US2516326A - Capacitor charge and discharge circuit for stroboscopes - Google Patents

Capacitor charge and discharge circuit for stroboscopes Download PDF

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US2516326A
US2516326A US694060A US69406046A US2516326A US 2516326 A US2516326 A US 2516326A US 694060 A US694060 A US 694060A US 69406046 A US69406046 A US 69406046A US 2516326 A US2516326 A US 2516326A
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discharge device
capacitor
discharge
electrode
cathode
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US694060A
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Dewey D Knowles
Cecil E Haller
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CBS Corp
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Westinghouse Electric Corp
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    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B41/00Circuit arrangements or apparatus for igniting or operating discharge lamps
    • H05B41/14Circuit arrangements
    • H05B41/30Circuit arrangements in which the lamp is fed by pulses, e.g. flash lamp

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  • a capacitor I3 is connected to the anode 3 of the discharge device. I through an inductor I5 and directly to the cathode 5 of the discharge device.
  • the capacitor I3 is charged through a resistor I1 from a source I9 which is preferably of the direct current type.
  • the starting electrode I is connected to the capacitor [3 through an auxiliary discharge device 2
  • is preferably of the type having an abrupt characteristic. It is. provided with an anode 23, a hot cathode and a control electrode 21 which are immersed in a gaseous medium.
  • the anode 23 is connected to the inductor I5 while the cathode 25 is connected to the starting electrode 1 through a current limiting resistor 29.
  • the control electrode 21 is provided with an anode 23, a hot cathode and a control electrode 21 which are immersed in a gaseous medium.
  • the anode 23 is connected to the inductor I5 while the cathode
  • 3 connected between the anode 3 and the oathode 5 of the main discharge device I is charged through a half-wave rectifier from an alternating source 34.
  • similar to the discharge device utilized in the embodiment shown in Fig. 1, is provided in series with the starting electrode 1 and the cooperative mercury pool 5.
  • is connected through the limiting resistor 29 to the starting electrode 1, and the anode 23 is connected to the positive plate 93 of the capacitor l3.
  • the main discharge device I is immediately energized under the influence of the residual potential difierence impressed on the capacitor and it remains energized until the capacitor is discharged. After this, the capacitor is recharged and the process is repeated. It is to be noted that here again a single capacitor I3 is utilized for the double purpose of supplying starting current and ignition potential.

Description

July 25, 1950 n. D. KNOWLES EI'AL 26 CAPACITOR CHARGE AND DISCHARGE CIRCUIT FOR S'I'ROBOSCOPES Original Filed May 17, 1935 2 Sheets-Sheet 1 Ma er- 33 Qac Illa far- WITNESSES: D I/tJ/ENTORS c ewey D. now/e5 3 2? and Cecil 1 Hal/er.
firm/L BY 960- I A'ITORNE D. D. K CAPACITOR CHARGE AND DISCHARGE CIRCUIT FOR STROBOSCOPES Original Filed May 17, 1935 2 Sheets-Sheet 2 l arlbb/e fFquency WITNESSES: I INVENTORS r Dewey Z7. mow/es and 6B l /5Ha //f" c I. I
A'ITOR Y Patented July 25, 1950 CAPACITOR CHARGE AND DISCHARGE CIRCUIT FOR STROBOSCOPES Dewey D. Knowles, Verona, N. J., and Cecil'E.
Haller, Lititz, Pa., assignors to Westinghouse Electric Corporation, East Pittsburgh, Pa., a corporation of Pennsylvania Application September 17, 1941, Serial No. 411,134,
now abandoned, which is a division of application Serial No. 120,940, January 16, 1937, now Patent No. 2,310,092, dated February 2, 1943, which in turn is a division of application Serial No. 22,012, May 17, 1935, now Patent No. 2,085,100, dated June 29, 1937. Divided and this application August 30, 1946, Serial No.
1 Claim.
Our invention relates to electric discharge apparatus and it has particular relation to the control of electric discharge devices of the type having a discharge initiating electrode, but not a discharge maintaining electrode such as a keepalive.
