US3367811A - Process of joining bodies with boron nitride - Google Patents
Process of joining bodies with boron nitride Download PDFInfo
- Publication number
- US3367811A US3367811A US392994A US39299464A US3367811A US 3367811 A US3367811 A US 3367811A US 392994 A US392994 A US 392994A US 39299464 A US39299464 A US 39299464A US 3367811 A US3367811 A US 3367811A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- boron nitride
- crucible
- vapors
- carbon
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
- C23C14/243—Crucibles for source material
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/003—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts
- C04B37/006—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts consisting of metals or metal salts
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
- C04B2235/6567—Treatment time
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/04—Ceramic interlayers
- C04B2237/08—Non-oxidic interlayers
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/04—Ceramic interlayers
- C04B2237/09—Ceramic interlayers wherein the active component for bonding is not the largest fraction of the interlayer
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/12—Metallic interlayers
- C04B2237/121—Metallic interlayers based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/12—Metallic interlayers
- C04B2237/126—Metallic interlayers wherein the active component for bonding is not the largest fraction of the interlayer
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/12—Metallic interlayers
- C04B2237/126—Metallic interlayers wherein the active component for bonding is not the largest fraction of the interlayer
- C04B2237/127—The active component for bonding being a refractory metal
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/341—Silica or silicates
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/343—Alumina or aluminates
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/345—Refractory metal oxides
- C04B2237/348—Zirconia, hafnia, zirconates or hafnates
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/363—Carbon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/60—Forming at the joining interface or in the joining layer specific reaction phases or zones, e.g. diffusion of reactive species from the interlayer to the substrate or from a substrate to the joining interface, carbide forming at the joining interface
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/62—Forming laminates or joined articles comprising holes, channels or other types of openings
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/70—Forming laminates or joined articles comprising layers of a specific, unusual thickness
- C04B2237/704—Forming laminates or joined articles comprising layers of a specific, unusual thickness of one or more of the ceramic layers or articles
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/70—Forming laminates or joined articles comprising layers of a specific, unusual thickness
- C04B2237/708—Forming laminates or joined articles comprising layers of a specific, unusual thickness of one or more of the interlayers
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/76—Forming laminates or joined articles comprising at least one member in the form other than a sheet or disc, e.g. two tubes or a tube and a sheet or disc
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/80—Joining the largest surface of one substrate with a smaller surface of the other substrate, e.g. butt joining or forming a T-joint
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/84—Joining of a first substrate with a second substrate at least partially inside the first substrate, where the bonding area is at the inside of the first substrate, e.g. one tube inside another tube
Definitions
- PROCESS OF JOINING BODIES WITH BORON NITRIDE Original Filed Nov. 8, 1962 CARBON United States Patent 3,367,811 PROCESS (9F .lOlNlNG BODHES WETH HURON NlTRlDlE Charles A. Baer, Princeton, N.J., and Philip J. Clough, Reading, and Robert W. Steeves, Nahant, Mass assignors, by mesne assignments, to National Research Corporation, Cambridge, Mass, a corporation of Massachusetts Original application Nov. 8, 1962, Ser. No. 236,365, now Patent No. 3,245,674, dated Apr. 12, 1965. Divided and this application Aug. 10, 1964, Ser. No. 392,994
- This invention relates to coating and more particularly to the coating of various substrates with aluminum.
- This application is a division of the copending application of Baer et al., Ser. No. 236,365, filed Nov. 8, 196-2, and now Patent No. 3,245,674.
- Still another object of the invention is to provide a source of aluminum vapors of the type described above which is simple to manufacture and use.
- Another object of the invention is to provide a source of the above type which can be produced from relatively inexpensive materials.
- Still another object of the invention is to provide a means for confining high-temperature vapors to produce a stream of aluminum vapors much more concentrated than can be produced by previously-known techniques.
