US2134527A - Method of igniting gas or vapor discharge spaces - Google Patents

Method of igniting gas or vapor discharge spaces Download PDF

Info

Publication number
US2134527A
US2134527A US47498A US4749835A US2134527A US 2134527 A US2134527 A US 2134527A US 47498 A US47498 A US 47498A US 4749835 A US4749835 A US 4749835A US 2134527 A US2134527 A US 2134527A
Authority
US
United States
Prior art keywords
potential
discharge
capacitor
anode
circuit
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
US47498A
Other languages
English (en)
Inventor
Mierdel Georg
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.)
Siemens Schuckertwerke AG
Siemens Corp
Original Assignee
Siemens 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 Siemens Corp filed Critical Siemens Corp
Application granted granted Critical
Publication of US2134527A publication Critical patent/US2134527A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

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

Definitions

  • the potential of the anode of the discharge spacewhich is to be ignited and thegrid of which is connected to a blocking potential is
  • the discharge space is, as in the usual applications of controlled rectifiers, provided with an auxiliary electrode which operates on the dis-- ,charge path between the anode and the cathode.
  • the auxiliary electrode preferably has the form of ,a control grid and the control grid is permanently and without change connected to Such a potential that the discharge space is blocked; that; accordingly, a potential connected to the anode cannot without further change ignite the discharge space.
  • Other electrode structures than the usual control grids, for example, shells, which envelop the discharge path either within orwithout the container enclosingthe discharge space,
  • the magnitudeuof the blocking potential which is'tobe connected to the ,control grid thedimensions of the discharge device utilized, and therefore particularly the dimensions of the control electrode and the geometric dimensionsof the discharge space between the cathode and the anode, are determining.
  • a negative direct current potential in series with a resistor in accordance with the character of the discharge vesselutilized is connectedbetween the control electrode and the cathode.
  • the potential source may be dispensed with, i. e., the control grid may be connected to the cathode only through a resistor. The latter connection is utilized only for thosevessels for which the so-called ignition characteristic line of the discharge vessel coincides with the cathode potential or lies in the positive region above it.
  • the discharge space which on the application of an anode potential (that may be either a direct cur rent or an alternating current potential) is under normal circumstances not ignited, may be ignited ifby any means whatever the anode potential is for ashort interval of time brought to the oathode potential or at least approximately to the cathode potential;
  • an anode potential that may be either a direct cur rent or an alternating current potential
  • various means may be utilized
  • a transformer may be connected in the anode circuit, in the secondaryof which a short'current impulse "is produced. The transformer is so connected that the potential peak introduced thereby in the anode circuit is opposite to the anode potential.
  • Control means of this type have, in the past, been utilized in rectifiers. Nevertheless the use has been heretofore in those rectifiers which, in contrast to the control method according to the invention, arenot ignited by a potential decrease but by a momentary potential increase of the anode.
  • Another particularly advantageous means for reducing the anode to the cathode potential consists of a cap acitor connected'in parallel to the discharge space through a switch whichis to be closed at the instant thedischarge space is to be ignited; The working potential impressed across the discharge space is then short-circuitedthrough the capacitor and by the'cha'rg ing current of the g capacitor, the anode potential is for a short interval of time reduced to a potential which is approximately equal to the cathode potential.
  • the charge onthe capacitor increases the anode potential rises immediately to its normal operating value. in addition to again discharge the capacitor after the discharge space is ignited thus to prepare it for the next ignition,for example, in cases where the discharge space of a rectifier is to be periodically ignited.
  • a resistor is connected in parallel with thecapacitor.
  • the magnitude of the resistor is such that it does not disturb the decrease of the anode potential at the instant that the capacitor circuit is connected in.
  • the time constant of the capacitor circuit determined by the capacitor and the resistor must be sogauged that the discharge period of the capacitor is small compared to the period of ignition of the discharge space.
  • resistor having characteristic capacity (distributed capacity) of such magnitude that the parallel capacitor may be dispensed with, may be utilized.
  • the invention may be utilized for the most diverse purposes.
  • a direct current network may be connected by the operation of the control method according to the invention.
  • the switch lying in the capacitor network is then preferably provided with two contacts which are operated in succession.
  • the iirst"contactth'e capacitor is connected in parallel tothe discharge space, While by the second contact the capacitor is short circuited for dis- Prefe'rably, means are provided charge purposes, preferably through a properly dimensioned resistor.
  • Particularly important is the new control method for conversion arrangements which operate with controlled rectifiers, accordingly, for controllable rectifiers, inverters and converters. In these conversion arrangements, the time point of the ignition of the discharge space is determined by the switching arrangement in the capacitor circuit.
  • rotating switch apparatus for example, of the machine commutator type, are utilized as they have been utilized heretofore with the usual grid controlled discharge paths.
  • Mechanical contacts may be entirely avoided if auxiliary discharge spaces, particularly gas or vapor discharge spaces which are ignited by the customary and well known means, are utilized in the capacitor circuit for switching purposes.
  • Gas or vapor discharge spaces are preferable for the present use, tohigh vacuum electron tubes because the switching load is practically unlimited, and because the capacitor circuit must be switched in, above all else, without delay.
  • Fig. 1 is a diagrammatic view of an embodiment of my invention
  • Fig. 2 is a diagrammatic view of a modification of my invention
  • Fig. 3 is a diagrammatic view showing another modification of my invention.
  • Fig. 4 is a diagrammatic view showing a further modification of my invention.
  • Fig. 5 is a diagrammatic view showing a still further modification of my invention.
  • Fig. 6 is a diagrammatic view of a circuit which is electrically equivalent to the Fig. 1 circuit and which is used in explaining the operation of my invention, and
  • Fig. '7 is a graph illustrating the operation of the circuit shown in Fig. 6.
  • FIG. 1 the connection for a controllable rectifier is illustrated as an embodiment of the invention.
  • a mercury vapor discharge vessel l is in the known manner provided with an anode 2, a control grid 3 and a mercury cathode 4, and by the operation of an auxiliary electrode 5, a permanently-burning excitation arc is maintained.
  • the control grid 3 is connected to the cathode through a battery 6 and a resistor T.
  • the battery 6 may be dispensed with, as has been mentioned before, if the discharge vessel is of such character that the connection between the control grid and the cathode sufiices to block the discharge.
  • This arrangement has the advantage that the connection conductors l6 (Fig. 5) be-- tween the control grid and the cathode may be disposed within the discharge vessel so that the separate bushings for the grids such as are necessary in the known grid controlled discharge devices may be eliminated.
  • a capacitor 8 is according to the invention connected in parallel with the discharge space of the discharge vessel.
  • the capacitor may be connected and disconnected by a switching device 9 which is to be periodically actuated.
