WO2012082583A2 - Corona ignition device having asymmetric firing tip - Google Patents

Corona ignition device having asymmetric firing tip Download PDF

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Publication number
WO2012082583A2
WO2012082583A2 PCT/US2011/064334 US2011064334W WO2012082583A2 WO 2012082583 A2 WO2012082583 A2 WO 2012082583A2 US 2011064334 W US2011064334 W US 2011064334W WO 2012082583 A2 WO2012082583 A2 WO 2012082583A2
Authority
WO
WIPO (PCT)
Prior art keywords
electrode
surface area
igniter
firing tip
fuel
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.)
Ceased
Application number
PCT/US2011/064334
Other languages
English (en)
French (fr)
Other versions
WO2012082583A3 (en
Inventor
John Anthony Burrows
James D. Lykowski
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.)
Federal Mogul Ignition LLC
Original Assignee
Federal Mogul Ignition Co
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
Application filed by Federal Mogul Ignition Co filed Critical Federal Mogul Ignition Co
Priority to JP2013544636A priority Critical patent/JP5945549B2/ja
Priority to KR1020137007799A priority patent/KR101892627B1/ko
Priority to CN201180059707.4A priority patent/CN103261676B/zh
Priority to EP11799932.6A priority patent/EP2652311A2/en
Publication of WO2012082583A2 publication Critical patent/WO2012082583A2/en
Publication of WO2012082583A3 publication Critical patent/WO2012082583A3/en
Anticipated expiration legal-status Critical
Ceased 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
    • F02P9/00Electric spark ignition control, not otherwise provided for
    • 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
    • F02P9/00Electric spark ignition control, not otherwise provided for
    • F02P9/002Control of spark intensity, intensifying, lengthening, suppression
    • F02P9/007Control 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
    • 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
    • F02P23/00Other ignition
    • F02P23/04Other physical ignition means, e.g. using laser rays
    • 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
    • F02P3/01Electric spark ignition installations without subsequent energy storage, i.e. energy supplied by an electrical oscillator
    • 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
    • H01T13/46Sparking plugs having two or more spark gaps
    • 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
    • H01T13/46Sparking plugs having two or more spark gaps
    • H01T13/467Sparking plugs having two or more spark gaps in parallel connection
    • 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
    • H01T13/50Sparking plugs having means for ionisation of gap
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01TSPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T21/00Apparatus or processes specially adapted for the manufacture or maintenance of spark gaps or sparking plugs
    • H01T21/02Apparatus or processes specially adapted for the manufacture or maintenance of spark gaps or sparking plugs of sparking plugs
    • 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
    • F02P23/00Other ignition
    • F02P23/04Other physical ignition means, e.g. using laser rays
    • F02P23/045Other physical ignition means, e.g. using laser rays using electromagnetic microwaves
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49231I.C. [internal combustion] engine making

Definitions

  • This invention relates generally to a corona discharge ignition system including an igniter for emitting a non-thermal plasma, and more specifically to a firing tip of the igniter.
  • the corona discharge ignition system includes an igniter with an electrode charged to a high radio frequency voltage potential, creating a strong radio frequency electric field in the combustion chamber.
  • the electric field causes a portion of a mixture of fuel and air in the combustion chamber to ionize and begin dielectric breakdown, facilitating combustion of the fuel-air mixture.
  • the electric field is preferably controlled so that the fuel-air mixture maintains dielectric properties and corona discharge occurs, also referred to as a non-thermal plasma.
  • the ionized portion of the fuel-air mixture forms a flame front which then becomes self-sustaining and combusts the remaining portion of the fuel-air mixture.
  • the electric field is also controlled so that the fuel-air mixture does not lose of all dielectric properties, which would create a thermal plasma and an electric arc between the electrode and grounded cylinder walls, piston, or other portion of the igniter, referred to as power- arcing.
  • the igniter of the corona discharge ignition system typically includes an electrode having an electrode body portion extending longitudinally from an electrode terminal end receiving the high radio frequency voltage, along an electrode center axis, to an electrode firing end.
