US2927043A - Aluminum coating processes and compositions - Google Patents

Aluminum coating processes and compositions Download PDF

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US2927043A
US2927043A US641245A US64124557A US2927043A US 2927043 A US2927043 A US 2927043A US 641245 A US641245 A US 641245A US 64124557 A US64124557 A US 64124557A US 2927043 A US2927043 A US 2927043A
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aluminum
flux
coating
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Alvin R Stetson
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Solar Aircraft Co
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    • 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
    • C23C24/106Coating with metal alloys or metal elements only

Definitions

  • This invention relates to methods and compositions for obtaining the deposition of a protective aluminum or aluminum alloy layer on articles of ferrous materials, stainless steels, and super alloys.
  • Metal powder suspension and hot dip processes have been known for manyyears and recognized as having many advantages over other coating processes, such as electroplating and molten metal spray, for example. Nevertheless, they have not enjoyed Wide commercial success because the results obtainable by their use have not in the past been consistently reproducible. Also, the coatings produced by such prior processes were not imperforate, uniform, or controllable in thickness frequently were not everywhere securely bonded to the basis metal. The hot dip processes tend to dissolve the basis metal in the aluminum bath and the coating thicknesses are limited.
  • the flux In the case of aluminum powder suspension processes in particular, the flux must also act to remove any oxides formed or present on the particles of aluminum powder and to form a continuous flux cover sealing the coating and basis metals from the atmosphere, to prevent further oxidation of these metals during the firing step.
  • 'It is the purpose of this invention to provide improved processes for covering metallic surfaces with protective metal coatings in which the surfaces to be coated are wetted with molten aluminum in the presence of a flux composition which has a fluxing action satisfying the requirements outlined above and which is adapted for use in my aluminizing process including powdered aluminum suspensions.
  • the flux compositions herein disclosed, however, are also excellent for use with molten metal coating processes.
  • a primary object of my present invention is to provide novel methods of developing a highly protective diffused aluminum or aluminum alloy coating of controllable thickness on ferrous and other metallic alloys, including the so'called super alloys.
  • a further important object of this invention is to provide novel flux compositions capable of use in aluminizing processes and particularly my new metal powder suspension processes.
  • Yet another object is the provision of a. series of novel slips particularly useful in carrying out my aluminum powder coating process.
  • Another object is the provision of novel aluminizing processes which are extremely useful in repairing and correcting the aluminum coatings on parts on which said coatings have been damaged by forming, welding, or finishing procedures subsequent to initial coating, regardless of the method used to obtain the initial coat.
  • Still another object is the provision ofprocesses by which may be obtained smooth aluminum coatings characterized by uniform thickness over all areas of complex parts involving louvres, weld seams, sharp corners that must be maintained, joints, and other like complexities.
  • Another object is to provide quicker, less expensive,
  • the metallic surface to be aluminized is wetted with molten aluminum in the presence of one of the fluxing agents described herein. This is accomplished by applying to the surface'of the basis metal article, by spraying or dipping or the like, a slip composed of a suspension of flux and aluminum powder in a liquid vehicle, with or without flow control agents, and heating the article thus coated to a temperature in excess of the melting point of aluminum in air, or preferably in an inert atmosphere such as nitrogen.
  • the aluminum becomes molten and evenly covers and uniformly wets and to some degree alloys with the basis metal, producing a superior coating of two phases: (1) an interphase of diffused aluminum, and (2) a surface layer of aluminum covered with flux.
  • the flux is subsequently removed by such means. as hot water wash or leaching.
  • a properly controlled heat treatment may subsequently be used to improve the oxidation and corrosion resistance of the protective layer by causing further diffusion of the aluminum or aluminum alloy into the basis metal as hereinafter amplified. Excellent results are obtained, however, without such diffusion treatment, and the use of a subsequent diffusion cycle is generally applicable to the stainless steels and super alloys to develop an erosion resistance as well as oxidation and corrosion resistance.
  • a slip comprising essentially aluminum or aluminum alloy powder and a chloride base flux carried in suspension in a liquid vehicle.
