US2898236A - Protective cermet coating method and materials - Google Patents

Protective cermet coating method and materials Download PDF

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US2898236A
US2898236A US629805A US62980556A US2898236A US 2898236 A US2898236 A US 2898236A US 629805 A US629805 A US 629805A US 62980556 A US62980556 A US 62980556A US 2898236 A US2898236 A US 2898236A
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aluminum
parts
coating
ceramic
frit
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US629805A
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John V Long
John V Furth
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Solar Aircraft Co
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Solar Aircraft Co
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    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/009After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/50Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
    • C04B41/51Metallising, e.g. infiltration of sintered ceramic preforms with molten metal
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/80After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
    • C04B41/81Coating or impregnation
    • C04B41/85Coating or impregnation with inorganic materials
    • C04B41/88Metals
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Description

2,898,236 I PROTECTIVE CERMET COATING METHOD JohnV. Long, San Diego, and John EurthjLa Jolla, Califi, assignor to Solar Aircraft Company, San Diego, Calif a corporation of California i No Drawing. Application December .21, 1956 Serial No. 629,805 7 21'Claims. (Cl. 117-124) 2,898,236 Patented A g- 47, 1
ice
lithia, and beryllia as principal constituents. These coat- I ings hav'elproven successful,:but the coating frit is:.quit'e i also increase the industrial applications of low firing 1955, for Protective Coating Methods andMaterials." i
It also relates to an improvement over the Protective C ating M th ds an Materi l disclosed in Ounce pending application Serial NO. 623,550, ,filed November 21, 19 6- v v .In our copending application Serial No. 512,315,, we di lose l minum-ceramic cermet. co tingsincluding Iceramic components, which contribute refractoriness, high temltcrature strength, and chemical and physical stability at high temperatures, and aluminum components which contribute ductility and high resistance to erosion and thermal and mechanical shock. We also disclose therein a method of providing ,an article with a ceramic-aluminum germet coating by an inexpensive production .process aluminum-ceramic cermet coatings. Drastic cost reduction, has been achieved by the present invention which utilizes a frit'costing'about 5 to 6 cents a pound because it iszmade'principally from a natural ingredient readily available at about4. cents a'pound. 1
It isthe primary object of the present invention'to provide novel ceramic-aluminum protective cermet coatings: which 'fire in .a range of from 1230 F.-.(the melting point of aluminum)? to 1300. F., with a preferred firing range bfifr0m'12-30 F. to l260-F. It is a principaI object of the present invention to provide low-cost, low-firing ceramic-aluminum protective cermet coatings and methods, which utilize low cost materials.
It is another object of this invention to provide such low-cost cermet coating compositions and methods-utiliz ing'a fluxing ceramic frit based on an inexpensive readily available natural borate that can be successfullyused in the ?as is state. It is a'related object to provide lowfiring-cermet coating compositions and methods utilizing,
jectives and improved results in aluminum-ceramic cermet comprising the steps of applying and firing on the article to be coated a slip composed of a water vehicle, aluminum or aluminum alloy powder, av suspension agent and binder, and a ceramic frit which forms the ceramic phase of t cend coating and also fluxes the aluminumpowder and coated surface during the firing cycle.
,I'he coatings disclosed in our copending application SerialiNo. 512,315 are fired at a minimum temperature of about 1350 F., and at temperatures up to 2200 F. These coatings are being used successfully in va large number of applications, on such metals .as mild steels, stainless steels, and the super alloys like N-155, Inconel and other high chromium-nickel based alloys. .-I-Io'wever, when certain alloys and/ or non-metallics aretobe coated, it is desirable to provide a coating whichfires at temperatures lower than the 1350 F. involved in our copending application. Forexample, the chro. mium-molybdenum-vanadium alloys, including. but not limited to Tirnken 1722 A(S) and General Electric Chromoloy, are worked in the annealed state; and the finished part is normalized at about 1750 F; then tempered at 1250 F. for from two to six hours. Elf subsequent to the tempering operation, a coating :were applied and fired at 1350 F. or higher, the work piece might be deleteriously atfected.
Therefore, when alloys like Timken 1722 A(S) and Chromoloy are to be coated, it is necessary to provide a coating which fires at a temperature not above the tempering point. and preferably fires atabout 1250? F. In our aforementioned application Serial No. 623,550, filed November 21, 1956, weldisclosesuccessful lo'w'firing cermet coating methods .and'materials developed to: ap plication to such alloys with a firing temperature-of about .1 0 The low firing aluminum-ceramic. cermet oa in disclosed in that appl ca i n are produced from coating as-set forth in our copending application Serial No. 512,315, of which this is a continuation in part. Itis-another object of-this invention to provide an aluminum-ceramic water vehicle coating slip, which is stabilized to prevent-aluminum-water reaction by=-small quantities of the boron oxide-alkaline earth oxide frit disclosed in our earlier application Serial No. 512,315.
As in the case of the coatings of our earlier copending application Serial No. 512,315, our present coatings are similarly obtained by applying to the work piece-a water vehicle slip that includes a mixture of aluminum powder with a ceramic fluxing frit and an aluminum-water reaction inhibitor, and firing the part in the desired temperature range, in a gas or electric furnace with an air atmosphere.
