US2467725A - Ignition system - Google Patents

Ignition system Download PDF

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US2467725A
US2467725A US770970A US77097047A US2467725A US 2467725 A US2467725 A US 2467725A US 770970 A US770970 A US 770970A US 77097047 A US77097047 A US 77097047A US 2467725 A US2467725 A US 2467725A
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Prior art keywords
transformer
condenser
distributor
spark
spark plug
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US770970A
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William E Berkey
Mertens Ernest K Von
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CBS Corp
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Westinghouse Electric Corp
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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
    • F02P13/00Sparking plugs structurally combined with other parts of internal-combustion engines
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01TSPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T13/00Sparking plugs
    • H01T13/40Sparking plugs structurally combined with other devices
    • H01T13/44Sparking plugs structurally combined with other devices with transformers, e.g. for high-frequency ignition
    • 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
    • F02P7/00Arrangements of distributors, circuit-makers or -breakers, e.g. of distributor and circuit-breaker combinations or pick-up devices
    • F02P7/02Arrangements of distributors, circuit-makers or -breakers, e.g. of distributor and circuit-breaker combinations or pick-up devices of distributors

Definitions

  • Our invention relates, generally, to ignition systems for internal combustion engines and, more particularly, to ignition systems for aircraft engines.
  • An object of our invention is to overcome the foregoing disadvantages of present aircraft ignition systems.
  • a more specific object of our invention is to so increase the reliability of an ignition system that it may be utilized with aircraft engines for higher altitude flying.
  • Another object of our invention is to simplify the timing of the system to the engine.
  • a further object of our invention is to prevent production of excess energy in the ignition system at high speeds.
  • Still another object of our invention is to provide a high frequency spark plug suitable for use in our improved ignition system.
  • current from either a low voltage generator or a battery charges a large capacitor until the distributor arm makes contact with one of the spark plug leads.
  • the capacitor then discharges through the distributor and the primary winding of a transformer coil located in the spark plug.
  • the current in the secondary winding of this coil charges a second capacitor located in the plug until the voltage reached is sufficient to break down a sealed gap built into the plug.
  • the discharge current from the second capacitor flows through the primary winding of a second transformer coil, also located in the plug, and the secondary winding of this coil develops sufiicient voltage to break down the ignition gap of the plug in the cylinder and fire the engine.
  • FIG. 1 is a diagrammatic view of an ignition system "embodying the principal features of our invention
  • Fig. 2 is an enlarged view, in vertical section, of a spark plug suitable for use in the system shown in Fig. 1, and
  • Fig. 3 is a view, in bottom plan, of the plug shown in Fig. 2.
  • the system shown therein comprises a direct-current generator iii, a battery H, a selector switch 12, a resistor it, a capacitor M, a distributor I5 and a spark plug it.
  • the generator I0 is of a relatively low voltage, for example, 24 volts, and is preferably of a type which will generate a substantially constant voltage over a relatively wide range of speed.
  • the generator may be driven by an aircraft engine (not shown).
  • the battery ll may be of the type usually utilized on airplanes for supplying direct-current energy.
  • the switch 62 may be utilized to connect the ignition system to either the battery H or the generator Hi.
  • the battery may be utilized as the source of energy for the ignition system during starting when the engine is operating at a low speed.
  • the battery also may be utilized to supply energy for the ignition system in case the generator Ill breaks down.
  • the current from either the generator I or the battery H charges the capacitor i4 through the resistor l3 and keeps the capacitor l4 charged until the arm of the distributor it makes contact with one of the spark plug conductors.
  • the capacitor i4 discharges through the distributor and a primary winding ll of a transformer coil i8 which is disposed within the spark plug I6.
  • the flow of current through the primary winding H induces a voltage in a secondary winding [9. This charges a second capacitor H with a voltage sufiicient to break down a sealed spark gap 22 which is disposed within the plug It.
  • flows through a primary winding 23 of a second transformer coil 24.
  • the flow of current through the primary winding 23 induces a voltage in a secondary winding 25.
