US3403295A - Voltage-multiplying, alternating-pulse circuits, notably for the ignition system of internal combustion engines - Google Patents

Voltage-multiplying, alternating-pulse circuits, notably for the ignition system of internal combustion engines Download PDF

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US3403295A
US3403295A US574329A US57432966A US3403295A US 3403295 A US3403295 A US 3403295A US 574329 A US574329 A US 574329A US 57432966 A US57432966 A US 57432966A US 3403295 A US3403295 A US 3403295A
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voltage
alternating
capacitor
internal combustion
thyratrons
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US574329A
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Castelet Gaetan De Coye De
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Renault SA
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Renault SA
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P3/00Other installations
    • F02P3/06Other installations having capacitive energy storage
    • F02P3/08Layout of circuits
    • F02P3/0807Closing the discharge circuit of the storage capacitor with electronic switching means
    • F02P3/0838Closing the discharge circuit of the storage capacitor with electronic switching means with semiconductor devices

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  • An alternating-current generator having a pair of thyratrons connected in series across a direct current source.
  • a monitoring-pulse generator is connected to the control members of the thyratrons to alternatively render them conductive.
  • a capacitor and the primary of a transformer are series connected between a point common to the thyratrons and to a terminal of the current source to develop and deliver the alternating current produced.
  • This invention relates to a device capable of generating relatively powerful alternating-current pulses across the terminals of a coil from .a direct-current source, a pair of electron relays of the threshold and snap-switching type, such as solid or gas thyratrons, at least one capacitor and a monitoring-pulse generator for controlling said relays.
  • a pair of threshold snap-switching electron relays are connected in series across the terminals of said directcurrent source of the alternating pulse generator according to this invention, said relays being rendered conducting alternately, by means of their relevant control members connected to the monitoring-pulse emitter.
  • a capacitor and the primary winding of a transformer having its secondary winding adapted to deliver said alternating pulses.
  • the device according to this invention is capable of charging said capacitor .at a voltage several times higher than that of the supply source. Under low-charge conditions of said coil it was observed that the voltage increase across the terminals of said capacitor was five to seven times the supply voltage.
  • thyratrons more particularly two solid thyratrons of the silicon type frequently referred to as thyristors
  • this device was capable of generating series of alternating pulses across the terminals of the aforesaid secondary winding without causing any one of said thyratrons to remain energized between successive pulse series, thus affording substantial savings in current, the thyratrons used being adapted to be blocked or unblocked by the control gate.
  • a circuit of this character is particularly useful for the ignition systems of the controlled-ignition type for internal combustion engines, when it is desired to produce several sparks per plug at each ignition.
  • a spark may be produced every 20 microseconds during 200 microseconds, it being understood that these figures are given by way of illustration, not in a limiting sense.
  • FIGURE 1 is a wiring diagram of the circuit according to this invention.
  • FIGURE 2 is an electrically equivalent circuit diagram 3,403,295. Patented Sept. 24, 1968 permitting an easier understanding of the voltage-multiplying process;
  • FIGURE 3 is an oscillogram showing a control signal fed to the control elements, notably in the case of an ignition system of internal combustion engine, and
  • FIGURE 4 shows under the same conditions the oscillogram of the voltage obtaining across the coil terminals.
  • a direct-current source 1 has its positive and negative output terminals 2 and 3 connected through a limiting resistance 4 to a capacitor 5.
  • a capacitor 5 In the path extending from the positive plate 6 of capacitor 5 to the negative plate 7 thereof are inserted in series a pair of solid silicon thyratrons 8 and 9, the anode of thyratron 8 being connected to the aforesaid plate 6, and the cathode of thyratron 9 being connected to the negative plate 7.
  • Both thyratrons 8 and 9 are of the inverted type, i.e., the gate control 10 of thyratron 8 acts upon the cathode whereas the gate control of thyratron 9 acts upon the anode.
  • the common circuit point 14 is connected to the plate 17 of a capacitor 16 having its other plate 18 connected through a return line to the negative line 3 and to the armature 7 through the primary winding 19 of a highvoltage transformer feeding through its secondary 20 the load (not shown) utilizing said alternating pulses.
  • This secondary winding 20 may thus be connected to the spark plugs of an internal combustion engine through a conventional distributor (not shown).
  • the capacity of capacitor 16 is but one fraction of that of capacitor 5.
  • each thyratron can be blocked by reversing the voltage produced by the primary winding 19, provided that the control signals have an adequate amplitude and interval between pulses.
  • control signals will appear in the form of trains of waves having a total duration t1, the relative time spacing of the signals being 22.
  • the voltage delivered by the secondary winding 20 and shown in FIGURE 4 will have the rate of the control signals.
  • trains of sparks having the desired duration can be produced with this device by using two conventional-type thyratrons.
  • the alternating control pulses are easily obtained as rectangular signal derivatives. If the source has a low impedance and permits a fast charging of capacitor 16, the storage capacitor 5 and resistance 4 may be dispensed with.
  • An alternating-pulse generator comprising a direct current source, a pair of semiconducting thyratrons of opposite polarities serially connected across said source and each having a control member, one said control member being connected to the anode of one thyratron and the other control member being connected to the cathode of the other thyratron, a monitoring-pulse generator having two outputs, said control members being connected to each other and to one of said output terminals with the other output terminal being connected to a common point between said thyratrons, a capacitor connected to said common point, and a transformer the primary winding of which is serially connected between said-capacitor and one terminal of said source and the secondary winding of which is adapted to deliver said alternating pulses.
  • an alternatingpulse generator in a means for feeding alternating pulses to spark plugs of an internal combustion engine, an alternatingpulse generator according to claim 1 wherein said secondary winding delivers said alternating pulses to said spark plugs.
  • a generator according to claim 2 wherein said monitoring-pulse generator as adapted to trigger said thyratrons in such a manner that a series of alternating pulses having a total duration ranging from 20 microseconds to 200 microseconds per ignition is obtained for each ignition.
  • monitoring-pulse generator comprises a base timer delivering alternating impulses and a gate circuit limiting the duration of the rate of ignition pulses to a determined duration.
  • An alternating-pulse generator according to claim 1 further comprising a storage capacitor connected across and charged by said source.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Synchronous Machinery (AREA)

