US3440490A - Ignition circuits - Google Patents
Ignition circuits Download PDFInfo
- Publication number
- US3440490A US3440490A US526236A US3440490DA US3440490A US 3440490 A US3440490 A US 3440490A US 526236 A US526236 A US 526236A US 3440490D A US3440490D A US 3440490DA US 3440490 A US3440490 A US 3440490A
- Authority
- US
- United States
- Prior art keywords
- gap
- spark
- capacitor
- control
- 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
Links
- 239000003990 capacitor Substances 0.000 description 30
- 238000004804 winding Methods 0.000 description 7
- 230000015556 catabolic process Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 2
- YXIWHUQXZSMYRE-UHFFFAOYSA-N 1,3-benzothiazole-2-thiol Chemical compound C1=CC=C2SC(S)=NC2=C1 YXIWHUQXZSMYRE-UHFFFAOYSA-N 0.000 description 1
- 241001598984 Bromius obscurus Species 0.000 description 1
- 241000220317 Rosa Species 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P9/00—Electric spark ignition control, not otherwise provided for
- F02P9/002—Control of spark intensity, intensifying, lengthening, suppression
- F02P9/007—Control of spark intensity, intensifying, lengthening, suppression by supplementary electrical discharge in the pre-ionised electrode interspace of the sparking plug, e.g. plasma jet ignition
Definitions
- IGNITION CIRCUITS Filed Feb. 9. 1966 if f United States Patent US. Cl. 31527 4 Claims ABSTRACT OF THE DISCLOSURE
- a source of power is used to provide pulses of current at the secondary of a transformer, these pulses of current charging a capacitor through a diode and a spark gap so that low energy sparks are produced at the spark gap each time the capacitor is charged.
- the increase in charge on the capacitor serves eventually to break down a control gap, which in turn breaks down another control gap of higher break down voltage to provide a discharge path for the capacitor through the spark gap, so producing a spark of higher energy.
- This invention relates to spark ignition circuits, and essentially resides in a spark ignition circuit in which sparks are produced at a spark gap, and at predetermined intervals the spark produced at the spark gap is of higher energy than the remaining sparks.
- FIGURES l and 2 are circuit diagrams illustrating two examples of the invention
- FIGURES 3 and 4 illustrate two possible forms of control gap for use in FIGURE 2
- FIGURE 5 is a circuit diagram illustrating another example.
- an ignition transformer 11 having a primary winding 12 in which alternating current is produced, either by connecting the primary winding to an AC. source 13 as shown, or by connecting the primary winding to a DC. source through a mechanical or electrical interrupting circuit.
- the secondary winding 14 of the transformer is bridged by the anode and cathode of a diode 15 in series with a control gap 16, the control gap being bridged by a capacitor 17 and a spark gap 18 in series.
- the spark gap in this example preferably has a low breakdown voltage, and could be a semi-conductor plug or a multi-gap plug.
- pulses of current pass through the diode 15 and charge the capacitor 17 through the spark gap 18. After a predetermined number of pulses, however, the voltage across the capacitor 17 reaches the breakdown voltage of the control gap 16, which conducts to cause the capacitor to discharge through the spark gap 18 and produce a spark of higher energy. The cycle is then repeated.
- the circuit shown in FIGURE 2 is modified so that the secondary winding is bridged by the anode and cathode of the diode 15 in series with the capacitor 17 and spark gap 18, the spark gap being bridged by parallel circuits one of which contains a resistor 19, and the other of which contains a resistor 21 in series with a first control gap having electrodes 22, 23.
- a point intermediate the resistor 21 and electrode 22 is connected to the cathode of the diode 15 through a second control gap having electrodes 24, 25 and preferably the two control signors to Rotax Limited, London, England, a British gaps are contained in the same envelope as shown.
- the capacitor 17 charges as in FIGURE 1, producing low energy sparks at the spark gap 18, and when the voltage across the capacitor 17 reaches a predetermined value, the control gap 24, 25 breaks down, the resulting ionisation immediately causing the control gap 22, 23 which has a higher breakdown voltage, to break down rapidly.