1 In preparing our slip, we first combine in parts by weight l00 parts of Gerstley borate (NaCaB O -8H- 'O), and 5 parts lithium carbonate (Llz oa). A typical chemical composition of Gerstley borate .(NaCaB5O -8H 0) Boron .trioxide (B 0 33.0 Calcium oxide (CaO) 15.9 Sodium oxide (Na O) 4.9 Water and organic matter -Q. 28.2 Silica (SiO a 9.5 Magnesia (MgO) 3,5 Alumina (A1 0 1.1 Iron oxide (Fe O .3 Carbon dioxide (CO 3.2 Undetermined 0.4
-' condition is obtained. During the smelting operation,
coating s ips i eluding a frit comprising borouoxid the ,water and CO of the Gerstley borate and the CO of the lithium carbonate volatilize out. The Gerstley'b'orate, loses water and carbon dioxide by volatilization up to about 31 percent of original weight. The final smelt:
therefore, containsby weight about 7 0 parts of the flbOYfig listed mineral constituents of .the Gerstley borate and about 2 parts lithia (M This smelt is then fritted, as by pouring into cold water, and the frit-is .dry milled to the preferred fineness; The end 'result'is a low melting borate frit, which costs about 8-10 cents a pound (compared to about $25 per pound for the low melting borate-beryllia frit of our application Serial No. 623,550, filed November 21, 1956).
In a preferred coating process, 30 parts of the smelted frit are combined with 1 to 3 parts' of the frit of our cermetv application Serial No. 512,315, 70 parts of aluminum powder, 5-10 parts of ball typeclay (suspen- V assigned firing cycle, .and that the lithia lowers the melting point sionagent), and 55 parts of water (or sufficient water to produce a slip of desired fluidity depending on-the method of applying .it). The frit. from our application SerialiNo'. 512,315 consists. essentially of boron oxideand bariumoxide whichmay be replaced .with an equal amount of calcium oxide, and if desired aluminum fluoride,-in a molar ratio of about BaO:3B O :0-% AlF The two fn'ts and the aluminumpowder. are preferably of 200 mesh and can' be finer, with no deleterious results .down to' -.400 mesh. The ingredients may be merely agitated or ball milled to secure thorough mixing.
and helps stabilize the boron oxide in the frit. The ceramic phase of the resulting cermet coating acts to plug up the porosity inherent in prior aluminum and aluminum alloy coatings.
In the above-discussed Gertsley borate frit example, the smelt is'composed of l00parts Gerstley borate and 5 parts lithium carbonate yielding a frit containing about Zparts lithia. It has been found that an increase to 7% parts of lithium carbonate will result in a frit con taining 3 parts of lithium oxide with an even lower melting point such such that the bisque will melt at about 1230 F., the melting point of aluminum.
In the present process, it is important that the glass phase be held tonot'more than 40 partsfrit to 60 parts of aluminum. However, it has been found that where it is desired that the end result be a coating with a decreased aluminum content, a'filler of zircon, silica or alumina may replace up to 20 parts of aluminum with the coating still containing an aluminum-glass ratio of 60-40. The filler is practically unaffected by the firing cycle, and remains as an inert constituent of the final coating.
We have provided by the foregoing compositions and methods a highly protective ceramic-aluminum coating specially suitable for alloys of the type discussed. In
' the resulting cermet coating, the ceramic phase coop- The small amount of said frit disclosed in-our appliously affecting the aluminum and generating hydrogen which might cause a dangerous explosion, so that the slip could not be stored and would have to be used within a short time after it is made.
The work piece should be reasonably free of grease and 4 oil but need not be cleaned as by sandblast or acid pickle. The work piece-is coated by spraying, painting, dipping, slushing,.v or other likemeans, and the coat dried to a-bisque either at room temperature or in artificial temperature up to 300 F. Thickness of the coat is not critical, and it has been found that an applied layer of from one to seven mils thick will fire to a satisfactory protective coating of approximately the bisque thickness.
Following the drying cycle, the part is firedat from 1-260 F. to 1300 F. (By a change in the lithia content, as discussedbelow, thefiring temperature may be re.-
duced to about 1230 F.) The part may be .fired in an air atmosphere. Firing need continue only long enough to bring the part to at least 1260 F. (or 1230" F.) and hold it at temperature for about five minutes. However, a longer firing time will not deleteriously aifect the coating, and, for this reason, the part may be tempered and coated during the same cycle. In many cases, the tempering will be carried out prior to final machining where close tolerances must be met, and machining may be carried out subsequent to coating. In some cases, it is preferable to coat the entire work piece, then machine following tempering; while in other cases, the areas to be. machined may bemasked, and the rest of the work piece coated Both methods are satisfactory. ..During firing, the aluminum melts and some of it coalesces into fields, while some of the aluminum grains remain as independent bits. Although the end coating is extremely tenacious and bonding is excellent, there appears to be very little diflusion of the aluminum into the surface of the work piece. While this would seem to indicate a ceramic or glass matrix full of aluminum, the resulting cermet coating is an aluminum coat full of ceramic or glass because of the 70-30 ratio of aluminum and frit. h
It appears from the evidence available that the boron oxide of the Gerstley borate fluxes both the aluminum powder and the surface of the work piece during the erates with the metallic phase to provide protection from oxidation, corrosion, acid attack, and erosion damage in continuous service temperatures up to 1300 F. for long periods of time, and in temperatures up to 1500 F. for short intermittent periods. The resulting coatings provide protection combining the high temperature strength, refractoriness, and chemical and physical stability of ceramic with the ductility and good resistance to erosion and thermal and mechanical shock of metals.
Although our presently disclosed coatings will find wid use in protecting alloys like those specifically discussed above, this use by no means is the limit of the coatings. For example, these coatings provide highly satisfactory protective layers for graphite, glass, and other nonmetallics, and are particularly useful where it is desirable that the piece to be coated not be subjected to high temperatures during processing.
