|Publication number||US2782867 A|
|Publication date||Feb 26, 1957|
|Filing date||Sep 3, 1952|
|Priority date||Sep 3, 1952|
|Publication number||US 2782867 A, US 2782867A, US-A-2782867, US2782867 A, US2782867A|
|Inventors||Hall Herbert J|
|Original Assignee||Research Corp|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (10), Referenced by (10), Classifications (11)|
|External Links: USPTO, USPTO Assignment, Espacenet|
Feb. 26, 1957 H. J. HALL PULSER CIRCUIT 2 Sheets-Sheet 1 Filed Sept. 3, 1952 95 6 09 ok on 5 22%? 1055mm m 253027202 56x6 m W 5095 E Q d W om III 3 E0252 5301 uzimou N R uwii zmozluz ozimom 3 5m HERBERT J. HALL ATTORNEY H. J. HALL PULSEIR CIRCUIT Feb. 26, 1957 2 Shee'ts-Sheet 2 Filed Sept. 3, 1952 mm. X: F
I NVENTOR HERBERT J, HALL WZOEhumm v m \mQZEGME op ATTORNE Y United States Patent PULSER CIRCUIT Herbert J. Hall, Hopewell Township, Mercer County, N. J., assignor to Research Corporation, New York, N. Y., a corporation of New York Application September 3, 1952, Serial No. 307,588 7 Claims. or. 1834 This invention relates to electrical pulser circuits, wherein a load is energized by a succession of discrete increments of electrical energy separated by intervals of substantially greater duration than the duration of the increments of electrical energy. in particular, it relates to pulse circuits energizing a load wherein interelectrode sparking may occur during normal operation. Typical examples of such sparking loads are magnetrons and electrostatic precipitators. in order to obtain maximum power output from a magnetron, or maximum collection efiiciency in an electrostatic precipitator, it is necessary to operate at the highest possible voltage which results in appreciable interelectrode sparking. It is a primary object of the invention to improve the operation of such circuits, particularly with reference to the above described sparking conditions.
To maintain stable operation and long tube life in pulse circuits of the type under consideration, disturbances caused by sparking in the load, by pulse transformer oscillations, or by stray capacitance circuit effects must either be eliminated or sufiiciently attenuated. These circuit disturbances are relatively small and easy to control at low power levels but they rapidly increase in magnitude and design importance as the power level is raised. Certain of them are also aggravated with long pulse durations, for example, pulse durations greater than 50 microseconds in the type of circuit under consideration. An electrical precipitator for cleaning gases comprising spaced insulated electrodes between which the gases pass and across which a high voltage electrical discharge is maintained by periodically supplied increments of electrical energy to remove particles by electrostatic action, is subject to wide variations in load conditions. The mixtures of gas and suspended solid and/or liquid particles which are treated by the precipitator are very variable in physical, chemical, and electrical characteristics due to changes at the origin of the mixtures depending on the operating conditions in the furnace which pro duces the mixtures. The electrodes must also be periodi cally rapped to loose particles clinging to them which have been precipitated out of the gas, and the resulting falling material also greatly alters the nature of the gap or load between the electrodes. As a result, spark-overs frequently take place between the electrodes which temporarily short circuit the precipitator and initiate transients which, unless prevented from doing so, will travel back to the power supply circuit and cause difiiculties of the type indicated above. A known system of the above type, together with certain means for minimizing some of the above described difficulties, is shown in U. S. Patent No. 2,509,548 to H. J. White. This patent shows the use of a rotary gap switch to provide the required periodic discharges. It has been found that greatly improved performance and stability may be obtained by using instead of such a gap switch, a high power hydrogen thyratron. The advantages of such use are applicable not only to precipitator circuits, but also to any circuit requiring high power load pulses, such, for example, as the commonly ice employed magnetron circuits widely used in radar or similar pulse applications. However, as the power levels handled are increased, it is found that the sparking (lifticulties are also increased, to the point where the precautions which have sufiiced for moderate power circuits are no longer adequate. As the power level increases, higher voltages employed require the use of large, oil-filled transformers and other components wherein it is more difiicult to keep stray capacitances low.
