SPARK PLUG WITH CERAMIC ELECTRODE TIP

Abstract

 A spark plug (20) for igniting a mixture of fuel and air of an internal combustion engine comprises a center electrode (22) and a ground electrode (24). At least one of the electrodes (22, 24) includes a body portion (28, 30) formed of thermally conductive material and a firing tip (32, 34) disposed on the body portion (28, 30). The firing tip (32, 34) includes a ceramic material, providing an exposed firing surface (36, 38). The ceramic material is an electrically conductive, monolithic ceramic material. The ceramic material of the firing tip (32, 34) includes at least one perovskite structure and/or at least one a spinel structure.

Description

CROSS REFERENCE TO RELATED APPLICATIONS

[0001] This application claims priority to U.S. Patent Application No. 14/577,174.

BACKGROUND OF THE INVENTION

1. Field of the Invention

[0002] The invention relates generally to ignition devices for internal combustion engines, such as spark plugs, and more particularly to the electrodes therefore.

2. Related Art

[0003] Internal combustion engines include ignition devices, such as spark ignition devices or spark plugs that extend to the combustion chamber and produce a spark to ignite a mixture of air and fuel. Recent advancements in engine technology are resulting in higher engine operating temperatures to achieve improved engine efficiency. These higher operating temperatures, however, are pushing electrodes of the spark plugs to the very limits of their material capabilities. Presently, Ni-based alloys, including nickel-chromium-iron alloys specified under UNS N06600, such as those sold under the trade names Inconel 600®, Nicrofer 7615®, and Ferrochronin 600®, are typically used as spark plug electrode materials.

[0004] As is well known, the resistance to high temperature oxidation of these Ni-based nickel-chromium-iron alloys decreases as their operating temperature increases. Since combustion environments are highly oxidizing, corrosive wear including deformation and fracture caused by high temperature oxidation and sulfidation can result and is particularly exacerbated at the highest operating temperatures. At the upper limits of operating temperature (e.g., 1400°F), tensile, creep rupture and fatigue strength also have been observed to decrease significantly which can result in deformation, cracking and fracture of the electrodes. Depending on the electrode design, specific operating conditions and other factors, these high temperature phenomena may contribute individually and collectively to undesirable corrosion and erosion of the electrode and diminished performance of the ignition device and associated engine, especially in high performance engines, such as those used in automobile racing.

[0005] High temperature firing tips have been employed in conjunction with the electrode materials described. These firing tips have been manufactured from a number of platinum group metals and metal alloys, such as platinum, iridium, rhodium, palladium, ruthenium and rhenium, as pure metals and together with themselves and various other alloy constituents, such as various rare earth elements, in various alloy combinations; gold and gold alloys; tungsten and tungsten alloys and the like. These high temperature firing tips have been attached to a body portion of the electrode materials described above, both center and ground electrodes, in various tip configurations using a wide variety of attachment and joining techniques, including resistance welding, laser welding, mechanical joining and the like, both separately and in various combinations.

[0006] Notwithstanding the electrode performance improvements attainable through the use of high temperature firing tips, there remain various aspects of these materials which limit their application and use in ignition device configurations and applications, for example susceptibility to other and new high temperature oxidation, erosion and corrosion mechanisms, such as those associated with small amounts of calcium and phosphorus, thermal expansion mismatch with various center and ground electrode materials and other aspects, such as the high cost of these materials, which serve to limit their usefulness in various ignition applications.

SUMMARY OF THE INVENTION

[0007] One aspect of the invention provides a spark plug for igniting a mixture of fuel and air of an internal combustion engine in accordance with Claim 1. Another aspect provides for a spark plug for igniting a mixture of fuel and air of an internal combustion engine according to Claim 8.

[0008] Another aspect of the invention provides a method of manufacturing a spark plug for igniting a mixture of fuel and air of an internal combustion engine in accordance with claim 15.

[0009] Yet another aspect of the invention provides an electrode for an ignition device according to Claim 14. The electrode comprises a body portion including a thermally conductive material, and a firing tip disposed on the body portion, wherein the firing tip includes a ceramic material. The ceramic material includes at least one perovskite structure and/or at least one spinel structure.

[0010] Another aspect of the invention provides a method of manufacturing an electrode for an ignition device. The method comprises compacting a ceramic material to form a firing tip, wherein the ceramic material includes at least one of a perovskite structure, a spinel structure, and a precursor material that forms a perovskite or spinel structure upon sintering. The method further comprises sintering the compacted ceramic material; and disposing the sintered ceramic material on a body portion including a thermally conductive material.

[0011] The electrode comprising the firing tip formed of the at least one perovskite structure and/or at least one spinel structure is economical to manufacture and provides a longer useful life, compared to other electrodes used in ignition devices. The combination of the thermally conductive body portion and ceramic firing tip provides resistance to high temperature oxidation, sulfidation, and related corrosion and erosion, while also effectively conducting heat from the firing tip to reduce the operating temperature at the firing tip.

BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Other advantages of the present invention will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:

Figure 1 is a cross-sectional view of a spark plug constructed in accordance with one embodiment of the invention;

Figure 1A is an enlarged cross-sectional view of the firing tips of the electrodes of Figure 1; and

Figures 2-11 are cross-sectional views of center electrodes according to other embodiments of the invention, including various different firing tip configurations.

DETAILED DESCRIPTION

[0013] One aspect of the invention provides a spark plug 20 for igniting a mixture of fuel and air of an internal combustion engine. As shown in Figures 1 and 1A, the spark plug 20 includes a center electrode 22 and a ground electrode 24 providing a spark gap 26 therebetween. At least one of the electrodes 22, 24 includes a body portion 28, 30 formed of a thermally conducive material and a firing tip 32, 34 formed of a ceramic material disposed on the body portion 28, 30. The ceramic material of the firing tip 32, 34 provides a firing surface 36, 38 for emitting a spark to ignite the mixture of fuel and air.