Description

p 1968 -G. DE COYE DE CASTELET 3,403,295
vOLTAGE-MULTIPLYING, ALTERNATINGPULSE CIRCUITS, NOTABLY FOR THE IGNITION SYSTEM OF INTERNAL COMBUSTION ENGINES Filed Aug. 25. 1966 United States Patent Claims. in. 315-239 ABSTRACT OF THE DISCLOSURE An alternating-current generator having a pair of thyratrons connected in series across a direct current source. A monitoring-pulse generator is connected to the control members of the thyratrons to alternatively render them conductive. A capacitor and the primary of a transformer are series connected between a point common to the thyratrons and to a terminal of the current source to develop and deliver the alternating current produced.
This invention relates to a device capable of generating relatively powerful alternating-current pulses across the terminals of a coil from .a direct-current source, a pair of electron relays of the threshold and snap-switching type, such as solid or gas thyratrons, at least one capacitor and a monitoring-pulse generator for controlling said relays.
A pair of threshold snap-switching electron relays are connected in series across the terminals of said directcurrent source of the alternating pulse generator according to this invention, said relays being rendered conducting alternately, by means of their relevant control members connected to the monitoring-pulse emitter. Between the circuit point common to said relays and one of the terminals of said D.C. source are disposed in series, a capacitor and the primary winding of a transformer having its secondary winding adapted to deliver said alternating pulses.
The device according to this invention is capable of charging said capacitor .at a voltage several times higher than that of the supply source. Under low-charge conditions of said coil it was observed that the voltage increase across the terminals of said capacitor was five to seven times the supply voltage. By using for example two thyratrons, more particularly two solid thyratrons of the silicon type frequently referred to as thyristors, it was observed that this device was capable of generating series of alternating pulses across the terminals of the aforesaid secondary winding without causing any one of said thyratrons to remain energized between successive pulse series, thus affording substantial savings in current, the thyratrons used being adapted to be blocked or unblocked by the control gate.
A circuit of this character is particularly useful for the ignition systems of the controlled-ignition type for internal combustion engines, when it is desired to produce several sparks per plug at each ignition. Thus, for example, a spark may be produced every 20 microseconds during 200 microseconds, it being understood that these figures are given by way of illustration, not in a limiting sense.
In order to aflFord a clearer understanding of this invention and of the manner in which the same may be carried out in practice, reference will now be made to the accompanying drawing in which:
FIGURE 1 is a wiring diagram of the circuit according to this invention;
FIGURE 2 is an electrically equivalent circuit diagram 3,403,295. Patented Sept. 24, 1968 permitting an easier understanding of the voltage-multiplying process;
FIGURE 3 is an oscillogram showing a control signal fed to the control elements, notably in the case of an ignition system of internal combustion engine, and
FIGURE 4 shows under the same conditions the oscillogram of the voltage obtaining across the coil terminals.
In the wiring diagram of FIGURE 1 a direct-current source 1 has its positive and negative output terminals 2 and 3 connected through a limiting resistance 4 to a capacitor 5. In the path extending from the positive plate 6 of capacitor 5 to the negative plate 7 thereof are inserted in series a pair of solid silicon thyratrons 8 and 9, the anode of thyratron 8 being connected to the aforesaid plate 6, and the cathode of thyratron 9 being connected to the negative plate 7. Both thyratrons 8 and 9 are of the inverted type, i.e., the gate control 10 of thyratron 8 acts upon the cathode whereas the gate control of thyratron 9 acts upon the anode. Under these conditions the two gates are electrically in parallel in relation to the circuit point 14 common to both thyratrons and connected by means of limiting resistances 12 and 13 to a known generator 15 of trains of alternating pulses, the first signal of one train of waves fed to the gates being positive, the following one being therefore negative in relation to point 14, as evidenced by FIGURE 3.
The common circuit point 14 is connected to the plate 17 of a capacitor 16 having its other plate 18 connected through a return line to the negative line 3 and to the armature 7 through the primary winding 19 of a highvoltage transformer feeding through its secondary 20 the load (not shown) utilizing said alternating pulses. This secondary winding 20 may thus be connected to the spark plugs of an internal combustion engine through a conventional distributor (not shown). The capacity of capacitor 16 is but one fraction of that of capacitor 5.
