US2412842A - Electronic discharge cathode - Google Patents

Electronic discharge cathode Download PDF

Info

Publication number
US2412842A
US2412842A US536996A US53699644A US2412842A US 2412842 A US2412842 A US 2412842A US 536996 A US536996 A US 536996A US 53699644 A US53699644 A US 53699644A US 2412842 A US2412842 A US 2412842A
Authority
US
United States
Prior art keywords
cathode
electron
current
magnetron
electrons
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
US536996A
Inventor
Percy L Spencer
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
Priority claimed from US412993A external-priority patent/US2411601A/en
Application filed by Raytheon Manufacturing Co filed Critical Raytheon Manufacturing Co
Priority to US536996A priority Critical patent/US2412842A/en
Priority to US674453A priority patent/US2430309A/en
Application granted granted Critical
Publication of US2412842A publication Critical patent/US2412842A/en
Priority to DER4400A priority patent/DE856669C/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J43/00Secondary-emission tubes; Electron-multiplier tubes
    • H01J43/02Tubes in which one or a few electrodes are secondary-electron emitting electrodes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/02Electrodes; Magnetic control means; Screens
    • H01J23/04Cathodes
    • H01J23/05Cathodes having a cylindrical emissive surface, e.g. cathodes for magnetrons

Definitions

  • This invention relates to an electronic discharge device, particularly of the magnetron type. and to a cathode for such a device capable of supplying large peak values of current.
  • An object of this invention is to produce an electron discharge device of the type which supplies high peak values of current with its cathode normally operating at a temperature substantially below that necessary to cause such peak values of current to be emitted thermionically.
  • Another object is to accomplish the above in a magnetron type ofgcharge device.
  • Another object is to cause such peak values of current to be supplied largely by secondary emission.
  • FIG. 1 and 2 ar diagrammatic representations of a magnetron illustrating certain principles of operation of my invention
  • Fig. 3 is a cross-sectional view of one embodiment of my novel cathode
  • Fig. 4 is a fragmentary view. partly in section of another embodiment of my nove1 cathode
  • FIG. 5 is an illustration of one type of magnetron incorporating my invention, the view in Fig. 5 being taken along line 5-5 in Fig. 6; and
  • Fig. 6 is a cross-section of the magnetron in Fig. 5 taken along line 6-6 of Fig. 5, together with a. diagrammatic representation of ,a circuit with which said magnetron may be used.
  • A1 and A represent two anodes of a split anode magnetron.
  • C is the centrally located cathode thereof.
  • a longitudinal magnetic field is impressed thereon in a direction at right angles to the plane of illustration in Fig. 1.
  • the cathode C is connected to a negative potential while the anodes A1 and A: are connected together to a positive potential.
  • Devices of this kind are evacuated to high vacuum conditions in which the gaseous atmosphere plays substantially no part in the discharge.
  • This type of magnetron when energized sets up high frequency oscillations, creating an oscillating electrostatic field between the anode A1 and A2. At one instant of time the anode A1 may be more positive than the anode A2.
  • FIG. 2 Under the conditions of operation which I contemplate in my invention, in addition to the action described in connection with Fig. 1, another action, as exemplified byFig. 2, also takes place.
  • the electron emission from C causes a swarm S of electrons in the space surrounding C.
  • An electron e'. which otherwise might follow the path as described in Fig. 1, however, encounters interference from the other electrons in the swarm S. and thus never reaches the anodes A1 or A2, but falls back onto the cathode.
  • the interaction between the electrons in the swarm S may impart considerable energy to the electron e by collision or otherwise by the time it reaches the cathode C.
  • the electrons s also may receive a considerable amount of energy directly from the oscillating field between the twoanodes Ar and A2.
  • the magnetic field tends to give to the electron e' a definite orbital period in its travel around C, which period is substantially equal to the period of oscillation of the voltage appearing between the anodes A1 and A2. This condition permits said oscillating field to arert its accelerating force upon the electron e in the proper phase and at the proper time to successively impart energy to said electron.
  • electrons of the a type can be'made to fail upon the cathode C with considerable speed and energy, which may be substantially above 100 volts. If the cathode C is made so as to be a good secondary electron emitter, then such impinging electron may give rise to the emission of several additional electrons.
  • the current due to secondary emission may be .made several times the current due to simple thermionic emission at the operating temperature of the cathode.