[0014] By forming the firing tip 32, 34 of the ceramic material, a lower operating temperature is provided at the firing tip 32, 34. By forming the body portion 28, 30 of a thermally conductive material, heat is effectively conducted away from the ceramic firing tip 32, 34. Thus, the electrode 22, 24 of the present invention, with the thermally conductive body portion 28, 30 and the ceramic firing tip 32, 34, provides a lower operating temperature at the firing tip 32, 34 than other electrodes formed entirely of the ceramic material. The reduced operating temperature at the firing tip 32, 34 extends the life of the spark plug 20. Further, the electrode 22, 24 of the present invention is more economical to manufacture than those with platinum group metal firing tips.

[0015] While the electrode 22, 24 is described for use in the particular spark plug 20 application of Figure 1, it will be appreciated that the electrode 22, 24 having the thermally conductive body portion 28, 30 and the ceramic firing tip 32, 34 can be used in other types of ignition devices.

[0016] As shown in Figure 1, the center electrode 22 extends longitudinally along a center axis A from a center electrode top end 40 to a center firing end 42. The body portion 28, 30 of the center electrode 22, referred to as a center body portion 28, extends from the center electrode top end 40 toward the center firing end 42. The center body portion 28 includes a thermally conductive material and is typically formed entirely of the thermal conductive material, but may be formed of multiple different thermally conductive materials. The center body portion 28 has a thermal conductivity sufficient to draw heat away from a center firing tip 32. In one embodiment, the center body portion 28 has a thermal conductivity of at least 20 Wm-K when measured at 20° C, and preferably at least 35 W/m-K when measured at 20° C. The thermally conductive material of the center body portion 28 is also electrically conductive. The center body portion 28 also typically has an electrically conductivity of at least 9 x 10⁵ siemens per meter (S/m). The thermally conductive material is typical metal, preferably nickel or nickel alloy, or a mixture of different metals.

[0017] The center electrode 22 can include a variety of different configurations, as shown in Figures 2-11. In one embodiment, as shown in Figures 10 and 11, the center body portion 28 includes a clad 44 of a first thermally conductive material, such as nickel, and a core 46 of a second thermally conductive material, such as copper, enrobed by the clad 44. The thermally conductive material of the core 46 is also electrically conductive.

[0018] As shown in Figure 2, the center body portion 28 has a first diameter D₁ extending perpendicular to the longitudinal center body portion 28. The first diameter D₁ of the center body portion 28 is typically 2.69 mm, 2.16 mm, 1.83 mm, or 1.32 mm. However, it will be understood by those of ordinary skill in the art that the center body portion 28 may have other dimensions. In one embodiment, as shown in Figures 2-6 and 9-11, the center body portion 28 presents a center hole 48 extending longitudinally along the center axis A and facing outwardly of the center electrode 22 at the center firing end 42. In the embodiment of Figure 10, the center hole 48 and the center firing tip 32 are spaced from the core 46 of the center body portion 28 by the clad 44. In the embodiment of Figure 11, the center hole 48 and the center firing tip 32 abut the core 46. In another embodiment, shown in Figures 3-10, the center electrode 22 has a diameter reduction, referred to as a third diameter D₃, along the center body portion 28 in a region spaced from the center firing end 42. In yet another embodiment, as shown in Figures 4 and 9, the center electrode 22 has the reduced third diameter D₃ along the center body portion 28 in the region spaced from the center firing end 42, and tapers from the center body portion 28 to the center firing end 42 forming a frustum of a cone along a segment of the center body portion 28 adjacent to the center firing end 42. In one embodiment, the third diameter D₃ of the center electrode 22 is 2.54 mm, 1.98 mm, 1.65 mm, or 1.16 mm, corresponding to the first diameters D₁ examples provided above. However, it will be understood by those of ordinary skill in the art that the center electrode 22 may have other dimensions. The center firing tip 32 also has a cylindrical geometry, but can comprise other shapes.

[0019] At least one of the electrodes 22, 24, but preferably both electrodes 22, 24 include the ceramic firing tip 32, 34. As shown in Figures 1-11, the center electrode 22 includes the firing tip 32, referred to as the center firing tip 32, formed of the ceramic material to provide a long-life center firing surface 36 for the spark plug 20. The center firing tip 32 extends transversely from the center firing end 42. The ceramic material of the center firing tip 32 presents the firing surface 36, referred to as a center firing surface 36, which is typically planar and faces outwardly for emitting a spark to ignite the mixture of fuel and air. In another embodiment, the center firing surface 36 is convex (not shown). In one embodiment, as shown in Figures 2-6 and 9-11, the center firing tip 32 is disposed in the center hole 48. The center firing tip 32 typically has a second diameter D₂ extending perpendicular to the center axis that is less than the first diameter D₁ of the center body portion 28. The second diameter D₂ of the center firing tip 32 is typically 1.5 mm, 1.0 mm, or 0.7 mm. However, it will be understood by those of ordinary skill in the art that center firing tip 32 may have other dimensions. The center firing tip 32 also has a cylindrical geometry, but can comprise other shapes.

[0020] In one embodiment, the center firing tip 32 comprises a monolithic ceramic rivet, as shown in Figures 6-8. In yet another embodiment, as shown in Figure 8, the firing tip 32, 34 includes a first section and a second section, wherein the first section is disposed on the body portion 28, 30 and includes a metal material, and the second section is disposed on the first section and includes the ceramic material.

[0021] The center firing tip 32 includes a ceramic material presenting the center firing surface 36, preferably a monolithic and electrically conductive or semi-conductive ceramic material. Typically, the center firing tip 32 is formed entirely of the electronically conductive ceramic material. In one embodiment, the ceramic material of the center firing tip 32 has an electrical conductivity of at least 10⁶ S/m. The appropriate ceramic material is used in the construction of the center firing tip 32, depending on the level of resistance desired and the temperatures to which the center electrode 22 is exposed. Further, the ceramic material can be provided as a homogeneous material over the entire structure of the center firing tip 32, or as a gradient or a composite. In one preferred embodiment, the ceramic material includes at least one of one of Titanium Diboride; Silicon Carbide; and Ternary Silicides, Nitrides and Carbides, such as Molybdenum Silicide Carbide (Mo₅Si₃C) or Titanium Carbonitride (TiCN), for example. Other examples of ceramic materials that can be used to form the center firing tip 32 are disclosed in U.S. Patent Application Nos. 12/200,244; 12/201,567; and 12/201,590, each to the present inventor, William J. Walker, Jr.

