|Publication number||US3875477 A|
|Publication date||Apr 1, 1975|
|Filing date||Apr 23, 1974|
|Priority date||Apr 23, 1974|
|Also published as||CA1064248A, CA1064248A1|
|Publication number||US 3875477 A, US 3875477A, US-A-3875477, US3875477 A, US3875477A|
|Inventors||John I Fredriksson, Samuel H Coes|
|Original Assignee||Norton Co|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (11), Referenced by (68), Classifications (25)|
|External Links: USPTO, USPTO Assignment, Espacenet|
United States Patent 1191 Fredriksson et al.
1 SILICON CARBIDE RESISTANCE IGNITER  Inventors: John I. Fredriksson, Holden; Samuel H. Coes. Northboro, both of Mass.
 Int. Cl. F23q 7/10  Field of Search 317/79, 80, 81. 98; 219/264, 270, 552, 553; 338/22. 262. 330;
[ Apr. 1, 1975 3.454.345 7/1969 Dyre 431/66 3.467.312 9/1969 Terrell 317/93 x 3.502.419 3/1970 Perl...; 431/66 3.597.139 8/1971 Elders 431/66 3.681.737 8/1972 Magnussoti 61 219/553 x Primary Examiner-volodymyr Y. Mayewsky Attorney. Agent, or Firm-Arthur A. Loiselle, Jr.
 ABSTRACT A monolithic ceramic resistance igniter of simple configuration is composed essentially of polycrystalline silicon carbide adapted for use in gas and liquid fuel burning systems. As a result of the combination of its sintered silicon carbide composition, its microstructure, controlled density and lar e cross-sectional area, the igniter possesses an unusual y high degree of physical ruggedness. The igniter will attain a temperature of about 1,000C in well under 20 seconds drawing a maximum of 6 amps at 132 volts, with a room temperature resistivity of 0. 10 to 1.70 ohm centimeters and a resistivity at about 1000C of from 0.06 to 0.26 ohm centimeter. The igniter also has a physical construction such that a high percentage of its hot surface area 12 Claims, 3 Drawing Figures  References Cited UNITED STATES PATENTS 1.906.963 5/1933 Hcyroth 338/330 2.001.297 5/1935 Boyles 338/330 2.735.881 2/1956 Mann..... 13/25 2.933.896 4/1960 Ferrie 431/262 X 3.282.324 11/1966 Romanelli 317/98 x 'adlates d'rwly the env'ronmen" 3372.305 3/1968 MlkUICC 317/98 SILICON CARBIDE RESISTANCE IGNITER BACKGROUND OF THE INVENTION The invention relates to igniters for fuel burning devices such as domestic and industrial liquid fuel and gas burning appliances. More particularly. the invention relates to ceramic resistance igniters for gas burning appliances such as kitchen ranges, furnaces, clothes dryers and the like.
The concept of non-pilot light igniters has been known for years. The earlier type of igniter was the incandescent wire device such as an electrically heated platinum wire coil. These are fragile and, in most applications, require a step-down transformer. Ceramic resistance igniters made their appearance in about l937. U.S. Pat. No. 2,089,394 describes a total electrical ignition system in which a ceramic resistance igniter composed of Durhy Material" is utilized to ignite a fluid fuel system. Durhy is a dense sintered silicon carbide impregnated with silicon. A U-shaped ceramic igniter is disclosed in U.S. Pat. No. 2,095,253 where the igniter is composed of sintered and silicon impregnated silicon carbide. This igniter element is formed by first performing l grit (142 microns) and finer silicon carbide material, into rods of suitable length, which are then fired to presinter the silicon carbide. The rods are then cut into the desired length and slotted to form a U-shaped element which is subsequently impregnated with silicon metal. Another basic type of silicon carbide igniter is that described in U.S. Pat. No. 3,052,8l4. This is a sparkplug type igniter as opposed to the pure resistance type mentioned above and is composed of silicon nitride bonded with silicon carbide. Still another silicon carbide igniter device is described in U.S. Pat. No. 3,282,324 as part of a complete ignition and heat injection system. ln this case the silicon carbide is a sintered silicon carbide cylinder having a spiral cut which provides a relatively small percentage of the hot area which radiates directly to the environment.
By nature of their use, resistance igniters must be small in dimension, particularly in terms of their crosssection and overall length. Because of these physical parameter restrictions, prior art silicon carbide igniters are very fragile. As a result, attempts have been made to physically reinforce ceramic resistance igniters by such approaches as that described in U.S. Pat. Nos. 3,372,305 and 3,467,8l2. Both of these igniters have a spiral configuration which is fabricated of a sintered tube of silicon carbide which is made as dense as possible. The spiral configuration is cut in the sintered silicon carbide tube, which is then supported by an aluminum oxide rod which passes through the opening of the spiral igniter body.