  • the electrode may include a firing tip adjacent the electrode firing end for emitting the radio frequency electric field.
  • the firing tip is symmetric relative to the electrode center axis.
  • the igniter of the corona discharge ignition system does not include any grounded electrode element in close proximity to the firing tip. Rather, the ground is provided by the cylinder walls or the piston of the internal combustion engine.
  • An example of a corona igniter with a symmetric firing tip is disclosed in U.S. Patent Application Publication No. US 2010/0083942 to Lykowski and Hampton.
  • the ignition source In internal combustion engine systems, especially non- homogeneous combustion systems, like gasoline direct ignition systems, placement of the ignition source relative to the fuel-air mixture is critical to a robust combustion.
  • the fuel is provided to the combustion chamber as a spray, but the spray is typically too rich in fuel to ignite directly and may be flammable only at the outside edges of the spray, where the fuel mixes with the air of the combustion chamber.
  • the igniter must be spaced from the fuel injector so that the firing tip is disposed in a predetermined location relative to the outside edge of the fuel spray.
  • the igniter is also preferably spaced from the fuel spray to prevent erosion and corrosion caused by the fuel spray.
  • One aspect of the invention provides an igniter for receiving a high radio frequency voltage and emitting a radio frequency electric field to ionize a portion of a fuel-air mixture and provide a corona discharge.
  • the igniter comprises an electrode including an electrode body portion extending longitudinally along an electrode center axis from an electrode terminal end, which receives the high radio frequency voltage, to an electrode firing end.
  • the electrode also includes a firing tip adjacent the electrode firing end for emitting the radio frequency electric field.
  • the firing tip is asymmetric relative to the electrode center axis.
  • Another aspect of the invention provides a method of forming the igniter.
  • the method comprises the steps of providing the electrode body portion extending longitudinally from the electrode terminal end along the electrode center axis to the electrode firing end.
  • the method includes disposing the firing tip on the electrode body portion adjacent the electrode firing end and asymmetrically relative to the electrode center axis.
  • Yet another aspect of the invention includes a corona ignition system providing a radio frequency electric field to ionize a portion of the fuel-air mixture and provide a corona discharge igniting the fuel-air mixture in a combustion chamber of an internal combustion engine.
  • the corona ignition system includes a cylinder block extending circumferentially around a space, and a cylinder head extending across the cylinder block.
  • a piston is disposed in the cylinder block and spaced from the cylinder head to provide a combustion chamber therebetween.
  • a fuel injector extends into the combustion chamber for spraying fuel into the combustion chamber.
  • the igniter with the asymmetric firing tip extends into the combustion chamber and is disposed between the fuel injector and the cylinder block. The igniter receives the high radio frequency voltage and emits the radio frequency electric field to ionize the fuel-air mixture and form the corona discharge.
  • Another aspect of the invention provides a method of forming the corona ignition system.
  • the method includes providing the cylinder block extending around the space and extending the cylinder head across the cylinder block.
  • the method includes disposing the piston in the cylinder block and spacing the piston from the cylinder head to provide the combustion chamber therebetween.
  • the method includes disposing the fuel injector in the combustion chamber for spraying fuel into the combustion chamber.
  • the method further includes providing the igniter and disposing the igniter in the combustion chamber for receiving the high radio frequency voltage and emitting the radio frequency electric field to ionize the mixture of fuel and air and form the corona discharge.
  • the step of providing the igniter includes forming the electrode by providing the electrode body portion extending longitudinally from the electrode terminal end to the electrode firing end.
  • the step of providing the igniter also includes disposing the firing tip on the electrode body portion adjacent the electrode firing end and asymmetrically relative to the electrode center axis.
  • the step of disposing the igniter in the combustion chamber includes positioning the igniter between the fuel injector and the cylinder block.
  • the corona igniter of the present invention provides numerous advantages over corona igniters with other designs, such as those including a symmetric firing tip.
  • the igniter can be disposed in a predetermined position relative to the fuel injector and cylinder block so that the corona discharge is formed in an optimal location for ignition and nowhere else. For example, a portion of the asymmetric firing tip having a greater surface area and producing a high electric field strength can be disposed closer to the fuel spray, while a portion of the firing tip having less surface area and producing a lower electric field strength is disposed closer to the cylinder block.