[0022] In one embodiment, the center firing tip 32 is formed of a ceramic material disclosed in U.S. Patent Application No. 12/200,244. The center firing tip 32 of this embodiment is preferably constructed entirely of a solid, one-piece, monolithic conductive or semi-conductive ceramic material. The ceramic materials can include, by way of example and without limitation, oxides, borides, nitrides, carbides, and silicides.

[0023] In one embodiment, the center firing tip 32 of the center electrode 22 is constructed of at least one oxide. For example, 100 weight percent (wt. %) of the center firing tip 32 could consist of the at least one oxide. Alternatively, at least 50 wt. %, or at least 70 wt. %, or at least 90 wt. %, or at least 95 wt. % of the center firing tip 32 could consist of the at least one oxide. The at least one oxide used to form the center firing tip 32 typically includes oxides of transition metals. In this embodiment, the oxides can include monoxides, such as TiO, VO, NbO, TaO, MnO, FeO, CoO, NiO, CuO, and ZnO; sesquioxides, such as V₂O₃, CrO₃, Fe₂O₃, RhO₃, In₂O₃, Th₂O₃, and Ga₂O₃; and dioxides such as TiO₂, VO₂, CrO₂, MoO₂, WO₂, RuO₂, ReO₂, OsO₂, RhO₂, IrO₂, PbO₂, NbO₂, MbO₂, MnO₂, PtO₂, GeO₂, and SnO₂.

[0024] In an exemplary embodiment, the at least one oxide of the center firing tip 32 comprises at least one perovskite structure, which is an oxide of two or more metals including at least one transition metal. The perovskite structures can have the general formulation ABO₃, wherein component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; and component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni. Examples of such perovskite structures include LaCrO₃, LaMnO₃, LaFeO₃, LaGaO₃, and LaCoO₃.

[0025] In another embodiment, at least a portion of the component A and/or at least a portion of the component B of the perovskite structure can be replaced or substituted with a another component C and/or component D. In other words, some of component A, or all of component A, could be replaced with component C and/or component D; and some of component B, or all of component B, could be replaced with component C and/or component D. In an exemplary embodiment, component C includes at least one of La, Ca, Ba, Sr, Y, and Gd; and is different from component A and B. Component D includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, and Ni; and is different from component A and B. For example, the perovskite structure with the formulation ABO₃ could be substituted with the additional component C and/or component D to form a perovskite with the general formulation (A_xC_1-x)BO₃, A(B_yD_1-y)O₃ or (A_xB_1-x)(C_yD_1-y)O₃, wherein x is between 0 and 0.5 and y is between 0 and 0.5. A specific example of the alternate perovskite structure is La_1-xSr_xMnO₃. wherein a portion of the La is substituted with Sr. In addition, in certain embodiments, there could be three or more elements that occupy component A, which are each selected from the list of component A above; and/or three or more elements that occupy component B, which are each selected from the list of component B above.

[0026] Furthermore, components C and D may include elements selected from a group that have a valence charge different from that of components A and/or B, so that the total amount of oxygen (O) can be greater than or less than 3. For example, the alternate perovskite structure could have the general formulation M_xN_1-yO_3-z, wherein component M comprises component A and at least one other metallic element; component N comprises component B and at least one other metallic element; x is in the range from 0.9 to 1.1; y is in the range from 0.9 to 1.1; and z is in the range from -0.2 to 0.2. In an exemplary embodiment, the at least one other metallic element of component M and/or component N is selected from the following group: La, Ca, Ba, Sr, Y, Gd, Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ni, Cu, Zn, Ag, Ga, Al, and Si. In this embodiment, the valence charge of the other metallic element of component M is different than the valence charge of component A, and the valence charge of the other metallic element of component N is different from the valence charge of component B.

[0027] In another embodiment, the at least one oxide used to construct the center firing tip 32 of the center electrode 22 comprises at least one spinel structure, instead of or in addition to the at least one perovskite structure. The spinel structure can have the general formulation AB₂O₄, wherein component A includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, and Cu; and component B includes at least one of Al, Cr, and Fe. An exemplary spinel structure is nickel ferrite, which is an electrically conducting spinel having the stoichiometric composition NiFe₂O₄. In one embodiment, the performance of the spinel is improved by changing the ratio of Ni and Fe, such that the general formulation of the spinel is Ni_1-xFe_2+xO₄ or Ni_1+xFe_2-xO₄, wherein x ranges from 0 to 0.5

[0028] In another embodiment, at least a portion of the component A and/or at least a portion of the component B of the spinel structure can be replaced with another component C and/or component D. In other words, some of component A, or all of component A, could be replaced with component C and/or component D; and some or component B, or all of component B, could be replaced with component C and/or component D. In an exemplary embodiment, component C includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, Cu, Mo, W, Cr and V; and component C is different from component A and B. Component D includes at least one of Al, Cr, Fe, Co, Ga and Mo; and component D is different from component A and B. Like the perovskite structures, the spinels can be substituted, in which case the general formulation would be M_xN_2-yO_4-z, wherein M comprises component A and at least one other metallic element; N comprises component B and at least one other metallic element; x ranges from -0.1 to 0.1; y ranges from -0.1 to 0.1; and z ranges from -0.2 to 0.2. In an exemplary embodiment, the at least one other metallic element of component M and/or component N is selected from the following group: Ge, V, Te, Ti, Sb, Nb, Ta, W, Sn, Hf, Zr, Sc, Bi, and In.

[0029] The center firing tip 32 constructed of the perovskite structure or spinel structure is manufactured by compacting and sintering the ceramic material. In one embodiment, the ceramic material initially provided for compacting and sintering includes at least one of the perovskite structures or spinel structures described above.