  • the potential of the secondary winding 25 becomes sufi'icient to break down the ignition gap between a central electrode 26 and outer electrodes 27 of the spark plug, the engine is fired.
  • Each contact member of the distributor may be connected to a plug it, similar to the one illustrated.
  • the cylinders of the engine may be tired consecutively.
  • the spark plug it utilized in connection with the present system is of a special construction. It contains the two transformer coils l8 and 24, the capacitor 25 and the sealed spark gap 22.
  • the plug It comprises a metal casing which is preferably divided into three sections 3!, 32 and 33. As shown, the lower end of the section 3
  • the conductor 39 is connected to a terminal M, which, in turn, is connected to one terminal of the primary winding I? of the transformer coil 18.
  • the other terminal of the primary winding i1 and one terminal of the secondary winding 19 are connected to the casing 32 by conductors 42.
  • the other terminal of the secondary winding I8 is connected to part of the plates of the capacitor 2
  • the capacitor and the spark gap 22 are disposed within the transformer l8.
  • the other plates of the capacitor 2i are connected to the casing 32 and hence to ground through the engine frame.
  • the other terminal of the spark gap 22 is connected to one terminal of the primary winding 23 by a conductor M.
  • the other terminal of the primary winding 23 and one terminal of the secondary winding 25 are connected. to the casing 32 by a conductor 45.
  • the other terminal of the secondary winding 25 is connected to the central electrode 26 by a conductor 18.
  • the transformer coil 2 is disposed within an insulating sleeve A l which, in turn, is disposed inside of the section 32 of the casing.
  • An insulating cap 4-8 is disposed between the transformer coil 24 and the enclosed spark gap 2'2.
  • the electrode 26 is substantially embedded in an insulating member 49.
  • the insulating members 4'! and 49 may be composed of porcelain or other suitable ceramic material.
  • the windings of the transformer coils and the plates of the capacitor may be insulated from each other by any suitable insulating material. Furthermore, certain of the electrical connections between the various members of the spark plug may be made by brushes, thereby facilitating the assembly of the parts of the plug.
  • and the spark gap 22 may be removed from the plug for inspection, and, if necessary, they may be replaced by new parts.
  • the firing characteristics of fouled spark plugs are also improved because of the steep discharge wave form produced in the system. Also, the timing of the system to the engine is greatly simplified over present systems, and utilizing the standard battery of an airplane eliminates any additional booster or vibrator circuit which is, at present, required for starting.
  • an ignition system for an internal combustion engine in combination, a source of direct current, a condenser charged by said source, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
  • an ignition system for an internal combustion engine in combination, a source of direct current, a resistor, a condenser charged by said source through said resistor, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
  • a direct current generator for an internal combustion engine, in combination, a direct current generator, a battery, a condenser, a switch for selectively connecting the condenser to either the battery or the generator to charge the condenser, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
  • a direct current generator for an internal combustion engine, in combination, a direct current generator, a battery, a resistor, a condenser, a switch for selectively connecting the condenser across either the battery or the generator to charge the condenser through the resistor, a transformer, a distributor for discharging said condenser through said transformer; a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
  • a direct current generator for an internal combustion engine, in combination, a direct current generator, a battery, a. resistor, a condenser, a switch for selectively connecting the condenser across either the battery or the generator to charge the condenser through the resistor, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer, both of said transformers, said spark gap and one of said condensers being disposed with said spark pl 6.
  • an ignition system for an internal combustion engine in combination, a source of direct current, a condenser charged by said source, a transformer having a primary winding and a secondary winding, a distributor for discharging said condenser through said primary winding, a second condenser charged by said secondary winding, a second transformer having a primary winding and a secondary winding, a spark gap for discharging said second condenser through the primary winding of said second transformer, and a spark plug having an electrode connected to the secondary winding of the second transformer.
  • a source of direct current a condenser charged by said source
  • a transformer having a primary winding and a secondary winding
  • a distributor for discharging said condenser through said primary winding
  • a second condenser charged by said secondary winding a second transformer having a primary winding and a secondary winding
  • a spark gap for discharging said second condenser through the primary winding of said second transformer
  • a spark plug having an electrode connected to the secondary winding of the second transformer, both of said transformers, said spark gap and said second condenser being disposed within said spark plug.
