEFF, OF WILKINSBU'RG, PENNSYLVANIA, ASSIGNQB TO WESTING- HOUSE ELECTRIC & MANUFACTURING COMZP{LN 'Y, A CORPORATION OF PENNSYL- VANIA SPACE-CURRENT DEVICE Application filed April 28, 1925-. Serial No. 26,339.
My invention relates to space-current devices and particularly to triode vacuum-tube devices.
An object of my invention is to provide, in
. a triode device, auxiliary supporting means for a grid electrode.
Another object of my invention is to provide, in a triode device, a more conveniently assembled grid lead.
Another object of my invention is to simplify the problems of manufacture of a highpower triode.
In the manufacture of high-power triode devices, it has been customary to embody therein a tubular metallic anode having an open end and a closed end, formed by drawing from a blank sheet of metal. In this construction, it has been customary to provide a glass portion closing the open end of the cylinder and having members adapted to support a cathode and a grid electrode. There is also provided a plurality of seal wires making connection to the grid and cathode members. This construction has been found satisfactory for service in the generation of radio-frequency oscillations of about the order of 1500 kc. or less, but, at higher frequencies, difiiculty has been experienced in conducting the charging current to the grid through the seals as previously made. Also, some difiiculty has been experienced in accurately positioning the unsupported end of the grid structure.
My invention provides means whereby a lower-resistance lead to the grid and a greater lateral stiflness thereof are obtained, and whereby inspection means are provided for the positioning of the grid electrode.
Other objects and structural details of my invent-ion will be apparent from the following description, when read in connection with the accompinying drawing, wherein:
The single figure is a view, partially in elevation and partially in section, of an embodiment of my invention.
In the drawing, a cylindrical metallic anode 1 has thinned edges to which glass members 2 and 3 are sealed. The glass member 2 has an integral re-entrant portion 4 to which is attached a jacket tube 5 and on which is formed a press 6, through which cathode leadwires 7, Sand 9. are inserted.
The jacket tube5 has mounted, near its free end, a grid-supporting band to which are attached. the grid foundation wires 12 and 14}. The structure so far described is, in general, similar to thestructure of the prior art except that no grid lead is provided through the glass closure member 2 in the device of my invention. I
The glass closure member 3 similarly has a re-entrant portion 15 havinga press lfi formed thereon. Through the press 16 is in serted a grid lead seal wire 17; Theupper ends of the longitudinal grid foundation Wires 12 and 1d are attached to a lead wire 18 which is connected to the seal wires 17 by a flexible member 19. The member 19 is formed of a flat sheet of metal having a pinrality of longitudinal slits defining a plurality of bars 20 and rolled around a small cylinder of substantially the size of the wires 17 and 18. The ends are then pressed toward each other to expand the middle section into a flexible portion intermediate a plurality of hub portions 21, which has a considerable lengthwise elasticity, but is relatively stiff laterally.
The seal wire 17, the flexible member 19 and the foundation wire 18 constitute a grid lead which is substantially straight and which is of a minimum length, having a minimum ohmic resistance and a minimum inductance. The low impedance values ensure a minimum energy loss and enable the structure to carry a larger current without undue heating or other difficulty.
The presence of the glass closure 3 at the upper end of the anode structure -1 permits inspection of the upper end of the grid structure and accurate positioning centrally with much less difficulty than occurs when the end of the anode 1 is closed by an opaque portion.
By this construction, I am enabled to simplify the manufacture of triode devices and am enabled to pass to the grid member a much higher charging current than is possible by previous constructions.
While I have shown but a single embodiment of my invention in the accompanying description, it is capable of various changes and modifications and it is desired, therefore, that only such limitations shall be imposed as are imposed by the prior art or by the accompanying claims.
I claim as my invention:
1. A space-current device having an envelope and an electrode and means for sup porting said electrode from opposite ends of said envelope including a hollow spheroid having co-directional slits in its walls.
2. A space-current device having a tubular electrode, another electrode therein, and means, attached to the opposite ends of said first electrode, for supporting and positioning said other electrode, including two endhubs connected by curvedbars of sheet metal evenly spaced around their peripheries.
3. In a vacuum tube, an electrode, supports therefor at each end of the tube, one of said supports including a yieldable connection comprising a cage-like member having bars co-directional with said supports.
In testimony whereof, I have hereunto subscribed my name this 22nd day of April ILIA E. MOUROMTSEFF.
US26339A 1925-04-28 1925-04-28 Space-current device Expired - Lifetime US1765605A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US26339A US1765605A (en) 1925-04-28 1925-04-28 Space-current device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US26339A US1765605A (en) 1925-04-28 1925-04-28 Space-current device

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US1765605A true US1765605A (en) 1930-06-24

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422819A (en) * 1944-08-15 1947-06-24 Eitel Mccullough Inc External anode electron tube
US2454786A (en) * 1942-07-17 1948-11-30 Standard Telephones Cables Ltd Electron discharge apparatus
US2523779A (en) * 1949-03-10 1950-09-26 Gen Electric Ionization gauge

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454786A (en) * 1942-07-17 1948-11-30 Standard Telephones Cables Ltd Electron discharge apparatus
US2422819A (en) * 1944-08-15 1947-06-24 Eitel Mccullough Inc External anode electron tube
US2523779A (en) * 1949-03-10 1950-09-26 Gen Electric Ionization gauge

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