[0030] In another embodiment, a precursor material is provided which upon sintering forms one of the perovskite structures or spinel structures. The precursor material typically includes common oxides and/or carbonates of the elements listed above. Exemplary precursor materials that can be compacted and sintered to form the center firing tip 32 from a perovskite structure include at least one of La₂O₃, CaCO₃, BaCO₃, SrCO₃, Y₂O₃, Gd₂O₃, Sc₂O₃, TiO₂, ZrO₂, HfO₂, Nb₂O₅, Ta₂O₅, MoO₃, Mo₂O₃, WO₃, ReO₃, V₂O₃, Cr₂O₃, MnO₂, Fe₂O₃, FeO, Fe₃O₄, RuO₄, CoO, NiO, and Ni₂O₃. Exemplary precursor materials that can be compacted and sintered to form the center firing tip 32 from a spinel structure include at least one of Li₂CO₃, CoO, MgCO₃, MgO, ZnO, NiO, Ni₂O₃, FeO, Fe₂O₃, Fe₃O₄, CdO, MnO₂, CuO, Al₂O₃, Al(OH)₃ and Cr₂O₃.

[0031] The borides include, for example, chemical compositions having the formula M_xB_y, where M is a metallic element, X is often 1, and Y is often 1, 2 or 6. Other examples include borides having an electrical resistivity in the range of 10^-5 to 10^-4 ohm-cm, and melting points in the range of 1600 to 3200 degrees Celcius. Specific examples include Zirconium Boride (ZrB₂; ZrB and ZrB₁₂); Hafnium Boride (HfB₂); Titanium Boride (TiB₂; TiB); Vanadium Boride (VB₂; VB); Tungsten Boride (W₂B₅); Chromium Boride (CrB₂; CrB); Molybdenum Boride beta-MoB, alpha-MoB, Mo₂B₅; Mo₂B; Niobium Boride (NbB₂; NbB); Tantalum Boride (TaB₂; TaB); Lanthanum Hexaboride (LaB₆); Barium Hexaboride (BaB₆); Calcium Hexaboride (CaB₆); and Cerium Hexaboride (CeB₆).

[0032] The nitrides can include, for example, chemical compositions having the formula M_xN_y, where M is a metallic element, N is nitride and X and Y are typically 1. The nitrides have an electrical resistivity in the range of 10^-5 to 10^-4 ohm-cm, and melting points in the range of 1400 to 3300 degrees Celcius. Examples of nitrides include Titanium Nitride (TiN); Zirconium Nitride (ZrN); Tantalum Nitride (TaN); Niobium Nitride (NbN); Vanadium Nitride (VN); and Hafnium Nitride (HfN).

[0033] Carbides are another possible ceramic material, including for example chemical compositions having the formula M_xC_y, where M is a metallic element, C is carbon and X and Y are typically 1. The carbides typically have an electrical resistivity in the range of 10^-5 to 10^-4 ohm-cm, and melting or sublimation points in the range of 1900 to 4000 degrees Celcius. Some examples include, Tantalum Carbide (TaC); Chromium Carbide (Cr₃C₂); Molybdenum Carbide (MoC; Mo₂C); Tungsten Carbide (WC; W₂C); Zirconium Carbide (ZrC); Titanium Carbide (TiC); Niobium Carbide (NbC); Hafnium Carbide (HfC); Vanadium Carbide (VC); Beryllium Carbide (Be₂C); Silicon Carbide (SiC); and Boron Carbide (B₄C).

[0034] The silicides include, for example, chemical compositions having the formula M_xSi_y, where M is a metallic element, Si is silicon and X is typically 1 and Y is typically 2. The silicides typically have an electrical resistivity in the range of 10^-5 to 10^-4 ohm-cm, and melting points in the range of 1500 to 2500 degrees Celcius. Some examples include, Molybdenum Silicide (MoSi₂); Niobium Silicide (NbSi₂); Titanium Silicide (TiSi₂); Tungsten Silicide (WSi₂; W₅Si₂); Chromium Silicide (CrSi₂; Cr₃Si); and Tantalum Silicide (TaSi₂).

[0035] In another embodiment, the center firing tip 32 is formed of a ceramic material disclosed in U.S. Patent Application No. 12/201,567. In this embodiment, the ceramic material has exceptionally high resistance to high temperature oxidation, erosion and corrosion. The general category of conductive ceramic materials of this embodiment may be referred to as transition metal nitrides, carbides, and carbonitrides due to their superior high temperature properties, including mechanical strength and resistance to certain high temperature oxidation, erosion and corrosion processes. Specifically, the ceramic materials include conductive ceramics of the form M_n+1AX_n, where M is a transition metal, A is a group IIIA or IVA element, X is nitrogen, or carbon, or both carbon and nitrogen, and n is 1, 2, or 3. While M may be any transition metal suitable for forming a conductive ceramic compound of the form described above, it is preferred that M be selected from a group consisting of Ti, Nb, Ta, V, Cr, Mo, Sc, Zr and Hf. Even more preferably, M may include Ti, Nb, Ta, V, and Cr, in various combinations. A may be any suitable group IIIA or IVA element or elements, including Al, Ga, In, Tl, Si, Ge, Sn, Pb, P, As and S, with Al and Si believed to be particularly preferred. X may be carbon, nitrogen or both carbon and nitrogen in various stoichiometric and non-stoichiometric proportions.

[0036] Exemplary ceramics of this embodiment include Ti₂AlC, Ti₂AlN, Ti₂Al(C0.5, N0.5), Nb₂AlC, (Nb, Ti)AlC, Ti₂AlC, V₂AlC, Cr₂AlC, Ti₄AlN₃, Ti₃AlC2, Ti₂GaC, V₂GaC, Cr₂GaC, Nb₂GaC, Mo₂GaC, Ta₂GaN, Cr₂GaN, Sc₂InC, Ti₂InC, Zr₂InC, Nb₂InC, Hf₂InC, Ti₂InN, Zr₂InN, Ti₂TlC, Zr₂TlC, Hf₂TlC, Zr₂TlN, Ti₃SiC₂, Ti₂GeC, V₂GeC, Cr₂GeC, Ti₃GeC₂, Ti₂SnC, Zr₂SnC, Hf₂SnC, Hf₂SnN, Ti₂PbC, Zr₂PbC, Hf₂PbC, V₂PC, Nb₂PC, V₂AsC, Nb₂AsC, Ti₂SC, Zr₂SC, Nb₂SC, and Hf₂SC. Of these (Nb, Ti)AlC, Ti₂AlC, Va₂AlC, Cr₂AlC, Ti₄AlN₃, Ti₃AlC₂ and Ti₃SiC₂ are believed to be preferred, with Ti₃SiC₂ and Ti₂AlC believed to be particularly preferred.