Still another type of resistance igniter is described in US. Pat. No. 3,454,345. This igniter is composed ofa sintered mixture of silicon carbide and silicon oxynitride wherein the silicon oxynitride functions as a bond for a relatively coarse lOF silicon carbide, i.e., a mixture of particles of 1,340 microns and finer in size with 10 percent by weight of silicon oxynitride. This silicon carbide/silicon oxynitride mixture is one manufactured and sold by the Norton Company, Worcester, Mass, and its foreign affiliates under the trademark CRYS- TOLON 63.
Despite the substantial amount of activity in the ceramic resistance igniter field, the igniters enjoying most widespread use today, for most applications, are still of the pilot light type. In view of the current energy crisis and the result of various surveys which show that pilot lights consume from l0 to 15 percent of the total gas consumed in this country, there is obviously a compelling need for an igniter to replace the presently used pilot light.
It is, therefore, a principal object of the present invention to provide a ceramic resistance igniter for liquid and gas fuel burning devices which is free of the foregoing deficiencies, and which is physically rugged, heats rapidly, survives hundreds of thousands of heating cycles, is simple electrically and structurally, has low susceptibility to premature burn out, and radiates primarily to the environment.
SUMMARY OF THE INVENTION Compositionally the ceramic igniter of the present invention consists of to 99.9 percent by weight of alpha silicon carbide, 0.05 to 0.50 percent by weight of aluminum, 0 to 4 percent by weight silica, 0 to 0.25 percent by weight of iron or iron-based compounds, a maximum of lOO parts per million of boron and a minor amount, generally not in excess of 0.25 percent, of miscellaneous impurities. The composition also contains a very small (on the order of 500 ppm) amount of nitrogen which is introduced into the silicon carbide by a doping process which will be described in more detail subsequently. The small amount of aluminum incorporated in the SiC is necessary to raise the high temperature (e.g. l,000C) resistivity of the igniter to a level on the order of 0.06 to 0.26 ohm centimeters. The boron content is preferably kept below 50 ppm to maintain reasonably low resistivity at both low and high temperatures, the low resistivity at room temperature being particularly important from the standpoint of heat up time.
The igniter shape is formed by conventional methods which result in said igniter having a controlled density of from about 2.60 to 2.70 grams per cubic centimeter. This controlled density has the advantage of producing a silicon carbide resistor with a higher resistivity than a more dense silicon carbide. thus facilitating the formation of an igniter with the required resistance, but with a relatively short electrical path. The importance of this latter feature relates to the fact that igniters generally are used in very limited spaces, therefore, must be small in size. The high resistivity of the controlled density igniters of the invention greatly facilitates this objective. As a result of the composition, density, and the processing employed, the resulting silicon carbide igniter is ideally suited as a fuel igniter for such devices as gas clothes dryers, in that the stringent requirements for such igniters are easily satisfied by the igniters of the invention. To be acceptable for such end uses, the igniter must have sufficient mechanical strength to resist severe physical forces; the present igniter will withstand a whipping type force of at least gs. Such an igniter must also be able to attain a temperature of about l,000C in less than 20 seconds while drawing a maximum of 6 amps at 132 volts, and in less than 60 seconds at an input of 80 volts; the present igniter easily satisfies these requrements by virtue of a room temperature resistivity of 0.l0 to L70 ohm centimeters, and a resistivity at approximately l,000C of 0.06 to 0.26 ohm centimeter. Its overall physical dimensions for gas fired clothes dryers and ranges is from 2.125 to 2.625 inches in length, with an effective cross-section of from 0.012 to 0.072 square inch. Finally, the present igniter has an inherent ability to withstand at least 200,000 heat-up and cool-down cycles. This is unexpected in view of the relatively low density of the igniter, but it is believed that this results from a combination of chemical composition, processing conditions involved in the fabrication of said igniter, and the high percentage of the heating area which radiates directly to the environment. By the expression area which radiates directly to the environment we mean hot area that does not see" other hot areas. Thus the inside surface of a cylindrical heating element would see other hot portions of the inside surface (or a hot support element) and would not be considered as radiating directly to the environment." The hot" area of the igniter of FIG. I is the surface of that part of the element of smallest cross-section, that is the portion of 8a, 8b, a, and 10b of minimum cross-section. In FIG. 2, about 55% of the surface of the hot area is outside" surface. To keep the outside surface above 50%, the thickness of the igniter should not be greater than twice the width of the legs. From the design of FIG. 3, the outside area will always be greater than 50%.