One of the useful applications of our described coating inventions presently in great demand is the sealing of ceramic insulation materials such as woven glass fibers or similar materials, to eliminate porosity and possible oil absorption; The above-disclosed'slip is sprayed, dipped, or otherwise. applied to the insulating material, and fired in the indicated temperature range. The result is a structure characterized by littleor no porosity, good insulating capabilities, and excellent resistance to corrosive and erosive influences. I Y
. It will'be appreciated that because our present coatings fire at comparatively low temperatures, the process is less expensive than other similar processes, the work piece issubject to less stress, and'simpler, cheaper equip ment can be used. I
The invention may be embodied in other specific forms without departing from the spirit or essential characteristics' thereof. The present embodiments are therefore tov be considered in all forms as illustrative and not restrictive, the scope of the-invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.
What is claimed and desired to be secured by United States Letters Patent is: I
1 1. The method of providing the surface of an article selectedfrom the-class consisting of metal, glass and ceramic with a cermet coating having both ceramic and metallic phases, which includes the steps of: applying to the surface to be coated a slip comprising a liquid vehicle, a cermet composition including from about 60 to 70 parts by weight of a metal selected from the group consisting of aluminum and aluminum base alloys, in particle form, and from about 30 to 40 parts by weight of the smelted and fritted product of a composition consisting essentially of Gerstley borate and lithia, and a suspension agent; and firing the surface at a temperature of at least about 1230 F. to form a cermet coating.
2. The method defined in claim 1, wherein the ceramic constituent comprises approximately 23 parts by weight lithia and about 70 parts by weight the mineral constituents of Gerstley borate.
3. The method defined in claim 1 wherein said coated article surface is fired at a temperature between 1230 F. and 1300 F.
4. The method defined in claim 3 wherein said coated article surface is fired at a temperature between 1260 F. and 1300 F.
5. A method as defined in claim 3 wherein said article is fired in an air atmosphere.
6. A heat reacted frit composition consisting essentially of lithia and the mineral constituents of Gerstley borate.
7. A cermet coating slip comprising: from about 60 to 70 parts by weight of a metal selected from the group consisting of aluminum and aluminum base alloys, in particle form; from about 30 to 40 parts by weight of the smelted and fritted pro-duct of a composition consisting essentially of Gerstley borate and lithia; 5-10 parts suspension agent; and a liquid vehicle in suflicient quantity to produce a slip of desired fluidity for coating articles.
8. A slip as defined in claim 7, wherein said liquid vehicle is water, and said slip contains 1 to 3 parts of a frit consisting essentially of boron oxide, and at least one alkaline earth oxide selected from the group consisting of barium oxide and calcium oxide in molar ratio of 3B O :BaO.
9. A slip as defined in claim 7, wherein the ratio of frit content to aluminum metal content does not exceed 40:60.
10. A slip as defined in claim 7, wherein up to 20 parts by weight of the aluminum metal powder is replaced by an inert filler material.
11. A slip as defined in claim 10, wherein said inert filler consists of at least one material selected from the group consisting of zircon, silica or alumina.
12. A slip as defined in claim 7, wherein said suspension agent is a ball type clay.
13. A slip as defined in claim 8, consisting of about 70 parts metal powder, approximately 30 parts of said Gerstley borate-lithia frit, 5 to parts ball type clay, and 1 to 3 parts of said last-mentioned frit.
14. A frit comprising a heat reacted smelted and fritted product of a mixture consisting essentially of about 100 parts Gerstley borate and 5 to 7 /2 parts lithium carbonate.
15. A heat reacted and fritted mixture consisting essentially of about 70 parts the mineral constituents of Gerstley borate and 23 parts lithia.
16. The method of preparing a ceramic frit which comprises the steps of admixing together about 100 parts by weight of Gerstley borate and between about 5 to 7 /2 parts by weight lithium carbonate, and smelting said mixture until a clear bubble-free melt is obtained, and fritting the smelted product.
17. The method of claim 16 wherein said mixture is smelted at about 2300 F. until clear.
18. The method of providing the surface of an article selected from the class consisting of metal, glass and ceramic with a cermet coating having both ceramic and metallic phases, which includes the steps of: applying to the surface to be coated a slip comprising an aqueous vehicle, a cermet composition from about to parts by weight of a metal selected from the group consisting of aluminum and aluminum base alloys, in particle form, and from about 30 to 40 parts by weight of the smelted and fritted product of a composition consisting essentially of Gerstley borate and lithia, a suspension agent, and an inhibitor for preventing reaction between the aluminum powder and the water vehicle; and firing the coated surface at a temperature of at least about 1230" F. to form a cermet coating.
19. A method of providing the surface of an article with a cermet coating as defined in claim 18, wherein said inhibitor is a frit consisting essentially of boron oxide, and at least one alkaline earth oxide selected from a group consisting of barium oxide and calcium oxide in molar ratio of 3B O :BaO.
20. A slip as defined in claim 7 wherein said last-mentioned frit further includes aluminum fluoride in molar ratio of up to /2AlF 21. A method as defined in claim 19 wherein said lastmentioned frit further includes aluminum fluoride in a molar ratio of up to /zAlF References Cited in the file of this patent UNITED STATES PATENTS 2,492,523 Coffeen et al Dec. 27, 1949 2,608,490 Donahey Aug. 26, 1952 2,775,531 Montgomery et a1 Dec. 25, 1956