  • the secondary electron emission can be made to increase enormously to carry such peak currents without substantial time delay.
  • such a device can be made to operate as an electron multiplying arrangement in which the normal thermionically-emitted electrons are multiplied to give an increased supply of electrons which in turn are again multiplied by a similar-process.
  • the cathode of the discharge device in a special form, as shown for example in Fig. 3.
  • the cathode illustrated consists of a sleeve I made of some suitable material, such as tantalum or nickel. In one example of this cathode the cylinder was about six millimeters in diameter,
  • Thesleeve is coated, except for the end portions thereof, with a layer 2 of a mixture of barium and strontium carbonates in a nitrocellulose-amylacetate binder. In some instances I prefer to add from one to one and one-half per cent. of borax in order to decrease the'evaporation rate of the coating material during operation.
  • the sleeve so coated is baked in air at a temperature of about 400 F.
  • a winding 3 preferably of tantalum wire, is wound over said coating. In the embodiment mentioned above, this wire has consisted of tantalum .004 inch in diameter, spaced .003 inch between adjacent turns.
  • the ends of the wire 3 may be welded directly to the sleeve I.
  • the cathode is again coated with the coating material described above and again baked in air at a temperature of about 400 F. Thereupon the coating is scraped off the outside of the cathode 4 a temperature or thermionic emission.
  • the ends of the sleeve I are closed by insulating plugs 'I-'
  • the ends of the heater coil 8 extend through said plugs so that heating current may be supplied thereto.
  • electrical connecter tab 8 has one end thereof structure. leaving the top surfaces 4 of the wire welded to the sleeve I and the other end welded to one of the heater ends 8, so that electrical connection may be established to the emitting surface of the cathode.
  • the cathode is wound with a flat ribbon 3, also preferably of tantalum.
  • This ribbon may be .0005 inch thick and .050 to .100 inch wide.
  • Such a ribbon may be initially coated with emitting materials, as described above, and wound upon the sleeve I with about half of each turn of the ribbon overlapping the preceding turn.
  • the coating may be baked in air as described above, and the coating scraped from the outside of the cathode structure, leaving the top surfaces 4 of the ribbon material 3' bare.
  • the cathode structures as described above possess the property of being excellent secondary electron emitters, particularly from the scraped tantalum surfaces, as well as good thermionic emitters from the exposed oxide surfaces.
  • the tantalum has a tendency to reduce the barium oxide, liberating small amounts of barium on the surface of the coating which tends to give excellent electron emission. Also the barium so liberated tends to coat the bare surfaces of the tantalum, making it an excellent secondary electron emitter. Even without any barium coating, tantalum in itself is a good secondary emitter.
  • Cathodes of'the type as illustrated in Figs. 3 and 4 may be incorporated, for example, in a magnetron of the type as illustrated in Figs. 5 and 6.
  • the magnetron therein illustrated comprises an envelope I I which is preferably made of a block of conducting material, such as copper.
  • This block forms the anode structure of the magnetron.
  • Said block has hollow end sections which are covered by end caps I2 and I3, likewise of conducting material, such as copper;
  • Between the hollow end sections of the block I I is a central bridging portion I4.
  • the portion I4 is provided with a central bore I5 within which is supported substantially at the center thereof a cathode I0 which, as pointed out above, is preferably of the type as illustrated in Figs. 3 and 4.
  • the cathode I0 is supported by a pair of lead-in conductors I6 and I1 fastened respectively to the ends 0 of th cathode structure, and sealed through glass seals I8 and I9 mounted at the outer ends of pipes 20 and 2
  • a plurality of slots 22 extend radially from the central bore I5 to within a short distance of the outer wall of the block I I.
  • oscillations are set up whose frequency and consequently whose wave length are determined primarily by the dimensions of each of the slots 22. It is also desirable that the value of the magnetic field is such as to impartto the electrons travelling around the cathode an orbital frequency substantially equal to the frequency of said oscillations. Moreover the voltage applied to the anode structure should be of the propervalue to cause such oscillations to occur and for the desired peak value of current to flow between the cathode and anode structure.
  • the oscillations produced in the slots 22 reinforce each other and may be led out from the tube by means of a coupling conductor 25 fastened to the cen ral bridge portion I4 in the central bore 15 betwe 11 two of the slots 22.