The present igniter is monolithic and self-supporting, needing no supporting device such as that required for the successful utilization of the silicon carbide igniter of US. Pat. Nos. 3,372,305 and 3,467,812. This results from the relatively great thickness, i.e., cross-sectional area of the present igniters as set forth above. The most desirable configuration is that of a leg having a hairpin shape including terminal connecting ends, because this shape presents at least 50 percent of the surface area of the hot zone of the igniter to the surrounding environment. With a high percentage of the heating area radiating outward, there is less tendency for hot spots to develop. This characteristic, plus the relatively large cross-section, minimizes premature burn out. It is even more desirable that the igniter be made of two legs of hairpin configuration to maximize the igniters ability to quickly ignite a fuel exposed thereto.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a longitudinal view of the largest surface area of the igniter of the present invention.
FIG. 2 is a sectional view of the igniter of FIG. 1.
FIG. 3 is a longitudinal view of the largest surface area of another embodiment of the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS The preferred physical configuration of the instant igniter is shown in FIGS. 1 and 2. Referring to FIG. 1 the wing shaped elements 4 and 6 are terminal connect ing ends. Coextensive with the terminal connecting ends and with each other are two hairpin shaped legs 8 and I0. The double hairpin configuration is completed by the approximately centrally located slot 12 which traverses from the end of the igniter opposite the terminal connecting ends towards said ends but stopping substantially short thereof; and a slot in each leg 8 and 10 identified as 14 and 16 respectively in FIG. 1. The electrical path begins at the terminal connecting ends 4 and 6 and traverses the legs through a substantial part of their length, forming two elements 8a, 8b and Illa and 10b for each leg. In the slots I4 and 16 at the terminal connecting ends thereof it is desirable, although not absolutely necessary, to include a portion of an electrically insulating cement such as a commercially available alumina based refractory cement. This is shown as small dabs l8 and 20. Larger quantities of refractory cement may be used if desired. Without the portion of cement so located in slots 14 and 16 there is the danger of shorting out or breaking of the igniter should any force be exerted on the terminal connecting ends 4 and 6 so as to force said ends toward one another. The ends or tips 22 and 24 of legs 8 and 10 respectively have a larger cross-section than the crosssection of their individual elements 80, 8b, 10a and 10b. This larger cross-sectional area of these ends causes them to remain relatively cool and causes concentration of the hot zone of the igniter in those portions of the two legs in between these ends 22 and 24 and the terminal connecting ends 4 and 6. This configuration exposes, for direct radiation to its environment, at least 50% of the total surface area of the igniters hot zone. In calculating the area of hot zone which radiates directly to the environment in FIGS. 1 and 2 the upper and lower surfaces (those parallel to the plane of the drawing) and the outer boundaries of the element would be considered as the applicable areas. The surfaces of the element defining the slots would not be so considered since they can radiate directly to their hotfacing surfaces.
In a preferred form for gas dryers the present igniter is from 2.125 to 2.625 inches in length, with the end 22 and 24 of the legs 8 and 10 each having an essentially rectangular cross-sectional area of from 0.020 to 0.039 square inch. Elements 8a, 8b, 10a and 10b of legs 8 and 10 each preferably have a cross-section of from 0.009 to 0.014 square inch, the slots forming said elements are preferably from 0.033 to 0.080 inch wide. There are many possible variants on the basic configuration of the present igniter, one such being that shown in Fig. 3 which has terminal connecting ends 26 and 28 and a single hairpin shaped leg 30 comprised of elements 30a and 30b, slot 32. Insulating cement 34, is included between the terminal connecting ends 26 and 28. The end 36 has a slightly larger cross-sectional area than elements 30a and 30b of leg 30.
In one method of forming the present igniters a casting slip is prepared having the preferred composition of 97 to 99.9% by weight of a 50% mixture of high purity 3.0 micron silicon carbide and IOOF silicon carbide, and 0.05 to 0.30% by weight of A1 0 The preparation of the slip, and the casting thereof into plaster molds, is taught in US. Pat. No. 2,964,823. The mold cavity has a cross-sectional configuration and dimensions corresponding to the outline of the igniter shown in FIG. 1 or FIG. 3. The length of the mold cavity is 12 inches although obviously said dimension could be longer or shorter if desired. The green billet thus cast is allowed to stand in the mold for 10 to 15 minutes after which it is removed and air dried for 8 to l6 hours at to C. To facilitate slicing of the billet into igniter blanks, the billet is impregnated with a 25% solution in isopropyl alcohol of a mixture of I00 parts by weight of Fapreg P3 and 2 parts by weight of Activator, both materials manufactured and sold by Quaker Oats Company. Other polymerizable organic material may also be used in place of the foregoing. The impregnation is carried out by immersion of the green billet in the solu tion. The saturated billet is heat treated at about 95C for at least l2 hours after which temperature is raised to about 190C and held there for 2 hours. The billet is then allowed to cool.