  • the radio frequency electrical field is emitted only from the surface area adjacent the fuel spray so that the corona discharge is formed optimally at the outside edge of the fuel spray.
  • the asymmetric firing tip also prevents power arcing between the firing tip and the cylinder block. Accordingly, the corona igniter of the present invention provides improved performance, compared to corona igniters including symmetric firing tips or other designs.
  • the igniter of the present invention is especially beneficial in non- homogeneous ignition systems, such as gasoline direct injection systems.
  • the asymmetric firing tip is especially advantageous when the fuel injector must remain centrally located in the combustion chamber.
  • the igniter can be moved away from the fuel spray to reduce corrosion and erosion, and closer to the cylinder block, without incurring the detrimental power arcing between the firing tip and cylinder block.
  • the asymmetric firing tip can be arranged to provide corona discharge projecting parallel to or away from the cylinder head, so that igniter can be moved closer to the cylinder head and away from the fuel spray.
  • Another advantage of the present invention is improved energy efficiency, as the corona discharge is only produced where it can usefully provide ignition.
  • Figure 1 is a cross-sectional view of a corona ignition system including an igniter according to one aspect of the invention
  • Figure 2A is a cross-sectional view of the igniter of Figure 1 with a first surface area shaded
  • Figure 2B is a top plan view of a firing tip of the igniter of Figure
  • Figure 3A is a cross-sectional view of the igniter of Figure 1 with a second surface area shaded
  • Figure 3B is a top plan view of a firing tip of the igniter of Figure
  • Figure 4A is a side view of a firing tip according to another embodiment of the invention.
  • Figure 4B is a top plan view of the firing tip of Figure 4A.
  • Figure 5A is a side view of a firing tip according to yet another embodiment of the invention.
  • Figure 5B is a top plan view of the firing tip of Figure 5A.
  • Figure 6A is a side view of a firing tip according to another embodiment of the invention.
  • Figure 6B is a top plan view of the firing tip of Figure 6A
  • Figures 7A-7M are a top plan views of numerous example firing tips according to other embodiments of the invention.
  • Figure 8 is an enlarged top plan view of the firing tip of Figures 1-
  • One aspect of the invention provides a corona ignition system including an igniter 20 disposed in a combustion chamber 22 of an internal combustion engine, as shown in Figure 1.
  • the corona igniter 20 emits a radio frequency electric field to ionize a portion of a fuel-air mixture and provide a corona discharge 24 in the combustion chamber 22.
  • the igniter 20 of the corona ignition system includes an electrode 26 with an asymmetric firing tip 28, also shown in Figure 1.
  • the asymmetric firing tip 28 allows the corona discharge 24 to be formed in an optimal location for ignition, preferably only at an outside edge 30 of a fuel spray, where the fuel mixes with the air.
  • the igniter 20 of the corona ignition system provides multiple benefits, including prevention of power arcing and improved energy efficiency.
  • the corona ignition system is typically incorporated into an internal combustion engine of an automotive vehicle.
  • the system includes a cylinder block 32 having a side wall 34 extending circumferentially around a cylinder center axis a c and presenting a space having a cylindrical shape.
  • the side wall 34 extends upwardly along the cylindrical space to a top end 36 surrounding a top opening.
  • a cylinder head 38 is disposed on the top end 36 and extends across the top opening of the cylinder block 32.
  • a piston 40 is disposed in the cylindrical space and along the side wall 34 of the cylinder block 32 for sliding along the side wall 34 during operation of the internal combustion engine.
  • the piston 40 is spaced from the cylinder head 38, so that the cylinder block 32 and the cylinder head 38 and the piston 40 together provide the combustion chamber 22 therebetween.
  • a fuel injector 42 is disposed in an injector slot 44 of the cylinder head 38 and extends transversely into the combustion chamber 22.
  • the fuel injector 42 provides fuel to the combustion chamber 22, typically in the form of a finely atomized spray.