- Still another object of the invention is to provide a mechanism for providing a high intensity stream of aluminum vapors capable of providing rapid coating of a discrete object with minimum transfer of heat to the object.
- a container for confining molten aluminum at elevated temperatures is provided by furnishing a refractory base 10 which is in the form of a crucible or other structure suitable for confining a substantial pool of molten aluminum.
- This base 10 is prefably formed of carbon or a refractory oxide such as magnesia, alumina or zirconia, or a refractory silicate such as zircon and the like.
- the base preferably does not contain any substantial quantities of materials which will outgas as the base is heated in a vacuum chamber to the elevated temperature of 1200 C. and above, which is necessary for aluminum evaporation.
- the invention will be initially described in connection with the utilization of a carbon crucible without attempting thereby to limit the invention.
- a carbon crucible which may be in the form of a cylindrical bucket or long boat, is formed 'as a solid piece or built up out of smaller pieces of carbon suitably attached together by carbon pins or the like.
- the whole interior surface of the crucible which is to be exposed to molten aluminum or aluminum vapors While the surface is at an elevated temperature, is then coated with a slurry of boron nitride 16 to a thickness on the order of M inch.
- This slurry is then dried, such as by baking in an oven, at a temperature on the order of 200 F. to drive off the water or other medium for forming the liquid phase in the slurry.
- the thus prepared crucible is positioned in a vacuum chamber and suitably supported so as to be heated by an induction coil, for example.
- Such a crucible has an extremely long life and is capable of operation at elevated temperatures in contact with molten aluminum for many hours.
- the boron nitride layer has been converted to an extremely hard, dense compound whose identity has not been clearly established. This is believed to be a reaction product between boron nitride and aluminum, and it has been found to form in the vapor state as Well as in the liquid state; that is, by reaction of boron nitride with aluminum vapors as well as the reaction of boron nitride with molten aluminum.
- This surface can also be formed, for example, when a cover is desired over the crucible to provide lateral or downward evaporation from the crucible.
- a deflecting top 14 is provided over the crucible, a suitable opening 12. being left between one portion of the cover and the main body of the crucible.
- This cover is also preferably formed of a refractory material, such as carbon, similar to the material of the crucible. It is equally coated with a layer of boron nitride and dried. The abutting surfaces of the crucible and cover are coated with a boron nitride layer. The crucible and cover are placed in the vacuum system, the crucible being charged with aluminum.
- the crucible and cover are then heated to about 1000 to 1300" C. and the boron nitride coating on the cover is reacted with aluminum vapors coming from the pool of aluminum confined by the source. These aluminum vapors react with the boron nitride coating at the elevated temperature of the cover. After a few minutes of operation, the aluminum vapors have reacted with the boron nitride coating to form a dense, hard surface which appears to be substantially impervious to and unreactive with aluminum vapors for long periods of time thereafter. The joint between the cover and the crucible has been converted to a hard, dense mass which is tight to liquid aluminum as well as to the aluminum vapors.
- a slurry is prepared by mixing 5 5 grams of powdered boron nitride in 121 cc. of water. This makes a paste having the con sistency of whipped cream. This paste is then applied, such as by a brush, to all those surfaces of a carbon crucible which are to be exposed to molten aluminum or aluminum vapors. This coating is preferably ,4 inch thick. The thus coated carbon body is air dried at about 200 F. Several coatings can be applied in sequence. In one preferred embodiment of the invention, a carbon crucible, having an internal diameter of 4 and a depth of 2 inches, is thus treated with boron nitride paste and air dried.
- the crucible is placed in a vacuum coating tank and is charged with 550 grams of aluminum. The crucible is then brought up to elevated temperatures on the order of 1200 to 1300 C. At the end of 35 minutes the major percentage of the aluminum has been evaporated. The tank is opened after the crucible is cooled to about 800 C. Another 250 grams of the solid aluminum is added to the remaining molten aluminum in the crucible. grams of titanium are also added to the melt at this time. The chamber is evacuated again and the crucible is brought up to operating temperature.