  • the coupling conductor 25 leads out from the magnetron through a glass seal 21 at the outer end of a pipe 25 likewise hermetically fastened through the wall of the envelope II adjacent the' upper hollow portion thereof.
  • the magnetron may be connected in any suitable circuit, one of which is shown diagrammatically in Fig. 6.
  • the cathode is supplied with heating current from the secondary winding 28 of a heating transformer 29 whose primary winding 30 is adapted to be connected to a suitable source of alternating current.
  • Interposed in the circuit of a. secondary winding 28 is a switch 3
  • a source of potential 33 which in a, practical embodiment may be of the order of 12,500 volts, is connected between the envelope ll, constituting the anode, and the lead-in wire I 6 for the cathode l0.
  • an interrupter or chopper 34 Interposed in the circuit for the source 33 is an interrupter or chopper 34 which interrupts the circuit so that the magnetron generates short pulses of high intensity high frequency oscillations.
  • the frequency of interruption may be of the order of two thousand times a second.
  • the duration of each energization of the tube may be of the order of a half a microsecond.
  • the cathode was raised to a temperature at which enough thermionic emission occurred to initiate the operation of the device, such emission being of the order of milliamperes and being much less than that required to supply peak currents of the order of amperes.
  • the heater 6 is supplied with heating energy so as to initially raise the cathode to a temperature at which some thermionic emission occurs.
  • This thermionic emission may emanate largely from the oxide coating which is exposed to the discharge area, through the spaces between the coiled winding on the outside of the cathode. Some of this thermionic emission may occur from the surface of the coiled winding itself, particularly if the metal thereof has a thin film of barium coated upon it.
  • the electrons which fall upon the cathode largely impinge upon the bare metal surface of the coiled external winding, and liberate the secondary electrons therefrom.
  • the oxide coating between the turns of this winding is largely shielded from such electron bombardment, and thus forms very little, if any, tendency for such bombardment to drive any of the oxide coating from the cathode.
  • such coating is always available to supply barium for the initial electron emission as well as barium which tends to increase the secondary electron-emitting qualities of the metal surface of the external winding.
  • An additional advantage of the construction which I have illustrated is that the surfaces from which the secondary electrons are emitted are directly electrically connected to the sleeve I by having the ends 5 welded thereto. In this way the current can flow through a direct low resistance metallic path to the very surface at which the electrons are being liberated. This is in contrast to the usual oxide-coated cathode in which the current must flow through the relatively high resistance oxide coating before it reaches the emitting surface. In this way the present cathode structure is much more effective and eflicient.
  • An electric discharge device including spaced anode and cathode electrodes the surface of one of which electrodes is covered in part with loose and outwardly projecting particles of material subject to being removed therefrom by the electrostatic forces between the two said electrodes,
  • said means comprising an electrostatic shield comprised of a helically wound wire coil having a coil-turn spacing and extending in contact for its full length with said electrode having the projecting particles, said coil being of highly refractory non-emissive metal and being electrically connectedto said electrode having the projecting particles, said coil having its convolutions exposed in front of said electrode having the projecting particles and in front of said projecting particles, said coil providing for the location thereon of the electrostatic lines of force in front of said electrode surface having the projecting particles and front or said particles in preference to the loca ion of said lines of force on the said electrode surface having the projecting particles, and said coil providing for the passage between the convolutions thereof of electrons to and from said electrode surface havin the projecting particles.
  • An electric discharge device comprising a cathode electrode provided with an electron emissive surface consisting of relatively loosely adherent material and an electrostatic shield memtending from end to end of the surface of said electron emissive surface and in contact thereher overlying and exposed in front of and c!- with throughout the length 01' said shield member and electrically connected to the electrode, said shield member consisting of high refractory non-emissive metal and having a plurality of openings therethrough for the free passage of electrons to and from the electrode surface.

