US3788293A - Low impedance capacitor discharge system and method - Google Patents
Low impedance capacitor discharge system and method Download PDFInfo
- Publication number
- US3788293A US3788293A US00305308A US3788293DA US3788293A US 3788293 A US3788293 A US 3788293A US 00305308 A US00305308 A US 00305308A US 3788293D A US3788293D A US 3788293DA US 3788293 A US3788293 A US 3788293A
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- United States
- Prior art keywords
- capacitor
- ignition device
- discharge
- primary
- supplemental
- Prior art date
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- Expired - Lifetime
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- 239000003990 capacitor Substances 0.000 title claims abstract description 147
- 238000000034 method Methods 0.000 title claims abstract description 31
- 230000000153 supplemental effect Effects 0.000 claims abstract description 48
- 238000004804 winding Methods 0.000 claims abstract description 18
- 238000007599 discharging Methods 0.000 claims description 12
- 238000002485 combustion reaction Methods 0.000 claims description 10
- 230000004907 flux Effects 0.000 claims description 7
- 229930195733 hydrocarbon Natural products 0.000 claims description 5
- 150000002430 hydrocarbons Chemical class 0.000 claims description 5
- 239000000446 fuel Substances 0.000 description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 241001417524 Pomacanthidae Species 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 210000003127 knee Anatomy 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- 230000001360 synchronised effect Effects 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
- ABSTRACT A low impedance capacitor discharge ignition system and method in which a supplemental capacitor is utilized on the secondary winding side of the high voltage transformer to avoid the impedance of the transformer in sustaining the gap ionization potential of the ignition device.
- Capacitor discharge ignition systems in common use generally employ a discharge capacitor which is alternatively connected between a source of direct current and the primary winding of a high voltage transformer having its secondary winding connected to the ignition device.
- the capacitor in such systems may receive direct current from a storage device or from a coil disposed in flux cutting proximity to a magnetic element movable in response to rotation of the engine.
- the switch means customarily employed to alternatively connect the capacitor to the source of direct current and to the primary winding of the high voltage transformer may be of the solid state type, e.g., a silicon controlled rectifier, and operable in response to engine rotation by means of a trigger coil disposed in flux cutting proximity to the same magnetic element as the current source.
- the switch may be breaker points mechanically operable in response to engine rotation in a conventional manner.
- Capacitor discharge ignition systems of the type above described suffer from the disadvantage that the charge in the capacitor is applied to the ignition device through the high voltage transformer. While the impedance of the high voltage transformer is generally quite small upon the initial application of the discharge pulse, the impedance of the high voltage transformer becomes quite large as the passage of current through the windings of the transformer is sustained. The impedance of the high voltage transformer thus significantly reduces the potential applied to the ignition device.
- the increased potential permits the combustion of leaner mixtures and the present invention has been successfully utilized with air/fuel ratios of about 30 to 1.
- This excessive air serves to cool the combustion below the knee in the emission/temperature curve, i.e., about 3,200 F, as a result of which the presence of unburned hydrocarbons is significantly reduced.
- FIG. 1 is a schematic circuit diagram of one embodiment of the present invention.
- FIG. 2 is a graph of the potential applied to the ignition device with respect to time.
- FIG. 3 is a schematic circuit diagram of the second embodiment of the present invention.
- a source of direct current (not shown) may be applied to the input terminals 10 and 12 and the input terminal 10 connected through a diode 14 to one terminal 16 of a single pole, double throw switch schematically illustrated.
- the other terminal 18 of the switch is connected to one end of the primary winding 20 of a high voltage transformer and the other end thereof is connected to the terminal 12.
- the switch arm 22 is operable to connect the primary capacitor 24 across the input terminals 10 and 12.
- the ignition device 30 may be paralleled by a supplemental capacitor 32 connected through diodes 36 and 38 to a terminal 40 intermediate the diode 28 and the ignition device 30.
- the supplemental capacitor 32 may in turn be paralleled by a suitable conventional source of direct current such as a battery 42 and a diode 44.
- the direct current applied to the input terminal 10 may be applied through the diode 14 to the capacitor 24 to charge the capacitor 24.
