[go: up one dir, main page]

US2030362A - Space discharge device - Google Patents

Space discharge device Download PDF

Info

Publication number
US2030362A
US2030362A US696974A US69697433A US2030362A US 2030362 A US2030362 A US 2030362A US 696974 A US696974 A US 696974A US 69697433 A US69697433 A US 69697433A US 2030362 A US2030362 A US 2030362A
Authority
US
United States
Prior art keywords
grid
anode
space discharge
stem
discharge device
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
US696974A
Inventor
William W Eitel
Mccullough Jack
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.)
Heintz & Kaufman Ltd
Original Assignee
Heintz & Kaufman Ltd
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 Heintz & Kaufman Ltd filed Critical Heintz & Kaufman Ltd
Priority to US696974A priority Critical patent/US2030362A/en
Application granted granted Critical
Publication of US2030362A publication Critical patent/US2030362A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00Details of vacuum tubes of the types covered by group H01J21/00
    • H01J19/42Mounting, supporting, spacing, or insulating of electrodes or of electrode assemblies
    • 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

Definitions

  • One of the objects of our invention is the provision of a self-supporting grid structure.
  • Another object of our invention is the provision of a grid structure which possesses a high degree of rigidity.
  • Still another object of our invention is the provision of a grid structure which may be produced expeditiously and economically.
  • a further object of our invention is to provide a grid having uniform field characteristics and one which minimizes distortion of the electron stream.
  • Another object is to provide a unique grid mounting.
  • Figure l is a vertical sectional view of a space discharge device incorporating the grid structure of our invention.
  • Figure 2 is a horizontal sectional view taken in a plane indicated by the line 2-2 of Figure 1.
  • Figure 3 is a plan view of a modified form of supporting means for the grid structure.
  • Figure 4 is a vertical sectional view of the structure shown in Figure 3.
  • our invention comprises a space discharge device provided with the usual evacuated envelope and contain g electrodes suitably mounted therein in coo erative relationship.
  • a third or control element is disposed between the electrodes and comprises a plurality of conductors disposed in spaced relationship about the axis of one of the electrodes, the conductors being fastened to a supporting member at one end, and interconnected at the other.
  • the grid with a frame comprising a plurality .emitting element or filament 6.
  • wires suitably anchored or fastened in the tube stem and which serve to support the grid rigidly.
  • the presence of these wires necessarily means that the spacing of the various cooperating elements must be increased to allow room for the supports.
  • These supports also tend, by the large surface exposed, to increase the grid to .anode capacity, and at the same time cause an obstruction to the electron flow which causes blank spots, orshadows, on the anode on which few electrons fall. Other portions of the anode may also become overcrowded and overheat,
  • the improved grid structure of our invention removes these objections; the only wires present being those which actually function as members of the control element. This removal of the support wires allows the elements to be spaced in such relationship as to provide a space discharge device possessing greatly improved characteristics, and provides uniform current densities on the anode.
  • the space discharge device of our invention comprises an evacuated envelope 2, provided at one end. thereof with the stem 3.
  • a rod 4 of heat resistant material is secured in the stem and serves as a support for the electron Leads I are provided which are secured to the free ends of the filament and are brought out through the stem adjacent the rod 4.
  • the grid structure is made up of ametallicband ll suitably secured, as by means of spot welding, to the ring 9.
  • This band has a plurality of wires l2 secured thereto and extending upwardly soas to lie in spaced radial relationship about the filament 6.
  • the upper ends of the wires l2 converge for a distance and are preferably crossed at a point l3 and secured together by welding.
  • An anode I4 is provided, which surrounds the grid and filament elements; and supports l6, secured in the envelope 2 and to the anode, are provided for holding the anode in position.
  • a terminal I] passing through the envelope at the top thereof is connected by a lead l8 to one of the anode supports.
  • Figures 3 and 4 illustrate a means for providing a maximum of rigidity.
  • the wires l2 are disposed as shown in Figure 1 except that where they cross at the top each wire is provided with an offset portion I9 which, together, provide an aperture 2
  • the support rod 4 is provided with an insulating projection or head 22 which is adapted to seat in the aperture, thereby adding the rigidity of the rod to that of the grid structure.
  • a space discharge tube comprising an envelope having a reentrant stem, a concentric anode, cathode and control electrode contained therein and mounted to have axes common with that of said stem, and support means for said control electrode consisting solely of a plurality of spaced conductive risers separately fused directly to the side wall of said stem.
  • a space discharge tube comprising an envelope having a reentrant stem, a concentric anode, cathode and control electrode contained therein and mounted to have axes common with that of said stem, and support means for said control electrode consisting solely of a plurality of spaced conductive risers separately fused directly to the side wall of said stem, said risers being inserted in the same plane and in equal spaced relationship around said side wall.
  • a space discharge tube comprising an envelope having a reentrant stem, a concentric anode, cathode and control electrode contained therein and mounted to have axes common with that of said stem, and support means for said control electrode consisting solely of a plurality of spaced conductive risers separately fused directly to the side wall of said stem, at least one of said risers passing completelythrough said side wall at the point of fusion to form an outside connection for said control electrode.
  • a space discharge device having an evacuated envelope and cooperating electrodes therein including a cathode elongated longitudinally of said tube and positioned substantially in the axis thereof, a control electrode enclosing said cathode v consisting of a. ring support, and a plurality of hairpin-shaped wires having the open ends thereof fastened to said support, and the bends thereof crossing at substantially said axis, said bends being fastened together .at said crossing.
  • a space discharge tube having an envelope, an axial cathode therein, an anode surrounding said cathode and a grid concentrically positioned between said anode and. cathode, said grid consisting solely of a plurality of hairpin-shaped wires disposed to describe a cylinder and a ring support therefor, the open ends of said hairpins being welded to said support, and the bends crossing and contacting each other above said cathode at said crossing, said bends being fastened together to maintain the straight runs of said hairpins in spaced relation.