Description

Dec KY, 1946.. N E 2,412,842
ELECTRON I C DI S CHARGE CATHODE Original Fil ed Sept. 30, 1941 2 Sheets-Sheet 1 Dec. 17, 1946.
P. L. SPENCER ELECTRONIC DISCHARGE I GATHODE Original Filed Sept; 30, 1941 2 Sheets-Sheet 2 F7615 hllllillllll Patented Dec. '17, 1946 UNITED srA'r ELECTRONIC DISCHARGE carnonn Percy L. Spencer, West Newton, Mara, assignor to Raytheon Manufacturing Company, Newton, Mass., a corporation of Delaware Original application September 30, 1941, Serial No. 412,993. Divided and this 23, 1944, Serial No. 538,998
1 2 Claims.
This is a division of my copending application, Serial No. 412,993, filed September 30, 1941, for an improvement in electronic discharge devices.
This invention relates to an electronic discharge device, particularly of the magnetron type. and to a cathode for such a device capable of supplying large peak values of current.
In electronic discharge devices, particularly of the magnetron type which are called upon to supply relatively large peak values of current, various difiiculties have heretofore existed. The cathodes of such devices have been heated to relatively high temperatures in an attempt to supply suincient thermionic emission to carry such peak values of current. Such cathodes have had an unusually short life due to the fact that the emissive coating with which the cathodes are normally coated was rapidly driven oil! from the cathode. This effect was increased by the fact that the load current through the tube tended to overheat and burn out the cathode. The arthas resorted to the use of complicated regulating and protective devices in order to protect the cathodesor such magnetrons from being burned out. However, such protective and regulating devices did not substantially affect the loss of coating due to high operating temperatures of the cathode which resulted in short life for such cathodes.
An object of this invention is to produce an electron discharge device of the type which supplies high peak values of current with its cathode normally operating at a temperature substantially below that necessary to cause such peak values of current to be emitted thermionically.
Another object is to accomplish the above in a magnetron type ofgcharge device.
Another object is to cause such peak values of current to be supplied largely by secondary emission.
A further object is to devise a cathode in such a device which will emit large numbers of sec--- description oiexemplifications thereof, reference application May being had to the accompanying drawings, where- Figs. 1 and 2 ar diagrammatic representations of a magnetron illustrating certain principles of operation of my invention;
Fig. 3 is a cross-sectional view of one embodiment of my novel cathode;
Fig. 4 is a fragmentary view. partly in section of another embodiment of my nove1 cathode;
Fig. 5 is an illustration of one type of magnetron incorporating my invention, the view in Fig. 5 being taken along line 5-5 in Fig. 6; and
Fig. 6 is a cross-section of the magnetron in Fig. 5 taken along line 6-6 of Fig. 5, together with a. diagrammatic representation of ,a circuit with which said magnetron may be used.
In Fig. 1 A1 and A: represent two anodes of a split anode magnetron. C is the centrally located cathode thereof. As is usual in this type of device, a longitudinal magnetic field is impressed thereon in a direction at right angles to the plane of illustration in Fig. 1. The cathode C is connected to a negative potential while the anodes A1 and A: are connected together to a positive potential. Devices of this kind are evacuated to high vacuum conditions in which the gaseous atmosphere plays substantially no part in the discharge. This type of magnetron when energized sets up high frequency oscillations, creating an oscillating electrostatic field between the anode A1 and A2. At one instant of time the anode A1 may be more positive than the anode A2. Under these conditions an electron e emitted from the cathode C is accelerated toward the anode A1 by the potential thereof. However, the magnetic field causes the electron e to travel in a curved path which deflects the elec tron to such an extent that it misses the anode A1 and falls upon the anode A2. This imparts a negative characteristic to the device, and causes it to operate as an oscillator. I
Under the conditions of operation which I contemplate in my invention, in addition to the action described in connection with Fig. 1, another action, as exemplified byFig. 2, also takes place. The electron emission from C causes a swarm S of electrons in the space surrounding C. An electron e'. which otherwise might follow the path as described in Fig. 1, however, encounters interference from the other electrons in the swarm S. and thus never reaches the anodes A1 or A2, but falls back onto the cathode. The interaction between the electrons in the swarm S may impart considerable energy to the electron e by collision or otherwise by the time it reaches the cathode C. Assuming the tube to be oscillating, the electrons s also may receive a considerable amount of energy directly from the oscillating field between the twoanodes Ar and A2. The magnetic field tends to give to the electron e' a definite orbital period in its travel around C, which period is substantially equal to the period of oscillation of the voltage appearing between the anodes A1 and A2. This condition permits said oscillating field to arert its accelerating force upon the electron e in the proper phase and at the proper time to successively impart energy to said electron.