- the movement of the switch arm 22 to the terminal 18 provides a discharge path for the capacitor 24 through the primary winding 20 of the high voltage transformer.
- the current pulse thus generated in the secondary winding 26 of the high voltage transformer is supplied through the diode 28 to the ignition device 30 and is of sufficient magnitude to ionize the gap thereof.
- the diode 14 may be eliminated by the use of the switch as described or alternatively the capacitor 24 may be directly connected to the terminal 16 and the switch disposed between the illustrated terminal 18 and the primary winding 20 of the high voltage transformer.
- the potential applied to the ignition device by the circuit of FIG. 1 thus operated may take the shape of the waveform illustrated in dashed lines in FIG. 2.
- the waveform includes a brief initial portion having an amplitude approximately one order of magnitude higher than the amplitude of the remainder of the waveform due to the impedance of the high voltage transformer.
- the supplemental capacitor 32 may be charged from the battery 42 through the diode 44. Once charged, the supplemental capacitor 32 may be discharged through the diodes 36 and 38 and the ignition device 30. The charge on the supplemental capacitor 32 may thus be dissipated through the ignition device 30 while avoiding the impedance of the high voltage transformer.
- the discharge of the primary capacitor 24 and the supplemental capacitor 32 be synchronized so that the discharge impulses are supreimposed on the ignition device 30.
- the operation of the switch 22 may be controlled in any suitable conventional manner in timed relationship to engine rotation.
- the simultaneous discharge of the capacitor 32 has been found for the circuit values hereinafter set forth to provide a threefold increase in the amplitude of the ignition device potential as shown in FIG. 2.
- the impedance of the ignition device 30 which acts as an open circuit during the charging of the capacitor 32 from the battery 42.
- the impedance of the spark gap drops sufficiently to provide a discharge path for the capacitor 32 through the diodes 36 and 38.
- the voltage drop across the diodes 36 and 38 is, moreover, sufficient to insure the effective disconnecting of the capacitor 32 from the ignition device 30 once the capacitor 32 has been discharged.
- the diodes 28, 36 and 38 may have a Kv. 2.5 amp rating for use with a 3 XV. 100 watt source 42 and a 1 microfarad capacitor 32.
- the normal 0.321 Kv. ionization sustaining potential applied to the ignition device 30 may be increased to approximately 3 Kv.
- a flywheel 50 is schematically illustrated having a permanent magnet 52 and pole pieces 54 and 56 for rotation in response to engine rotation.
- a current coil 58 may be disposed in flux cutting proximity to the flywheel 50 and may be connected across a primary capacitor 60 by way of a diode 62.
- the diode 62-capacitor 60 interconnection may be connected through a switch 68 to the primary winding 70 of a high voltage transformer to provide a discharge path for the capacitor 60 through the primary winding 70.
- the secondary winding 72 of the high voltage transformer may be connected through a diode 74 across the ignition device.
- the switch 68 may be any suitable conventional switch and may. for example, be a silicon controlled rectifier having a gate electrode connected to a trigger be applied through a full wave rectifier 88 to the supplemental capacitor 64 to effect the charging thereof.
- the ionization of the spark gap of the ignition device 76 provides a discharge path for the capacitor 64 through a diode 80 and the ignition device 30.
- the novel method and system of the present invention significantly increases the ignition device gap ionization sustaining potential by means of a supplemental capacitor and a discharge path therefore excluding the impedance of the high voltage transformer through which the gap ionization potential is initially applied.
- the efficiency of an internal combustion engine may be significantly increased, particularly at low engine speeds, and the emission of unburned hydrocarbons significantly reduced.
- the size of the primary capacitor may be significantly reduced for any predetermined gap ionization sustaining potential.
- a method of sustaining the duration of the gap ionization potential applied to an ignition device in a capacitor ignition system comprising the steps of:
- a low impedance capacitor discharge ignition system comprising:
- first switch means operable to connect said primary capacitor to said first source of direct current to charge said primary capacitor therefrom and to connect said primary capacitor to said high voltage transformer to discharge said primary capacitor through the primary winding thereof;
- an ignition device connected in series with the secondary winding of said transformer to receive a gap ionizing potential upon the discharge of said primary capacitor
- circuit means operable to connect said supplemental capacitor to said second source of direct current to charge said supplemental capacitor therefrom and to connect said supplemental capacitor to said ignition device to discharge said supplemental capacitor through said ignition device in timed relation to the discharge of said primary capacitor.