This application is a division of our application Serial No. 411,134, filed September 17, 1941, now abandoned; which is in turn a division of our application Serial No. 120,940, filed January 16, 1937 which has become Patent No. 2,310,092 issued Feb. 2, 1943; which is in turn a division of our application Serial No. 22,012, filed May 17, 1935 which has become Patent No. 2,085,100 issued June 29, 1937.
It is an object of our invention to provide a circuit for controlling the initiation. and extinction of the discharge in a discharge device of the mercury pool type that is equipped with a discharge initiating electrode.
Another object of our invention is to provide apparatus for periodically energizing a discharge device of the mercury pool type that is equipped with a discharge initiating electrode,
A further object of our invention is to provide apparatus for energizing and deenergizing, with variable periodicity, a discharge device of the type that is normally completely deenergized.
More specifically stated, it is an object of our invention to provide apparatus for energizing and deenergizing, with precisely determinable periodicity, a discharge device of the type that is equipped with a discharge starting electrode, but not with a discharge maintaining electrode.
In the following discussion and in the claim, we shall refer to a discharge device having a plurality of principal electrodes and a plurality or pair of starting electrodes. Such an expression is drawn with the thought in mind that it shall denominate a discharge device having at least four electrodes, 1. e., separate pairs of principal and starting electrodes.
In the preferred structure of the discharge device utilized in the practice of our invention, however, only three electrodes are utilized; an anode, a mercury pool cathode and a starting electrode, preferably composed of boron carbide or silicon carbide, a portion of which is immersed in the mercury. The mercury pool thus serves the double function of cathode and starting electrode cooperative witha boron or silicon carbide electrode. The use of the mercury in the double capacity is, of course, in th interest of economy and convenience and should in noway limit the tance from the pool and in initiating th discharge a spark may be ignited between the starting electrode and the pool. Moreover, the starting electrode may be a band surrounding the envelope of the discharge device in the region of the pool. It is to be noted, however, that while discharges of the latter types may be utilized, they. offer diliculties when used for stroboscopic pur poses. To ignite such discharge devices considerable and persistent starting potential is required and as far as we are aware, the operation of such is uncertain. However, it
discharge devices should b kept in mind that while the discharge devices of the type incorporating the silicon or boron carbide starting electrode are preferable for stroboscopic work, where the discharge devices of the last-mentioned types have utility and where the teaching of our invention is otherwise fol-- lowed such use of the discharge devices are equivalent which fall within the scope of our invention. 1
In accordance with our invention, a source of electrical energy is connected across the principal electlodes'of the discharge device and a capacitor is connected in parallel with the principal elec In the circuit ofthe starting electrodes of the discharge device a valve is connected:
trodes.
The supply of starting current through the valve and the rate of charge and discharge *of the capacitor are so timed that the discharge devicelarity in the appended claim. The invention ,it-
self, however, both as to its organization and its method of operation, together with additional objects and advantages thereof, will best be understood from the following description of specific embodiments when read in connection with the accompanying drawings, in which:
Figure l is a diagrammatic view showing an embodiment of our invention;
Fig. 2 is a diagrammatic view showing a modification of our invention;
Fig. 3 is a graph illustrating the operation of the apparatus shown in Fig. 2;
Fig. 4 is a diagrammatic view showing a further modification of our invention;
Fig. 5 is a diagrammatic view showing a still further modification of our invention; and
Fig. 6 is a graph illustrating the operation of the apparatus shown in Fig. 5.
Our invention is illustrated herein as utilized in a stroboscope. For stroboscopic purposes, a luminous discharge which can be ignited and extinguished with a precise periodicity is a desideratum. However, as will be manifest from the following description, our invention. may also be utilized for other purposes.
The apparatus shown in Fig. 1 comprises a discharge device I having an anode 3, a mercury pool cathode 5, and a starting electrode I composed of a high resistive material such as boron carbide or silicon carbide, a portion of which is immersed in the mercury 5. When the discharge device I is energized, as shall be explained hereinafter, the radiations emitted by the luminous spot formed on the mercury pool surface are projected on the body 9 under observation which is illustrated as the spoke of a rotating wheel II. The discharge device I is energized and deenergized at a periodicity corresponding to the periodicity of the wheel II and when the spoke 9- is observed in the illumination emitted by spot, it appears to be at rest. When we refer hereinafter to an electrode or a material of the igniter type we mean thereby an electrode such as I or the material of which it is formed. The
material in question may be not only Of silicon carbide or boron carbide but any other substance which when contacting an electrode and operated by current has the property of facilitating the initiation of an are between said electrode and another electrode.