Due to the above eflects, electrons of the a type can be'made to fail upon the cathode C with considerable speed and energy, which may be substantially above 100 volts. If the cathode C is made so as to be a good secondary electron emitter, then such impinging electron may give rise to the emission of several additional electrons. The current due to secondary emission may be .made several times the current due to simple thermionic emission at the operating temperature of the cathode. In addition, when the tube is called upon to supply greatly increased peaks of current, then the secondary electron emission can be made to increase enormously to carry such peak currents without substantial time delay. In other words, such a device can be made to operate as an electron multiplying arrangement in which the normal thermionically-emitted electrons are multiplied to give an increased supply of electrons which in turn are again multiplied by a similar-process.
In accordancewith my invention I utilize such secondary emission to supply alarge part of the peak currents which such a device may be called upon to supply. For this purpose I prefer to construct the cathode of the discharge device in a special form, as shown for example in Fig. 3. The cathode illustrated consists of a sleeve I made of some suitable material, such as tantalum or nickel. In one example of this cathode the cylinder was about six millimeters in diameter,
and about fifteen millimeters long. Thesleeve is coated, except for the end portions thereof, with a layer 2 of a mixture of barium and strontium carbonates in a nitrocellulose-amylacetate binder. In some instances I prefer to add from one to one and one-half per cent. of borax in order to decrease the'evaporation rate of the coating material during operation. The sleeve so coated is baked in air at a temperature of about 400 F. Thereupon a winding 3, preferably of tantalum wire, is wound over said coating. In the embodiment mentioned above, this wire has consisted of tantalum .004 inch in diameter, spaced .003 inch between adjacent turns. In orderto retain the winding upon the cathode and to insure good electrical contact with the underlying sleeve, the ends of the wire 3 may be welded directly to the sleeve I. After the wire 3 has been wound upon the cathode, the cathode is again coated with the coating material described above and again baked in air at a temperature of about 400 F. Thereupon the coating is scraped off the outside of the cathode 4 a temperature or thermionic emission. The ends of the sleeve I are closed by insulating plugs 'I-'|, preferably of alumina. The ends of the heater coil 8 extend through said plugs so that heating current may be supplied thereto. An
' electrical connecter tab 8 has one end thereof structure. leaving the top surfaces 4 of the wire welded to the sleeve I and the other end welded to one of the heater ends 8, so that electrical connection may be established to the emitting surface of the cathode.
Instead of making the cathode as illustrated in Fig. 3, it can take a variety of other forms, one of which is illustrated in Fig. 4. In this figure, instead of using round wire, the sleeve I is wound with a flat ribbon 3, also preferably of tantalum. This ribbon, for example, may be .0005 inch thick and .050 to .100 inch wide. Such a ribbon may be initially coated with emitting materials, as described above, and wound upon the sleeve I with about half of each turn of the ribbon overlapping the preceding turn. Here again the coating may be baked in air as described above, and the coating scraped from the outside of the cathode structure, leaving the top surfaces 4 of the ribbon material 3' bare.
The cathode structures as described above possess the property of being excellent secondary electron emitters, particularly from the scraped tantalum surfaces, as well as good thermionic emitters from the exposed oxide surfaces. The tantalum has a tendency to reduce the barium oxide, liberating small amounts of barium on the surface of the coating which tends to give excellent electron emission. Also the barium so liberated tends to coat the bare surfaces of the tantalum, making it an excellent secondary electron emitter. Even without any barium coating, tantalum in itself is a good secondary emitter.
