US1731889A - Gaseous conduction device - Google Patents

Gaseous conduction device Download PDF

Info

Publication number
US1731889A
US1731889A US570975A US57097522A US1731889A US 1731889 A US1731889 A US 1731889A US 570975 A US570975 A US 570975A US 57097522 A US57097522 A US 57097522A US 1731889 A US1731889 A US 1731889A
Authority
US
United States
Prior art keywords
electrode
tube
electrodes
cathode
anode
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
US570975A
Inventor
Donle Harold Potter
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 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 Co filed Critical Raytheon Co
Priority to US570975A priority Critical patent/US1731889A/en
Application granted granted Critical
Publication of US1731889A publication Critical patent/US1731889A/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
    • H01J17/38Cold-cathode tubes
    • H01J17/40Cold-cathode tubes with one cathode and one anode, e.g. glow tubes, tuning-indicator glow tubes, voltage-stabiliser tubes, voltage-indicator tubes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00Discharge tubes and lamps
    • H01J2893/0064Tubes with cold main electrodes (including cold cathodes)
    • H01J2893/0065Electrode systems
    • H01J2893/0067Electrode assembly without control electrodes, e.g. including a screen

Definitions

  • Figure l illustrates one form of apparatus involving my invention for halt wave rectifi-y cation, the tube being shown in longitudinal section and the circuit being shown diagrammatically.
  • higs. 2 and 3 are longitudinal sectional views oil tubes with modified electrode construction.
  • 'lhe electrodes d and 5 are of suitable con- .fducting material enclosed in an envelope or fvessel such as the tube 0.
  • This tube may be ot ordinary glass and should be exhausted or evacuated to a suitable degree.
  • l have found a pressure of approximately: ⁇ a millimeter ot mercury to be satisfactory. ⁇
  • An 1nert gas may be present in the tube at a corren Spending pressure.
  • the electrode d is provided with an orilice or hole 7 in the approximate center olf' its 'lace opposite the active surface of the electrode 5.
  • the electrode l has a cylindrical part 8 which. lorms a wall spaced radially from the airis oi:n
  • the other electrode 5 may also have a cylindrical extension 9.
  • Figure 1 shows a circuit with an alternat ing current generator 10 and a transformer 11.
  • a pulsating direct current flows in the work circuit from the imperforate electrode 5 to the perforate electrode 4.
  • an ionization glow very nearly lls the central part of the perforate cathode electrode 4.
  • This glow is separated from the walls of the cathode by a narrow dark space. Projecting from the anode 5 through the orifice 7 a small conical column of very intense light will be seen. It is impossible while watching the device in operation, to distinguish the exact .junction bctween the general glow throughout the interior of the cathode and this brilliant column emanating from the anode.
  • the imperforate electrode 12 is of a substantially larger mass than the electrode 5.
  • the electrode 13 in this case is provided with an orifice 14 leading to a chamber 15 which is vclosed at 16 at the top. In some cases the larger mass is desirable in order to provide additional thermal capacity.
  • the closed end. 16 of the chamber serves to shield the tube from the secondary aXial bombardment which passes through the orifice 14. This end portion 16 also serves to supplement the electrostatic field tending to drive electrons through the orifice when the electrode 13 is the cathode.
  • the electrodes should be as close together as possible, to eliminate a two-way discharge between the faces.
  • the electrodes may be initially placed or adj usted' fartherapart for lower voltages where the electrons will necessarily be required to traverse a longer distance in order to absorb sufficient energy to ionize the gaseous atoms. With higher potentials the electrons start out. at high velocities and acquire sufficient energy a very short distance from their starting points. In such cases the electrodes inust be very close together.
  • the electrodesy should be of suiicient/area and mass to avoid overheating u nder the conditions for which the tube is designed.
  • the anode 17 is supported directly by the glass of the tube 21 and the cathode 18 is supported in any suitable manner away from the inner wall of the tube.
  • the cathode has a comparatively thin wall extending parallel to the axis of the orifice 19 and forms the chamber 2O in which the ionization takes place. lin some cases it may be desirable to space the cathode away from the wall of the tube for instance to avoid the effect of inequalities of manufacture in dimensions and the eect of possible expansion of the electrodes or contraction of the tube.
  • the end of the cathode adjacent the anode constitutes the face corresponding to the faces of the other forms of cathodes.
  • lin my former application referred to, l have specifically claimed the full wave rectiiication form of device having two anodes. While such form of tube is perhaps more ecient than two single anode tubes as herein shown and claimed, nevertheless,'the single anode tube device has advantages in simplicity and cheapness of construction and avoids the necessity of a comparatively wide separation of two anodes Within a single tube. 'llwo of the single anode tubes may be connected in the divided transformer circuit where full wave rectification is desired.
  • a rectifier comprising an envelope containing a rare inert gas, two flat faced disk electrodes mounted in said container with their adjacent faces so close together as to minimize ionization under one direction of applied potential, one of said electrodes having a passage opposite the face of the other to provide an ionizing path.
  • a gaseous discharge device comprising a hollow cathode having an interior active surface which is solid at operating temperatures, an anode presented to the interior of said hollow cathode from the exterior thereof, insulating material disposed around the outer surfaces of said electrodes to maintain them in desired position and restrict the discharge to the interior of said cathode.
  • a gaseous discharge device comprising a hollow electrode having an opening in one side, another electrode presented to said opening-and spaced therefrom a distance of the order of magnitude of the mean free path of the electrons present in the gas, insulating material surrounding both of said electrodes to maintain them in desired relationship to each other and contacting with the outer sur* faces only of the electrodes.