- the aluminum evaporation rate in the second run is found to be equal to or greater than the aluminum evaporation rate in the first run, the effect of the titanium addition being to remove any small amounts of aluminum carbide formed by penetration of aluminum through pinholes or cracks in the boron nitride coating.
- a carbon crucible having an internal diameter of 2 inches and a depth of 2 /2 inches is provided with a /2 inch hole near the top thereof.
- This crucible is also provided with a close fitting carbon cover.
- the inner surfaces of the crucible and cover (as well as the mating surfaces of the crucible and cover) are then coated with boron nitride and heated as above.
- This provides a source which produces a concentrated stream of aluminum vapors traveling laterally from the hole near the top. If the crucible is tilted somewhat the stream of vapors can be directed downwardly as well as laterally.
- This arrangement is particularly suited for coating discrete objects such as nuts and bolts or powders which are most conveniently coated from above while being supported on a vibrating tray or the like.
- the slurry of boron nitride can be prepared using numerous vehicles other than water. However, from the standpoint of cost and freedom from residual material which might outgas in the vacuum system, water is preferred. Equally wettin agents or binding agents can be added to the boron nitride, but these have been found to be unnecessary. For complex structures they can be helpful.
- carbon is a preferred material from the standpoint of structural strength at elevated temperatures and freedom from decomposition at elevated temperatures.
- Other refractory substances can be employed; for example, refractory oxides such as magnesia, alumina and zirconia or refractory silicates such as zircon can be protected by the application of a boron nitride coating. While metals can be given a temporary coating with boron nitride, the high solubility of all metals in molten aluminum precludes their use since any pinhole or crack in the boron nitride coating causes rapid failure of any of the metals.
- the improved aluminum vapor source can be employed in many types of coating devices such as those shown in the following US. patents: 2,622,401, 2,643,201, and 2,879,739 and the copending application of Cerych, Clought and Steeves Ser. No. 795,424, filed Feb. 25, 1961, now abandoned, to mention only a few of its uses.
Description
Feb. 6, 1968 A.BAER ETAL 3,367,811
PROCESS OF JOINING BODIES WITH BORON NITRIDE Original Filed Nov. 8, 1962 CARBON United States Patent 3,367,811 PROCESS (9F .lOlNlNG BODHES WETH HURON NlTRlDlE Charles A. Baer, Princeton, N.J., and Philip J. Clough, Reading, and Robert W. Steeves, Nahant, Mass assignors, by mesne assignments, to National Research Corporation, Cambridge, Mass, a corporation of Massachusetts Original application Nov. 8, 1962, Ser. No. 236,365, now Patent No. 3,245,674, dated Apr. 12, 1965. Divided and this application Aug. 10, 1964, Ser. No. 392,994
2 Claims. (Cl. 156-89) ABSTRACT OF THE DHSCLUSURE The high temperature reaction product of boron nitride and aluminum is used to secure together pieces of carbon or refractory oxides to form a joint which is resistant to high temperature molten aluminum.
This invention relates to coating and more particularly to the coating of various substrates with aluminum. This application is a division of the copending application of Baer et al., Ser. No. 236,365, filed Nov. 8, 196-2, and now Patent No. 3,245,674.
In the vacuum evaporation of aluminum where aluminum is heated to an elevated temperature on the order of 1200 to 1300 C., or above, one of the principal technical problems to be solved has been to find a crucible which is resistant to attack by the high-temperature aluminum. The same problem is encountered when a portion of the aluminum-evaporating source which is at elevated temperatures is exposed to a high density of aluminum vapors. This situation arises in those cases where it is desired to deflect or concentrate the flowing aluminum vapors to provide, for example, lateral or downward evaporation.