- first switch means and said circuit means are operable to initiate the discharge of said primary and supplemental capacitors at substantially the same time.
- a method of reducing the emission of hydrocarbons from an internal combustion engine having an ignition device by increasing the power applied to the ignition device comprising the steps of:
- a low impedance capacitor discharge system comprising:
- movable magnetic means a coil disposed in flux cutting proximity to the path in which said magnetic means moves;
- unidirectional current means for connecting said coil to said first and second capacitors
- first switch means operable in synchronism with movement of said magnetic means for connecting said first capacitors to said discharge device through said transformer
- second unidirectional current means for connecting said second capacitor to said discharge device in synchronism with the discharge of said first capacitor.
- said means for applying a gap ionizing potential to said ignition device includes a first capacitor, movable magnetic means, a coil disposed in flux cutting proximity to the path in which said magnetic means moves, and first switch means operable in synchronism with movement of said 7 8 magnetic means for connecting said first capacitor to diode means for connecting said second capacitor said ignition device through said transformer; and, to Said ignition device in synchronism with the wherein said means for applying a gap ionization sustaining potential to said ignition device includes a second capacitor, a source of direct current, and
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- 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)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
Description
Claims (22)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US30530872A | 1972-11-10 | 1972-11-10 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3788293A true US3788293A (en) | 1974-01-29 |
Family
ID=23180271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00305308A Expired - Lifetime US3788293A (en) | 1972-11-10 | 1972-11-10 | Low impedance capacitor discharge system and method |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3788293A (en) |
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3885541A (en) * | 1973-07-23 | 1975-05-27 | Teledyne Ind | Dual ignition coil for internal combustion engine |
| US4029072A (en) * | 1973-08-27 | 1977-06-14 | Toyota Jidosha Kogyo Kabushiki Kaisha | Igniting apparatus for internal combustion engines |
| US4033316A (en) * | 1975-06-03 | 1977-07-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Sustained arc ignition system |
| DE2701070A1 (en) * | 1976-07-26 | 1978-02-02 | Sigma Electronics Planning Kk | IGNITION DEVICE WITH SPARK PLUG |
| US4103659A (en) * | 1974-08-05 | 1978-08-01 | Donigian Donald S | Ignition system |
| US4203403A (en) * | 1973-04-28 | 1980-05-20 | Nippondenso Co., Ltd. | Ignition device for an internal combustion engine |
| US4223656A (en) * | 1978-10-27 | 1980-09-23 | Motorola, Inc. | High energy spark ignition system |
| DE3015611A1 (en) * | 1979-04-24 | 1980-10-30 | Nissan Motor | PLASMA JET IGNITION SYSTEM |
| US4301782A (en) * | 1977-09-21 | 1981-11-24 | Wainwright Basil E | Ignition system |
| US4366801A (en) * | 1980-09-18 | 1983-01-04 | Nissan Motor Company, Limited | Plasma ignition system |
| US4369758A (en) * | 1980-09-18 | 1983-01-25 | Nissan Motor Company, Limited | Plasma ignition system |
| FR2516719A1 (en) * | 1981-11-13 | 1983-05-20 | Mere Malleray Et Cie Snc | High voltage generating circuit for IC engine ignition - has lower voltage sustaining discharge and high voltage to start discharge through generator active between electrode gaps |