Landscapes

  • Lasers (AREA)
  • Electron Sources, Ion Sources (AREA)

Description

Oct. 15, 19Z9 H. P. DONLE Y i 7311389 GAsEoUs coNDUcTIoN DEVICE Filed June 26, 1.922
Patented Ot. 15, 1929 UNITED STATES PAT-ENT OFFICE 'HARLD POTTER DONLE, 0F MERIDEN, CONNECTICUT, ASSIGNCR, BY MESNE ASSIGN- MENTS, T0 RAYTHEON INC., 0F CAMBRIDGE, MASSACHUSETTS, A. CRPORATIN i DF MASSACHUSETTS GASEOU'S CONDUCTION BEVICE Application led June 26,
ABy suitably forming and locating the electrodes I have found that I can secure predominating one-way transmission and consequently rectification.
ll have been able to obtain rectification 'in this way with several diderent constructions.
Figure l illustrates one form of apparatus involving my invention for halt wave rectifi-y cation, the tube being shown in longitudinal section and the circuit being shown diagrammatically.
higs. 2 and 3 are longitudinal sectional views oil tubes with modified electrode construction.
'lhe electrodes d and 5 are of suitable con- .fducting material enclosed in an envelope or fvessel such as the tube 0. This tube may be ot ordinary glass and should be exhausted or evacuated to a suitable degree. l have found a pressure of approximately:` a millimeter ot mercury to be satisfactory.` An 1nert gas may be present in the tube at a corren Spending pressure.
The electrode d is provided with an orilice or hole 7 in the approximate center olf' its 'lace opposite the active surface of the electrode 5.
rlhese electrodes are placed' with their facesl so close together as to prevent or minimize ionization between the adjacent surfaces. The electrode l has a cylindrical part 8 which. lorms a wall spaced radially from the airis oi:n
. the orice 7. The other electrode 5 may also have a cylindrical extension 9.
192e. serial No. 570,975.
Figure 1 shows a circuit with an alternat ing current generator 10 and a transformer 11. When the tube is connected as shown a pulsating direct current flows in the work circuit from the imperforate electrode 5 to the perforate electrode 4. When this type of tube is in operation an ionization glow very nearly lls the central part of the perforate cathode electrode 4. This glow is separated from the walls of the cathode by a narrow dark space. Projecting from the anode 5 through the orifice 7 a small conical column of very intense light will be seen. It is impossible while watching the device in operation, to distinguish the exact .junction bctween the general glow throughout the interior of the cathode and this brilliant column emanating from the anode.
For the purpose of further explaining what I understand to be the action of this device I may state my belief as to its theory of operation. When the perforate electrode l is sub3ected to the negative potential of the A. C. wave to be rectified thus making the lmperforate electrode 5 the anode and the periorate electrode l the cathode,- all negative particles within the cathode will be repelled from its walls toward its center and literally forced through the hole 7 to the anode 5. The particles moving from the cathode to the anode under normal conditions in a tube having a cathode oi approXimately li diameter will collide with gas molecules alter traveling about fi@ of an inch. llhe electrons resulting from such collisions will pass axially of the tube and through the relatively large current to pass during the "corresponding half wave of the alternating potential to be rectified. i
On the other hand, when the alternating potential reverses, so making the electrode 4 temporarily positive, the few negative particles which may pass through the hole 7 or may otherwise be within the wallsof the electrode 4 encounter lonly a wealr electrostatic field which does not tend to draw them strongly in anyparticular direction. Consequently, they do not attain sufficient velocity to produce substantial ionization. Other negative particles or electrons which are located between the opposing surfaces of the two electrodes but which do not pass through the orifice 7 will travel directly to the electrode 4 (now positively charged) without attaining sufiicient velocity to cause ionization.
20j Consequently, no current or only a small current can pass through the tube when the alternating potential to be rectified is applied in this inverse direction.
In the construction shown in Figure 2 the imperforate electrode 12 is of a substantially larger mass than the electrode 5. The electrode 13 in this case is provided with an orifice 14 leading to a chamber 15 which is vclosed at 16 at the top. In some cases the larger mass is desirable in order to provide additional thermal capacity. The closed end. 16 of the chamber serves to shield the tube from the secondary aXial bombardment which passes through the orifice 14. This end portion 16 also serves to supplement the electrostatic field tending to drive electrons through the orifice when the electrode 13 is the cathode. I wish it understood that the relative size and proportions of the various parts may be modified within the scope of my invention, but in any case the space between the adjacent faces of the electrodes shouldbe less than the free mean path required for ionization.
For high voltages the electrodes should be as close together as possible, to eliminate a two-way discharge between the faces. The electrodes may be initially placed or adj usted' fartherapart for lower voltages where the electrons will necessarily be required to traverse a longer distance in order to absorb sufficient energy to ionize the gaseous atoms. With higher potentials the electrons start out. at high velocities and acquire sufficient energy a very short distance from their starting points. In such cases the electrodes inust be very close together.
In any case the electrodesy should be of suiicient/area and mass to avoid overheating u nder the conditions for which the tube is designed. f