Cathodes of'the type as illustrated in Figs. 3 and 4 may be incorporated, for example, in a magnetron of the type as illustrated in Figs. 5 and 6. The magnetron therein illustrated comprises an envelope I I which is preferably made of a block of conducting material, such as copper. This block forms the anode structure of the magnetron. Said block has hollow end sections which are covered by end caps I2 and I3, likewise of conducting material, such as copper; Between the hollow end sections of the block I I is a central bridging portion I4. The portion I4 is provided with a central bore I5 within which is supported substantially at the center thereof a cathode I0 which, as pointed out above, is preferably of the type as illustrated in Figs. 3 and 4. The cathode I0 is supported by a pair of lead-in conductors I6 and I1 fastened respectively to the ends 0 of th cathode structure, and sealed through glass seals I8 and I9 mounted at the outer ends of pipes 20 and 2| hermetically fastened within the walls of the block I I adjacent the upper and lower hollow end sections. A plurality of slots 22 extend radially from the central bore I5 to within a short distance of the outer wall of the block I I.
when such a magnetron is placed between suitable magnetic poles 23 and 24 to create a longitudinal magneticfield and the device is energized, oscillations are set up whose frequency and consequently whose wave length are determined primarily by the dimensions of each of the slots 22. It is also desirable that the value of the magnetic field is such as to impartto the electrons travelling around the cathode an orbital frequency substantially equal to the frequency of said oscillations. Moreover the voltage applied to the anode structure should be of the propervalue to cause such oscillations to occur and for the desired peak value of current to flow between the cathode and anode structure. The oscillations produced in the slots 22 reinforce each other and may be led out from the tube by means of a coupling conductor 25 fastened to the cen ral bridge portion I4 in the central bore 15 betwe 11 two of the slots 22. The coupling conductor 25 leads out from the magnetron through a glass seal 21 at the outer end of a pipe 25 likewise hermetically fastened through the wall of the envelope II adjacent the' upper hollow portion thereof.
The magnetron may be connected in any suitable circuit, one of which is shown diagrammatically in Fig. 6. In this circuit the cathode is supplied with heating current from the secondary winding 28 of a heating transformer 29 whose primary winding 30 is adapted to be connected to a suitable source of alternating current. Interposed in the circuit of a. secondary winding 28 is a switch 3| and a current-regulating resistance 32. A source of potential 33, which in a, practical embodiment may be of the order of 12,500 volts, is connected between the envelope ll, constituting the anode, and the lead-in wire I 6 for the cathode l0. Interposed in the circuit for the source 33 is an interrupter or chopper 34 which interrupts the circuit so that the magnetron generates short pulses of high intensity high frequency oscillations. The frequency of interruption may be of the order of two thousand times a second. The duration of each energization of the tube may be of the order of a half a microsecond.
I have constructed a. considerable number of devices substantially as shown in Figs. 5 and 6 and embodying a cathode as illustrated in Fig. 3, as well as the various parameters recited herein. Tubes of this kind were designed to produce oscillations of a wave length of about three centimeters. In such a tube I have found that during each half micro-second during which the device was energized, the anode current rose substantially instantaneously to a value of about twelve amperes and continued throughout at this value for substantially each period of energization. The average anode current throughout the entire time was of the order of about fourteen milliamperes.
In starting the operation of such a device, the cathode was raised to a temperature at which enough thermionic emission occurred to initiate the operation of the device, such emission being of the order of milliamperes and being much less than that required to supply peak currents of the order of amperes. However, as pointed out above,
when operation started, peak currents of the order of amperes were supplied. Furthermore, after the operation of the device had begun, it was possible to open the heating circuit by the switch 3|, and the device continued in operation with no discernible difference, the tube continuing to generate oscillations in the same Way and to substantially the same degree as before the opening of said circuit. Also under these conditions, when the pole pieces 23 and 24 were deenergized so as to remove the magnetic field on the device, the current to the anode structure fell to zero and the operation of the device ceased. This is in strong contrast to the usual magnetron device in which if during operation the magnetic field is deenergized, the current between the cathode and the anode structure rises rapidly.