Some progress has been made in providing aluminumresistant structures, but these structures have not always been adequately simple to construct or cheap to maintain. While some progress has been made, great difliculty has been experienced in providing a complete satisfactory method for producing such a source, particularly one which is of a complex geometric shape. Equally, the art has only with difliculty been able to produce a stream of aluminum vapors which is directed laterally or downwardly from the source. Such a stream is particularl useful when discrete objects such as nuts and bolts and powders are to be coated, or when two sides of a continuous substrate are to be coated at the same time.
Accordingly, it is a principal object of the present invention to provide a method for producing a source of aluminum vapors which can have wide latitude of design and still be reasonably simple and inexpensive to construct.
Still another object of the invention is to provide a source of aluminum vapors of the type described above which is simple to manufacture and use.
Another object of the invention is to provide a source of the above type which can be produced from relatively inexpensive materials.
Still another object of the invention is to provide a means for confining high-temperature vapors to produce a stream of aluminum vapors much more concentrated than can be produced by previously-known techniques.
Still another object of the invention is to provide a mechanism for providing a high intensity stream of aluminum vapors capable of providing rapid coating of a discrete object with minimum transfer of heat to the object.
Other objects of the invention will in part be obvious and will in part appear hereinafter.
3,36 7,8 l l Patented Feb. f5, 1968 The invention accordingly comprises the process involving the several steps and the relation and the order of one or more of such steps with respect to each of the others and the apparatus possessing the features, properties and the relation of components which are exemplified in the following detailed disclosure, and the scope of the application of which will be indicated in the claims.
For a fuller understanding of the nature and objects of the invention, reference should be had to the following detailed description taken in connection with the drawing which is a diagrammatic, schematic, sectional View of one preferred embodiment of the invention.
In the present invention, a container for confining molten aluminum at elevated temperatures is provided by furnishing a refractory base 10 which is in the form of a crucible or other structure suitable for confining a substantial pool of molten aluminum. This base 10 is prefably formed of carbon or a refractory oxide such as magnesia, alumina or zirconia, or a refractory silicate such as zircon and the like. The base preferably does not contain any substantial quantities of materials which will outgas as the base is heated in a vacuum chamber to the elevated temperature of 1200 C. and above, which is necessary for aluminum evaporation. For convenience, the invention will be initially described in connection with the utilization of a carbon crucible without attempting thereby to limit the invention.
A carbon crucible, which may be in the form of a cylindrical bucket or long boat, is formed 'as a solid piece or built up out of smaller pieces of carbon suitably attached together by carbon pins or the like. The whole interior surface of the crucible, which is to be exposed to molten aluminum or aluminum vapors While the surface is at an elevated temperature, is then coated with a slurry of boron nitride 16 to a thickness on the order of M inch.
This slurry is then dried, such as by baking in an oven, at a temperature on the order of 200 F. to drive off the water or other medium for forming the liquid phase in the slurry. The thus prepared crucible is positioned in a vacuum chamber and suitably supported so as to be heated by an induction coil, for example. Such a crucible has an extremely long life and is capable of operation at elevated temperatures in contact with molten aluminum for many hours.
While the exact reason is not fully understood, it has also been found that the addition of titanium, zirconium, hafnium, vanadium, niobium or tantalum to the molten aluminum tends to maintain an appreciably higher evaporation rate. This is believed to be the result of minimizing any appreciable concentration of aluminum carbide in the melt due to pin hole porosity of the boron nitride coating which would otherwise permit penetration of the coating and attack of the crucible by the aluminum.
After a period of operation of the crucible, it was found that the boron nitride layer has been converted to an extremely hard, dense compound whose identity has not been clearly established. This is believed to be a reaction product between boron nitride and aluminum, and it has been found to form in the vapor state as Well as in the liquid state; that is, by reaction of boron nitride with aluminum vapors as well as the reaction of boron nitride with molten aluminum.