A capacitor I3 is connected to the anode 3 of the discharge device. I through an inductor I5 and directly to the cathode 5 of the discharge device. The capacitor I3 is charged through a resistor I1 from a source I9 which is preferably of the direct current type. The starting electrode I is connected to the capacitor [3 through an auxiliary discharge device 2| and the inductor I5. The auxiliary discharge device 2| is preferably of the type having an abrupt characteristic. It is. provided with an anode 23, a hot cathode and a control electrode 21 which are immersed in a gaseous medium. The anode 23 is connected to the inductor I5 while the cathode 25 is connected to the starting electrode 1 through a current limiting resistor 29. The control electrode 21. is connected to the cathode 25 through a variablebiasing battery- 3 I In operation, the auxiliary discharge device 2I is normally deenergized. The capacitor I3 is charged through the resistor II in series therewith. When it attains a difference of potential predetermined by the magnitude of the bias in the control circuit of the auxiliary discharge device the latter is energized and a pulse of current is transmitted between the starting electrode I and the mercury pool 5. A discharge is, therefore, initiated between the principal electrodes 3 and 5 of the main discharge device I which persists for an interval of time predetermined by the relative magnitudes of the inductor I5 and the capacitor I3. The capacitor I3 is discharged when the main discharge device I is energized and when the main discharge device is extinguished, the capacitor is recharged and the above-described process is repeated. Since the electrode I and the mercury 5 both cooperate to produce an arc, they may be designated together as a plurality of starting electrodes.
The excitation of the main discharge device I is periodic. The periodicity of the excitation may be varied either by varying the resistor II in series with the capacitor I3, and thus varying the rate of charging of the capacitor, or by varying the biasing battery in the control circuit of the auxiliary discharge device, and thus varying the magnitude of the charge which is to be applied to the capacitor to produce excitation of the auxiliary discharge device. In the practice of our invention, either of these elements is so varied that the frequency of discharge of the main discharge device corresponds to the frequency of movement of the body 9 under observation. This correspondence is attained by subjecting the body 9 to the illumination from the discharge device and by slowly varying the resistor or the control battery until the body appears to be at rest.
In the apparatus shown in Fig. 2, the proper periodicity of illumination is attained by utilizing the output of a master oscillator 33, the frequency of which may be varied. Here again, a capacitor I3 is connected between the mercury pool 5 and the anode 3. of the main discharge device I. The capacitor I3 is charged from a source 34 through an auxiliary discharge device 35 of the type having an anode 31, a cathode 39 and a control electrode 4|. If the source 34' utilized for charging is of the alternating current type, the auxiliary discharge device 535 should preferably be of the asymmetric type and should be so connected to the capacitor I3 that the capacitor plate 63 which is connected to the anode 3 of the main discharge device I is charged positive.
The excitation of the auxiliary discharge device 35' is controlled. from the master oscillator 33. A potential provided by the master oscillator 33 is impressed between the control electrode 4| and the cathode 39 through a secondary section 45 of a suitable transformer 41 and the discharge device 35 is energized at a frequency corresponding tothat of the master oscillator.
The master oscillator 33 also provides current impulses for energizing the main discharge device. For this purpose, another secondary section 4 9 of the transformer 47 is connected between the starting electrode 'I- and the mercury pool 5- of the main discharge device I through a suitable rectifier 5I. Half-Wave impulses produced by the oscillator 33 are thus transmitted through the starting electrode 7 of the main discharge device I and periodically initiate the discharge in the main discharge device, the anode-cathode potential being supplied by the capacitor I3.