Landscapes

  • Discharge Lamps And Accessories Thereof (AREA)

Description

Feb. 11, 1936. w w rr- ET AL 2,030,362
SPACE DISCHARGE DEVICE Filed Nov. 7, 1955 INVENTORS WILL/AM w. E/TEL.
JACK Mc CULLOUGH.
ATTORNEY Patented Feb. 11, 1 936 PATENT. OFFICE SPACE nrscmmoE DEVICE William w. Eitcl and Jack McCullough, San Bruno, Calif., assignors to Heintz & Kaufman, #6., San Francisco, Call! a corporation of Application November 7, 1933, Serial No. 696,971
5 Claims. (Cl. 250-275) Our invention relates to space' discharge devices and particularly to the control element or grld structure for such devices.
One of the objects of our invention is the provision of a self-supporting grid structure.
Another object of our invention is the provision of a grid structure which possesses a high degree of rigidity.
Still another object of our invention is the provision of a grid structure which may be produced expeditiously and economically.
A further object of our invention is to provide a grid having uniform field characteristics and one which minimizes distortion of the electron stream.
Another object is to provide a unique grid mounting.
Other objects of our invention will be apparent or will be specifically pointed out in the description forming a part of this specification, but we do not limit ourselves to the embodiment of our invention herein described, as various forms may be adopted within the scope of the claims.
Referring to the drawing 2 Figure l is a vertical sectional view of a space discharge device incorporating the grid structure of our invention.
Figure 2 is a horizontal sectional view taken in a plane indicated by the line 2-2 of Figure 1.
Figure 3 is a plan view of a modified form of supporting means for the grid structure; and
Figure 4 is a vertical sectional view of the structure shown in Figure 3. v
Considered broadly, our invention comprises a space discharge device provided with the usual evacuated envelope and contain g electrodes suitably mounted therein in coo erative relationship. A third or control element is disposed between the electrodes and comprises a plurality of conductors disposed in spaced relationship about the axis of one of the electrodes, the conductors being fastened to a supporting member at one end, and interconnected at the other.
One of the difliculties encountered in the construction of space discharge devices is the provision of a satisfactory mounting for the control element or grid. Due to its location between the anode and the cathode, it is imperative that the mounting be sufliciently rigid to prevent vibrational movement of the grid proper so as not to cause fluctuating variations in grid to anode capacity which would disturb the balance of the circuits in which the device was operating.
For this reason it is the usual practice to provide the grid with a frame comprising a plurality .emitting element or filament 6.
of wires suitably anchored or fastened in the tube stem and which serve to support the grid rigidly. The presence of these wires necessarily means that the spacing of the various cooperating elements must be increased to allow room for the supports. These supports also tend, by the large surface exposed, to increase the grid to .anode capacity, and at the same time cause an obstruction to the electron flow which causes blank spots, orshadows, on the anode on which few electrons fall. Other portions of the anode may also become overcrowded and overheat,
The improved grid structure of our invention removes these objections; the only wires present being those which actually function as members of the control element. This removal of the support wires allows the elements to be spaced in such relationship as to provide a space discharge device possessing greatly improved characteristics, and provides uniform current densities on the anode.
In greater detail the space discharge device of our invention comprises an evacuated envelope 2, provided at one end. thereof with the stem 3. A rod 4 of heat resistant material is secured in the stem and serves as a support for the electron Leads I are provided which are secured to the free ends of the filament and are brought out through the stem adjacent the rod 4.