  • the capacitor 8 is shunted by a discharge resistor Ill.
  • the alternating current source II is connected to the discharge vessel I through the current consumption load I2.
  • the discharge vessel operates as a rectifier, the current transmission of which or the mean potential delivered by which may be regulated with the aid of the switching apparatus 9.
  • an auxiliary discharge device I8 (Fig. 2) which is periodically ignited may be utilized as has been explained before.
  • the arrangement may, moreover, be improved by connecting an inductor IS in the anode circuit as viewed from the load side before the connection of the capacitor parallel circuit.
  • the inductor prevents the potential of the anode from being raised sooner than is desired by the current flowing out of the load circuit or out of the feeding source when the capacitor is connected
  • a transformer in the secondary 22 of which a short current impulse is produced is shown as connected in the anode circuit. The transformer is so connected that the potential peak introduced thereby in the anode circuit is opposite to the anode potential.
  • a switch 24 with two contacts 26 and 28 is shown in the capacitor circuit.
  • The'contacts 26 and 28 are operated in succession.
  • the capacitor is connected in parallel to the :1
  • a thyratron S may be regarded as connected through an ohmic resistor R and an inductor L (leakage inductance, inductance of the conductors, etc.), to a direct current source with the potential U0.
  • the grid potential may be assumed to be so low that the tube does not, itself, become ignited.
  • an ignition is to be effected by the actuation of a suitable switch mechanism by the operation of which the anode is connected to the capacitor C which is normally 0 maintained without a difference of potential by a parallel connected resistor.
  • the method operates in the case in which the grid potential is low enough to block for double the anode potential.
  • This point relates to the variation of the grid potential by reason of the capacitive effect of the anode potential.
  • the measure of this is the time constant of the grid circuit given by the capacity between grid and cathode and the series resistor of the grid. If this time constant is very large, the grid potential varies in proportion with the anode potential and may, therefore, take on a value which is not sufiicient for blocking the discharge when the anode potential rises. In general, however, the time constant of the grid circuit will be smaller than the oscillation period of the anode circuit. Also in such a case, the effective grid potential is greater than the static value, as simple consideration will show, during the rise of the anode potential and accordingly during the Whole of the first half Wave of the circuit closing oscillation, so that in this case there is also the possibility of ignition.
  • the invention has a series of important advantages over the known controllable electric discharge spaces. All interlocking of the circuit by control electrodes of the discharge path disappears.
  • the control grid may even, under certain circumstances, be connected with one of the other electrodes within the discharge container, so
  • the invention has the advantage that the potential is not increased but decreased.
  • Method of igniting a gas or vapor discharge device connected in a circuit having distributed impedance .particularly for the purpose of control of a rectifier which comprises reducing the potential of the anode of the discharge device, to the grid of which a blocking potential is connected, for a short interval of time, at least approximately to the potential of the cathode for producing an interelectrode potential impulse to ignite said device.
  • Apparatus according to claim 1 characterized by the fact that, by the operation of a transformerlying in the anode circuit a potential impulse opposite to the anode potential is produced at the instant of ignition.
  • Translating apparatus comprising an electric discharge device having a control electrode and a plurality of principal electrodes, said discharge device being connected in a circuit having distributed impedance, means for impressing a potential difference between said principal electrodes, means for maintaining a potential difference between said control electrode and one of said principal electrodes that is of such magnitude that said discharge device is normally deenergized and means for momentarily connecting said principal electrodes to produce an interelectrode' impulse for energizing said discharge device.
  • Apparatus according .to claim 4 characterized by the fact that the last means includes a capacitor, which is to be momentarily connected between the principal electrodes when the discharge device is to be energized, said capacitor being shunted by a resistor.
  • Apparatus according to claim 4 character'- ized by the fact that the last means includes a resistor with distributed capacity, which is to be momentarily connected between the principal electrodes when the discharge device is to be energized.
  • the last means includes a capacitor circuit, which is to be momentarily connected between the principal electrodes when the discharge device is to be energized and a rotating contact device constructed in the manner of a commutator for making the momentary connection.
  • Translating apparatus comprising an electric discharge device having a control electrode and a plurality of principal electrodes, said discharge device being connected in a circuit having distributed impedance, means for impressing a potential difference between said principal electrodes, means for maintaining a potential difference between said control electrode and one of said principal electrodes that is of such magnitude that said discharge device is normally deenergized and means including an auxiliary discharge device for momentarily connecting said principal electrodes to produce an interelectrode impulse for energizing said discharge device.
  • Apparatus according to claim 4 particularly for working circuits which are connected in for comparatively large time intervals by the discharge device which is to be ignited, characterized by the fact that the last means includes a capacitor circuit and a switch, with two contacts to be successively actuated in the capacitor circuit, the first of the switches connecting the capacitor in parallel to the discharge device while by the operation of the second of the switches the capacitor is short circuited for discharge purposes.
  • Apparatus according to claim 4 characterized by the fact that the potential difference between the control electrode and the one principal electrode is zero and the conductor connecting the control electrode to the one principal electrode is within the container of the discharge device.
  • Translating apparatus comprising an electric discharge device having a control electrode and a plurality of principal electrodes, said discharge device being connected in a circuit having distributed impedance, means for impressing a potential difference between said principal electrodes, means for maintaining a potential difference between said control electrode and one of said principal electrodes that is of such magnitude that said discharge device is normally deenergized, means including a capacitor circuit for momentarily connecting said principal electrodes to produce an interelectrode impulse for energizing said discharge device and an inductor connected in the anode circuit of said discharge device as viewed from the load circuit before the connection of the capacitor circuit.
  • Apparatus according to claim 4 characterized by that the last means includes a capacitor, which is to be momentarily connected between the principal electrodes when the discharge device is to be energized.
  • Apparatus according to claim 4 characterized by that the last means includes a capacitor, which is to be momentarily connected between the principal electrodes when the discharge device is to be energized, and a resistor shunting said capacitor, the time constant of the capacitor and resistor network being small compared to the periodicity of the difference of potential impressed between the principal electrodes.
  • Apparatus according to claim 4 characterized by that the last means includes a capacitor, and means for periodically connecting the capacitor between said principal electrodes for a short interval 01' time to energize the discharge device.

