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GB2326195A - A capacitor discharge ignition circuit - Google Patents

A capacitor discharge ignition circuit Download PDF

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Publication number
GB2326195A
GB2326195A GB9810332A GB9810332A GB2326195A GB 2326195 A GB2326195 A GB 2326195A GB 9810332 A GB9810332 A GB 9810332A GB 9810332 A GB9810332 A GB 9810332A GB 2326195 A GB2326195 A GB 2326195A
Authority
GB
United Kingdom
Prior art keywords
capacitor
inductance
ignition
voltage
switching means
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.)
Granted
Application number
GB9810332A
Other versions
GB9810332D0 (en
GB2326195B (en
Inventor
Richard Arthur George Kinge
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.)
Smiths Group PLC
Original Assignee
Smiths Group PLC
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 GBGB9712110.7A external-priority patent/GB9712110D0/en
Application filed by Smiths Group PLC filed Critical Smiths Group PLC
Priority to GB9810332A priority Critical patent/GB2326195B/en
Publication of GB9810332D0 publication Critical patent/GB9810332D0/en
Publication of GB2326195A publication Critical patent/GB2326195A/en
Application granted granted Critical
Publication of GB2326195B publication Critical patent/GB2326195B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • 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

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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)

Abstract

An ignition system has an input circuit 3 comprising a voltage source 30 with a first capacitor 32 connected across the voltage source 30 and a plurality of charging circuits 1A, 1B, 1C, each controlled by a common trigger 40, connected to the input circuit 3 and an ignition output; where the charging circuits 1A, 1B, 1C comprise a series connection of a switch 10, preferably a thyristor, an inductance 12 and a second capacitor 13 connected across the first capacitor 32 of the input circuit such that when the switch 10 is closed, as no charge is stored on capacitor 13 all the voltage appears across the inductance 12 resulting in a high peak voltage at igniter 2A. The current rises, limited by inductance 12 causing capacitor 13 to be charged, until the voltage across the capacitor 13 equals the voltage across capacitor 32 and energy is stored in inductance 12. At this point energy stored in inductance 12 is transferred to the capacitor 13, increasing the voltage before discharging charge from capacitor 13 followed by remaining charge on capacitor 32 across igniter 2A.