  • the fuel spray provided by the fuel injector 42 presents the outside edge 30 forming a conical shape, as shown in Figure 1.
  • the fuel injector 42 is typically located centrally in the cylinder and extends longitudinally along the cylinder center axis a c .
  • the fuel injector 42 can alternatively be air guided or wall guided, and the location of the fuel injector 42 may vary depending on the type of combustion system. In many internal combustion engine applications, the fuel injector 42 must be located centrally relative to the cylinder block 32, and it is impossible to move the fuel injector 42.
  • the cylinder head 38 also includes an igniter slot 46 between the fuel injector 42 and the cylinder block 32 for receiving the corona igniter 20.
  • the igniter 20 can extend parallel to or at an angle relative to the cylinder center axis a c and into the combustion chamber 22.
  • the igniter 20 receives the high radio frequency voltage and emits the radio frequency electric field to ionize a portion of the fuel-air mixture and form the corona discharge 24.
  • the precise location of the igniter 20 varies depending on the combustion system.
  • the location of the igniter 20 may be determined by an alignment method disclosed in U.S. Patent Application Publication No. 2010/0083942, or another method.
  • the igniter 20 is disposed in a predetermined position relative to the cylinder block 32 and the fuel injector 42 and the cylinder head 38 and the piston 40, which allows the corona discharge 24 to be formed in an optimal location for combustion.
  • the igniter 20 can be disposed a predetermined distance from the fuel injector 42 and the cylinder block 32 and the piston 40, and disposed at a predetermined angle relative to the fuel injector 42 and the cylinder head 38 and the cylinder block 32.
  • the igniter 20 is also disposed in a predetermined location relative to the outside edge 30 of the fuel spray.
  • the igniter 20 can be disposed approximately at a 30 degree angle relative to the fuel injector 42, as shown in Figure 1, so that the firing tip 28 is disposed in an optimal location adjacent the outside edge 30 of the fuel spray, and so that other portions of the igniter 20 are spaced further from the harsh environment created by the fuel spray.
  • the electrode 26 of the igniter 20 has an electrode center axis a e extending longitudinally from an electrode terminal end 48 receiving the high radio frequency voltage to an electrode firing end 50.
  • the electrode 26 includes an electrode body portion 52 formed of a first electrically conductive material extending longitudinally from the electrode terminal end 48 along the electrode center axis a e to the electrode firing end 50.
  • the first electrically conductive material of the electrode body portion 52 includes nickel or a nickel alloy.
  • the electrode body portion 52 has an electrode diameter D e being perpendicular to the electrode center axis a e .
  • the electrode body portion 52 is symmetric relative to the electrode center axis a e .
  • the electrode body portion 52 is also symmetric relative to a hypothetical plane 54 extending through and longitudinally along the electrode center axis a e , as shown in Figures 2B and 3B.
  • the plane 54 has an injector side 56, which would face generally toward the fuel injector 42 of Figure 1, and an opposite wall side 58 which would face generally toward the side wall 34 of the cylinder block 32 of Figure 1.
  • the electrode 26 of the corona ignition system includes the firing tip 28 surrounding and adjacent the electrode firing end 50 for emitting the radio frequency electric field to ionize a portion of the fuel-air mixture in the combustion chamber 22 and provide the corona discharge 24.
  • the firing tip 28 is formed of a second electrically conductive material, preferably including at least one element selected from Groups 4-12 of the Periodic Table of the Elements.
  • the firing tip 28 typically has a tip diameter D t that is greater than the electrode diameter D e of the electrode body portion 52.
  • the firing tip 28 of the igniter 20 is disposed in a predetermined position relative to the cylinder block 32 and the fuel injector 42 and the cylinder head 38 and the piston 40, which allows the corona discharge 24 to be formed in the optimal location for combustion.
  • the firing tip 28 can be disposed a predetermined distance from the fuel injector 42 and the cylinder block 32 and the cylinder head 38 and the piston 40, and at a predetermined angle relative to the fuel injector 42 and the cylinder block 32 and the cylinder head 38 and the piston 40.