The theory of operation above set forth as to the device of Figure 1 also applies to that of Figure 2. When the electrode 13 becomes negative electrons are vigorously repelled from the walls of the chamber 15 toward its center and through the orifice 14 axially toward the anode 12. In this movement they set up extensive ionization and consequently the device becomes a good conductor for the negative half-wave of potential applied to the electrode 13. On the other hand, when the electrode 12 is negatively charged the electrons repelled from it to the adjacent face of the electrode 13 travel so short a distance that ionization is absent or negligible. Such of them as are in the orifice 14 or as are propelled into it are not strongly attracted by the walls of the chamber 15 in any particular direction and they therefore cause little, if any, ionization. Consequently for the half wave which makes the electrode 12 temporarily a cathode, the conductivity of the tube is negligible.
I have referred to the tube as being evacuated or exhausted to a suitable degree. -It will be understood from this that I consider it necessary that a tube contain some gas in order that ionization can take place. 'Various gases may be employed, but, of course, the gas should be inert with respect to the electrodes so that no deleterious effect is produced. Nitrogen, helium, neon, argon and even hydrogen are generally considered inert with respect to various conductors commonly employed as electrodes in vacuum tube devices, and I have found them satisfactory in this case. Some gases may be more desirable than others with certain electrodes. It is desirable that the electrodes be designed so that the rectifier may operate continuously without overheating. It is, of course, Well understood that some electrodes within a vacuum tube device absorb some gases and during the operation of the tube gradually give up part of the absorbed gases when operated for any length of time. This absorption and release of gas depends quantitatively upon the particular gas and electrode material utilized. To produce a tube of long life and stability it is therefore desirable to take this into account so that the released gas may be utilized to aid in maintaining the desired pressure within the vacuum tube.
In order to determine whether or not the electrodes in any particular device are properly located, i.e. so closely spaced as to minimize ionization in the inverse current flow direction, one may apply across the terminals of the device under test a direct current potential of the order of the alternating current potential to be rectified. IVhen the imperforate electrode is made positive the tube will ionize as above described and considerable current will How. However, when the imperforate electrode is made negative there will be substantially no ionization and negligible or no current will fiow, if the spacing between the electrodes is sufficiently small for proper operation of my rectifier.
In the construction shown in Figure 3 the anode 17 is supported directly by the glass of the tube 21 and the cathode 18 is supported in any suitable manner away from the inner wall of the tube. 1n this case the cathode has a comparatively thin wall extending parallel to the axis of the orifice 19 and forms the chamber 2O in which the ionization takes place. lin some cases it may be desirable to space the cathode away from the wall of the tube for instance to avoid the effect of inequalities of manufacture in dimensions and the eect of possible expansion of the electrodes or contraction of the tube. The end of the cathode adjacent the anode constitutes the face corresponding to the faces of the other forms of cathodes. Although the construction differs mechanically and in detail from the other forms herein shown, the same theory .of operation appears to apply.
lin my former application referred to, l have specifically claimed the full wave rectiiication form of device having two anodes. While such form of tube is perhaps more ecient than two single anode tubes as herein shown and claimed, nevertheless,'the single anode tube device has advantages in simplicity and cheapness of construction and avoids the necessity of a comparatively wide separation of two anodes Within a single tube. 'llwo of the single anode tubes may be connected in the divided transformer circuit where full wave rectification is desired.
From the foregoing it will be evident that in Figs. 1 and 2 the insulating wall of the tube 6 bridges the space between the anode and cathode aroundthe discharge opening in the cathode to which the anode is presented7 thereby obstructing discharge between the' anode and the exterior of the cathode as well as accurately positioning the electrodes relatively to each other. llt will also be apparent that the bottom 4 of the member 8 in Fig. 1 constitutes an obstruction and by virtue of the surrounding insulation 6,.all the current must iiow through the opening 7 in the obstructionythe active cathode surface being confined to the interior surface of member 9..
il claim:
1. A rectifier comprising an envelope containing a rare inert gas, two flat faced disk electrodes mounted in said container with their adjacent faces so close together as to minimize ionization under one direction of applied potential, one of said electrodes having a passage opposite the face of the other to provide an ionizing path.
2. A gaseous discharge device comprising a hollow cathode having an interior active surface which is solid at operating temperatures, an anode presented to the interior of said hollow cathode from the exterior thereof, insulating material disposed around the outer surfaces of said electrodes to maintain them in desired position and restrict the discharge to the interior of said cathode.
3. A gaseous discharge device comprising a hollow electrode having an opening in one side, another electrode presented to said opening-and spaced therefrom a distance of the order of magnitude of the mean free path of the electrons present in the gas, insulating material surrounding both of said electrodes to maintain them in desired relationship to each other and contacting with the outer sur* faces only of the electrodes.
HAROLD POTTER DONLE.
US570975A 1922-06-26 1922-06-26 Gaseous conduction device Expired - Lifetime US1731889A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US570975A US1731889A (en) 1922-06-26 1922-06-26 Gaseous conduction device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US570975A US1731889A (en) 1922-06-26 1922-06-26 Gaseous conduction device