  • a spark plug having a casing and an electrode insulated from the casing, a condenser, a spark gap, and two transformers all disposed within the casing, said condenser being charged by one of said transformers and discharged by said spark gap through the other transformer, said electrode being connected to said other transformer.
  • a spark plug having a casing and an electrode insulated from the casing, a condenser, a spark gap, and two transformers all disposed within the casing, each one of said transformers having a primary winding and a secondary winding, said condenser being charged by the secondary winding of one transformer and discharged by said spark gap through the primary winding of the other transformer, said electrode being connected to the secondary winding of said other transformer.
  • a spark plug having a casing and an electrode insulated from the casing, a condenser, a spark gap, and two transformers all disposed within the casing, one of said transformers surrounding said condenser and said spark gap, said condenser being charged by said one transformer and discharged by said spark gap through the other transformer, said electrode being connected to said other transformer.

Description

April 19,- l949. w. E. BERKEY ET AL IGNITION SYSTEM Filed Aug. 28, 1947 1 INVENTORS h/i/l/ am EBerAe y and 57/? e s f- K Van Mgr/ens.
Patented Apr. 19, 1949 UNITED STATES PATENT OFFICE IGNITION SYSTEM William E. Berkey, River Forest, 111., and Ernest K. Von Mertens, West Hartford, Conn., assignors to Westinghouse Electric Corporation, East Pittsburgh, Pa., a corporation of Pennsylvania Claims. 1
Our invention relates, generally, to ignition systems for internal combustion engines and, more particularly, to ignition systems for aircraft engines.
The reliability and performance of present aircraft magnetos and ignition distribution systems do not equal that of aircraft engines now in production or under development. This is true particularly with regard to performance at high altitudes, life of the system between overhauls, susceptibility to contamination and moisture, and to spark plug performance.
An object of our invention, generally stated, is to overcome the foregoing disadvantages of present aircraft ignition systems.
A more specific object of our invention is to so increase the reliability of an ignition system that it may be utilized with aircraft engines for higher altitude flying.
Another object of our invention is to simplify the timing of the system to the engine.
A further object of our invention is to prevent production of excess energy in the ignition system at high speeds.
Still another object of our invention is to provide a high frequency spark plug suitable for use in our improved ignition system.
Other objects of our invention will be explained fully hereinafter or will be apparent to those skilled in the art.
In accordance with one embodiment of our invention, current from either a low voltage generator or a battery charges a large capacitor until the distributor arm makes contact with one of the spark plug leads. The capacitor then discharges through the distributor and the primary winding of a transformer coil located in the spark plug. The current in the secondary winding of this coil charges a second capacitor located in the plug until the voltage reached is sufficient to break down a sealed gap built into the plug. The discharge current from the second capacitor flows through the primary winding of a second transformer coil, also located in the plug, and the secondary winding of this coil develops sufiicient voltage to break down the ignition gap of the plug in the cylinder and fire the engine.
For a better understanding of the nature and objects of our invention, reference may be had to the following detailed description, taken in conjunction with the accompanying drawing, in which:
Figure 1 is a diagrammatic view of an ignition system "embodying the principal features of our invention;
Fig. 2 is an enlarged view, in vertical section, of a spark plug suitable for use in the system shown in Fig. 1, and
Fig. 3 is a view, in bottom plan, of the plug shown in Fig. 2.
Referring to Fig. 1 of the drawing, the system shown therein comprises a direct-current generator iii, a battery H, a selector switch 12, a resistor it, a capacitor M, a distributor I5 and a spark plug it. The generator I0 is of a relatively low voltage, for example, 24 volts, and is preferably of a type which will generate a substantially constant voltage over a relatively wide range of speed. The generator may be driven by an aircraft engine (not shown). The battery ll may be of the type usually utilized on airplanes for supplying direct-current energy.