  • the firing tip 28 is also disposed in a predetermined location relative to the outside edge 30 of the fuel spray.
  • the firing tip 28 is disposed adjacent the fuel spray so that the corona discharge 24 is formed at the outside edge 30 of the fuel spray, as shown in Figure 1.
  • the method of U.S. Patent Application Publication No. 2010/0083942, or another method, can be used to determine the position of the firing tip 28 relative to the fuel injector 42 and the fuel spray. Since the firing tip 28 is asymmetric, the igniter 20 can be disposed closer to the side walls 34 of the cylinder block 32, relative to igniters of the prior art corona ignition systems, without incurring power arcing between the firing tip 28 and the cylinder block 32. Accordingly, the majority of the igniter 20 can be spaced further from the fuel spray and thus is less susceptible to erosion and corrosion caused by the harsh environment created by the fuel spray.
  • the firing tip 28 is asymmetric relative to the electrode body portion 52, so that the corona discharge 24 can be formed in an optimal location for ignition. As shown in Figures 2B and 3B, with regard to the plane 54 extending longitudinally through the electrode center axis a e , the asymmetric firing tip 28 presents a first surface area Ai on the injector side 56 of the plane 54 and a second surface area A 2 on the opposite wall side 58 of the center plane 54.
  • the surface areas Ai, A 2 include the total area of all outward facing surfaces of the firing tip 28 exposed to the combustion chamber 22, including top, bottom, and side surfaces.
  • the first surface area Ai of the firing tip 28 faces and extends outwardly generally toward the fuel injector 42 and the second surface area A 2 of the firing tip 28 faces generally toward the cylinder block 32 but does not extend outwardly.
  • the first surface area Ai of the firing tip 28 is greater than the second surface area A 2 of the firing tip 28 such that the firing tip 28 is asymmetric relative to the plane 54.
  • Figures 2A and 2B show the firing tip 28 according to one embodiment, wherein a portion of the first surface area is shaded, and Figures 3A and 3B show the same firing tip 28 with a portion of the second surface area A 2 shaded.
  • the surface areas Ai, A 2 of the firing tips 28 can be determined according to any surface area measurement technique known in the art.
  • the radio frequency electric field emitted from the first surface area Ai facing the fuel injector 42 of the corona ignition system is stronger than the radio frequency electric field emitted from the second surface area A 2 facing the cylinder block 32 so that the corona discharge 24 can be formed in an optimal area of the combustion chamber 22.
  • the electrical field is emitted from the first surface area Ai so that corona discharge 24 is formed optimally in the fuel spray or in a flammable region along the outside edge 30 of the fuel spray, with no electrical field emissions from the second surface area A 2 . Accordingly, the corona ignition system provides a strong combustion of the fuel-air mixture, with no power arcing between the second surface area A 2 of the firing tip 28 and the cylinder block 32, which would hinder combustion.
  • Ai, A 2 of the firing tip 28 depends, in part, on distance from the center axis a c .
  • the first surface area Ai extends a first distance di away from the electrode center axis a c and the second surface area A 2 extends a second distance d 2 away from the electrode center axis a c .
  • the first distance di is greater than the second distance d 2 . The greater distance helps provide a stronger radio frequency electric field being emitted from the first surface area Ai facing the fuel injector 42 than the second surface area A 2 facing the cylinder block 32.
  • the design of the firing tip 28 can vary, and examples of the firing tip 28 are disclosed in Figures 1-8.
  • the first surface area Ai is at least two times greater than the second surface area A 2 , or at least three times greater, or at least four times greater, or more than four times greater.
  • the firing tip 28, typically the first surface area Ai, which is shaded, includes at least one projection 60 extending away from the electrode body portion 52 and presenting a portion of the first surface area Ai.
  • both the first and second surface areas Ai, A 2 of the firing tip 28 present at least one projection 60, or a plurality of projections 60, and the first surface area Ai presents more projections 60 than the second surface area A 2 .
  • the projections 60 of the firing tip 28 preferably extend outwardly and downwardly away from the electrode 26 body potion.
  • the igniter 20 is disposed such that the projection 60 of the firing tip 28 extends toward the fuel spray.