[0037] In another embodiment, the center firing tip 32 is formed of a ceramic material disclosed in U.S. Patent Application No. 12/201,590. In this embodiment, the center firing tip 32 comprises a composite ceramic structure. The composite structure may have at least two different consistent materials, and can either be a ceramic-ceramic composition, or a ceramic-metal (cermet) composition, depending on the specific attributes sought in the specific application. If constructed as a ceramic-ceramic composite, one exemplary composite structure example includes a composite of silicon nitride (Si₃N4) and molybdenum disilicide (MoSi₂).

[0038] In one preferred embodiment, the center firing tip 32 is formed of a ceramic-ceramic composite having a uniform composition throughout the firing tip 32. In alternate embodiment, the concentration of the composition may vary across the width of the center firing tip 32, in a cross-section taken generally perpendicular to the center axis A. Accordingly, the center firing tip 32 of the alternate embodiment has a non-uniform concentration of the different ceramic materials as viewed along a cross-section taken generally perpendicular to the center axis A. The difference in composition across the width may provide the center firing tip 32 with an insulating peripheral outer portion and a conductive inner portion surrounded and encapsulated by the outer portion. The inner portion may be exposed or closed along the center firing end 42 and along the center firing surface 36.

[0039] In one exemplary embodiment, without limitation, the composition of the outer portion of the center firing tip 32 can be provided having about 28 percent MoSi₂ and about 72 percent Si₃N₄. The composition of the inner portion can be provided having about 43 percent MoSi₂ and about 57 percent Si₃N₄. Accordingly, the inner portion provides a conductive inner region and the outer portion provides an insulating region. It should be recognized that the aforementioned composite materials are by way of example, and that other materials could be used. For example, the insulating ceramic composite material could be provided as aluminum oxide, aluminum nitride, aluminum oxy-nitride, or silicon aluminum oxynitride, while the conductive ceramic material could be provided as titanium nitride, titanium diboride.

[0040] The center firing tip 32 of this embodiment could be provided as a ceramic-metal (cermet) composition, the conductive composite material could be provided as a metal, such as platinum, iridium, nickel or an alloy of nickel, for example. As previously mentioned, the percent concentration of the each of the insulating and conductive ceramic composite materials can be varied across the width of the center firing tip 32 and/or along the length of the center firing tip 32, depending on the performance requirements desired.

[0041] A variety of methods can be used to attach the center firing tip 32 to the center body section. In one embodiment, a braze 50 attaches the center firing tip 32 to the center body portion 28. The brazing can be done using an active braze alloy, such as Ticusil, Gold-ABA, Gold-ABA-V, or other braze alloys provided by Wesgo Metals. Alternatively, reactive air brazing can be used to attach the center firing tip 32 to the center body portion 28. The reactive air brazing typically involves using a copper oxide-silver single phase liquid to join the metal of the center body portion 28 and the ceramic material of the center firing tip 32. The center firing tips 32 of Figures 2-4, 7, 8, 10, and 11 may be attached by brazing.

[0042] In another embodiment, the center electrode 22 includes a retaining element 52 disposed along the center firing end 42 for attaching the center firing tip 32 to the center body portion 28. In one embodiment, as shown in Figures 5 and 6, the retaining element 52 includes a ledge or other mechanical locking feature facing inwardly toward the center axis A. The retaining element 52 and center firing end 42 together present the center hole 48 therebetween for receiving the center firing tip 32 and mechanically attaching the center firing tip 32 to the center body portion 28. In the embodiment of Figure 6, the retaining element 52 is attached to the center body portion 28 by a laser weld 86. In yet another embodiment, as shown in Figure 9, the center firing tip 32 is attached to the center body portion 28 by forming indentations 82, holes, grooves, or notches along the center firing tip 32 adjacent the center firing end 42, and melting a portion of the center body portion 28 at the center firing end 42, adjacent the indentations, so that the body portion 28 flows into the indentations and solidifies, providing the melted portion 88 of Figure 9. The melted portion 88 secures the center firing tip 32 to the center body portion 28.

[0043] As shown in Figure 1, the spark plug 20 further includes other elements such as those typically found in spark plugs 20 of internal combustion engines. For example, the spark plug 20 includes an insulator 56 disposed annularly around the center electrode 22. The insulator 56 extends longitudinally from an insulator upper end 58, along the center body portion 28, toward the center firing end 42, and to an insulator firing end 60. The center firing end 42 projects outwardly of the insulator firing end 60.

[0044] The insulator 56 is formed of an electrically insulating material, such as alumina. The insulator 56 preferably has a very low dielectric loss factor, and an electrical conductivity significantly less than the electrical conductivity of the center electrode 22, such as an electrical conductivity of not greater than 10^-12 S/m.

[0045] The spark plug 20 of Figure 1 includes a terminal 62 formed of an electrically conductive material received in the insulator 56 and extending from a first terminal end 64 to a second terminal end 66, which is electrically connected to the center electrode top end 40 of the center electrode 22. The terminal 62 is formed of an electrically conductive material. A resistor layer 68 is disposed between and electrically connects the second terminal end 66 of the terminal 62 and the center electrode top end 40 of the center electrode 22 for transmitting energy from the terminal 62 to the center electrode 22. The resistor layer 68 is formed of an electrically resistive material, such as a glass seal.

[0046] The spark plug 20 further includes a shell 70 disposed annularly around and longitudinal along the insulator 56 from an upper shell end 72 to a lower shell end 74. The insulator firing end 60 and the center firing end 42 project outwardly of the lower shell end 74, as shown in Figure 1. The spark plug 20 engages with the engine by means of a threaded portion of the shell 70, where the threads 84 may be 14 mm, 12 mm, or 10 mm, and preferably 12 mm. However, it will be understood by those of ordinary skill in the art that other threads, or other means of engaging with the engine, can be used. The shell 70 is formed of a metal material, such as steel. The spark plug 20 can include at least one packing element 54, such a gasket, cement, or other sealing compound, disposed between the insulator 56 and the shell 70 for providing a gas-tight seal between the shell 70 and the insulator 56. The packing element 54 can also be disposed between the insulator 56 and the terminal 62.