As shown, the switch 62 may be utilized to connect the ignition system to either the battery H or the generator Hi. Thus, the battery may be utilized as the source of energy for the ignition system during starting when the engine is operating at a low speed. The battery also may be utilized to supply energy for the ignition system in case the generator Ill breaks down.
The current from either the generator I or the battery H charges the capacitor i4 through the resistor l3 and keeps the capacitor l4 charged until the arm of the distributor it makes contact with one of the spark plug conductors. When the distributor arm engages a contact member connected to a spark plug conductor, the capacitor i4 discharges through the distributor and a primary winding ll of a transformer coil i8 which is disposed within the spark plug I6. The flow of current through the primary winding H induces a voltage in a secondary winding [9. This charges a second capacitor H with a voltage sufiicient to break down a sealed spark gap 22 which is disposed within the plug It. The discharge current from the second capacitor 2| flows through a primary winding 23 of a second transformer coil 24. The flow of current through the primary winding 23 induces a voltage in a secondary winding 25. When the potential of the secondary winding 25 becomes sufi'icient to break down the ignition gap between a central electrode 26 and outer electrodes 27 of the spark plug, the engine is fired.
Each contact member of the distributor may be connected to a plug it, similar to the one illustrated. Thus, the cylinders of the engine may be tired consecutively. By selecting favorable circuit components, it is possible to make and break the circuits through the distributor at a small current and low voltage without objectionable arcing at the distributor.
Since the voltage at the distributor is relatively low, for example, 24 volts, no complicated insulation problems arise. All timing and compensating may be done at the distributor by properly spacing the contact members engaged by the distributor arm. Thus, the advancement or retarding of the spark may be done at the distributor.
As illustrated in Fig. 2, the spark plug it utilized in connection with the present system is of a special construction. It contains the two transformer coils l8 and 24, the capacitor 25 and the sealed spark gap 22.
The plug It comprises a metal casing which is preferably divided into three sections 3!, 32 and 33. As shown, the lower end of the section 3| is provided with a threaded portion 3 for insertion into the engine cylinder in the usual manner. The lower end of the section 32 is threaded into the upper end of the section 3i by means of threads 35. The lower end of the section 33 is threaded onto the upper end of the section by means of threads 36. A flanged metal sleeve 37 is threaded onto the upper end of the section 33 to retain a metal sheath 38 which encloses a conductor 39. The conductor 39 may be connected to one of the contact members on the distributor i5.
As shown, the conductor 39 is connected to a terminal M, which, in turn, is connected to one terminal of the primary winding I? of the transformer coil 18. The other terminal of the primary winding i1 and one terminal of the secondary winding 19 are connected to the casing 32 by conductors 42. The other terminal of the secondary winding I8 is connected to part of the plates of the capacitor 2| and to one terminal of the spark gap 22 by a conductor 43. The capacitor and the spark gap 22 are disposed within the transformer l8. The other plates of the capacitor 2i are connected to the casing 32 and hence to ground through the engine frame.
As shown, the other terminal of the spark gap 22 is connected to one terminal of the primary winding 23 by a conductor M. The other terminal of the primary winding 23 and one terminal of the secondary winding 25 are connected. to the casing 32 by a conductor 45. The other terminal of the secondary winding 25 is connected to the central electrode 26 by a conductor 18.
The transformer coil 2 is disposed within an insulating sleeve A l which, in turn, is disposed inside of the section 32 of the casing. An insulating cap 4-8 is disposed between the transformer coil 24 and the enclosed spark gap 2'2. The electrode 26 is substantially embedded in an insulating member 49. The insulating members 4'! and 49 may be composed of porcelain or other suitable ceramic material.
The windings of the transformer coils and the plates of the capacitor may be insulated from each other by any suitable insulating material. Furthermore, certain of the electrical connections between the various members of the spark plug may be made by brushes, thereby facilitating the assembly of the parts of the plug. The capacitor 2| and the spark gap 22 may be removed from the plug for inspection, and, if necessary, they may be replaced by new parts.