| US4418660A (en) * | 1981-04-07 | 1983-12-06 | Nissan Motor Company, Limited | Plasma ignition system using photothyristors for internal combustion engine |
| US4433669A (en) | 1981-06-12 | 1984-02-28 | Nissan Motor Company, Limited | Plasma ignition system for an internal combustion engine |
| US4448181A (en) * | 1981-06-09 | 1984-05-15 | Nissan Motor Company, Limited | Plasma ignition system for an internal combustion engine |
| US4538586A (en) * | 1983-12-21 | 1985-09-03 | Textron, Inc. | Capacitive discharge ignition with long spark duration |
| WO1993004279A1 (en) * | 1991-08-23 | 1993-03-04 | Massachusetts Institute Of Technology | Dual energy ignition system |
| US5630384A (en) * | 1996-01-17 | 1997-05-20 | Unison Industries Limited Partnership | Magneto-based ignition system for reciprocating internal combustion engine having a capacitive discharge booster for aiding engine starting |
| US6484707B1 (en) | 2000-09-29 | 2002-11-26 | Unison Industries, Inc. | Method and apparatus for generating a sustained arc at a sparking device |
| US6771519B2 (en) | 2000-09-29 | 2004-08-03 | Unison Industries, Inc. | Method and apparatus for generating high voltage |
| US20100252007A1 (en) * | 2009-04-01 | 2010-10-07 | James Gonzales | Electrostatic air charging system for an internal combustion engine |
| US20100319644A1 (en) * | 2009-06-18 | 2010-12-23 | Ecoignition | Energy efficient plasma generation |
| EP2908393A3 (en) * | 2005-04-19 | 2015-12-16 | Knite, Inc. | Method and apparatus for operating traveling spark igniter at high pressure |
| US11715935B2 (en) | 2011-07-26 | 2023-08-01 | Knite, Inc. | Traveling spark igniter |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2348298A (en) * | 1942-06-17 | 1944-05-09 | Rotax Ltd | Auxiliary spark ignition apparatus for internal combustion engines |
| US3234430A (en) * | 1962-07-04 | 1966-02-08 | Bosch Robert Gmbh | Ignition circuit for internal combustion engines which prevents ignition skipping |
| US3658044A (en) * | 1970-12-08 | 1972-04-25 | Alden L Safstrom | Capacitor discharge ignition system |
-
1972
- 1972-11-10 US US00305308A patent/US3788293A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2348298A (en) * | 1942-06-17 | 1944-05-09 | Rotax Ltd | Auxiliary spark ignition apparatus for internal combustion engines |
| US3234430A (en) * | 1962-07-04 | 1966-02-08 | Bosch Robert Gmbh | Ignition circuit for internal combustion engines which prevents ignition skipping |
| US3658044A (en) * | 1970-12-08 | 1972-04-25 | Alden L Safstrom | Capacitor discharge ignition system |
Cited By (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4203403A (en) * | 1973-04-28 | 1980-05-20 | Nippondenso Co., Ltd. | Ignition device for an internal combustion engine |
| US3885541A (en) * | 1973-07-23 | 1975-05-27 | Teledyne Ind | Dual ignition coil for internal combustion engine |
| US4029072A (en) * | 1973-08-27 | 1977-06-14 | Toyota Jidosha Kogyo Kabushiki Kaisha | Igniting apparatus for internal combustion engines |
| US4103659A (en) * | 1974-08-05 | 1978-08-01 | Donigian Donald S | Ignition system |
| US4033316A (en) * | 1975-06-03 | 1977-07-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Sustained arc ignition system |
| DE2701070A1 (en) * | 1976-07-26 | 1978-02-02 | Sigma Electronics Planning Kk | IGNITION DEVICE WITH SPARK PLUG |
| US4301782A (en) * | 1977-09-21 | 1981-11-24 | Wainwright Basil E | Ignition system |
| US4223656A (en) * | 1978-10-27 | 1980-09-23 | Motorola, Inc. | High energy spark ignition system |
| DE3015611A1 (en) * | 1979-04-24 | 1980-10-30 | Nissan Motor | PLASMA JET IGNITION SYSTEM |
| US4308488A (en) * | 1979-04-24 | 1981-12-29 | Nissan Motor Co., Ltd. | Plasma jet ignition system |