Claims (1)

1. THE METHOD OF PROVIDING THE SURFACE OF AN ARTICLE SELECTED FROM THE CLASS CONSISTING OF METAL, GLASS AND CERAMIC WITH A CERMET COATING HAVING BOTH CERAMIC AND METALLIC PHASES, WHICH INCLUDES THE STEPS OF: APPLYING TO THE SURFACE TO BE COATED A SLIP COMPRISING A LIQUID VEHICLE, A CERMET COMPOSITION INCLUDING FROM ABOUT 60 TO 70 PARTS BY WEIGHT OF A METAL SELECTED FROM THE GROUP CONSISTING OF ALUMINUM AND ALUMINUM BASE ALLOYS, IN PARTICLES FORM, AND FROM ABOUT 30 TO 40 PARTS BY WEIGHT OF THE SMELTED AND FRITTED PRODUCT OF A COMPOSITION CONSISTING ESSENTIALLY OF GERSTLEY BORATE AND LITHIA, AND A SUSPENSION AGENT; AND FIRING THE SURFACE AT A TEMPERATURE OF AT LEAST ABOUT 1230*F. TO FORM A CERMET COATING.
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3023492A (en) * 1958-11-19 1962-03-06 Gen Electric Metalized ceramic member and composition and method for manufacturing same
US3180742A (en) * 1961-06-27 1965-04-27 Dwight G Bennett Elevated temperature resistant ceramic structural adhesives
US3203815A (en) * 1962-12-21 1965-08-31 North American Aviation Inc High-temperature protective coating for metals
US3238489A (en) * 1962-06-11 1966-03-01 Dale Electronics Electrical resistor
US3238488A (en) * 1962-01-15 1966-03-01 Beckman Instruments Inc Variable resistor
US3255033A (en) * 1961-12-28 1966-06-07 Ibm Electroless plating of a substrate with nickel-iron alloys and the coated substrate
US3278785A (en) * 1960-12-12 1966-10-11 Gen Motors Corp Spark plug having porcelain insulator protected by plasma-jet deposited refractory coating
US3295934A (en) * 1962-01-12 1967-01-03 Saint Gobain Manufacture of complex aluminous metal-glass products of high strength
US3403043A (en) * 1964-04-14 1968-09-24 Int Standard Electric Corp Ceramic-metal seals
US3772043A (en) * 1970-09-04 1973-11-13 Rockwell International Corp Cermet protective coating glass frit
EP0007131A1 (en) * 1978-07-07 1980-01-23 Reimbold & Strick GmbH & Co. KG Enamelled sound absorber and method for its enamelling
WO1998035917A1 (en) * 1997-02-18 1998-08-20 Technology Partners Inc. Metal-ceramic composite coatings, materials, methods and products