According to the invention, an arrangement is provided wherein the pulse-forming network (or at least the capacitances associated with the pulse-forming network) may be isolated from the pulse transformer and the load circuit by placing the thyratron or other unidirectional switching device between it and the pulse transformer. in addition, all stray capacitances to ground associated with the charging circuit, thyratron filament transformer and grid-coupling transformer are so arranged as to add in parallel with the capacitance of the pulse-forming net- Work and are thus discharged through the pulse transformer and not directly through the thyratron. Furthermore, the pulse transformer primary is isolated from the pulse-forming network charging circuit, at least in the direction of current flow in which damage could be done, and one side of the pulse-forming network is grounded. These features of the new circuit eliminate most of the disadvantages above recited, or minimize them to a point where they are no longer obiectionable. it has been found that the maximum x a ses of the circuit which will be described below obi. red when the thyratrcn grid circuit is provided with very low impedance. in the order of between 50 and ohms, as against 300 or more ohms usually employs-l. The use of this low grid circuit impedance has been found to simplify both tube and circuit design problems.
The specific nature of the invention, as well as other objects and advantages thereof, Will clearly appear from a description of a preferred embodiment as shown in the accompanying drawings in which:
Fig. l is a schematic circuit diagram of the improved circuit applied to generalized pulse load which is indicated by way of example as a magnetron; and
Fig. 2 shows a modification of the above circuit applied to the energization of several sections of a conventional electrical precipitator.
Referring to Fig. 1, condensers 2 of a pulse-forming network generally indicated at 4, are charged to a suitable voltage from a D. C. power supply 6 through reactor 8 and a diode It). The energy thus stored is periodically dischar ed through inductances 12 and the primary of the pulse transformer 14 by means of the hydrogen thyratron 16. The negative voltage pulse obtained is amplified by the pulse transformer and may be fed to a utilization device shown as a magnetron 17 connectcd across the secondary terminals. The shape of the pulse is controlled by the particular design of the pulseforming network. The circuit is normally operated with a small post-pulse reverse voltage across the thyratron to assist in the deionization thereof, as is well understood. In the case of heretofore used circuits, if magnetron sparking should occur, a large reverse voltage appears across the condensers of the pulse-forming network and causes the charging voltage on the following pulse to rise considerably above its normal value. The use of a unidirectional shunting diode may serve to minimize this effect, if the operation is restricted to moderate power levels. However, at high power levels such as are contemplated in the present invention, this situation obviously results in unstable performance, producing a fluctuating output voltage which may perpetuate sparking, cause insulation overstresses in the circuit, and may cause the thyratron to go into continuous conduction grease? with complete cessation of normal operation. Moreover,
in the prior art circuits, a number of stray capacitances, such as those of the various inductance elements to ground, must be discharged directly through the thyratron. This causes high peak currents and rapid rates of rise which may damage the thyratron. As the power level increases, higher voltages employed require the use of large, oil-filled transformers and other components wherein it is even more difficult to keep stray capacitances low. The improved circuit of Fig. 1 minimizes all of the above difficulties to the point where satisfactory operation is readily obtainable. It will be noted that the thyratron is now placed between the pulse-forming network and the pulse transformer, and the D. C. power a supply is grounded on the positive side. One side of the pulse-forming network is accordingly now at ground po' tential and the other side is isolated against the previously described disturbances by the thyratron 16. A conventional damping circuit is also shown at 18 to reduce the effect of reverse polarity pulses. A damping diode 19 may also be provided across network 4 if desired. All stray capacitancesto ground associated with the charging circuit, thyratron filament transformer and grid-coupling transformer now add in parallel with the capacitance 2 of the pulse-forming network and are thus discharged through the pulse transformer and not directly through the thyratron. This circuit eliminates the major difiiculties of the prior art circuits and permits stable operation at high power with sparking loads. Transient voltages due either to load sparking or normal pulse transformer oscillations are attenuated in the damping circuit 18 placed directly across the pulse transformer primary. Additional protection against such transients affecting the voltage across the network is obtained by the isolating properties of the thyratron. In order to obtain maximum effect of these isolating properties and to maintain stable operation, it has been found that the thyratron grid circuit must have a low impedance in the order of between 50 and 190 ohms. -As in all pulse circuits, operation should be adjusted for some reverse voltage swing across the network, in this case, positive, to permit rapid deionization of the thyratron. A low grid circuit impedance is conveniently obtained from a conventional low power pulser 22 with a 50 ohm resistor load 20 in series vwith the thyratron cathode feeding a 1:1 isolating transgenerally indicated at 22, and contains no novel feature except for the low-resistance element 20.