[0047] The ground electrode 24 of the spark plug 20 is attached to the lower shell end 74 of the shell 70. The ground electrode 24 comprises the body portion 30, referred to as a ground body portion 30, extending from a ground electrode top end 76, which is attached to the lower shell end 74, to a ground firing end 78. The ground body portion 30 extends transversely from the lower shell end 74 and curves toward the center electrode 22 to the ground firing end 78.

[0048] Like the center body portion 28 of the center electrode 22, the ground body portion 30 also includes a thermally conductive material, which is typically selected from the same group of materials as the thermally conductive material of the center body portion 28, but can be a different material. In one embodiment, the ground body portion 30 includes the clad 44 of the thermally conductive material, such as nickel, enrobing the core 46 of another thermally conductive material, such as copper. The ground body portion 30 has a thermal conductivity sufficient to draw heat away from a ceramic ground firing tip 34. The ground body portion 30 has a thermal conductivity of at least 20 Wm-K when measured at 20° C, and preferably at least 35 W/m-K when measured at 20° C.

[0049] The ground body portion 30 also has an electrical conductivity of at least 9 x 10⁵ S/m. As shown in Figure 1, the ground body portion 30 has a first length l₁ extending parallel to the center axis A. In one embodiment (not shown), the ground body portion 30 includes a clad of a first thermally conductive material, such as nickel, and a core of a second thermally conductive material, such as copper, enrobed by the clad. The thermally conductive material of the core is also electrically conductive.

[0050] As alluded to above, the ground electrode 24 preferably includes a firing tip 34, referred to as the ground firing tip 34, extending transversely from the ground firing end 78 toward the center firing tip 32. The ground firing tip 34 has a second length l₂ extending parallel to the center axis A, which is generally less than the first length l₁, but may be longer than the first length l₁. The ground firing tip 34 also preferably includes one of the ceramic materials described above with regard to the center firing tip 32. The ceramic material of the ground firing tip 34 can be the same as or different from the ceramic material of the center firing tip 32. The ceramic material of the ground firing tip 34 provides the firing surface 36, 38, referred to as a ground firing surface 38, facing the center firing surface 36 and exposed to the combustion chamber.

[0051] As shown in Figures 1 and 1A, the ground firing surface 38 is spaced and parallel to the center firing surface 36 to provide the spark gap 26 therebetween. However, in an alternate embodiment, only one of the electrodes 22, 24 includes the firing tip 32, 34, and the spark gap 26 is provided in part by another type firing surface of the electrode 22, 24 without the firing tip 32, 34. In one embodiment, the ground firing tip 34 has a rectangular cross-section, but can comprise a variety of shapes, being the same as or different from the center firing tip 32. The ground firing tip 34 can be attached to the ground body portion 30 by a variety of methods, such as those discussed with regard to the center firing tip 32 and the center body portion 28. In one embodiment, the ground body portion 30 presents a ground hole 80 extending longitudinally along the center axis A and facing outwardly of the ground electrode 24 at the ground firing end 78.

[0052] In one embodiment, the ground firing tip 34 of the ground electrode 24 is constructed of at least one oxide. For example, 100 weight percent (wt. %) of the ground firing tip 34 could consist of the at least one oxide. Alternatively, at least 50 wt. %, or at least 70 wt. %, or at least 90 wt. %, or at least 95 wt. % of the ground firing tip 34 could consist of the at least one oxide. The at least one oxide used to form the ground firing tip 34 typically includes oxides of transition metals. In this embodiment, the oxides can include monoxides, such as TiO, VO, NbO, TaO, MnO, FeO, CoO, NiO, CuO, and ZnO; sesquioxides, such as V₂O₃, CrO₃, Fe₂O₃, RhO₃, In₂O₃, Th₂O₃, and Ga₂O₃; and dioxides such as TiO₂, VO₂, CrO₂, MoO₂, WO₂, RuO₂, ReO₂, OsO₂, RhO₂, IrO₂, PbO₂, NbO₂, MbO₂, MnO₂, PtO₂, GeO₂, and SnO₂.

[0053] The at least one oxide of the ground firing tip 34 can also include oxides of two or more metals, which include at least one transition metal. Such oxides include perovskite structures with the general formulation ABO₃, wherein component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; and component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni. Examples of such perovskite structures include LaCrO₃, LaMnO₃, LaFeO₃, LaGaO₃, and LaCoO₃.

[0054] In another embodiment, at least a portion of the component A and/or at least a portion of the component B of the perovskite structure can be replaced or substituted with a another component C and/or component D. In other words, some of component A, or all of component A, could be replaced with component C and/or component D; and some of component B, or all of component B, could be replaced with component C and/or component D. In an exemplary embodiment, component C includes at least one of La, Ca, Ba, Sr, Y, and Gd; and is different from component A and B. Component D includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, and Ni; and is different from component A and B. For example, the perovskite structure with the formulation ABO₃ could be substituted with the additional component C and/or component D to form a perovskite with the general formulation (A_xC_1-x)BO₃, A(B_yD_1-y)O₃ or (A_xB_1-x)(C_yD_1-y)O₃, wherein x is between 0 and 0.5 and y is between 0 and 0.5. A specific example of the alternate perovskite structure is La_1-xSr_xMnO₃, wherein a portion of the La is substituted with Sr. In addition, in certain embodiments, there could be three or more elements that occupy component A, which are each selected from the list of component A above; and/or three or more elements that occupy component B, which are each selected from the list of component B above.

[0055] Furthermore, components C and D may include elements selected from a group that have a valence charge different from that of components A and/or B, so that the total amount of oxygen (O) can be greater than or less than 3. For example, the alternate perovskite structure could have the general formulation M_xN_1-yO_3-z, wherein component M comprises component A and at least one other metallic element; component N comprises component B and at least one other metallic element; x is in the range from 0.9 to 1.1; y is in the range from 0.9 to 1.1; and z is in the range from -0.2 to 0.2. In an exemplary embodiment, the at least one other metallic element of component M and/or component N is selected from the following group: La, Ca, Ba, Sr, Y, Gd, Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ni, Cu, Zn, Ag, Ga, Al, and Si. In this embodiment, the valence charge of the other metallic element of component M is different than the valence charge of component A, and the valence charge of the other metallic element of component N is different from the valence charge of component B.