Description

IGNITION SYSTEMS AND METHODS This invention relates to ignition systems and methods.
High energy ignition systems are usually of the capacitor discharge kind where electrical energy is stored in a capacitor and is then rapidly discharged to an igniter or spark plug, producing an intense spark sufficient to ignite a fuel-air mixture. A solid state igniter may require a voltage of up to about 2000volts to ensure reliable ignition in a gas-fuelled or oil-fuelled turbine. Once the flash has occurred, the voltage collapses to near zero while a large current flows, commonly in excess of 1 500amps, for the duration of the spark, until the energy stored in the capacitor has been dissipated. Various different arrangements are used to perform the switching operation by which the charged capacitor is connected to the igniter.
For example, gas discharge tubes can be used, but these are bulky, expensive and can be delicate. Solid state switches, such as thyristors, have various advantages in that they are robust, compact and easily controlled. One problem with solid state switches is that those capable of handling very high voltages and currents are very expensive.
It is an object of the present invention to provide an improved ignition system.
According to one aspect of the present invention there is provided an ignition circuit including a first capacitor, a voltage source connected across said first capacitor, a series connection of switching means, an inductance and a second capacitor connected across said first capacitor, and an ignition output connected to receive the charge on said second capacitor, such that when the switching means is closed, energy stored in said first capacitor is transferred to said second capacitor via said inductance, which acts to increase the voltage applied to the second capacitor and to said output.
The circuit may include a unidirectional current device connected across the first capacitor in a reversed biased sense. The switching means is preferably a solid-state switch such as a thyristor. The second capacitor is preferably connected to one end of the inductance, the ignition output being connected across a series connection of the second capacitor and the inductance, and the energy stored on the first capacitor being supplied to a tapping of the inductance between its ends. The series connection preferably includes a unidirectional current device. The circuit may include a resistor connected in parallel across the second capacitor.
According to another aspect of the present invention there is provided a ignition system including an input circuit including a first capacitor and a voltage source connected across the first capacitor; a plurality of charging circuits connected with the input circuit, wherein each charging circuit includes a series connection of switching means, an inductance and a second capacitor connected across the first capacitor, and an ignition output connected to receive the charge on the second capacitor, such that when the switching means is closed, energy stored in the first capacitor is transferred to the second capacitor via the inductance, which acts to increase the voltage applied to the second capacitor and to the output; and a triggering unit connected with the switching means of each charging circuit.
According to a further aspect of the present invention there is provided a method of producing ignition including the steps of storing electrical energy in a first device, transferring a part of the energy stored in the first device to a second device via means to increase the voltage above a level for discharge and subsequently transferring energy remaining in the first device to the discharge.
According to yet another aspect of the invention there is provided an arrangement for performing a method according to the above further aspect of the invention.
An ignition system and method according to the present invention will now be described, by way of example, with reference to the accompanying drawing, which is a circuit diagram of the system.
The system includes several charging circuits 1 A, 1B and 1 C, only three of which are shown, connected to respective high energy, solid state discharge igniters 2A, 2B and 2C. All the charging circuits 1 A to 1C are connected to a common input circuit 3.
The input circuit 3 includes a current-limited voltage source 30 connected across a parallel arrangement of a diode 31 and a main storage capacitor 32. The cathode of the diode 31 is connected to the positive output of the source 30, so that it is reverse biased. The voltage source 30 is of the kind that will safely withstand momentary short circuits applied to its output. The output terminals 33 and 34 of the input circuit are taken across the capacitor 32.
Each charging circuit 1A to 1C is identical, so only the circuit 1A will be described here. The circuit 1A has switching means 10 in the form of a thyristor or a similar solid state switch connected, at one terminal, to the positive output terminal 33 of the input circuit 3.
The other terminal of the thyristor 10 is connected to the anode of a power diode 11, the cathode of which is connected to a tapping 12' between opposite ends of an inductor 12, such as an air-cored coil or other device with inductance capable of maintaining its inductance while passing a large discharge current. One end terminal of the inductor 12 is connected to one electrode of a second, supplementary capacitor 13; the diode 11, inductor 12 and capacitor 13 together form a series resonant circuit. The second capacitor 13 has a smaller capacity than the first capacitor 32 and has a power resistor 14 connected in parallel with it.
The other electrode of the capacitor 13 is connected to the other input of the charging circuit 1A, which is, in turn connected to the negative terminal 34 of the input circuit 3. The other end terminal of the inductor 12 is connected to one output terminal 15 of the charging circuit; the other output terminal 16 is connected to the other, negative electrode of the capacitor 13.
In this way, the output terminals 15 and 16 of the charging circuit 1 A are taken across a series connection of the capacitor 13 and the inductor 12, these terminals being connected across the igniter 2A.
The gate electrode of the thyristor switch 10 in each charging circuit 1 A to 1C is connected to a triggering unit 40. This triggering unit 40 controls closing of the thyristors in each circuit 1A to 1C, so that the igniters 2A to 2C are fired in the desired sequence.
In operation, the switch 10 is assumed initially to be open and the capacitors 32 and 13 to be discharged. Current flows from the source 30 to charge the main storage capacitor 32. The triggering circuit 40 leaves the switch 10 open for sufficient time to allow the capacitor 32 to charge fully. When the triggering circuit 40 closes the switch 10, the charge on the capacitor 32 is connected to the series resonant circuit of the diode 11, apart of the inductor 12 and capacitor 13. At the instant of closure of the switch 10, the capacitor 13 is discharged and so the full voltage of the capacitor 32 appears across a part of the inductor coil 12. By transformer action, this voltage is instantaneously stepped up at the other end of the winding for application to the igniter 2A. The rate of change of current is controlled and limited by the inductance 12, thereby protecting the thyristor 10 from excessively high peak values. As the current increases, energy is stored in the inductor 12 until the voltage on the supplementary capacitor 13 equals that on the main capacitor 32. When this level is reached, there is no further increase in current through the inductor 12. At this time, the voltage across the inductor 12 has fallen to zero and so the initial high voltage spike on the igniter 2A ends.
The inductor 12 now acts to maintain the established current flow in the way well known in series resonant circuits. The energy stored in its inductance is transferred into the supplementary capacitor 13, further increasing its voltage to a level that can be almost twice that of the main capacitor 32 and to a level that exceeds the firing voltage of the igniter 2A. In this way, the igniter 2A is subjected to an initial very high voltage spike of short duration, followed by a sustained high voltage until discharge occurs. The diode 11 prevents the high voltage produced on the supplementary capacitor 13 discharging back to the main capacitor 32. The diode 11 also limits the reverse voltage seen by the switching device 10, which can be important because some thyristors are asymmetric and cannot withstand reverse voltages.
Because the discharge energy in the present arrangement is derived from a relatively low voltage store, it tends to prolong the discharge giving a greater effect on lighting the fuel. The circuit could include an optional additional diode 21 having its cathode connected between the switching device 10 and the diode 11, and with its anode connected to the output terminal 16.
When the igniter 2A fires and the supplementary capacitor 13 is discharged, a large current flows directly from this capacitor to the igniter. When the voltage on the supplementary capacitor 13 has fallen towards zero, the main discharge current from the main capacitor 32 then flows to the igniter 2A. The rate of change of this current is controlled by the inductor 12 to prevent destructive levels being reached in the thyristor 10. The diode 31 in the input circuit 3 prevents reverse voltages on the main capacitor 32, which could otherwise be caused by stray resonances or the like.
The triggering circuit 40 is arranged to open the switch 10 after a time sufficient for both capacitors 32 and 13 to have discharged, so that the main capacitor 32 can be charged again. In some cases, the igniter 2A may not fire, such as because of contamination or a hostile environment, thereby causing the capacitor 13 to retain its charge after a firing cycle.
The value of the resistor 14 is chosen to be such as to allow any such residual charge on the capacitor 13 to be fully discharged during the time the switch 10 is open before the next firing cycle, so that the full resonant voltage on the supplementary capacitor is repeated for the next firing cycle. In this way, all the energy stored in the main capacitor 32 at the start is available for dissipation at the igniter, although its distribution varies during the cycle. The resistance connected across the capacitor could instead be provided by a positive temperature coefficient thermistor. This would have the advantage that, if the switch 10 should fail in a closed state so that a high voltage was applied for a prolonged period across the supplementary capacitor, the power dissipated in the resistance would reduce as it heated, thereby making it self limiting.
It will be appreciated that different forms of switching device could be used, instead of a thyristor.
The present invention enables the voltage rating of the switching device 10 to be less than that required to produce breakdown at the igniter, and may be as low as approximately half this voltage. The inductor 12 provides a definable and controlled rate of change of current through the switching device 10, thus permitting reliable operation regardless of the type or condition of the igniter.