  • the projections 60 of the first surface area Ai preferably include sharp edges to promote the radio frequency electrical field emissions and the optimally located corona discharge 24.
  • the second surface area A 2 preferably includes fewer or no sharp edges thus preventing radio frequency electrical field emissions and power arcing between the second surface area A 2 and the cylinder block 32, cylinder head 38, or piston 40, which could be detrimental to combustion. Any unavoidable edges of the second surface area A 2 are preferably as round as practically possible.
  • the firing tip 28 may include an outward surface 62 being free of sharp edges and presenting a portion of the second surface area A 2 .
  • the sharpness at particular points of the firing tip 28 can be defined by a spherical radius r.
  • the spherical radius r at a particular point along one of the surface areas Ai, A 2 of the firing tip 28 is determined using a hypothetical, three-dimensional sphere having a radius r at the particular point.
  • the spherical radius r is the radius of the three-dimensional sphere.
  • a spherical radius r between 0 and 0.010 inches may be described as a sharp edge.
  • Figure 8 shows spherical radii ri, r 2 presented by portions of the firing tip 28 of Figures 1-3.
  • the outward surface 62 presenting the second surface area A 2 is round.
  • the firing tip 28 is asymmetric relative to the electrode center axis a e and the plane 54 extending along the electrode center axis a e .
  • the firing tip 28 is symmetric relative to itself, but disposed on the electrode body portion 52 asymmetrically so that the firing tip 28 is asymmetric relative to the electrode center axis a e .
  • the top planar views of Figures 7 illustrate various possible firing tips 28, which are only examples and do not limit the possible designs of the present invention.
  • the firing tip 28 presents a triangular shape, such as an isosceles triangular shape.
  • the firing tip 28 presents a quadrilateral shape.
  • FIG. 28 is bifurcated or includes a plurality of divisions 64 presenting the first surface area Ai and the second surface area A 2 .
  • Figures 4A, 5A, and 6A show side views of bifurcated firing tips 28, and 4B, 5B, and 6B show top plan views of the same firing tips 28.
  • the firing tip 28 may include two divisions 64 or a plurality of divisions 64 together forming the asymmetric firing tip 28.
  • the firing tip 28 is disposed perpendicular relative to the electrode body portion 52 so that firing tip 28 and electrode 26 provide a 90 degree angle therebetween.
  • the firing tip 28 is disposed at an angle relative to the electrode body portion 52 so that firing tip 28 and electrode body portion 52 provide angles other than 90 degrees therebetween.
  • Another aspect of the invention provides a method of forming the igniter 20. The method comprises the steps of providing the electrode body portion 52 extending longitudinally from the electrode terminal end 48 along the electrode center axis a e to the electrode firing end 50. The electrode body portion 52 provided is symmetric relative to the electrode center axis a e . Next, the method includes disposing the firing tip 28 on the electrode body portion 52 adjacent the electrode firing end 50 such that the firing tip 28 is asymmetric relative to the electrode center axis a e .
  • the igniter 20 of the corona ignition system includes other elements typically found in a corona igniter 20, such as an insulator 66, a terminal 68, a conductive seal layer 70, and a shell 72.
  • the insulator 66 is disposed in the cylinder head 38 annularly around and longitudinally along the electrode body portion 52. As shown in Figure 1, the insulator 66 extends from an insulator upper end 74 to an insulator lower end 76 spaced from the electrode firing end 50 such that the electrode firing end 50 and the firing tip 28 are disposed outwardly of the insulator lower end 76.
  • the insulator 66 includes a matrix formed of an electrically insulating material, such as alumina.
  • the electrically insulating material has a permittivity capable of holding an electrical charge.
  • the insulating material also has an electrical conductivity less than the electrical conductivity of the electrode body portion 52 and the firing tip 28.
  • the insulator 66 includes an insulator body region 78 disposed in the cylinder head 38 and extending from the insulator upper end 74 toward the insulator lower end 76.
  • the insulator body region 78 presents an insulator body diameter Di generally perpendicular to the longitudinal electrode body portion 52.