This surface can also be formed, for example, when a cover is desired over the crucible to provide lateral or downward evaporation from the crucible. In this case, a deflecting top 14 is provided over the crucible, a suitable opening 12. being left between one portion of the cover and the main body of the crucible. This cover is also preferably formed of a refractory material, such as carbon, similar to the material of the crucible. It is equally coated with a layer of boron nitride and dried. The abutting surfaces of the crucible and cover are coated with a boron nitride layer. The crucible and cover are placed in the vacuum system, the crucible being charged with aluminum. The crucible and cover are then heated to about 1000 to 1300" C. and the boron nitride coating on the cover is reacted with aluminum vapors coming from the pool of aluminum confined by the source. These aluminum vapors react with the boron nitride coating at the elevated temperature of the cover. After a few minutes of operation, the aluminum vapors have reacted with the boron nitride coating to form a dense, hard surface which appears to be substantially impervious to and unreactive with aluminum vapors for long periods of time thereafter. The joint between the cover and the crucible has been converted to a hard, dense mass which is tight to liquid aluminum as well as to the aluminum vapors.
As a result of the techniques described above, it is possible to produce sources for molten aluminum having a wide range of geometric configurations and a control of aluminum vapors which permits upward, sideways or downward direction of the vapors. The above described method of forming a vapor-tight joint can also be used to form joints which also withstand molten aluminum, such as when a large source is to be built from a number of pieces of carbon.
In one preferred embodiment of the invention, a slurry is prepared by mixing 5 5 grams of powdered boron nitride in 121 cc. of water. This makes a paste having the con sistency of whipped cream. This paste is then applied, such as by a brush, to all those surfaces of a carbon crucible which are to be exposed to molten aluminum or aluminum vapors. This coating is preferably ,4 inch thick. The thus coated carbon body is air dried at about 200 F. Several coatings can be applied in sequence. In one preferred embodiment of the invention, a carbon crucible, having an internal diameter of 4 and a depth of 2 inches, is thus treated with boron nitride paste and air dried. The crucible is placed in a vacuum coating tank and is charged with 550 grams of aluminum. The crucible is then brought up to elevated temperatures on the order of 1200 to 1300 C. At the end of 35 minutes the major percentage of the aluminum has been evaporated. The tank is opened after the crucible is cooled to about 800 C. Another 250 grams of the solid aluminum is added to the remaining molten aluminum in the crucible. grams of titanium are also added to the melt at this time. The chamber is evacuated again and the crucible is brought up to operating temperature. The aluminum evaporation rate in the second run is found to be equal to or greater than the aluminum evaporation rate in the first run, the effect of the titanium addition being to remove any small amounts of aluminum carbide formed by penetration of aluminum through pinholes or cracks in the boron nitride coating.
In another embodiment of the invention a carbon crucible having an internal diameter of 2 inches and a depth of 2 /2 inches is provided with a /2 inch hole near the top thereof. This crucible is also provided with a close fitting carbon cover. The inner surfaces of the crucible and cover (as well as the mating surfaces of the crucible and cover) are then coated with boron nitride and heated as above. This provides a source which produces a concentrated stream of aluminum vapors traveling laterally from the hole near the top. If the crucible is tilted somewhat the stream of vapors can be directed downwardly as well as laterally. This arrangement is particularly suited for coating discrete objects such as nuts and bolts or powders which are most conveniently coated from above while being supported on a vibrating tray or the like.
While several preferred embodiments of the invention have been described above, numerous modifications thereof can be employed without departing from the spirit of the invention. The slurry of boron nitride can be prepared using numerous vehicles other than water. However, from the standpoint of cost and freedom from residual material which might outgas in the vacuum system, water is preferred. Equally wettin agents or binding agents can be added to the boron nitride, but these have been found to be unnecessary. For complex structures they can be helpful.
Similarly, carbon is a preferred material from the standpoint of structural strength at elevated temperatures and freedom from decomposition at elevated temperatures. Other refractory substances can be employed; for example, refractory oxides such as magnesia, alumina and zirconia or refractory silicates such as zircon can be protected by the application of a boron nitride coating. While metals can be given a temporary coating with boron nitride, the high solubility of all metals in molten aluminum precludes their use since any pinhole or crack in the boron nitride coating causes rapid failure of any of the metals.