The operation of this circuit will now be explained with reference to the electrically equivalent circuit diagram illustrated in FIGURE 2, wherein the thyratrons 8 and 9 are replaced by fixed contacts 8 and 9 a movable contact blade 14' being disposed between these contacts having diodes 8 and 9 mounted in series thereacross. The rnovement of contact blade 14' simulates the energization of the thyratrons by their relevant gates under the influence of the monitoring pulse generator 15.
(1) From a positive voltage of plate 6 in relation to plate 7, this positive voltage being equal to the voltage T of source 1, closing the contact 8 14' will bring the voltage of plate 17 of capacitor 16 substantially to the aforesaid voltage value T, this also applying therefore to the winding 19 through which a current i is gradually produced as the voltage across the terminals of said winding decreases and plate 18 is charged in relation to 17. After the voltage across the terminals of winding 19 has attained zero value a reverse voltage appears as i decreases. Under these conditions, plate 18 is charged toward T and plate 17 remains at +T, the discharge being prevented by the diode 8 Thus, the difference in potential between these plates 17 and 18 is 2T.
(2) As contact 9 14 is closed, armature 17 resumes substantially the potential of the negative terminal 3 as a current develops in winding 19, the same process as decribed in paragraph (1) hereinabove being repeated but with opposite signs. Upon completion of the cycle, the capacitor is charged at a value approximating 2T but reversed, plate 17 being negative in relation to plate 18.
(3) Reclosing contacts 8 14' will cause the voltages of capacitors 5 and 16 to add themselves and a voltage value approaching 3T is fed to winding 19. At the end of the cycle, as the plate 17 remains connected to the plate 6 of capacitor 5, the value acquired by the other capacitor 16 approximates 4T.
(4) In fact, the voltage increase of capacitor 16 is attended by an increment in the coil losses, notably in the spark and a stabilized condition is obtained after a few cycles. I
Referring again to the wiring diagram of FIGURE 1, it will be readily understood that each thyratron can be blocked by reversing the voltage produced by the primary winding 19, provided that the control signals have an adequate amplitude and interval between pulses.
As illustrated in FIGURE 3, these control signals will appear in the form of trains of waves having a total duration t1, the relative time spacing of the signals being 22.
The voltage delivered by the secondary winding 20 and shown in FIGURE 4 will have the rate of the control signals.
In the specific case of the ignition system of internal combustion engines, trains of sparks having the desired duration can be produced with this device by using two conventional-type thyratrons. The alternating control pulses are easily obtained as rectangular signal derivatives. If the source has a low impedance and permits a fast charging of capacitor 16, the storage capacitor 5 and resistance 4 may be dispensed with.
I claim:
1. An alternating-pulse generator comprising a direct current source, a pair of semiconducting thyratrons of opposite polarities serially connected across said source and each having a control member, one said control member being connected to the anode of one thyratron and the other control member being connected to the cathode of the other thyratron, a monitoring-pulse generator having two outputs, said control members being connected to each other and to one of said output terminals with the other output terminal being connected to a common point between said thyratrons, a capacitor connected to said common point, and a transformer the primary winding of which is serially connected between said-capacitor and one terminal of said source and the secondary winding of which is adapted to deliver said alternating pulses.
2. In a means for feeding alternating pulses to spark plugs of an internal combustion engine, an alternatingpulse generator according to claim 1 wherein said secondary winding delivers said alternating pulses to said spark plugs.
3. A generator according to claim 2 wherein said monitoring-pulse generator as adapted to trigger said thyratrons in such a manner that a series of alternating pulses having a total duration ranging from 20 microseconds to 200 microseconds per ignition is obtained for each ignition.
4. A generator according to claim 1 wherein said monitoring-pulse generator comprises a base timer delivering alternating impulses and a gate circuit limiting the duration of the rate of ignition pulses to a determined duration.
5. An alternating-pulse generator according to claim 1 further comprising a storage capacitor connected across and charged by said source.
References Cited I UNITED STATES PATENTS 3,257,566 6/1966 White 30788.5 3,211,964 10/1965 Thorne 307-88.5 3,163,782 12/1964 Ross 7-88.5 2,175,900 10/1939 Knight 315177 JOHN W. HUCKERT, Primary Examiner.
J. R. SHEWMAKER, Assistant Examiner.
US574329A 1965-09-06 1966-08-23 Voltage-multiplying, alternating-pulse circuits, notably for the ignition system of internal combustion engines Expired - Lifetime US3403295A (en)