As pointed out above, the heater 6 is supplied with heating energy so as to initially raise the cathode to a temperature at which some thermionic emission occurs. This thermionic emission may emanate largely from the oxide coating which is exposed to the discharge area, through the spaces between the coiled winding on the outside of the cathode. Some of this thermionic emission may occur from the surface of the coiled winding itself, particularly if the metal thereof has a thin film of barium coated upon it. However, during operation the electrons which fall upon the cathode largely impinge upon the bare metal surface of the coiled external winding, and liberate the secondary electrons therefrom. The oxide coating between the turns of this winding is largely shielded from such electron bombardment, and thus forms very little, if any, tendency for such bombardment to drive any of the oxide coating from the cathode. However, such coating is always available to supply barium for the initial electron emission as well as barium which tends to increase the secondary electron-emitting qualities of the metal surface of the external winding. An additional advantage of the construction which I have illustrated is that the surfaces from which the secondary electrons are emitted are directly electrically connected to the sleeve I by having the ends 5 welded thereto. In this way the current can flow through a direct low resistance metallic path to the very surface at which the electrons are being liberated. This is in contrast to the usual oxide-coated cathode in which the current must flow through the relatively high resistance oxide coating before it reaches the emitting surface. In this way the present cathode structure is much more effective and eflicient.
By my present invention I have been enabled to construct practical magnetron devices which have generated enormous peak quantities of microwave length power entirely outside of the range of anything which has heretofore been practicable with such devices.
Of course it is to be understood that this invention is not limited to the particular details as described above as many equivalents will suggest themselves to those skilled in the art. For example, it may be possible to incorporate oertain fundamental features of this invention in other devices which are called upon to supply high peak values of current, particularly in connection with micro-Wave generators, 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 electric discharge device including spaced anode and cathode electrodes the surface of one of which electrodes is covered in part with loose and outwardly projecting particles of material subject to being removed therefrom by the electrostatic forces between the two said electrodes,
means to prevent the removal of said particles of material, said means comprising an electrostatic shield comprised of a helically wound wire coil having a coil-turn spacing and extending in contact for its full length with said electrode having the projecting particles, said coil being of highly refractory non-emissive metal and being electrically connectedto said electrode having the projecting particles, said coil having its convolutions exposed in front of said electrode having the projecting particles and in front of said projecting particles, said coil providing for the location thereon of the electrostatic lines of force in front of said electrode surface having the projecting particles and front or said particles in preference to the loca ion of said lines of force on the said electrode surface having the projecting particles, and said coil providing for the passage between the convolutions thereof of electrons to and from said electrode surface havin the projecting particles.
2. An electric discharge device comprising a cathode electrode provided with an electron emissive surface consisting of relatively loosely adherent material and an electrostatic shield memtending from end to end of the surface of said electron emissive surface and in contact thereher overlying and exposed in front of and c!- with throughout the length 01' said shield member and electrically connected to the electrode, said shield member consisting of high refractory non-emissive metal and having a plurality of openings therethrough for the free passage of electrons to and from the electrode surface.
PERCY L. SPENCER.
US536996A 1941-09-30 1944-05-23 Electronic discharge cathode Expired - Lifetime US2412842A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US536996A US2412842A (en) 1941-09-30 1944-05-23 Electronic discharge cathode
US674453A US2430309A (en) 1941-09-30 1946-06-05 Electronic discharge device
DER4400A DE856669C (en) 1941-09-30 1950-10-04 Electron source with small dimensions for supplying a high peak current in connection with a short wave tube