Landscapes

  • Plasma Technology (AREA)
  • Generation Of Surge Voltage And Current (AREA)
US47498A 1935-01-23 1935-10-30 Method of igniting gas or vapor discharge spaces Expired - Lifetime US2134527A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE447239X 1935-01-23

Publications (1)

Publication Number Publication Date
US2134527A true US2134527A (en) 1938-10-25

Family

ID=6537989

Family Applications (1)

Application Number Title Priority Date Filing Date
US47498A Expired - Lifetime US2134527A (en) 1935-01-23 1935-10-30 Method of igniting gas or vapor discharge spaces

Country Status (4)

Country Link
US (1) US2134527A (en))
FR (1) FR796967A (en))
GB (1) GB447239A (en))
NL (1) NL44177C (en))

Also Published As

Publication number Publication date
NL44177C (en))
GB447239A (en) 1936-05-14
FR796967A (fr) 1936-04-18

Similar Documents

Publication Publication Date Title
US2147472A (en) High current impulse device
US1921704A (en) Electric valve circuits
US2347715A (en) Arc starting device
US2134527A (en) Method of igniting gas or vapor discharge spaces
US1965416A (en) Electric valve circuits
US2231591A (en) Electric valve circuit
US2247057A (en) Electric valve converting system
US2276861A (en) High voltage rectifier
US1418022A (en) Discharge-tube relay for undulatory currents
US2083202A (en) Arrangement for generating tilting oscillations
US2333593A (en) Power translating device
US2112034A (en) Electrical discharge device
US2263307A (en) Electric valve cikcuit
US2537383A (en) Device for extinguishing a discharge tube having a mercury cathode
US2141927A (en) Arc-back suppression
US2162519A (en) Electric discharge apparatus
US2248626A (en) Electric valve circuit
US2905880A (en) Voltage regulating system
US1975164A (en) Grid-controlled mercury arc tube
US2078883A (en) Grid-controlled gas-filled tube
US1995176A (en) Electric discharge apparatus
US2247167A (en) Electric valve circuits
US2190799A (en) Starting circuit for electric valve apparatus
US2359144A (en) Vapor-electric device
US2259289A (en) Half-wave spot welding