Publications (1)

Publication Number Publication Date
US1731889A true US1731889A (en) 1929-10-15

Family

ID=24281826

Family Applications (1)

Application Number Title Priority Date Filing Date
US570975A Expired - Lifetime US1731889A (en) 1922-06-26 1922-06-26 Gaseous conduction device

Country Status (1)

Country Link
US (1) US1731889A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419236A (en) * 1943-06-08 1947-04-22 Raytheon Mfg Co Electrical gaseous discharge device having constant starting characteristics
US2855820A (en) * 1955-06-10 1958-10-14 Cons Electrodynamics Corp Method of spectroscopic gas analysis
US3538371A (en) * 1968-06-04 1970-11-03 Fairchild Camera Instr Co Glow discharge display device with suppressor plate

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419236A (en) * 1943-06-08 1947-04-22 Raytheon Mfg Co Electrical gaseous discharge device having constant starting characteristics
US2855820A (en) * 1955-06-10 1958-10-14 Cons Electrodynamics Corp Method of spectroscopic gas analysis
US3538371A (en) * 1968-06-04 1970-11-03 Fairchild Camera Instr Co Glow discharge display device with suppressor plate

Similar Documents

Publication Publication Date Title
US2643297A (en) Gas discharge transmission arrangement
US1731889A (en) Gaseous conduction device
US2217187A (en) Electrical discharge apparatus
US1863702A (en) Gaseous conduction method and apparatus
US2201817A (en) Electronic discharge method and apparatus
US2504231A (en) Gaseous discharge device
US3043984A (en) Travelling wave tubes
US3614440A (en) Gas ionizer devoid of coaxial electrodes
US2680207A (en) Auxiliary electrode for ultrahighfrequency gaseous discharge switching devices
US3471733A (en) High current vacuum gap devices
US2459199A (en) Arc discharge device
US1714403A (en) Electrical apparatus
US1617179A (en) Electrical apparatus
US2192162A (en) Gas discharge tube
US2217186A (en) High current space discharge device
US1714405A (en) Electrical apparatus
US2117054A (en) Luminescent tube
US2502236A (en) Gaseous discharge device
US3248603A (en) Mean free path gaseous discharge tube and circuit thereof
US2558664A (en) Switch tube
US2716197A (en) Ion source
US2768320A (en) Microwave gas tubes
US2419236A (en) Electrical gaseous discharge device having constant starting characteristics
US3157784A (en) Ion source for a mass spectrometer
US2440511A (en) Radiation detector