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US412993A US2411601A (en) 1941-09-30 1941-09-30 Electronic discharge device
US536996A US2412842A (en) 1941-09-30 1944-05-23 Electronic discharge cathode
US674453A US2430309A (en) 1941-09-30 1946-06-05 Electronic discharge device

Publications (1)

Publication Number Publication Date
US2412842A true US2412842A (en) 1946-12-17

Family

ID=27410966

Family Applications (2)

Application Number Title Priority Date Filing Date
US536996A Expired - Lifetime US2412842A (en) 1941-09-30 1944-05-23 Electronic discharge cathode
US674453A Expired - Lifetime US2430309A (en) 1941-09-30 1946-06-05 Electronic discharge device

Family Applications After (1)

Application Number Title Priority Date Filing Date
US674453A Expired - Lifetime US2430309A (en) 1941-09-30 1946-06-05 Electronic discharge device

Country Status (2)

Country Link
US (2) US2412842A (en)
DE (1) DE856669C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2749470A (en) * 1952-06-11 1956-06-05 Int Standard Electric Corp Indirectly heated cathodes
US3093757A (en) * 1957-12-30 1963-06-11 Westinghouse Electric Corp Device for converting thermal energy into electrical energy

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463372A (en) * 1945-10-03 1949-03-01 Jr Peter W Forsbergh Cathode structure for magnetrons
US2498775A (en) * 1948-01-16 1950-02-28 Westinghouse Electric Corp Cathode construction
US2905852A (en) * 1954-06-15 1959-09-22 Bell Telephone Labor Inc Electron discharge device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2749470A (en) * 1952-06-11 1956-06-05 Int Standard Electric Corp Indirectly heated cathodes
US3093757A (en) * 1957-12-30 1963-06-11 Westinghouse Electric Corp Device for converting thermal energy into electrical energy

Also Published As

Publication number Publication date
US2430309A (en) 1947-11-04
DE856669C (en) 1952-11-24

Similar Documents

Publication Publication Date Title
US2411601A (en) Electronic discharge device
US2452075A (en) Velocity modulation electron discharge tube
US4297612A (en) Electron gun structure
US2218386A (en) Discharge device
US2450763A (en) Ultra high frequency generator vacuum tube and cathode structure therefor
US2545120A (en) Cathode-ray tube arc-over preventive
US2412842A (en) Electronic discharge cathode
US2416661A (en) Dispenser type cathode electric discharge device
US1874753A (en) Controlled arc discharge apparatus
US2967260A (en) Electron tube
US2488716A (en) Electric high-pressure discharge tube
US3896332A (en) High power quick starting magnetron
US2316276A (en) Electron discharge apparatus
US2435246A (en) Gaseous discharge device containing perforated starting electrodes
US2437279A (en) High-power microwave discharge tube
US2241345A (en) Electron emissive cathode
US2323560A (en) Electron discharge apparatus
US2313646A (en) Gaseous discharge lamp
US2070816A (en) Gas-filled discharge tube
US2975317A (en) Beam control device
US2818528A (en) Electron discharge device
US2247688A (en) Method of making electron discharge devices
US2459199A (en) Arc discharge device
US3192425A (en) X-ray tube with adjustable electron beam cross-section
US3013180A (en) Magnetron device and system