To provide for precise operation of the main discharge device I, the secondaries 45 and 49 of the oscillator transformer 41 are so wound that the initiating discharge through the starting electrodes of the main. discharge device after the capacitor I3 has been charged and when the auxiliary discharge dea is only transmitted vice 35 blocks the charging current. Preferably, the potential supplied'to the control circuit of theauxiliary discharge device 35 is m opposite phase to the potential supplied between the starting electrodes I and of-the main discharge device I, to accomplish this purpose.
The operation of the apparatus is illustrated in Fig. 3. In this view, the full-line sinecurve 53 representsthe control potential supplied by the oscillator 33 to the auxiliary discharge device 35. The broken-line sine curve 55 represents the control potential supplied between the starting electrodes 1 and 5. It will be noted that the fullline and the broken-line curves 53 and 55 are in opposite phase. The potential difference impressed on the capacitor I3 is represented by the full-line curve 51 rising above the sine curves. If the resistance in series with the capacitor I3 is comparatively small, the capacitor may be charged during the interval corresponding to a single half-wave of the potential supplied by the oscillator 33 as illustrated. During the succeeding half cycle, sufiicient current is transmitted between the starting electrode 1 and the mercury pool 5 of the main discharge device to energize the main discharge device I and the main discharge device having been energized, the capacitor I3 is discharged.
A rectifier 59 is connected between the anode 3 and the cathode 5 of the main discharge device I to prevent the current in the main discharge device from oscillating. The cathode 6| of the rectifier 59 is connected to the anode 3 of the main discharge device I and the anode 63 of the rectifier is connected to the mercury pool 5. If there is a tendency to oscillate, the rectifier network absorbs the oscillations.
In the apparatus shown in Fig. 4, the capacitor I3 connected between the anode and the cathode of the main discharge device is charged during a predetermined interval of time and after it has been so charged, it is discharged during a later interval of time.
For this purpose, an auxiliary discharge device 35 similar to the discharge device utilized inthe modification shown in Fig. 2 is provided in series with the power source 34 and the capacitor |3. The cathode 39 of the auxiliary discharge device 35 is connected to the plate 43 of the capacitor l3 that is to be charged positive and the anode 3! is connected to the source. Normally, the discharge device 35 is in non-conductive condition by reason of the functioning of a biasing battery 55 connected between the cathode 39 and the control electrode 41 which maintains the interval of time, the control electrode 4| is at the same potential as the cathode 39. The discharge device, therefore, passes current to charge the capacitor l3. The total resistance in series with the capacitor is comparatively low and the capacitor is charged in a short interval of time.
To ignite the main discharge device I, a second commutator mounted on the shaft 11 of the commutator 69 and rotating in synchronism is provided. The second commutator I5 is provided 'with a conducting segment 19 which iis directly connected 'to the starting electrode 1. A brush 8| 'in'coritact with the surface of the commutator i5 isconnected to that plate 43' of the capacitor |3 which is charged positive through a suitable impedance 83. The impedance properly regulates the starting impulse of current when it'is transmitted,
Theconducting segment 19 on the last-mentioned commutator i5 is displaced in phase with respect to the conducting segment 1| of the firstmentioned capacitor 59. It operates when contacted by its brush 8! to discharge the capacitor 3, after it'has been charged, through the starting electrode! and the mercury pool 5. The charge on the capacitor I3 is not exhausted by the impulse transmitted through the starting electrode 1' and the'residual difference of potential is of sufficient magnitude to cause'the main discharge device! to become energized. When the main discharge device is energized, the starting elec-} trode circuit isshunted out. It will be seen from the above description that a small portion of the 'chargeon the capacitor is utilized to ignite the dischargedevice after-which the residual charge is utilized in" producing the main discharge. A single-capacitor serves the double function of providing starting current and discharge potential. The periodicity of the discharge produced in the main discharge device may be varied by varying the speed of the commutators 59 and 15.
In the apparatus shown in Fig. 5, the capacitor |3 connected between the anode 3 and the oathode 5 of the main discharge device I is charged through a half-wave rectifier from an alternating source 34. To discharge the capacitor l3 through the starting electrode 1, an auxiliary discharge device 2|, similar to the discharge device utilized in the embodiment shown in Fig. 1, is provided in series with the starting electrode 1 and the cooperative mercury pool 5. The cathode '25 of the auxiliary discharge device 2| is connected through the limiting resistor 29 to the starting electrode 1, and the anode 23 is connected to the positive plate 93 of the capacitor l3.