  • auxiliary components of the slip are a suspending agent and a binder. Small amounts of a refractory oxide, iron, nickel or a mixture thereof may also be included in the slip for purposes which will be described hereinafter. Table I shows the general constituency of slips according to my invention:
  • the aluminum powder may vary considerably in both chemical composition and physical properties with no deleterious effect on the final protective coating.
  • pure aluminum or silicon-aluminum alloys are preferred since these exhibit the most satisfactory resistance to corrosion and oxidation.
  • a grain size of minus 100 mesh plus 400 mesh is preferred when standard dip and spray techniques are used, in general any grain size is useful in my process.
  • the size used is governed by the requirements of the specific application. Also, both atomized aluminum powder and flake aluminum can be successfully used in my process, although atomized powder is the preferred material.
  • the fluxing agent is a critical factor in the production of satisfactory coatings as pointed out above.
  • My new improved fiuxing agent is a chloride base flux consisting of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists essentially of lithium fluoride and cryolite. Examples of flux compositions I have found satisfactory are listed in Table II.
  • compositions 1 through 6 inclusive function satisfactorily on steels having less than about 15 points of carbon, and composition 7 functions satisfactorily on alloys of both low and high carbon content. Since compositions 1 through 6 are the more water soluble they are preferably used where applicable, because they can be readily removed by inexpensive non-deleterious water wash.
  • the melting point of the flux may be varied by varying the ratio of KCl to NaCl.
  • the ratio of KCl to NaCl should not be less than 1:1.2 and is preferably about 1:1.
  • the ratio may be varied to obtain the desired melting point for each alloy.
  • the most satisfactory flux composition has an aggregate chloride content of from 70% to 88% by weight of the total, the chlorides being present in a potassium chloride-sodium chloride ratio between 1.3:1 and 121.2.
  • the aggregate fluoride content is preferably 12% to 3 0% by weight of the total, with the lithium fluoride rang ing from 3.5% to 20%, the cryolite from 8.5% to 20%, and aluminum fluoride from 0 to 20% of the total. I have found that this combination of lithium fluoride, cryo lite, and aluminum fluoride is more satisfactory than any of the fluoride components singly.
  • the fluorides which are the active constituents of the flux, promote the wetting and flotation of the basis metal oxides (which will be iron oxides if the basis metal is ferrous) and the aluminum oxides.
  • the flux is formulated to clean the surface of the basis metal prior to the melting of the aluminum. Otherwise, agglomeration of the aluminum powder will pre vent complete coverage of the work piece.
  • the flux compositions of Table II provide this necessary cleaning action. Being the first constituent of the bisque to melt, the flux first washes the surface of the basis metal free of the oxides existing or formed on the basis metal prior to the fusion of the flux. Further oxidation is prevented by the flux cover. Then, as the aluminum melts, the flux dissolves and washes away the aluminum oxide on the aluminum powder. When both basis metal and aluminum are free of oxide, the aluminum flows evenly over and wets the surface of the basis metal to form a diffused layer of aluminum in solid solution with the basis metal topped by a layer of pure aluminum or aluminum alloy.
  • the fluorides which are the active constituents of the flux, promote the dissolution, wetting and flotation of the basis metal oxides and the oxides of aluminum.
  • liquid vehicle selected will vary with requirements of the specific application. Although I prefer to use an organic solvent such, for example, as methyl alcohol,
  • the coating cycle should be completed within 30 minutes when water is the vehicle,- or there will be a strong possibility of reaction with the finely divided aluminum powder and the water with possibly dangerous hydrogen generation.
  • Any organic solvent, such as above noted is superior to water as a vehicle, especially in production where'long life of the slip is essential, and the coating cycle frequently may not be completed within 30 minutes I after the slip is made.
  • the suspension agent acts in part as a binder, providing a hard bisque when the slip is dried so that the article coated can be more readily handled.
  • the binding action may be enhanced by addition of any of the coumarone-indene type resins.
  • Methyl alcohol has proven to be an unexpectedly especially good solvent for the aluminizing processes of this invention. It is the only slip vehicle discovered to date which does not require an auxiliary binder to obtain a hard bisque that can be handled after drying. Crystallization on drying provides the necessary dry bisque strength for handling the parts. Hence, the use of methanol obviates the addition of a hydrocarbon binder, such as coumarone-indene resins, which must be burned out in the firing cycle. Higher quality coatings can be obtained with a methanol vehicle for this reason.