Secured in the stem are a plurality of risers 8 which carry a ring 9 comprising the'supporting base for the grid structure. The grid structure is made up of ametallicband ll suitably secured, as by means of spot welding, to the ring 9. This band has a plurality of wires l2 secured thereto and extending upwardly soas to lie in spaced radial relationship about the filament 6. The upper ends of the wires l2 converge for a distance and are preferably crossed at a point l3 and secured together by welding.
An anode I4 is provided, which surrounds the grid and filament elements; and supports l6, secured in the envelope 2 and to the anode, are provided for holding the anode in position. A terminal I], passing through the envelope at the top thereof is connected by a lead l8 to one of the anode supports.
While the grid structure as shown in Figure 1 is self-supporting, it is desirable, in some cases, to provide additional supportfor this element. Figures 3 and 4 illustrate a means for providing a maximum of rigidity. The wires l2 are disposed as shown in Figure 1 except that where they cross at the top each wire is provided with an offset portion I9 which, together, provide an aperture 2|. The support rod 4 is provided with an insulating projection or head 22 which is adapted to seat in the aperture, thereby adding the rigidity of the rod to that of the grid structure.
The specific form of grid structure just described possesses marked superiority over the usual types of grid construction in simplicity and ease of construction, in stability against vibrations and in lending itself to improved design of all types of electronic operated devices.
It is to be understood that, while the grid structure of our invention is shown as being incorporated in the familiar form of three-element vacuum tube, our device may be incorporated in any type of device where the control of electron flow is desirable.
We claim:
1. A space discharge tube comprising an envelope having a reentrant stem, a concentric anode, cathode and control electrode contained therein and mounted to have axes common with that of said stem, and support means for said control electrode consisting solely of a plurality of spaced conductive risers separately fused directly to the side wall of said stem.
2. A space discharge tube comprising an envelope having a reentrant stem, a concentric anode, cathode and control electrode contained therein and mounted to have axes common with that of said stem, and support means for said control electrode consisting solely of a plurality of spaced conductive risers separately fused directly to the side wall of said stem, said risers being inserted in the same plane and in equal spaced relationship around said side wall.
3. A space discharge tube comprising an envelope having a reentrant stem, a concentric anode, cathode and control electrode contained therein and mounted to have axes common with that of said stem, and support means for said control electrode consisting solely of a plurality of spaced conductive risers separately fused directly to the side wall of said stem, at least one of said risers passing completelythrough said side wall at the point of fusion to form an outside connection for said control electrode.
4. A space discharge device having an evacuated envelope and cooperating electrodes therein including a cathode elongated longitudinally of said tube and positioned substantially in the axis thereof, a control electrode enclosing said cathode v consisting of a. ring support, and a plurality of hairpin-shaped wires having the open ends thereof fastened to said support, and the bends thereof crossing at substantially said axis, said bends being fastened together .at said crossing.
5. A space discharge tube having an envelope, an axial cathode therein, an anode surrounding said cathode and a grid concentrically positioned between said anode and. cathode, said grid consisting solely of a plurality of hairpin-shaped wires disposed to describe a cylinder and a ring support therefor, the open ends of said hairpins being welded to said support, and the bends crossing and contacting each other above said cathode at said crossing, said bends being fastened together to maintain the straight runs of said hairpins in spaced relation.
WILLIAM W. EITEL. JACK MCCULLOUGH.
US696974A 1933-11-07 1933-11-07 Space discharge device Expired - Lifetime US2030362A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US696974A US2030362A (en) 1933-11-07 1933-11-07 Space discharge device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US696974A US2030362A (en) 1933-11-07 1933-11-07 Space discharge device