[0056] The at least one oxide used to construct the ground firing tip 34 of the ground electrode 24 could alternatively comprise a spinel structure having the general formulation AB₂O₄, wherein component A includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, and Cu; and component B includes at least one of Al, Cr, and Fe. An exemplary spinel structure is nickel ferrite, which is an electrically conducting spinel having the stoichiometric composition NiFe₂O₄. In one embodiment, the performance of the spinel is improved by changing the ratio of Ni and Fe, such that the general formulation of the spinel is Ni_1-xFe_2+xO₄ or Ni_1+xFe_2-xO₄, wherein x ranges from 0 to 0.5.

[0057] In another embodiment, at least a portion of the component A and/or at least a portion of the component B of the spinel structure can be replaced with another component C and/or component D. In other words, some of component A, or all of component A, could be replaced with component C and/or component D; and some or component B, or all of component B, could be replaced with component C and/or component D. In an exemplary embodiment, component C includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, Cu, Mo, W, Cr and V; and component C is different from component A and B. Component D includes at least one of Al, Cr, Fe, Co, Ga and Mo; and component D is different from component A and B. Like the perovskite structures, the spinels can be substituted, in which case the general formulation would be M_xN_2-yO_4-z, wherein M comprises component A and at least one other metallic element; N comprises component B and at least one other metallic element; x ranges from -0.1 to 0.1; y ranges from -0.1 to 0.1; and z ranges from -0.2 to 0.2. In an exemplary embodiment, the at least one other metallic element of component M and/or component N is selected from the following group: Ge, V, Te, Ti, Sb, Nb, Ta, W, Sn, Hf, Zr, Sc, Bi, and In.

[0058] The ground firing tip 34 constructed of the perovskite structure or spinel structure is manufactured by compacting and sintering the ceramic material. In one embodiment, the ceramic material initially provided for compacting and sintering includes at least one of the perovskite structures or spinel structures described above.

[0059] In another embodiment, a precursor material is provided which upon sintering forms one of the perovskite structures or spinel structures. The precursor material typically includes common oxides and/or carbonates of the elements listed above. Exemplary precursor materials that can be compacted and sintered to form the ground firing tip 34 from a perovskite structure include at least one of La₂O₃, CaCO₃, BaCO₃, SrCO₃, Y₂O₃, Gd₂O₃, Sc₂O₃, TiO₂, ZrO₂, HfO₂, Nb₂O₅, Ta₂O₅, MoO₃, MO₂O₃, WO₃, ReO₃, V₂O₃, Cr₂O₃, MnO₂, Fe₂O₃, FeO, Fe₃O₄, RuO₄, CoO, NiO, and Ni₂O₃. Exemplary precursor materials that can be compacted and sintered to form the ground firing tip 34 from a spinel structure include at least one of Li₂CO₃, CoO, MgCO₃, MgO, ZnO, NiO, Ni₂O₃, FeO, Fe₂O₃, Fe₃O₄, CdO, MnO₂, CuO, Al₂O₃, Al(OH)₃ and Cr₂O₃.

[0060] Another aspect of the invention provides a method of forming the spark plug 20 described above. The method includes providing the electrode 22, 24 by compacting the ceramic material to form the firing tip 32, 34; sintering the compacted ceramic material; and disposing the firing tip 32, 34 on the body portion 28, 30, either before or after sintering. The method can include disposing the ceramic firing tip 32, 34 on the center electrode 22, the ground electrode 24, or both. In one embodiment, the method includes forming a hole 48, 80 along the center axis A, and disposing the firing tip 32, 34 in the hole 48, 80.

[0061] In another embodiment, the method of forming the spark plug 20 includes brazing the firing tip 32, 34 to the body portion 28, 30. As stated above, the brazing step can include using an active braze alloy, such as Ticusil, Gold-ABA, Gold-ABA-V, or other braze alloys provided by Wesgo Metals. Alternatively, the brazing can include reactive air brazing, which typically involves using a copper oxide-silver single phase liquid to join the metal of the body portion 28, 30 and the ceramic material of the firing tip 32, 34.

[0062] Alternatively, the method can include mechanically attaching the firing tip 32, 34 to the body portion 28, 30. A retaining element 52 can be used to attach the firing tip 32, 34 to the body portion 28, 30. In one embodiment, the method includes brazing or laser welding the retaining element 52 to the body portion 28, 30. In yet another embodiment, the firing tip 32, 34 is attached to the body portion 28, 30 by forming indentations 82, holes, grooves, or notches along sides of the firing tip 32, 34 adjacent the body portion 28, 30, heating, and melting a portion of the body portion 28, 30 at the firing end 42, 78 adjacent the holes. The body portion 28, 30 flows into the holes and solidifies, providing the melted portion 88 of Figure 9, securing the firing tip 32, 34 to the body portion 28, 30.

[0063] In one exemplary embodiment, the method first comprises compacting the ceramic material to form the firing tip 32, 34, wherein the ceramic material includes at least one of a perovskite structure, a spinel structure, and a precursor material that forms a perovskite or spinel structure upon sintering. The method further includes sintering the compacted ceramic material; and disposing the sintered ceramic material on the body portion 28, 30 including a thermally conductive material, either before or after the sintering step.

[0064] Obviously, many modifications and variations of the present invention are possible in light of the above teachings and may be practiced otherwise than as specifically described while within the scope of the appended claims. These antecedent recitations should be interpreted to cover any combination in which the inventive novelty exercises its utility. In addition, the reference numerals in the claims are merely for convenience and are not to be read in any way as limiting.

Claims

1. A spark plug (20) for igniting a mixture of fuel and air of an internal combustion engine, comprising:

an electrode (22, 24) having a body portion including a thermally conductive material;

said electrode (22, 24) having a firing tip (32, 34) disposed on said body portion (28, 30);

said firing tip (32, 34) including a ceramic material, and said ceramic material including at least one perovskite structure,

wherein the at least one perovskite structure includes the formulation ABO₃, wherein component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni; and at least a portion of component A and/or at least a portion of component B of the perovskite structure is replaced with component C and/or component D, wherein component C is different from components A and B and includes at least one of La, Ca, Ba, Sr, Y, and Gd; and component D is different from components A and B and includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni.