  • the thickness of the finished coating may readily be controlled to within one-thousandth of an inch by varying the amount of aluminum powder applied to each unit area of the surface being coated. This may be done either by varying the thickness of the layer of slip deposited on the surface or by varying the concentrate of aluminum powder in the slip. If, however, the aluminum powder is supplied in too great amount, as for the purpose of obtaining an extremely thick coating, it may tend to flow too freely about on the surface when melted during the firing cycle. This may cause the coating alloy to drip from the surface edges or accumulate at low points on the surface of the article, causing the finished coating to be non-uniform in thickness.
  • Low alloy steels are usually coated with 3 mils of aluminum, while the higher alloys of chromium and nickel and chromium-nickel-iron and cobaltnickel-chromium-iron, withother alloying elements, usually require only approximately 1 mil of aluminum.
  • Low alloy parts coated to 3 mils thickness have been tested in air at furnace temperatures of 1500 F. for more than 1000 hours with no measurable oxidation.
  • the 18-8 stainless steels have been tested for 20 hours at 2400 F. with no change in the original thickness of the sample through oxidation. Other results with various metals and alloys have been equally satisfactory.
  • the part to be aluminized may be degreased, then cleaned by such methods as light pickle or light sandblast.
  • light pickle or light sandblast it should be understood that, where in many prior art processes, a heavy pickle and sandblast are required to develop a rough surface to improve adherence, I have found that my process will develop a superior bond equally well on a smooth surface, for example, a No. 4 finish stainless steel, which is classed as a mirror finish.
  • the absence of any need for roughening the surface of the part preparatory to application of my coatings presents many advantages, among which are the saving in time and cost of preparing the surface for coating, and the ability to coat thin sheet material such as metal foil and the like which cannot withstand the extensive treatment required for surface roughening.
  • a further advantage is presentedwhere a relatively thin coating is to be applied to a smooth surface. Since the surface need not be roughened prior to being coated, the coating may be made very thin without sacrifice of appearance due to the inability of such a coating
  • the part After the part has been cleaned it is spray, brush, or dip coated with aluminizing slip and the slip dried, preferably, but not necessarily, in an oven.
  • the part may then be fired to cause the flux and aluminum powder to melt and the aluminum to alloy with the basis metal. Firing should be just long enough to bring the part to heat and hold it approximately 5 minutes.
  • the time at temperature is determined by the extent of diffusion desired. I have found, for example, that for many parts fabricated of .050-.078 sheet, the firing cycle is completed in from 5 to 10 minutes at a temperature range of l220-l500 F.
  • the temperature' is determined by the thickness of the article, the diffusion desired, and the need to melt the flux before excessive oxidationof the basis metal develops.
  • the flux residue may be removed in a hot water wash.
  • a passivating treatment in dilute nitric acid may follow to produce a clean, white surface.
  • Subsequent heat treatment of the thus-coated article may be utilized to improve the oxidation and corrosion resistance of the protective coating layer by causing further diffusion of the aluminum or aluminum alloy into the basis metal.
  • this heat treatment may be carried out in a temperature range of 15001750 F. for about one hour; for the stainless steels and other high alloys, a temperature in the range of 1750-2150" F. is desirable if the time is limited to one hour.
  • the temperature and time are related, and a lower temperature may be successfully employed if the time is extended.
  • this further diifusion and adequate protection develop automatically when the protected part is subjected to service temperatures above900 F. for an extends period of time. Excellent results are obtained, however, without diffusion, and the use of a diffusion cycle is generally applicable to the stainless steels and super alloys to develop an erosion resistance as well as the oxidation and corrosion resistance.
  • Example A employs the preferred step of firing in an inert atmosphere, followed by diffusion treatment which gives better results with a super alloy like L 605.
  • atomized aluminum powder preferably Alcoa atomized aluminum Type 101.
  • ('2) Cycle of operation vapor degrease, light sandblast, apply slip by spraying approximately 7 mils bisque; fire in a nitrogen atmosphere minutes at 1300 F.; rinse off flux in hot water; dip in hot nitric acid solution 140 F. for 1 minute to remove last traces of flux; diffuse in air 3 hours at 1850 F.; vapor blast with 220 grit sand for satin finish, if desired.