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2492523A (en) * 1948-01-20 1949-12-27 Metal & Thermit Corp Acid resistant enamel frit and ferrous metal coated with enamel made from same
US2608490A (en) * 1950-08-01 1952-08-26 Foote Mineral Co Low-temperature vitreous enamels
US2775531A (en) * 1949-05-10 1956-12-25 Univ Ohio State Res Found Method of coating a metal surface

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2492523A (en) * 1948-01-20 1949-12-27 Metal & Thermit Corp Acid resistant enamel frit and ferrous metal coated with enamel made from same
US2775531A (en) * 1949-05-10 1956-12-25 Univ Ohio State Res Found Method of coating a metal surface
US2608490A (en) * 1950-08-01 1952-08-26 Foote Mineral Co Low-temperature vitreous enamels

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3023492A (en) * 1958-11-19 1962-03-06 Gen Electric Metalized ceramic member and composition and method for manufacturing same
US3278785A (en) * 1960-12-12 1966-10-11 Gen Motors Corp Spark plug having porcelain insulator protected by plasma-jet deposited refractory coating
US3180742A (en) * 1961-06-27 1965-04-27 Dwight G Bennett Elevated temperature resistant ceramic structural adhesives
US3255033A (en) * 1961-12-28 1966-06-07 Ibm Electroless plating of a substrate with nickel-iron alloys and the coated substrate
US3295934A (en) * 1962-01-12 1967-01-03 Saint Gobain Manufacture of complex aluminous metal-glass products of high strength
US3238488A (en) * 1962-01-15 1966-03-01 Beckman Instruments Inc Variable resistor
US3238489A (en) * 1962-06-11 1966-03-01 Dale Electronics Electrical resistor
US3203815A (en) * 1962-12-21 1965-08-31 North American Aviation Inc High-temperature protective coating for metals
US3403043A (en) * 1964-04-14 1968-09-24 Int Standard Electric Corp Ceramic-metal seals
US3772043A (en) * 1970-09-04 1973-11-13 Rockwell International Corp Cermet protective coating glass frit
EP0007131A1 (en) * 1978-07-07 1980-01-23 Reimbold & Strick GmbH & Co. KG Enamelled sound absorber and method for its enamelling
WO1998035917A1 (en) * 1997-02-18 1998-08-20 Technology Partners Inc. Metal-ceramic composite coatings, materials, methods and products
US6001494A (en) * 1997-02-18 1999-12-14 Technology Partners Inc. Metal-ceramic composite coatings, materials, methods and products

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