Fig. 2 shows the novel circuit of the invention applied to the energization of an electrical precipitator generally indicated at 24. The central electrode of the precipitator is supplied by lead 26. Similar leads 28, 30, and 32 supply similar sections of the same or adjacent precipitators, and are successively energized by rotary switch 34 .which connects them in turn to the secondary of the pulse transformer 14. The rotary switch is driven by any suitable motor 36, which typically may be an alternating current motor running at 3600 R. P. M. A typical pulse repetition rate might be 480 per second distributed to the four sections shown. Motor 36 also drives a small alternator .38, conveniently of the permanent magnet type, which, for the 480 cycle per second output above indicated, might be a 16-pole machine, or alternately a 240 cycle alternator having 8 poles could be used with a full-wave rectifier to supply the synchronizing voltage for a 480 per second pulse rate. The output alternator 38 is used to synchronize the driver circuit trigger pulse rate so that thyratron 16 will be properly synchronized with the positions of the distributor switch 34. The output of the alternator 38 is fed into a conventional adjustable phase shift network 40, for proper adjustment of the overall system.
In Fig. 2 the pulse-forming network is simplified by reducing it to a pulse condenser 42 and an inductance 44 which now may be separated in the circuit as shown; this inductance, for example, may be the leakage inductance of the pulse transformer, thereby considerably simplifying the circuit while retaining the advantages of Fig. 1 by locating the pulse condenser 42 as shown. It may be noted again that, in the circuit of Figs. 1 and 2, the pulse condenser is charged directly from the D.-C. power supply and not through the primary of the pulse transformer as is common practice in conventional pulse circuits. In this way, post pulse oscillations of the transformer circuit cannot modulate the charging voltage waveform and thus cause unstable operation. A hold-off diode 46 is inserted, in accordance with known practice, between pulse transformer 14 and the distributor switch 34. Since the high power hydrogen thyratron employed is of the type which usually has an internal hydrogen reservoir, and a heater, the circuit illustrates at 48 a suitable method of obtaining adjustable heater voltage therefor.
Grid-coupling pulse transformer 50 is shown with its primary connected in series with the trigger circuit pulseforming network and the load resistor 20a connected on the secondary side. The transformer is connected to supply a positive output pulse. Transformer 50 may conveniently have a 1:1 ratio, and 20a is a non-inductive resistance of from 50 to ohms. A driver circuit pulse-forming network 52, supplied by low-power hydrogen thyratron 51, may consist of a condenser and inductance in series, or any other well known circuit for this purpose may be used. The leakage inductance of the transformer 50, with proper design, may be used as the series inductance in the driver circuit pulse-forming network, thus eliminating one component; The charging resistor 54 in the driver circuit may, if desired, be replaced by a linear charging choke to increase the electrical efficiency of the system. If this is done the charging choke inductance should preferably be designed for resonant charging with the capacitance in the pulseforming network at the desired pulse repetition rate.
It will be apparent that the embodiments shown are only exemplary and that various modifications can be made in construction and arrangement within the scope of the invention as defined in the appended claims.
1. A pulser circuit for loads subject to random sparking comprising a pulse transformer for supplying said load, a D. C. power supply, pulse forming circuit elements including capacitance means connected across and between the positive and thenegative sides of said power 'supply so as to be charged thereby, a high-power thyratron having a control grid and being connected between the negative side to which said capacitance means is connected and one side of said pulse transformer the cathode of said thyratron being in said negative side, the positive side of said capacitance means and said pulse transformer being connected to a common ground, a trigger circuit for periodically biasing the grid of said thyratron to firing condition the grid circuit being of very low impedance.
2. The invention according to claim 1, wherein the common ground is the positive side of the D. C. power supply.
3. The invention according to claim 1 wherein the low-impedance circuit has an impedance value in the range between 50 and 100 ohms.