- the capacitor 17 now discharges through the control gaps and the spark gap in series, the second resistor preventing the capacitor from being short-circuited through the control gap 24, 25.
- the circuit shown in FIGURE 2 can' be used where the spark gap 18 has a high breakdown voltage, for example, where an ordinary air-gap plug is used.
- the operation is substantially the same, although it is of course necessary to adjust the circuit values.
- a gas filled container 27 may as shown in FIGURE 4 be provided with one electrode 22, 24 which is common to both gaps, and a further pair of electrodes 23, 25 which are spaced from the common electrode by dilferent distances.
- FIGURE 5 there are provided a pair of capacitors 31, 32 which are connected in series with diodes 33, 34 respectively across the secondary windings 35, 36 of a pair of transformers 37, 38 the primary windings 39, 40 of which may be connected to a common supply or to separate A.C. sources 41, 42 or interrupted D.C. sources.
- the capacitor 31 is bridged by a control gap 43 in series with a spark gap 44, whilst the capacitor 32 is bridged by a control gap 45 and an inductor 46 in series with the gap 44.
- the capacitors 31, 32 are charged at the same rate, but the gap 43 has a lower breakdown voltage than the gap 45.
- the inductor 46 is not essential, but is preferably included to prevent one capacitor from discharging into the other capacitor when both control gaps are conducting.
- Switch means may be incorporated to ensure that after the spark of higher energy has been produced, no sparks of lower energy are produced for a predetermined period of time. Whereafter a plurality of low energy sparks are produced, followed by another high energy spark and a further delay and so forth.
- the capacitors 31, 32 could be charged from the same source, and the spark gap 44 can be an ordinary spark gap, or a multi-gap plug.
- a variation of this example is a common spark gap which may be of the type containing one common electrode which is earthed, one main electrode for connection to the control gap 45 through the inductor 46, and one auxiliary electrode for connection to the control gap 43.
- a spark ignition circuit in which sparks are produced at a spark gap and at predetermined intervals the spark produced at the spark gap is of higher energy than the remaining sparks, said spark ignition circuit comprising in combination a pair of terminals, means for supplying pulses of current to said pair of terminals at predetermined intervals, a circuit connected across said pair of terminals and including in series a diode, a capacitor and said spark gap, each pulse of current applied to said terminals charging said capacitor through said diode and said spark gap and producing a low energy spark at said spark gap, first and second control gaps each having a first plate and a second plate, a resistor and second control gaps to one side of said capacitor, a connection between the second plate of the first gap and the other side of said capacitor, and a connection between the second plate of the second control gap and the side of said spark gap remote from said capacitor, said second control gap having a higher breakdown voltage than said first control gap, and said first control gap breaking down when the voltage across said capacitor reaches a predetermined value, and serving when it breaks down to
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Generation Of Surge Voltage And Current (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB572965 | 1965-02-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3440490A true US3440490A (en) | 1969-04-22 |
Family
ID=9801540
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US526236A Expired - Lifetime US3440490A (en) | 1965-02-10 | 1966-02-09 | Ignition circuits |
Country Status (2)
Country | Link |
---|---|
US (1) | US3440490A (enrdf_load_stackoverflow) |