The billet is sliced into igniter blanks preferably about 0.135 inch in thickness. The slicing is best accomplished with a diamond cut-off wheel. The three slots 12, 14 and 16 of FIG. 1 are cut into the blanks, again with a diamond cut-off wheel.
The green igniters are placed in a graphite holder and fired at 2,200 to 2,450C in a reducing atmosphere for A to 4 hours. The fired igniters are subjected to a subsequent firing, in nitrogen, at 1,500 to 2,000C for to 180 minutes, maintaining the nitrogen environment until the temperature in the furnace has dropped to 800C.
The terminal connecting ends 4 and 6 in FIG. I are then coated with a metal, preferably aluminum or an aluminum alloy. This may be accomplished by any known method such as dipping of the ends into molten metal or flame spraying. The ends should also be sandblasted lightly prior to applying the metal coating.
The final step in the fabrication of the present igniter is the placing of the refractory, electrically insulating cement, l8 and 19 in FIG. I. The cement may be essentially and refractory, electrically insulating cement but the preferred cement is the high alumina type. The quantity of cement required, for the purposes stated above, is small e.g. an amount of cement to fill the slots 14 and 16 of FIG. 1, approximately A inch in from the far edge ofthe terminal connecting ends. The slots may be filled further, if desired.
For optimum performance the igniter should be composed of from 97 to 99.9% by weight of polycrystalline silicon carbide, 0.1 to 0.3% by weight of aluminum added as aluminum oxide in the original mixture, less than 50 parts per million of boron, and not more than 0.20% of miscellaneous impurities. It would also appear that an indeterminate amount ofnitrogen must be introduced into the structure by subjecting the initial green igniters first to a standard non-oxidizing type of firing step at about 2,200C or above, followed by firing in a nitrogen atmosphere at l,500 to 2,000C. Attempts to combine these two steps into one fail to affect the desired electrical properties in the final igniter. This is believed to be due to the different rates of N diffusion into the SiC crystals at the two different temperatures. When N, is present during the initial high temperature firing (2,200 to 2,400C) it diffuses in sufficient quantities into the body of the SiC so that bulk SiC has a low resistivity both at room and high temperatures thus providing too much current flow at the high temperature (over 6 amps at 132 volts). It is believed that when the igniter is fired in nitrogen at the lower temperature (l,500 to 2,000C) a small but sufficient amount of nitrogen diffuses into the surface of the fine silicon carbide particles, which bridge the larger particles, to lower the room temperature resistivity of the igniter without significantly affecting the high temperature resistivity. As a result this added N lowers the igniter response time, e.g., the time for the igniter to reach the desired fuel ignition temperature.
Some prior art gas and liquid fuel igniters have the inherent shortcoming of room temperature resistivities that are too high, and elevated temperature resistivities that are too low for the most effective and efficient op eration. The igniter of the present invention is free of this problem having a preferred resistivity at room temperature of from 0.15 to 0.5 ohm centimeter and at about 1,000C of at least 0.1 ohm centimeter, resulting in a response time at volts of 10 to 60 seconds to attain approximately 1,000C.
This unique set of resistivities results primarily from the combination of the introduction of the prescribed amount of aluminum into the crystal lattice of the silicon carbide, and the post-firing nitrogen treatment which introduces a relatively high percentage of nitrogen into the crystal lattice of the finer silicon carbide grains. This same treatment (it is believed) introduces only a very small percentage of nitrogen into the crystal lattice of the larger SiC crystals. The effect of the presence of aluminum is to increase the resistivity of the body, both at room temperature and at elevated tern perature; the latter is desirable but the former is not. The nitrogen treatment subsequent to the initial firing reverses or compensates for the undesirable increase in the room temperature resistivity caused by the introduction of the aluminum, i.e., the nitrogen decreases the room temperature resistivity. The resulting igniter thus has a heretofore unknown combination of a relatively high elevated temperature resistivity and a low room temperature resistivity.
The oxygen content of the finished igniter is between about 0.04 to 0.1%. After use the oxygen content will increase substantially due to surface oxidation of the silicon carbide grains. This additional oxygen is not detrimental so long, as it is on the surface of the fired igniter and not between the SiC grains of the igniter where it would introduce a high resistance. In some cases it may be desirable to oxidize the igniters prior to sale or to apply an oxide coating on the finished igniter; these techniques are known in the art.