| US4366801A (en) * | 1980-09-18 | 1983-01-04 | Nissan Motor Company, Limited | Plasma ignition system |
| US4369758A (en) * | 1980-09-18 | 1983-01-25 | Nissan Motor Company, Limited | Plasma ignition system |
| US4418660A (en) * | 1981-04-07 | 1983-12-06 | Nissan Motor Company, Limited | Plasma ignition system using photothyristors for internal combustion engine |
| US4448181A (en) * | 1981-06-09 | 1984-05-15 | Nissan Motor Company, Limited | Plasma ignition system for an internal combustion engine |
| US4433669A (en) | 1981-06-12 | 1984-02-28 | Nissan Motor Company, Limited | Plasma ignition system for an internal combustion engine |
| FR2516719A1 (en) * | 1981-11-13 | 1983-05-20 | Mere Malleray Et Cie Snc | High voltage generating circuit for IC engine ignition - has lower voltage sustaining discharge and high voltage to start discharge through generator active between electrode gaps |
| US4538586A (en) * | 1983-12-21 | 1985-09-03 | Textron, Inc. | Capacitive discharge ignition with long spark duration |
| WO1993004279A1 (en) * | 1991-08-23 | 1993-03-04 | Massachusetts Institute Of Technology | Dual energy ignition system |
| JP3135263B2 (en) | 1991-08-23 | 2001-02-13 | マサチューセッツ インスチテュート オブ テクノロジー | Dual energy ignition system |
| US5630384A (en) * | 1996-01-17 | 1997-05-20 | Unison Industries Limited Partnership | Magneto-based ignition system for reciprocating internal combustion engine having a capacitive discharge booster for aiding engine starting |
| US6771519B2 (en) | 2000-09-29 | 2004-08-03 | Unison Industries, Inc. | Method and apparatus for generating high voltage |
| US6484707B1 (en) | 2000-09-29 | 2002-11-26 | Unison Industries, Inc. | Method and apparatus for generating a sustained arc at a sparking device |
| EP2908393A3 (en) * | 2005-04-19 | 2015-12-16 | Knite, Inc. | Method and apparatus for operating traveling spark igniter at high pressure |
| US11419204B2 (en) | 2005-04-19 | 2022-08-16 | Knite, Inc. | Method and apparatus for operating traveling spark igniter at high pressure |
| US12158132B2 (en) | 2005-04-19 | 2024-12-03 | Knite, Inc. | Method and apparatus for operating traveling spark igniter at high pressure |
| US20100252007A1 (en) * | 2009-04-01 | 2010-10-07 | James Gonzales | Electrostatic air charging system for an internal combustion engine |
| US8640677B2 (en) * | 2009-04-01 | 2014-02-04 | James Gonzales | Electrostatic air charging system for an internal combustion engine |
| US20100319644A1 (en) * | 2009-06-18 | 2010-12-23 | Ecoignition | Energy efficient plasma generation |
| US8555867B2 (en) | 2009-06-18 | 2013-10-15 | Arvind Srinivasan | Energy efficient plasma generation |
| US11715935B2 (en) | 2011-07-26 | 2023-08-01 | Knite, Inc. | Traveling spark igniter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: MCCULLOCH CORPORATION A MD CORP. Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:BLACK & DECKER INC., A DE CORP.;REEL/FRAME:004134/0336 Effective date: 19830505 |
|
| AS | Assignment |
Owner name: CITICORP INDUSTRIAL CREDIT, INC., NEW YORK Free format text: MORTGAGE;ASSIGNORS:MC CULLOCH CORPORATION;MC CULLOCH OVERSEAS N.V.;REEL/FRAME:004158/0190 Effective date: 19830331 Owner name: CITICORP INDUSTRIAL CREDIT, INC., 450 MAMARONECK A Free format text: MORTGAGE;ASSIGNORS:MC CULLOCH CORPORATION;MC CULLOCH OVERSEAS N.V.;REEL/FRAME:004158/0190 Effective date: 19830331 |
|
| AS | Assignment |
Owner name: MCCULLOCH CORPORATION, A CORP. OF MD. Free format text: RELEASED BY SECURED PARTY;ASSIGNOR:CITICORP NORTH AMERICA, INC., FORMERLY KNOWN AS CITICORP INDUSTRIAL CREDIT, INC.;REEL/FRAME:005365/0004 Effective date: 19900530 Owner name: FIRST UNION NATIONAL BANK OF NORTH CAROLINA ONE F Free format text: SECURITY INTEREST;ASSIGNOR:MCCULLOCH CORPORATION;REEL/FRAME:005337/0736 Effective date: 19900530 |