From the foregoing description, it is apparent that we have provided an ignition system which has numerous advantages over previously known systems. Thus, the pres'entsystem will function properly at very high altitudes, since the transformer coils are built into the spark plug. The life of the system has been greatly increased, since the energy source consists of a low tension directcurrent generator with a battery as an auxiliary source. Because of the low distribution voltage, all causes of disintegration of the insulating materials have been eliminated.
Furthermore, failures due to moisture and contamination have been eliminated because of the low voltage used for distribution. The life of the spark plug electrodes is improved by unipolarlty sparks, by the absence of large capacitance in the distribution system and by the reduction of excess energy at high speeds.
The firing characteristics of fouled spark plugs are also improved because of the steep discharge wave form produced in the system. Also, the timing of the system to the engine is greatly simplified over present systems, and utilizing the standard battery of an airplane eliminates any additional booster or vibrator circuit which is, at present, required for starting.
Since numerous changes may be made in the above-described construction and different embodiments of the invention may be made without departing from the spirit and scope thereof, it is intended that all matter contained in the foregoing description or shown in the accompanying drawing shall be interpreted as illustrative and not in a limiting sense.
We claim as our invention:
1. In an ignition system for an internal combustion engine, in combination, a source of direct current, a condenser charged by said source, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
2. In an ignition system for an internal combustion engine, in combination, a source of direct current, a resistor, a condenser charged by said source through said resistor, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
3. In an ignition system for an internal combustion engine, in combination, a direct current generator, a battery, a condenser, a switch for selectively connecting the condenser to either the battery or the generator to charge the condenser, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
4. In an ignition system for an internal combustion engine, in combination, a direct current generator, a battery, a resistor, a condenser, a switch for selectively connecting the condenser across either the battery or the generator to charge the condenser through the resistor, a transformer, a distributor for discharging said condenser through said transformer; a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer.
5. In an ignition system for an internal combustion engine, in combination, a direct current generator, a battery, a. resistor, a condenser, a switch for selectively connecting the condenser across either the battery or the generator to charge the condenser through the resistor, a transformer, a distributor for discharging said condenser through said transformer, a second condenser charged by said transformer, a second transformer, a spark gap for discharging said second condenser through said second transformer, and a spark plug having an electrode connected to the second transformer, both of said transformers, said spark gap and one of said condensers being disposed with said spark pl 6. In an ignition system for an internal combustion engine, in combination, a source of direct current, a condenser charged by said source, a transformer having a primary winding and a secondary winding, a distributor for discharging said condenser through said primary winding, a second condenser charged by said secondary winding, a second transformer having a primary winding and a secondary winding, a spark gap for discharging said second condenser through the primary winding of said second transformer, and a spark plug having an electrode connected to the secondary winding of the second transformer.
7. In an ignition system for an internal combustion engine, in combination, a source of direct current, a condenser charged by said source, a transformer having a primary winding and a secondary winding, a distributor for discharging said condenser through said primary winding, a second condenser charged by said secondary winding, a second transformer having a primary winding and a secondary winding, a spark gap for discharging said second condenser through the primary winding of said second transformer, and a spark plug having an electrode connected to the secondary winding of the second transformer, both of said transformers, said spark gap and said second condenser being disposed within said spark plug.
8. A spark plug having a casing and an electrode insulated from the casing, a condenser, a spark gap, and two transformers all disposed within the casing, said condenser being charged by one of said transformers and discharged by said spark gap through the other transformer, said electrode being connected to said other transformer.
9. A spark plug having a casing and an electrode insulated from the casing, a condenser, a spark gap, and two transformers all disposed within the casing, each one of said transformers having a primary winding and a secondary winding, said condenser being charged by the secondary winding of one transformer and discharged by said spark gap through the primary winding of the other transformer, said electrode being connected to the secondary winding of said other transformer.
10. A spark plug having a casing and an electrode insulated from the casing, a condenser, a spark gap, and two transformers all disposed within the casing, one of said transformers surrounding said condenser and said spark gap, said condenser being charged by said one transformer and discharged by said spark gap through the other transformer, said electrode being connected to said other transformer.