  • Cycle of operation vapor degrease; pickle in 50 percent inhibited muriatic acid; neutralize in percent sodium carbonate solution at 200 F apply slip by spraying to a uniform 8 mil bisque; fire in air at 1300 F. for 2 minutes; soak in hot water for 2 minutes to remove flux; air-water blast to remove last of flux.
  • the coating may be easily repaired by cleaning the affected area, brushing or spraying a layer of the slip over the area, and torch or furnace firing at the correct temperature. However, the part may be stripped of the coating and reprocessed, if desired.
  • My improved processes employing cold dipped or sprayed aluminum powder slips are particularly adapted to uses in which the part to be aluminized is of complex geometry or very large size, and to uses in which the aluminum coating must be relatively thicker of very uniform thickness to meet close dimensional tolerances.
  • these processes present many advantages over hot dip processes which are, in general, restricted to use with articles which are of such shape as to permit excess aluminum to be easily drained or shaken therefrom while the aluminum is still in the molten state.
  • the same fluxing agents described above with reference to my aluminum powder process may successfully be used in hot dip processes, however, and that these fiuxing agents will yield outstanding results when so employed.
  • the flux is not mixed with aluminum powder, but is separately applied to the surface of the part being coated, and the surface thus iluxed is then immersed in a bath of molten aluminum.
  • the flux may be applied to the surface of the part in the form of a slurry which is brushed or sprayed onto the surface of the part and permitted to dry thereon, or by melting a quantity of flux to form a liquid bath into which the part is dipped to coat its surface with flux.
  • aluminum used in the claims is defined as meaning a metal selected from the group consisting of aluminum and aluminum base alloys,
  • a method of applying a protective aluminum coating to the surface of a metallic article which comprises coating said article at room temperature with a mixture of aluminum in particle form and a Water soluble flux in an organic vehicle, said mixture containing a minimum of 25 percent by weight of said flux, said flux consisting essentially of from 70 to 88 percent by weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio between 1.311 and 1:12, and from 30 to 12 percent by weight in the aggregate of lithium fluoride, cryolite and aluminum fluoride, with the lithinum fluoride ranging from 3.5 to 20 percent, cryolite from 8.5 to 20 percent, and aluminum fluoride 0 to 20 percent of the total, heating said coated article to a temperature above the melting point of said flux and said aluminum powder to cause a layer of aluminum to wet and cover the article, and removing said water soluble flux by leaching in water.
  • a protective metal coating which comprises coating the su face of the article with a composition including as essential ingredients thereof between 75 to 25 parts by weight of aluminum in particle form and 25 to 75 parts by weight of a fiuxing agent consisting essentially of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists of alkali metal fluorides
  • a fiuxing agent consisting essentially of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists of alkali metal fluorides
  • a fluxing agent consisting essentially of from 70 to 88 percent by Weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio between 13:1 and 1:1.2 and from 30 to 12 percent by weight in the aggregate of lithium fluoride, cryolite and aluminum fluoride with the lithium fluoride ranging from 3.5 to 20 percent, cryolite from 8.5 to 20 percent, and aluminum I fluoride 0 to 20 percent of the total.
  • a method of coating stainless steels and other high alloys as defined in claim 9, wherein the heat treatment consists of subjecting the metallic article to a temperature of from l850-l950 F. for at least one hour. 7
  • a method of coating stainless steels and other high alloys as defined in claim 9, wherein the heat treatment consists of subjecting the article to a temperature of from 17502150 F. for approximately one hour.
  • liquid vehicle is water and the slip also includes a corrosion inhibiting agent and suspension agent.
  • a composition including as essential ingredients between to 25 parts by weight of aluminum in particle form and 25 to 75 parts by weight of a fluxing agent consisting essentially of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists of lithium fluoride, and at least one material from the group consisting of cryolite and aluminum fluoride.
  • a fluxing agent consisting essentially of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists of lithium fluoride, and at least one material from the group consisting of cryolite and aluminum fluoride.
  • An aluminizing slip comprising an aqueous suspension of the composition claimed in claim 20 and containing also a suspension agent and a corrosion inhibiting agent.