Where the expression percent or 7r is used in the specification and claims it is intended to mean weight percent unless clearly stated to have some other meaning.
What is claimed is:
l. A ceramic resistance igniter, comprised of a pair of terminal connecting ends and a hot-zone extending therefrom and having a composition consisting essentially of from to 99.9% by weight of silicon carbide, 0.05 to 0.50% by weight of aluminum, 0 to 4% by weight of silicon oxide, 0 to 0.25% by weight if iron or compounds thereof, a maximum of parts per million of boron, and up to 0.25% by weight of miscellaneous impurities, said composition having been sintered and then exposed to a nitrogen atmosphere at a temperature of from l,500C to 2,000C for 15 to 180 minutes.
2. The ceramic resistance igniter of claim 1 having electrical characteristics such that said igniter draws a maximum of 6 amps at 132 volts and has an impact resistance of at least gs.
3. The ceramic resistance igniter of claim 2 having a response time at 80 volts of 60 seconds or less to attain 1,000C and an operational life of at least 200,000 cycles.
4. A monolithic ceramic resistance igniter, comprised of a pair of terminal connecting ends and a hotzone extending therefrom and having a composition consisting essentially of from 95 to 99.9% by weight of polycrystalline silicon carbide, 0 to 4% by weight of silicon oxide, 0 to 0.25% by weight of iron or compounds thereof, 0 to 50 parts per million of boron, and up to 0.25% by weight of miscellaneous impurities; said silicon carbide containing from 0.05 to 0.50% by weight of aluminum in the crystal lattice thereof and nitrogen being introduced into said crystal lattice by subjecting said composition to an atmosphere of nitrogen at a temperature of from 1,500C to 2,000C for 15 to 180 minutes.
5. The ceramic resistance igniter of claim 4 having a room temperature resistivity of 0. 10 to 1.70 ohm centimeters and a resistivity at l,000C ot0.06 to 026 ohm centimeter.
6. A sintered ceramic resistance igniter, comprised of a pair of terminal connecting ends and a hot-zone extending therefrom and having a composition consisting essentially of from 97 to 99.9% by weight of polycrystalline silicon carbide, 0.1 to 0.3% by weight of aluminum contained in the crystal lattice of said silicon carbide, to 100 parts per million of boron, and from 0 to 0.2% by weight of miscellaneous impurities, said composition having been doped with nitrogen by heating at 1,500C to 2,000C for 15 to 180 minutes; said ceramic igniter having a room temperature resistivity of 0.15 to 0.5 ohm centimeter, a resistivity at l,800F of at least 0.1 ohm centimeter. a response time of to 60 seconds to attain 1,000C, an operational life of at least 200,000 cycles, an impact resistance of at least 125 gs, and the further property that said igniter draws a maximum of 6 amps at 132 volts.
7. A sintered ceramic resistance igniter, comprised of a pair of terminal connecting ends and a hot-zone extending therefrom and having a composition consisting essentially of from 95 to 99.9% by weight of polycrystalline alpha silicon carbide, 0 to 4% by weight of silicon oxide, 0 to 100 parts per million of boron, 0.05 to 0.5% by weight of aluminum, said composition having first been preformed and fired at 2,250C to 2,450C in an inert atmosphere followed by firing in a nitrogen atmosphere at from 1,500C to 2,000C for to 180 minutes; said igniter having a density of 2.60 to 2.70 gms/cc. and having resistivity at room temperature of from 0.10 to 1.70 ohm centimeters and at l,000C of from 0.06 to 0.26 ohm centimeter.
8. A sintered ceramic resistance igniter, comprised of a pair of terminal connecting ends and a hot-zone extending therefrom and having a composition consisting essentially of from to 99.9% by weight of polycrystalline alpha silicon carbide, 0 to 4% by weight of silicon oxide, 0 to parts per million of boron, 0.05 to 0.5% by weight of aluminum, said igniter having a density of 2.60 to 2.70 gms/cc, having resistivity at room temperature of from 0.10 to 1.70 ohm centimeters and at 1,000C of from 0.06 to 0.26 ohm centimeter, and having at least 50% of the surface area of the hot zone of the igniter radiating directly to the environment.