2. The spark plug (20) of claim 1, wherein at least 50 wt. % of said firing tip (32, 34) consists of the at least one perovskite structure.

3. The spark plug (20) of claim 1, wherein the at least one perovskite structure includes one of the following formulations: (A_xC_1-x)BO₃, A(B_yD_1-y)O₃, or (A_xB_1-x)(C_yD_1-y)O₃; wherein component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni; x is between 0 and 0.5; and y is between 0 and 0.5.

4. The spark plug (20) of claim 3, wherein the at least one perovskite structure includes La_1-xSr_xMnO₃.

5. The spark plug (20) of claim 1, wherein the at least one perovskite structure includes the formulation M_xN_1-yO_3-z, wherein component M comprises component A and at least one other metallic element; component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; component N comprises component B and at least one other metallic element; component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni; x ranges from 0.9 to 1.1; y ranges from 0.9 to 1.1; and z ranges from -0.2 to 0.2.

6. The spark plug (20) of claim 5, wherein the at least one other metallic element of component M includes at least one of La, Ca, Ba, Sr, Y, Gd, Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ni, Cu, Zn, Ag, Ga, Al, and Si; and the at least one other metallic element of component N includes at least one of La, Ca, Ba, Sr, Y, Gd, Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ni, Cu, Zn, Ag, Ga, Al, and Si.

7. The spark plug (20) of claim 6, wherein the at least one other metallic element of component M has a valence charge different from the valence charge of component A; and the at least one other metallic element of component N has a valence charge different from the valence charge of component B.

8. A spark plug (20) for igniting a mixture of fuel and air of an internal combustion engine, comprising:

an electrode (22, 24) having a body portion (28, 30) including a thermally conductive material;

said electrode (22, 24) having a firing tip (32, 34) disposed on said body portion (28, 30);

said firing tip (32, 34) including a ceramic material, and said ceramic material including at least one spinel structure,

wherein the spinel structure has the formulation AB₂O₄, wherein component A includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, and Cu; component B includes at least one of Al, Cr, and Fe; and at least a portion of component A and/or at least a portion of component B is replaced with component C and/or component D; wherein component C is different from component A and B and includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, Cu, Mo, W, Cr and V; and component D is different from component A and B and includes at least one of Al, Cr, Fe, Co, Ga and Mo..

9. The spark plug (20) of claim 8, wherein at least 50 wt. % of said firing tip consists of the at least one spinel structure.

10. The spark plug (20) of claim 8, wherein the spinel structure is nickel ferrite having the formulation Ni_1-xFe_2+xO₄ or Ni_1+xFe_2-xO₄; and x ranges from 0 to 0.5.

11. The spark plug (20) of claim 10, wherein the nickel ferrite has the formulation NiFe₂O₄.

12. The spark plug (20) of claim 8, wherein the spinel structure has the formulation M_xN_2-yO_4-z, wherein component M comprises component A and at least one other metallic element; component N comprises component B and at least one other metallic element; x ranges from -0.1 to 0.1; y ranges from -0.1 to 0.1; and z ranges from -0.2 to 0.2.

13. The spark plug (20) of claim 12, wherein the at least one other metallic element of M is selected from the following group: Ge, V, Te, Ti, Sb, Nb, Ta, W, Sn, Hf, Zr, Sc, Bi, and In; and the at least one other metallic element of N is selected from the following group: Ge, V, Te, Ti, Sb, Nb, Ta, W, Sn, Hf, Zr, Sc, Bi, and In.

14. An electrode (22, 24) for an ignition device (20), comprising:

a body portion (28, 30) including a thermally conductive material;

a firing tip (32, 34) disposed on said body portion (28, 30);

said firing tip (32, 34) including a ceramic material, and said ceramic material including at least one of a perovskite structure and a spinel structure,

wherein the perovskite structure includes the formulation ABO₃, wherein component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni; and at least a portion of component A and/or at least a portion of component B of the perovskite structure is replaced with component C and/or component D, wherein component C is different from components A and B and includes at least one of La, Ca, Ba, Sr, Y, and Gd; and component D is different from components A and B and includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni., wherein at least a portion of component A and/or at least a portion of component B of the perovskite structure is replaced with component C and/or component D,

and wherein the spinel structure has the formulation AB₂O₄, wherein component A includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, and Cu; component B includes at least one of Al, Cr, and Fe; and at least a portion of component A and/or at least a portion of component B is replaced with component C and/or component D; wherein component C is different from component A and B and includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, Cu, Mo, W, Cr and V; and component D is different from component A and B and includes at least one of Al, Cr, Fe, Co, Ga and Mo.

15. A method of manufacturing an electrode (22, 24) for an ignition device (20), comprising the steps of:

compacting a ceramic material to form a firing tip, wherein the ceramic material includes at least one of a perovskite structure, a spinel structure, and a precursor material that forms a perovskite or spinel structure upon sintering;

sintering the compacted ceramic material; and

disposing the sintered ceramic material on a body portion including a thermally conductive material,

wherein the perovskite structure includes the formulation ABO₃, wherein component A includes at least one of La, Ca, Ba, Sr, Y, and Gd; component B includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni; and at least a portion of component A and/or at least a portion of component B of the perovskite structure is replaced with component C and/or component D, wherein component C is different from components A and B and includes at least one of La, Ca, Ba, Sr, Y, and Gd; and component D is different from components A and B and includes at least one of Sc, Ti, Zr, Hf, Nb, Ta, Mo, W, Re, V, Cr, Mn, Tc, Fe, Ru, Co, Rh, Ga, and Ni., wherein at least a portion of component A and/or at least a portion of component B of the perovskite structure is replaced with component C and/or component D,

and wherein the spinel structure has the formulation AB₂O₄, wherein component A includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, and Cu; component B includes at least one of Al, Cr, and Fe; and at least a portion of component A and/or at least a portion of component B is replaced with component C and/or component D; wherein component C is different from component A and B and includes at least one of Li, Co, Mg, Zn, Ni, Fe, Cd, Mn, Cu, Mo, W, Cr and V; and component D is different from component A and B and includes at least one of Al, Cr, Fe, Co, Ga and Mo.

Drawing