The control circuit of the auxiliary discharge device 2| is supplied from a transformer 81, the primary 99 of which is connected across the secondary 9| of the main power supply transformer 93. However, the terminals of the primary 89 of the auxiliary transformer 81 are so arranged with respect to the terminals of the secondary 9| of the main transformer 93 that the potential supplied in the control circuit of the auxiliary device 2| is displaced in phase with respect to the potential supplied by the secondary 9| of the main transformer.
In Fig. 6, the operation of the apparatus is illustrated graphically. The full-line sine curve 95 represents the potential supplied by the main transformer 93 and the broken-line sine curve 91 represents the control potential supplied by the auxiliary transformer. Since the resistance in series with the capacitor l3 and the half-wave rectifier 85 is small, the capacitor I3 is quickly charged during the half cycles during which the potential output of the main transformer 93 is such that rectifier B5 is conductive. The dot-dash curve 99 represents the charging operation. After the capacitor |3 is charged and the charging operation is discontinued, the control potential supplied to the auxiliary discharge device 2| attains a value of sufficient magnitude to energize the auxiliary discharge device. The capacitor |3 is then discharged through the discharge device 2! and through the starting electrode 1 of the main discharge device I'. The main discharge device I is immediately energized under the influence of the residual potential difierence impressed on the capacitor and it remains energized until the capacitor is discharged. After this, the capacitor is recharged and the process is repeated. It is to be noted that here again a single capacitor I3 is utilized for the double purpose of supplying starting current and ignition potential.
Our invention has been herein shown and described as utilizing a main discharge device I in which the cathode is a, mercury pool. The principal advantage of such a discharge device resides in the intense cathode spot which forms on the surface of the cathode when the discharge device is energized. Discharge devices having cathodes of other types have been utilized by us and on the surface of the cathode in certain of these discharge devices a cathode spot also forms. We have found this is particularly true of discharge devices in which the cathode is composed of such metals as cadmium, zinc, sodium, potassium, or alloys. of these metals. In the claim which follows, we shall refer to a discharge device having a. mercury cathode or a mercury pool cathode.
We intend bythis expression to cover the general case of a cathode on which a cathode spot forms and the expression shall be taken to include cathodes of all types on which a cathode spot forms.
We claim as our invention;
An electrical system comprising a capacitor; means. for charging said capacitor, a discharge channel for said capacitor including an asymmetrically conductive main electric discharge device, said channel having a tendency to cause the current in said main discharge device to oscillate thereby to tend to produce back discharge of said capacitor through said discharge device; and unidirectional by-pass means connected in shunt with said discharge device in inverse conductive direction thereto to prevent said current in said main discharge device from oscillating.
DEWEY D. KNOWLES. CECIL E. HAILER.
REFERENCES CITED UNITED STATES PATENTS Name Date Rava Mar. 18, 1941 Number
US694060A 1946-08-30 1946-08-30 Capacitor charge and discharge circuit for stroboscopes Expired - Lifetime US2516326A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703374A (en) * 1951-01-15 1955-03-01 Fruengel Frank Stroboscopic light source
US2840763A (en) * 1954-03-08 1958-06-24 Westinghouse Electric Corp Stroboscopic lamp control arrangements
DE1136775B (en) * 1959-11-30 1962-09-20 Akad Wissenschaften Ddr Noble gas discharge lamp, preferably for generating light pulses

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2235385A (en) * 1939-03-23 1941-03-18 Rava Alexander Welding method and apparatus

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2235385A (en) * 1939-03-23 1941-03-18 Rava Alexander Welding method and apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703374A (en) * 1951-01-15 1955-03-01 Fruengel Frank Stroboscopic light source
US2840763A (en) * 1954-03-08 1958-06-24 Westinghouse Electric Corp Stroboscopic lamp control arrangements
DE1136775B (en) * 1959-11-30 1962-09-20 Akad Wissenschaften Ddr Noble gas discharge lamp, preferably for generating light pulses

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