4. A pulse-charging system for energizing an electric precipitator comprising pulse-forming circuit elements including capacitor means, circuit elements including a series inductance means connecting a source of uni- 5 directional current across said capacitor means, pulsing circuit elements including a thyratron having a control grid and an inductance means connected in series across said capacitor means, said inductance means being supplied by the plate current of the thyratron the cathode of said thyratron and one side of said capacitor being associated with the negative side of said source of unidirectional current means for supplying periodic triggering pulses to the grid of said thyratron to periodically fire same, and circuit elements including a unidirectional current passing device connecting said pulsing circuit with complementary electrodes of a precipitator device.
5. The invention according to claim 4 including a low impedance input circuit between said means for supplying periodic triggering pulses and the thyratron grid, the impedance of the grid circuit being between 50 and 100 ohms.
6. The device according to claim 4 wherein the precipitator device comprises a number of similar precipitator sections, successive switching means for connecting said pulsing circuit in succession with each of said precipitator sections, an A. C. generator device driven in synchronism with the operation of said successive 6 switching means, phase shifting means supplied by the output of said generator, and an operative connection between said phase shifting means and said means for supplying periodic triggering pulses whereby the output of said last means is synchronized with the operation of said successive switching means.
7. The invention according to claim 6 wherein said successive switching means is a rotary switch, and a common driving motor for said rotary switch and said A. C. generator.
References Cited in the file of this patent UNITED STATES PATENTS 2,000,019 Heinrich et al. May 7, 1935 2,400,456 Haine et al. May 14, 1946 2,405,069 Tonks July 30, 1946 2,405,071 Tonks July 30, 1946 2,429,471 Lord Oct. 21, 1947 2,438,962 Burlingame et al Apr. 6, 1948 2,446,838 Lawrence Aug. 10, 1948 2,470,550 Evans May 17, 1949 2,481,925 Hegbar Sept. 13, 1949 2,646,503 Winter July 21, 1953
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US2000019 *||Dec 3, 1931||May 7, 1935||Int Precipitation Co||Art of electrical precipitation|
|US2400456 *||Dec 18, 1943||May 14, 1946||Vickers Electrical Co Ltd||Spark gap electrical apparatus|
|US2405069 *||Feb 23, 1942||Jul 30, 1946||Gen Electric||Pulse generating system|
|US2405071 *||Oct 1, 1943||Jul 30, 1946||Gen Electric||Pulse generating system|
|US2429471 *||Feb 21, 1944||Oct 21, 1947||Gen Electric||Pulse generating circuit|
|US2438962 *||Aug 7, 1944||Apr 6, 1948||Colonial Radio Corp||Protection of thyratron in impulse generating circuits|
|US2446838 *||Jul 25, 1944||Aug 10, 1948||Rca Corp||Pulse forming circuit|
|US2470550 *||Feb 28, 1946||May 17, 1949||Rca Corp||Pulse producing apparatus|
|US2481925 *||Jun 29, 1943||Sep 13, 1949||Rca Corp||Pulse modulator|
|US2646503 *||Nov 29, 1945||Jul 21, 1953||Us Navy||Balanced sweep circuit|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US2879389 *||Dec 28, 1955||Mar 24, 1959||North American Aviation Inc||Magnetic pulse generator|
|US2933690 *||Mar 20, 1957||Apr 19, 1960||Baum Peter A||Boot-strap type driver circuit for producing high voltage pulses|
|US2965832 *||Oct 3, 1957||Dec 20, 1960||Tenny Lode||Electric wave circuit|
|US3076106 *||Sep 25, 1957||Jan 29, 1963||Rca Corp||Inductive circuits|
|US3242464 *||Jul 31, 1961||Mar 22, 1966||Rca Corp||Data processing system|
|US3363402 *||Aug 7, 1964||Jan 16, 1968||Detroit Edison Co||Control system for electrical precipitators|
|US3981695 *||Nov 2, 1973||Sep 21, 1976||Heinrich Fuchs||Electronic dust separator system|
|US4133649 *||Aug 2, 1977||Jan 9, 1979||High Voltage Engineering Corporation||Reduced power input for improved electrostatic precipitation systems|
|US4183736 *||Aug 2, 1976||Jan 15, 1980||High Voltage Engineering Corporation||Electrostatic precipitation|
|US4386395 *||Dec 19, 1980||May 31, 1983||Webster Electric Company, Inc.||Power supply for electrostatic apparatus|
|U.S. Classification||96/54, 307/106, 327/303, 96/82, 331/87, 307/108, 307/327|
|International Classification||H03K3/55, H03K3/00|