WILLIAM E. BERKEY. ERNEST K. VON MERTENS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,370,077 Whisler Mar. 1, 1921 2, 93,848 Randolph Sept. 21, 1937 2,378,705 Harmon June 19, 1945 2,378,893 Berkey June 26, 1945
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2876270A (en) * 1959-03-03 Electronic radio frequency ignition
US3248604A (en) * 1962-01-09 1966-04-26 James R Richards Fuel ignition system preventing radio frequency interference
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
US3939814A (en) * 1975-01-10 1976-02-24 Energy Innovations Device for prolonging ignition spark
FR2591819A1 (en) * 1985-12-18 1987-06-19 Beru Werk Ruprecht Gmbh Co A PITCH OF SPARK PLUG
FR2599431A1 (en) * 1986-06-03 1987-12-04 Renault Sport ELECTROMAGNETIC COIL AND IGNITION DEVICE FOR INTERNAL COMBUSTION ENGINE COMPRISING SUCH A COIL.
US4770152A (en) * 1986-11-07 1988-09-13 Toyota Jidosha Kabushiki Kaisha Ignition device for an internal combustion engine
EP0344387A1 (en) * 1988-05-31 1989-12-06 Société à Responsabilité Limitée L'ELECTRICFIL INDUSTRIE Ignition unit comprising a combined spark plug and transformer for a cylinder of a thermal engine with spark ignition
US5642721A (en) * 1992-01-06 1997-07-01 Ikeya; Kaname Double ignition system for internal combustion engines, ignition plug for double ignition systems, and electric spark generator
EP1351355A3 (en) * 2002-04-01 2006-06-07 Denso Corporation Ignition device for an internal combustion engine and a manufacturing method therefor

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1370077A (en) * 1919-05-31 1921-03-01 Essex Motors Distributer unit for ignition systems
US2093848A (en) * 1933-05-22 1937-09-21 Donald W Randolph Method and apparatus for producing ignition
US2378705A (en) * 1943-01-22 1945-06-19 Wico Electric Co Ignition system and magneto therefor
US2378893A (en) * 1942-03-10 1945-06-26 Westinghouse Electric Corp Ignition system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1370077A (en) * 1919-05-31 1921-03-01 Essex Motors Distributer unit for ignition systems
US2093848A (en) * 1933-05-22 1937-09-21 Donald W Randolph Method and apparatus for producing ignition
US2378893A (en) * 1942-03-10 1945-06-26 Westinghouse Electric Corp Ignition system
US2378705A (en) * 1943-01-22 1945-06-19 Wico Electric Co Ignition system and magneto therefor

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2876270A (en) * 1959-03-03 Electronic radio frequency ignition
US3248604A (en) * 1962-01-09 1966-04-26 James R Richards Fuel ignition system preventing radio frequency interference
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
US3939814A (en) * 1975-01-10 1976-02-24 Energy Innovations Device for prolonging ignition spark
FR2591819A1 (en) * 1985-12-18 1987-06-19 Beru Werk Ruprecht Gmbh Co A PITCH OF SPARK PLUG
FR2599431A1 (en) * 1986-06-03 1987-12-04 Renault Sport ELECTROMAGNETIC COIL AND IGNITION DEVICE FOR INTERNAL COMBUSTION ENGINE COMPRISING SUCH A COIL.
EP0248717A1 (en) * 1986-06-03 1987-12-09 Renault Sport Electromagnetic bobbin and ignition device for an internal-combustion engine comprising such a bobbin
US4770152A (en) * 1986-11-07 1988-09-13 Toyota Jidosha Kabushiki Kaisha Ignition device for an internal combustion engine
EP0344387A1 (en) * 1988-05-31 1989-12-06 Société à Responsabilité Limitée L'ELECTRICFIL INDUSTRIE Ignition unit comprising a combined spark plug and transformer for a cylinder of a thermal engine with spark ignition
US5642721A (en) * 1992-01-06 1997-07-01 Ikeya; Kaname Double ignition system for internal combustion engines, ignition plug for double ignition systems, and electric spark generator
EP1351355A3 (en) * 2002-04-01 2006-06-07 Denso Corporation Ignition device for an internal combustion engine and a manufacturing method therefor

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