SE (1) | SE338693B (enrdf_load_stackoverflow) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3673423A (en) * | 1969-10-17 | 1972-06-27 | Neutra Cuatro Sa | Electronic high frequency pulse generator |
FR2344725A1 (fr) * | 1976-03-19 | 1977-10-14 | Bosch Gmbh Robert | Procede et dispositif pour produire des etincelles d'allumage |
US4317068A (en) * | 1979-10-01 | 1982-02-23 | Combustion Electromagnetics, Inc. | Plasma jet ignition system |
US4384239A (en) * | 1982-01-04 | 1983-05-17 | Micron Industries Corporation | Electrical circuit for gaseous discharge lamp |
US20080206258A1 (en) * | 2005-05-25 | 2008-08-28 | Klaus Pekari | Novel Tetrahydropyridothiophenes |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB929070A (enrdf_load_stackoverflow) * | ||||
US2175900A (en) * | 1939-10-10 | knight | ||
US2476773A (en) * | 1945-05-08 | 1949-07-19 | W Dan Bergman Ab | Discharge lamp with light flashes |
US2834917A (en) * | 1956-01-31 | 1958-05-13 | Air Liquide | Device for starting and stabilizing a welding arc |
US2889480A (en) * | 1953-07-30 | 1959-06-02 | Air Liquide | Device for assisting the ignition of a welding arc and stabilizing the same |
US2938147A (en) * | 1959-02-17 | 1960-05-24 | John J Rose | Continuous ignition system for a turbojet engine |
US3030548A (en) * | 1960-03-07 | 1962-04-17 | Gen Motors Corp | Ignition circuit |
US3052817A (en) * | 1958-03-19 | 1962-09-04 | Republic Aviat Corp | Method of and means for energizing spark-machining apparatus |
US3213258A (en) * | 1962-05-15 | 1965-10-19 | Gen Motors Corp | Electrical stock removal method and apparatus |
US3267329A (en) * | 1963-04-03 | 1966-08-16 | Bendix Corp | Electrical ignition apparatus using a high voltage breakdown and a condenser followup through the ignition gap |
US3376470A (en) * | 1965-08-12 | 1968-04-02 | Atomic Energy Commission Usa | Capacitor discharge circuit for starting and sustaining a welding arc |
-
1966
- 1966-02-07 SE SE01497/66A patent/SE338693B/xx unknown
- 1966-02-09 US US526236A patent/US3440490A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB929070A (enrdf_load_stackoverflow) * | ||||
US2175900A (en) * | 1939-10-10 | knight | ||
US2476773A (en) * | 1945-05-08 | 1949-07-19 | W Dan Bergman Ab | Discharge lamp with light flashes |
US2889480A (en) * | 1953-07-30 | 1959-06-02 | Air Liquide | Device for assisting the ignition of a welding arc and stabilizing the same |
US2834917A (en) * | 1956-01-31 | 1958-05-13 | Air Liquide | Device for starting and stabilizing a welding arc |
US3052817A (en) * | 1958-03-19 | 1962-09-04 | Republic Aviat Corp | Method of and means for energizing spark-machining apparatus |
US2938147A (en) * | 1959-02-17 | 1960-05-24 | John J Rose | Continuous ignition system for a turbojet engine |
US3030548A (en) * | 1960-03-07 | 1962-04-17 | Gen Motors Corp | Ignition circuit |
US3213258A (en) * | 1962-05-15 | 1965-10-19 | Gen Motors Corp | Electrical stock removal method and apparatus |
US3267329A (en) * | 1963-04-03 | 1966-08-16 | Bendix Corp | Electrical ignition apparatus using a high voltage breakdown and a condenser followup through the ignition gap |
US3376470A (en) * | 1965-08-12 | 1968-04-02 | Atomic Energy Commission Usa | Capacitor discharge circuit for starting and sustaining a welding arc |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3673423A (en) * | 1969-10-17 | 1972-06-27 | Neutra Cuatro Sa | Electronic high frequency pulse generator |
FR2344725A1 (fr) * | 1976-03-19 | 1977-10-14 | Bosch Gmbh Robert | Procede et dispositif pour produire des etincelles d'allumage |
US4317068A (en) * | 1979-10-01 | 1982-02-23 | Combustion Electromagnetics, Inc. | Plasma jet ignition system |
US4384239A (en) * | 1982-01-04 | 1983-05-17 | Micron Industries Corporation | Electrical circuit for gaseous discharge lamp |
US20080206258A1 (en) * | 2005-05-25 | 2008-08-28 | Klaus Pekari | Novel Tetrahydropyridothiophenes |
Also Published As
Publication number | Publication date |
---|---|
SE338693B (enrdf_load_stackoverflow) | 1971-09-13 |
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