While specific forms of apparatus have not been illustrated, the improved aluminum vapor source can be employed in many types of coating devices such as those shown in the following US. patents: 2,622,401, 2,643,201, and 2,879,739 and the copending application of Cerych, Clought and Steeves Ser. No. 795,424, filed Feb. 25, 1959, now abandoned, to mention only a few of its uses.
Since certain changes can be made in the above process and apparatus without departing from the scope of the invention herein involved, it is intended that all matter contained in the above description shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. A process of joining bodies formed of a material selected from the group consisting of carbon and the refractory oxides and silicates to provide a joint capable of resisting attack of aluminum at elevated temperatures on the order of 1200 C. and above, said process comprising the steps of bringing the bodies into juxtaposition, applying a layer of boron nitride to the juxtaposed surfaces of said bodies, contacting said boron nitride layer with aluminum metal, heating said aluminum metal to a temperature on the order of 1000 C. to 1300 C. to combine aluminum with said boron nitride layer to form a hard, solid reaction product of said boron nitride and aluminum which reaction product strongly unites said juxtaposed bodies.
2. The process of forming a joint between two pieces of carbon, the joint being capable of resisting attack of aluminum at elevated temperatures on the order of 1200 C. and above, the process comprising the steps of coating the surfaces to be joined with boron nitride, heating the surfaces in a non-oxidizing atmosphere to a temperature of at least 1000 C. and exposing the thus heated joint to aluminum at said elevated temperature for sulficient time to cause substantial reaction between the aluminum, boron nitride and carbon at the joint with the formation of a hard solid reaction product which strongly unites said two pieces of carbon, said reaction product being unreactive with aluminum and being wettable by aluminum.
References Cited UNITED STATES PATENTS 1,605,205 11/1926 Bellamy 15689 X 2,839,413 6/1958 Taylor 10655 X 2,877,532 3/1959 Heine 52305 2,937,101 5/1960 Nelson et .al. 10655 2,970,061 1/1961 Burnett 10671 2,996,412 8/1961 Alexander 117107.1 X
EARL M. BERGERT, Primary Examiner.
H. F. EPST-ElN, Assistant Examiner.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US392994A US3367811A (en) | 1962-11-08 | 1964-08-10 | Process of joining bodies with boron nitride |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US236365A US3245674A (en) | 1960-04-25 | 1962-11-08 | Crucible coated with reaction product of aluminum and boron nitride coating |
US392994A US3367811A (en) | 1962-11-08 | 1964-08-10 | Process of joining bodies with boron nitride |
Publications (1)
Publication Number | Publication Date |
---|---|
US3367811A true US3367811A (en) | 1968-02-06 |
Family
ID=26929710
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US392994A Expired - Lifetime US3367811A (en) | 1962-11-08 | 1964-08-10 | Process of joining bodies with boron nitride |
Country Status (1)
Country | Link |
---|---|
US (1) | US3367811A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3509017A (en) * | 1966-07-22 | 1970-04-28 | North American Rockwell | Multi-layered pyrolized para-polyphenylene structures and method of making same |
US3607613A (en) * | 1968-05-27 | 1971-09-21 | Sylvania Electric Prod | Electrically conductive refractory bodies |
FR2414078A1 (en) * | 1978-01-10 | 1979-08-03 | Union Carbide Corp | CONTAINER FOR VACUUM METAL EVAPORATION AND ITS REALIZATION PROCESS |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1605205A (en) * | 1924-05-30 | 1926-11-02 | Western Electric Co | Method of securing a union between elements |