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FR30550A FR1492019A (en) 1965-09-06 1965-09-06 Alternating pulse voltage multiplier circuit, especially for ignition of internal combustion engines

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DE (1) DE1288129B (en)
ES (1) ES330906A1 (en)
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OA (1) OA02255A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3509443A (en) * 1968-11-27 1970-04-28 Gen Electric Pulse circuit for supplying two closely spaced electric pulses
US3656046A (en) * 1970-06-18 1972-04-11 Galbraith Pilot Marine Corp Power conversion system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2175900A (en) * 1939-10-10 knight
US3163782A (en) * 1963-07-25 1964-12-29 Ling Temco Vought Inc Multiple delay line solid state pulse modulator
US3211964A (en) * 1963-04-05 1965-10-12 Ampex Actuator power supply
US3257566A (en) * 1961-08-21 1966-06-21 Hoffman Electronics Corp Complementary controlled rectifier switch

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2175900A (en) * 1939-10-10 knight
US3257566A (en) * 1961-08-21 1966-06-21 Hoffman Electronics Corp Complementary controlled rectifier switch
US3211964A (en) * 1963-04-05 1965-10-12 Ampex Actuator power supply
US3163782A (en) * 1963-07-25 1964-12-29 Ling Temco Vought Inc Multiple delay line solid state pulse modulator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3509443A (en) * 1968-11-27 1970-04-28 Gen Electric Pulse circuit for supplying two closely spaced electric pulses
US3656046A (en) * 1970-06-18 1972-04-11 Galbraith Pilot Marine Corp Power conversion system

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FR1492019A (en) 1967-08-18
GB1160901A (en) 1969-08-06
DE1288129B (en) 1969-01-30
ES330906A1 (en) 1967-09-16
OA02255A (en) 1970-05-05

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