  • the insulator 66 also includes an insulator nose region 80 extending from the insulator body region 78 to the insulator lower end 76.
  • the insulator nose region 80 presents an insulator nose diameter D n generally perpendicular to the longitudinal electrode body portion 52 and tapering to the insulator lower end 76. As shown in Figures 2A and 3 A, the insulator nose diameter D n is less than the insulator body diameter Di.
  • the insulator body region 78 is disposed in the cylinder head 38 and is not exposed to the combustion chamber 22, while the insulator nose region 80 extends into the combustion chamber 22.
  • the insulator nose region 80 is disposed at a predetermined angle relative to the cylinder head 38, as shown in Figure 5A.
  • the insulator nose region 80 extends perpendicular to the cylinder head 38, as shown in Figures 4A and 5A.
  • the insulator body region 78 is typically encased by the shell 72, which secures the igniter 20 to the cylinder head 38, and the insulator nose region 80 extends outwardly of the shell 72 into the combustion chamber 22.
  • the insulator 66 and shell 72 typically include a center axis longitudinally aligned with the electrode center axis a e and one another, as shown in Figures 1-6.
  • the insulator 66 is disposed in a predetermined location relative to the fuel injector 42, the fuel spray, the cylinder head 38, and the cylinder block 32 so that the corona discharge 24 can be formed in an optimal location. Since the firing tip 28 is asymmetric, the igniter 20 can be disposed closer to the side walls 34 of the cylinder block 32, compared to igniters of the prior art corona ignition systems, without incurring power arcing between the firing tip 28 and the cylinder block 32. Accordingly, the insulator 66 of the igniter 20 can be spaced further from the fuel injector 42 and thus is less susceptible to erosion and corrosion caused by the harsh environment surrounding the fuel injector 42.
  • the igniter 20 also includes a terminal 68 formed of an electrically conductive material received in the insulator 66.
  • the terminal 68 includes a first terminal end 82, which is electrically connected to a terminal wire (not shown), which is electrically connected to a power source (not shown).
  • the first terminal end 82 receives the high frequency voltage from the power source and transmits the high radio frequency voltage through a second terminal end 84 and to the electrode 26.
  • the terminal 68 is electrically connected to the electrode terminal end 48 by a conductive seal layer 70 formed of an electrically conductive material.
  • the conductive seal layer 70 is disposed between and electrically connects the second terminal end 84 and the electrode terminal end 48 for providing the energy from the terminal 68 to the electrode 26.
  • the shell 72 of the igniter 20 is formed of a metal material disposed in the cylinder head 38 and annularly around the insulator 66.
  • the shell 72 extends longitudinally along the insulator 66 from an upper shell end 86 to a lower shell end 88 such that the insulator nose region 80 projects outwardly of the lower shell end 88, as shown in Figures 1, 2A, and 3 A.
  • the shell 72 may include plurality of threads engaging the injector slot 44 of the cylinder head 38 and securing the igniter 20 to the cylinder head 38.
  • Another aspect of the invention provides a method of forming the corona ignition system.
  • the method includes providing the cylinder block 32 extending circumferentially around the cylindrical space, and extending the cylinder head 38 across the cylinder block 32.
  • the method includes disposing the piston 40 in the cylinder block 32 and spacing the piston 40 from the cylinder head 38 to provide the combustion chamber 22 therebetween.
  • the method further includes disposing the fuel injector 42 in the combustion chamber 22 for spraying fuel into the combustion chamber 22.
  • the method next includes providing the igniter 20 and disposing the igniter 20 in the combustion chamber 22 for receiving the high radio frequency voltage and emitting the radio frequency electric field to ionize the fuel-air mixture and form the corona discharge 24.
  • the step of providing the igniter 20 includes forming the electrode 26 by providing the electrode body portion 52 extending longitudinally from the electrode terminal end 48 along the electrode center axis a e to the electrode firing end 50 and being symmetric relative to the electrode center axis a e .
  • the step of providing the igniter 20 also includes disposing the firing tip 28 on the electrode body portion 52 adjacent the electrode firing end 50 and such that the firing tip 28 is asymmetric relative to the electrode center axis a e .