9. A ceramic resistance igniter, comprised of a pair of terminal connecting ends and a hot-zone extending therefrom and having a composition consisting of from 95 to 99.9% by weight of silicon carbide, 0.05 to 0.5% by weight of aluminum, 0.04 to 0.1% by weight of oxygen, 0 to 4% by weight of silicon oxide, 0 to 0.25% by weight of iron or compounds thereof, a maximum of 100 parts per million of boron, said composition having been exposed to a nitrogen atmosphere at a temperature of from 1,500C to 2,000C for 15 to 180 minutes.
10. The ceramic resistance igniter of claim 9 wherein said ends having been treated with an aluminum alloy.
11. A monolithic ceramic resistance igniter having a flat elongated configuration essentially rectangular in cross-section, including terminal connecting means at one end, a hot zone extending therefrom comprised of at least one leg having a hairpin shape, where the end of said leg opposite the terminal connecting ends has a greater cross-section than the cross-section of the individual elements making up said hairpin shaped leg, and having at least 50% of the surface area of said hot zone radiating directly to the environment.
12. The monolithic ceramic resistance igniter of claim 11 comprised of polycrystalline silicon carbide and consisting of two interconnected hairpin shaped legs, the overall length of said igniter being from 2.125 to 2.625 inches, the ends of said legs opposite the terminal connecting ends having a cross-sectional area of from 0.013 to 0.049 square inch, the elements of said hairpin shaped legs having a cross-section of from 0.006 to 0.018 square inch, and the width of the slots separating said elements being from 0.012 to 0.080
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US1906963 *||Nov 17, 1931||May 2, 1933||Globar Corp||Impregnated silicon carbide article and the manufacture thereof|
|US2001297 *||Dec 19, 1931||May 14, 1935||Heating Unit Corp||Electrical resistance unit|
|US2735881 *||Dec 27, 1952||Feb 21, 1956||Metal-impregnated heating rods for electric|
|US2933896 *||Jun 4, 1956||Apr 26, 1960||Snecma||Ignition devices for combustion chambers|
|US3282324 *||Oct 11, 1965||Nov 1, 1966||Ram Domestic Products Company||Automatic fuel ignition and heat detection system|
|US3372305 *||Apr 15, 1966||Mar 5, 1968||Carborundum Co||Silicon carbide igniter|
|US3454345 *||Mar 2, 1967||Jul 8, 1969||Danfoss As||Fuel igniting and flame sensing resistor with fuel feed control|
|US3467812 *||Mar 29, 1967||Sep 16, 1969||Carborundum Co||Igniter-thermistor assembly|
|US3502419 *||Nov 3, 1967||Mar 24, 1970||Tappan Co The||Flame-proving ignition system for gas burners|
|US3597139 *||Jul 9, 1969||Aug 3, 1971||Whirlpool Co||Dual coil gas burner control circuit|
|US3681737 *||May 18, 1970||Aug 1, 1972||Bengt Magnusson||Electric resistance heater|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US4001145 *||Nov 18, 1974||Jan 4, 1977||Ngk Spark Plug Co., Ltd.||Glassy resistor composition for use in a resistor incorporated spark plug|
|US4006106 *||Sep 29, 1975||Feb 1, 1977||Ngk Spark Plug Co., Ltd.||Self sealable glassy resistor composition for a resistor sealed spark plug|
|US4120827 *||Mar 12, 1976||Oct 17, 1978||The Carborundum Company||Fuel igniter comprising a novel silicon carbide composition and process for preparing the composition|
|US4205363 *||Jun 29, 1978||May 27, 1980||The Carborundum Company||Fuel ignitor comprising a novel silicon carbide composition|
|US4241292 *||Oct 20, 1978||Dec 23, 1980||Sanders Associates, Inc.||Resistive heater|
|US4302659 *||Feb 15, 1980||Nov 24, 1981||Kabushiki Kaisha Tokai Rika Denki Seisakusho||Ceramic heater-element to be used for cigarette-lighters|