US2839413A (en) * | 1956-03-12 | 1958-06-17 | Carborundum Co | Refractory body containing boron nitride |
US2877532A (en) * | 1957-09-13 | 1959-03-17 | Heine Henry William | Manufacture of acoustic fireproof tiles |
US2937101A (en) * | 1957-06-06 | 1960-05-17 | Gen Electric | Heat resistant composition |
US2970061A (en) * | 1957-12-11 | 1961-01-31 | William H Burnett | Building units and method of producing the same |
US2996412A (en) * | 1958-10-10 | 1961-08-15 | Continental Can Co | Art of depositing metals |
-
1964
- 1964-08-10 US US392994A patent/US3367811A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1605205A (en) * | 1924-05-30 | 1926-11-02 | Western Electric Co | Method of securing a union between elements |
US2839413A (en) * | 1956-03-12 | 1958-06-17 | Carborundum Co | Refractory body containing boron nitride |
US2937101A (en) * | 1957-06-06 | 1960-05-17 | Gen Electric | Heat resistant composition |
US2877532A (en) * | 1957-09-13 | 1959-03-17 | Heine Henry William | Manufacture of acoustic fireproof tiles |
US2970061A (en) * | 1957-12-11 | 1961-01-31 | William H Burnett | Building units and method of producing the same |
US2996412A (en) * | 1958-10-10 | 1961-08-15 | Continental Can Co | Art of depositing metals |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3509017A (en) * | 1966-07-22 | 1970-04-28 | North American Rockwell | Multi-layered pyrolized para-polyphenylene structures and method of making same |
US3607613A (en) * | 1968-05-27 | 1971-09-21 | Sylvania Electric Prod | Electrically conductive refractory bodies |
FR2414078A1 (en) * | 1978-01-10 | 1979-08-03 | Union Carbide Corp | CONTAINER FOR VACUUM METAL EVAPORATION AND ITS REALIZATION PROCESS |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3084060A (en) | Process of coating a refractory body with boron nitride and then reacting with aluminum | |
US3245674A (en) | Crucible coated with reaction product of aluminum and boron nitride coating | |
US3227431A (en) | Crucible externally lined with filamentary carbon | |
US3830173A (en) | Tuyere formed by cementing a ceramic liner in a metal tube | |
US3419404A (en) | Partially nitrided aluminum refractory material | |
US3385723A (en) | Carbon article coated with beta silicon carbide | |
SE8604949D0 (en) | TITANIUM COMPOSITE HAVING A POROUS SURFACE AND PROCESS FOR PRODUCING THE SAME | |
US3517432A (en) | Diffusion bonding of ceramics | |
SE463873B (en) | SEAT AND MIXING FOR THE formation of a cohesive ELF-SURFACE MASK ON A SURFACE AND ACCORDING TO THE RECOVERY MASS | |
JPS61104062A (en) | Method for sealing pore of metallic or ceramic thermally sprayed coated film | |
US3367811A (en) | Process of joining bodies with boron nitride | |
KR960001433B1 (en) | Method for surface bonding of ceramic bodies | |
CS199377B1 (en) | Connecting method of at least two ceramic materials | |
US3288573A (en) | High temperature resistant member and process for forming | |
US4126654A (en) | Alumina or alumina-chromia refractories | |
US3415631A (en) | Protective coated article | |
Barkalow | Mechanisms of hot corrosion attack of ceramic coating materials | |
US3155534A (en) | Method of making magnesia-alumina spinel bodies | |
Guha et al. | Microstructural Inhomogeneity in Sintered Pb (Mg1/3Nb2/3) O3‐PbTiO3 Based Dielectrics | |
US3736222A (en) | Ceramic articles and method of sealing ceramics | |
JPS60238472A (en) | Laser thermal spraying method | |
US1121890A (en) | Method for manufacturing utensils and the like from the oxids of the rare earths, thorium oxid, zirconium oxid, and the like. | |
US1311324A (en) | dalen | |
US1017748A (en) | Process of case-hardening metals and alloys. | |
JPH0268488A (en) | Cordierite type functionally gradient materials |