  • An aluminizing slip consisting essentially of the composition defined in claim 20 in suspension in an organic solvent.
  • An aluminizing slip consisting essentially of the composition as defined in claim 24, further including a suspension agent.
  • An aluminizing slip consisting essentially of the composition as defined in claim 20, further including a suspension agent.
  • An aluminizing slip consisting essentially of a sus pension of the composition defined in claim 20 in methanol.
  • An aluminizing slip composition as defined in claim 33 having as a further constituent up to 10 parts by weight in the aggregate of at least one metal selected from the group consisting of iron and nickel.
  • An aluminizing slip as defined in claim 35 further comprising a binder agent.
  • a method of applying a protective aluminum coating to the surface of a metallic article which comprises coating said article with a mixture of aluminum in particle form and a water soluble metal halide flux suspended in a liquid vehicle, said mixture containing a minimum of 25% by weight of said flux, heating said article coated with said mixture to a temperature above the rnelting'point of said liux and said aluminum to cause a layer of aluminum to wet and cover the article, and removing said water soluble flux by leaching in water.
  • a method of applying a protective aluminum coating to the surface of a metallic article which comprises coating .s'aid article at room temperature with a mixture of aluminum in particle form and a water soluble flux in a methanol vehicle, said mixture containing a minimum of 25 percent by weight of said flux, said flux consisting essentially of from 70 to 88 percent by weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio between 1.321 and 1:12, and from 30 to 12 percent'by Weight in the aggregate of lithium fluoride, cryolite and aluminum fluoride, with the lithium fluoride ranging from 3.5 to 20 percent, cryolite from 8.5 to 20 percent, and aluminum fluoride 0 to 20 percent of the total, and heating said coated article in an inert atmosphere to a temperature of at least about 1220 F. and maintaining the coated article at said temperature a sufiicient time to cause a layer of aluminum to wet and cover and alloy with said metal article.

Description

United States Patent ALUMINUM COATING PROCESSES AN COMPOSITIONS Alvin R. Stetson, San Diego, Calif.,'assignor to Solar Aircraft Company, San Diego, Calif., a corporation of California No Drawing. Application February 20, 1957 Serial No. 641,245
41 Claims. (Cl. 117---63) This invention relates to methods and compositions for obtaining the deposition of a protective aluminum or aluminum alloy layer on articles of ferrous materials, stainless steels, and super alloys.
This application is a continuation-in-part of my earlier application Serial No. 430,455, filed May 17, 1954, for Aluminum Coating Processes, and now abandoned.
It is well known in the art that aluminum, when applied to ferrous alloys and other metallic alloys, exhibits certain desirable properties being particularly adapted to protecting the basis metal from oxidation for long periods of time at temperatures up to and exceeding 2000 F.
There are many examples of aluminum coating and plating in the prior art. Included among these are processes in which the part to be coated is first covered, as by spraying or dipping, with a suspension of aluminum powder in a liquid vehicle, and then is fired to cause the aluminum to diffuse to form a solid solution and intermetallics with the basis metal of the coated part. A typical process of this type is disclosed in United States Patent No. 1,817,888 to Lowe. Processes in which the part is hot dipped in a bath of molten aluminum to provide an aluminum coating difiusion bonded to the basis metal have also been developed. One process of this general type is disclosed in United States Patent No. 2,569,097 to Grange.
Metal powder suspension and hot dip processes have been known for manyyears and recognized as having many advantages over other coating processes, such as electroplating and molten metal spray, for example. Nevertheless, they have not enjoyed Wide commercial success because the results obtainable by their use have not in the past been consistently reproducible. Also, the coatings produced by such prior processes were not imperforate, uniform, or controllable in thickness frequently were not everywhere securely bonded to the basis metal. The hot dip processes tend to dissolve the basis metal in the aluminum bath and the coating thicknesses are limited. Furthermore, such hot dip processes are not adapted to coating articles of complex form or in which maintenance and coverage of sharp corners, and minimization of distortion are important; Also, certain of these prior processes employ fiuxing agents which remain embedded as particles of slag in the finished coating, thus weakening the coating mechanically and rendering it susceptible to formation of perfora tions or pinholes on subsequent removal of the slag in Patented Mar. 1, 1960 ice with the basis metal. The flux must also be easily washed or otherwise removed from the finished coating, and not be embedded therein so as to cause discontinuities in the coating when removed. In the case of aluminum powder suspension processes in particular, the flux must also act to remove any oxides formed or present on the particles of aluminum powder and to form a continuous flux cover sealing the coating and basis metals from the atmosphere, to prevent further oxidation of these metals during the firing step. 'It is the purpose of this invention to provide improved processes for covering metallic surfaces with protective metal coatings in which the surfaces to be coated are wetted with molten aluminum in the presence of a flux composition which has a fluxing action satisfying the requirements outlined above and which is adapted for use in my aluminizing process including powdered aluminum suspensions. The flux compositions herein disclosed, however, are also excellent for use with molten metal coating processes.