Publications (1)

Publication Number Publication Date
US2030362A true US2030362A (en) 1936-02-11

Family

ID=24799270

Family Applications (1)

Application Number Title Priority Date Filing Date
US696974A Expired - Lifetime US2030362A (en) 1933-11-07 1933-11-07 Space discharge device

Country Status (1)

Country Link
US (1) US2030362A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422828A (en) * 1941-10-10 1947-06-24 Eitel Mccullough Inc Thermionic tube
US2431767A (en) * 1943-08-14 1947-12-02 Eitel Mccullough Inc Electrode mounting in electron discharge tube
US2447501A (en) * 1941-02-15 1948-08-24 Int Standard Electric Corp Grid electrode for electron discharge devices
US2750560A (en) * 1951-09-25 1956-06-12 Bendix Aviat Corp Electron discharge tube
US2901657A (en) * 1956-07-30 1959-08-25 Eitel Mccullough Inc Electrode structure for electron

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447501A (en) * 1941-02-15 1948-08-24 Int Standard Electric Corp Grid electrode for electron discharge devices
US2422828A (en) * 1941-10-10 1947-06-24 Eitel Mccullough Inc Thermionic tube
US2431767A (en) * 1943-08-14 1947-12-02 Eitel Mccullough Inc Electrode mounting in electron discharge tube
US2750560A (en) * 1951-09-25 1956-06-12 Bendix Aviat Corp Electron discharge tube
US2901657A (en) * 1956-07-30 1959-08-25 Eitel Mccullough Inc Electrode structure for electron

Similar Documents

Publication Publication Date Title
US2030362A (en) Space discharge device
US1628982A (en) Electron-discharge device
US2358200A (en) Grid assembly structure
US2469331A (en) Electron tube
US2472942A (en) Electron tube
US2859371A (en) Electron discharge device structure
US2554078A (en) Electron discharge device and locking means therefor
US2350270A (en) Cathode assembly structure
US2267450A (en) Electron discharge device
US2003012A (en) Grid glow tube structure
US3407328A (en) Directly heated cathode supporting structure
US1961269A (en) Electron discharge apparatus
US2430218A (en) Electron tube with secondary emissive grid
US3213313A (en) Frame support for grid
US2111602A (en) Electron discharge device
US2284495A (en) Electron tube mount of the shielded element type
US2010159A (en) Thermionic tube
US2222669A (en) Electrode structure
US2170410A (en) Electron discharge tube
US1565570A (en) Electron-discharge device
US2376040A (en) Electron tube
US2400081A (en) Thermionic tube
US3254259A (en) Electron discharge device and cantilever support means therefor
US1980341A (en) Vacuum tube grid construction
US1480219A (en) Vacuum tube