|US4326039 *||Jun 25, 1980||Apr 20, 1982||Elektroschmelzwerk Kempten Gmbh||Dense shaped articles of polycrystalline β-silicon carbide and process for the manufacture thereof by hot-pressing|
|US4328529 *||Sep 27, 1979||May 4, 1982||Emerson Electric Co.||Silicon carbide igniters|
|US4337498 *||Sep 5, 1980||Jun 29, 1982||Tokai Konetsu Kogyo Co., Ltd.||Small ignition device comprising string-like silicon carbide heating element affixed to terminal supports|
|US4433233 *||Oct 23, 1981||Feb 21, 1984||Emerson Electric Co.||Silicon carbide heating elements|
|US4443361 *||Apr 1, 1983||Apr 17, 1984||Emerson Electric Co.||Silicon carbide resistance element|
|US4475029 *||Mar 1, 1983||Oct 2, 1984||Nippondenso Co., Ltd.||Ceramic heater|
|US4475030 *||Sep 25, 1981||Oct 2, 1984||Caterpillar Tractor Co.||Glow plug having resiliently mounted ceramic surface-ignition element|
|US4486651 *||Jan 24, 1983||Dec 4, 1984||Nippon Soken, Inc.||Ceramic heater|
|US4499366 *||Nov 21, 1983||Feb 12, 1985||Nippondenso Co., Ltd.||Ceramic heater device|
|US4633064 *||May 30, 1985||Dec 30, 1986||Nippondenso Co., Ltd.||Sintered ceramic electric heater with improved thermal shock resistance|
|US4634837 *||Mar 29, 1985||Jan 6, 1987||Nippon Soken, Inc.||Sintered ceramic heater element|
|US4644133 *||Feb 25, 1986||Feb 17, 1987||Nippondenso Co., Ltd.||Ceramic heater|
|US4671058 *||Nov 15, 1984||Jun 9, 1987||Nippondenso Co., Ltd.||Heating device|
|US4723069 *||Sep 16, 1986||Feb 2, 1988||Toyota Jidosha Kabushiki Kaisha||Ceramic heater|
|US4741692 *||Oct 1, 1985||May 3, 1988||Babcock-Hitachi Kabushiki Kaisha||Burner igniter with a ceramic heater|
|US4864186 *||Mar 29, 1988||Sep 5, 1989||Milewski John V||Single crystal whisker electric light filament|
|US4935118 *||Mar 21, 1986||Jun 19, 1990||Norton Company||Self heated sensor package|
|US5045237 *||Oct 14, 1988||Sep 3, 1991||Norton Company||Refractory electrical device|
|US5085804 *||Feb 25, 1991||Feb 4, 1992||Norton Company||Refractory electrical device|
|US5191508 *||May 18, 1992||Mar 2, 1993||Norton Company||Ceramic igniters and process for making same|
|US5322824 *||May 27, 1993||Jun 21, 1994||Chia Kai Y||Electrically conductive high strength dense ceramic|
|US5391075 *||Jul 9, 1993||Feb 21, 1995||Robinson; Edgar C.||Multi-fuel burner|
|US5527180 *||Jul 11, 1994||Jun 18, 1996||International Thermal Investments Ltd.||Infrared burner|
|US5785911 *||Jun 7, 1995||Jul 28, 1998||Saint-Gobain/Norton Industrial Ceramics Corp.||Method of forming ceramic igniters|
|US5786565 *||Jan 27, 1997||Jul 28, 1998||Saint-Gobain/Norton Industrial Ceramics Corporation||Match head ceramic igniter and method of using same|
|US6078028 *||Feb 19, 1999||Jun 20, 2000||Saint-Gobain Industrial Ceramics, Inc.||Solderless ceramic igniter having a leadframe attachment|
|US6085738 *||Feb 21, 1995||Jul 11, 2000||International Thermal Investments Ltd.||Multi-fuel burner and heat exchanger|
|US6297183||Jul 28, 1999||Oct 2, 2001||Saint-Gobain Ceramics And Plastics, Inc.||Aging resistant porous silicon carbide ceramic igniter|
|US6562745||Jul 24, 2001||May 13, 2003||Saint-Gobain Ceramics And Plastics, Inc.||Aging resistant, porous silicon Carbide ceramic igniter|
|US6582629||Dec 20, 1999||Jun 24, 2003||Saint-Gobain Ceramics And Plastics, Inc.||Compositions for ceramic igniters|
|US6616890 *||Jun 15, 2001||Sep 9, 2003||Harvest Precision Components, Inc.||Fabrication of an electrically conductive silicon carbide article|
|US6759624 *||May 7, 2002||Jul 6, 2004||Ananda H. Kumar||Method and apparatus for heating a semiconductor wafer plasma reactor vacuum chamber|
|US6777650||Feb 4, 2000||Aug 17, 2004||Saint-Gobtain Industrial Ceramics, Inc.||Igniter shields|
|US7061363 *||Apr 11, 2003||Jun 13, 2006||Robert Bosch Gmbh||Passive, high-temperature-resistant resistor element for measuring temperature in passenger and commercial vehicles|