  • the step of disposing the igniter 20 in the combustion chamber 22 includes positioning the igniter 20 between the fuel injector 42 and the cylinder block 32.
  • the method includes disposing the firing tip 28 in a predetermined location relative to the fuel injector 42 and the cylinder block 32. In another embodiment, the method includes disposing the firing tip 28 at a predetermined angle relative to the fuel injector 42 and the cylinder block 32.
  • the electrode 26 of the igniter 20 is charged to a high radio frequency voltage potential, creating a radio frequency electric field in the combustion chamber 22.
  • the electric field is controlled so that the fuel-air mixture in the combustion chamber 22 maintains dielectric properties.
  • the electrode 26 emits a non-thermal plasma including multiple streams of ions forming a corona to ionize a portion of the fuel-air mixture in the combustion chamber 22.
  • the corona ignition system of the present invention with the asymmetric firing tip 28 provides numerous benefits over other corona ignition systems having different designs, such as those without the asymmetric firing tip 28, especially in non-homogeneous combustion systems, like gasoline direct ignition systems.
  • the asymmetric firing tip 28 can provide an optimally located ignition source providing a robust combustion of the fuel-air mixture.
  • the asymmetric firing tip 28 can be arranged to provide corona discharge 24 projecting parallel to or away from the cylinder head 38, so that the igniter 20 can be moved closer to the cylinder head 38 and away from the fuel spray to reduce erosion and corrosion caused by the fuel spray.
  • the igniter 20 can also be moved away from the fuel spray and closer to the cylinder block 32 without creating the detrimental power arcing.
  • the present invention also uses energy more efficiently than systems including igniters with symmetric firing tips or other designs.
  • the electrical field emissions and corona discharge 24 are only formed on the side of the firing tip 28 facing the fuel spray, where it can usefully provide ignition, rather than on both sides of the firing tip 28, where a significant amount of the electrical field emissions would not contribute to ignition and therefore would be wasted energy.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Plasma & Fusion (AREA)
  • Optics & Photonics (AREA)
  • Spark Plugs (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Electromagnetism (AREA)
PCT/US2011/064334 2010-12-14 2011-12-12 Corona ignition device having asymmetric firing tip Ceased WO2012082583A2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2013544636A JP5945549B2 (ja) 2010-12-14 2011-12-12 非対称な着火を有するコロナ点火装置
KR1020137007799A KR101892627B1 (ko) 2010-12-14 2011-12-12 비대칭 점화 팁을 구비한 코로나 점화장치
CN201180059707.4A CN103261676B (zh) 2010-12-14 2011-12-12 具有非对称点火尖端的电晕点火装置
EP11799932.6A EP2652311A2 (en) 2010-12-14 2011-12-12 Corona ignition device having asymmetric firing tip

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US42284910P 2010-12-14 2010-12-14
US61/422,849 2010-12-14

Publications (2)

Publication Number Publication Date
WO2012082583A2 true WO2012082583A2 (en) 2012-06-21
WO2012082583A3 WO2012082583A3 (en) 2012-12-13

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PCT/US2011/064334 Ceased WO2012082583A2 (en) 2010-12-14 2011-12-12 Corona ignition device having asymmetric firing tip

Country Status (6)

Country Link
US (1) US9103313B2 (enExample)
EP (1) EP2652311A2 (enExample)
JP (1) JP5945549B2 (enExample)
KR (1) KR101892627B1 (enExample)
CN (1) CN103261676B (enExample)
WO (1) WO2012082583A2 (enExample)

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Also Published As

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KR20130140653A (ko) 2013-12-24
CN103261676A (zh) 2013-08-21
US9103313B2 (en) 2015-08-11
EP2652311A2 (en) 2013-10-23
US20120199088A1 (en) 2012-08-09
JP2014501431A (ja) 2014-01-20
WO2012082583A3 (en) 2012-12-13
CN103261676B (zh) 2016-04-20
JP5945549B2 (ja) 2016-07-05
KR101892627B1 (ko) 2018-08-27

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