Claims (14)

1. An ignition circuit including a first capacitor, a voltage source connected across said first capacitor, a series connection of switching means, an inductance and a second capacitor connected across said first capacitor, and an ignition output connected to receive the charge on said second capacitor, such that when the switching means is closed, energy stored in said first capacitor is transferred to said second capacitor via said inductance, which acts to increase the voltage applied to the second capacitor and to said output.
2. An ignition circuit according to Claim 1 including a unidirectional current device connected across said first capacitor in a reversed biased sense.
3. An ignition circuit according to Claim 1 or 2, wherein said switching means is a solid state switch.
4. An ignition circuit according to Claim 3, wherein said switching means is a thyristor.
5. An ignition circuit according to any one of the preceding claims, wherein said second capacitor is connected to one end of said inductance, wherein said ignition output is connected across a series connection of said second capacitor and said inductance, and wherein the energy stored on said first capacitor is supplied to a tapping of said inductance between its ends.
6. An ignition circuit according to any one of the preceding claims, wherein said series connection includes a unidirectional current device.
7. An ignition circuit according to any one of the preceding claims including a resistor connected in parallel across said second capacitor.
8. An ignition circuit substantially as hereinbefore described with reference to the accompanying drawing.
9. An ignition system including an input circuit including a first capacitor and a voltage source connected across said first capacitor; a plurality of charging circuits connected with said input circuit, wherein each said charging circuit includes a series connection of switching means, an inductance and a second capacitor connected across said first capacitor, and an ignition output connected to receive the charge on said second capacitor, such that when the switching means is closed, energy stored in said first capacitor is transferred to said second capacitor via said inductance, which acts to increase the voltage applied to the second capacitor and to said output; and a triggering unit connected with the switching means of each said charging circuit.
10. An ignition system substantially as hereinbefore described with reference to the accompanying drawing.
11. A method of producing ignition including the steps of storing electrical energy in a first device, transferring a part of the energy stored in said first device to a second device via means to increase the voltage above a level for discharge and subsequently transferring energy remaining in the first device to said discharge.
12. A method substantially as hereinbefore described with reference to the accompanying drawing.
13. An arrangement for performing a method according to Claim 11 or 12.
14. Any novel and inventive feature or combination of features as hereinbefore described.
GB9810332A 1997-06-12 1998-05-15 Ignition systems and methods Expired - Fee Related GB2326195B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9810332A GB2326195B (en) 1997-06-12 1998-05-15 Ignition systems and methods

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9712110.7A GB9712110D0 (en) 1997-06-12 1997-06-12 Ignition systems and methods
GB9810332A GB2326195B (en) 1997-06-12 1998-05-15 Ignition systems and methods

Publications (3)

Publication Number Publication Date
GB9810332D0 GB9810332D0 (en) 1998-07-15
GB2326195A true GB2326195A (en) 1998-12-16
GB2326195B GB2326195B (en) 2001-01-10

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ID=26311696

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9810332A Expired - Fee Related GB2326195B (en) 1997-06-12 1998-05-15 Ignition systems and methods

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Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1452122A (en) * 1973-10-10 1976-10-13 British Gas Corp Electrical circuit arrangements for igniting gaseous fuels
EP0371930A1 (en) * 1988-11-23 1990-06-06 MARELLI AUTRONICA S.p.A. A thyristor ignition system for an internal combustion engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1452122A (en) * 1973-10-10 1976-10-13 British Gas Corp Electrical circuit arrangements for igniting gaseous fuels
EP0371930A1 (en) * 1988-11-23 1990-06-06 MARELLI AUTRONICA S.p.A. A thyristor ignition system for an internal combustion engine

Also Published As

Publication number Publication date
GB9810332D0 (en) 1998-07-15
GB2326195B (en) 2001-01-10

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20040515