|US7195722||Mar 19, 2003||Mar 27, 2007||Saint-Gobain Ceramics And Plastics, Inc.||Compositions for ceramic igniters|
|US7342201 *||Nov 25, 2000||Mar 11, 2008||Nanogate Ag||Silcon carbide element|
|US7759618||Jul 16, 2004||Jul 20, 2010||Sandvik Materials Technology Uk Limited||Silicon carbide heating elements|
|US8133430 *||Aug 4, 2010||Mar 13, 2012||Surface Igniter Llc||Methods for fabricating polycrystalline SiC electrical devices|
|US8434292 *||Dec 17, 2007||May 7, 2013||State Of Franklin Innovations, Llc||Ceramic-encased hot surface igniter system for jet engines|
|US8678270 *||Mar 15, 2012||Mar 25, 2014||Delphi Technologies, Inc.||Hot zone igniter|
|US20030160220 *||Mar 19, 2003||Aug 28, 2003||Saint-Gobain Industrial Ceramics, Inc.||Compositions for ceramic igniters|
|US20030189036 *||Feb 26, 2003||Oct 9, 2003||Lg Electronics Inc.||Silicon carbide electric heating element|
|US20040021548 *||Apr 11, 2003||Feb 5, 2004||Albrecht Geissinger||Passive, high-temperature-resistant resistor element for measuring temperature in passenger and commercial vehicles|
|US20060198420 *||Jul 16, 2004||Sep 7, 2006||Beatson John G||Silicon carbide heating elements|
|US20080141651 *||Dec 17, 2007||Jun 19, 2008||Eason Martin P||Ceramic-encased hot surface igniter system for jet engines|
|US20110089161 *||Jun 3, 2009||Apr 21, 2011||Sandvik Materials Technology Uk Limited||Electrical Resistance Heating Element|
|US20110148011 *||Aug 4, 2010||Jun 23, 2011||Colopy Curtis M||Polycrystalline sic electrical devices and methods for fabricating the same|
|US20120175405 *||Mar 15, 2012||Jul 12, 2012||Delphi Technologies, Inc.||Hot zone igniter|
|DE3233319A1 *||Sep 8, 1982||Mar 8, 1984||Webasto Werk Baier Kg W||Verdampfungsbrenner|
|DE3235841A1 *||Sep 28, 1982||Apr 21, 1983||Norton Co||Poroeser feuerfester gegenstand mit einer oxidations-schutzschicht|
|EP1407192A2 *||Jun 12, 2002||Apr 14, 2004||Harvest Precision Components, Inc.||Fabrication of an electrically conductive silicon carbide article|
|EP1407192A4 *||Jun 12, 2002||Aug 25, 2004||Harvest Prec Components Inc||Fabrication of an electrically conductive silicon carbide article|
|EP1812754A2 *||Oct 28, 2005||Aug 1, 2007||SAINT-GOBAIN CERAMICS & PLASTICS, INC.||Ceramic igniter|
|EP1812754A4 *||Oct 28, 2005||Feb 22, 2012||Saint Gobain Ceramics||Ceramic igniter|
|WO1986005882A1 *||Mar 24, 1986||Oct 9, 1986||Norton Company||Self heated sensor package|
|WO1996011361A1 *||Oct 5, 1995||Apr 18, 1996||Saint-Gobain/Norton Industrial Ceramics Corporation||High voltage ceramic igniter|
|WO1997045676A1||May 23, 1997||Dec 4, 1997||International Thermal Investments Ltd.||Multi-fuel burner with adjustable metering valve|
|WO2003017723A2||Aug 17, 2002||Feb 27, 2003||Saint-Gobain Ceramics & Plastics, Inc.||Ceramic igniters with sealed electrical contact portion|
|WO2003032367A2 *||Jun 12, 2002||Apr 17, 2003||Harvest Precision Components, Inc.||Fabrication of an electrically conductive silicon carbide article|
|WO2003032367A3 *||Jun 12, 2002||Jul 10, 2003||Harvest Prec Components Inc||Fabrication of an electrically conductive silicon carbide article|
|WO2016060975A1 *||Oct 12, 2015||Apr 21, 2016||Specialized Component Parts Limited, Inc.||Hot surface igniters and methods of making same|
|WO2016097661A1||Dec 18, 2015||Jun 23, 2016||Saint-Gobain Centre De Recherches Et D'etudes Europeen||Filters comprising sic membranes incorporating nitrogen|
|U.S. Classification||361/264, 252/516, 431/262, 219/553, 338/330, 431/66, 501/88, 219/270|
|International Classification||H01C7/00, F23Q7/22|
|Cooperative Classification||C04B2235/46, C04B2235/72, C04B2235/3826, C04B2235/3272, C04B2235/723, C04B35/565, C04B2235/3217, C04B2235/658, C04B2235/5436, C04B2235/661, C04B2235/77, C04B2235/6027, C04B2235/94, F23Q7/22|