Therefore, a primary object of my present invention is to provide novel methods of developing a highly protective diffused aluminum or aluminum alloy coating of controllable thickness on ferrous and other metallic alloys, including the so'called super alloys.
It is also a major object of this invention to provide novel methods of applying a protective aluminum coating to a metallic surface by wetting the surface with molten aluminum in the presence of a fluxing agent promoting the formation of an imperforate coating of substantially uniform controllable thickness.
A further important object of this invention is to provide novel flux compositions capable of use in aluminizing processes and particularly my new metal powder suspension processes.
Yet another object is the provision of a. series of novel slips particularly useful in carrying out my aluminum powder coating process.
It is also an object to provide novel aluminizing compositions including as auxiliary ingredients agents for controlling fluidity and flow-out of the essential ingredients, in order that aluminum coatings of predetermined thickness and superior protective ability may be obtained.
It is still another object of the present invention to provide new improved aluminum coating processes and a novel coating slip composition therefor using methanol as a vehicle, thereby obtaining unexpected advantages in the coating processes with improved coating results.
It is another object of this invention to provide a new powder suspension coating process utilizing an inert atmosphere in such manner as to obtain improved aluminum coatings, especially for coating parts of large cross section or parts made of the so-called super alloys.
It is still a further object of this invention to provide novel aluminum coating processes and new fluxes therefor which are water soluble, whereby the flux is removable from the coated article by water wash or leaching at low cost on a practical production basis and deleteri ous effects on the coated article during flux removal are avoided.
Another object is the provision of novel aluminizing processes which are extremely useful in repairing and correcting the aluminum coatings on parts on which said coatings have been damaged by forming, welding, or finishing procedures subsequent to initial coating, regardless of the method used to obtain the initial coat.
Still another object is the provision ofprocesses by which may be obtained smooth aluminum coatings characterized by uniform thickness over all areas of complex parts involving louvres, weld seams, sharp corners that must be maintained, joints, and other like complexities.
Another object is to provide quicker, less expensive,
and simpler methods of aluminizing steel and other alloys, which may, be practiced with facilities generally considered standard items in any porcelain enarneling plant.
Further objects and advantages will become apparent as the description proceeds in connection with the appended claims.
' In carrying-out my improved aluminizing process, the metallic surface to be aluminized is wetted with molten aluminum in the presence of one of the fluxing agents described herein. This is accomplished by applying to the surface'of the basis metal article, by spraying or dipping or the like, a slip composed of a suspension of flux and aluminum powder in a liquid vehicle, with or without flow control agents, and heating the article thus coated to a temperature in excess of the melting point of aluminum in air, or preferably in an inert atmosphere such as nitrogen. During the heating or firing cycle, the aluminum becomes molten and evenly covers and uniformly wets and to some degree alloys with the basis metal, producing a superior coating of two phases: (1) an interphase of diffused aluminum, and (2) a surface layer of aluminum covered with flux. The flux is subsequently removed by such means. as hot water wash or leaching.
A properly controlled heat treatment may subsequently be used to improve the oxidation and corrosion resistance of the protective layer by causing further diffusion of the aluminum or aluminum alloy into the basis metal as hereinafter amplified. Excellent results are obtained, however, without such diffusion treatment, and the use of a subsequent diffusion cycle is generally applicable to the stainless steels and super alloys to develop an erosion resistance as well as oxidation and corrosion resistance.
In my aluminum powder suspension process, a first consideration is the provision of a slip comprising essentially aluminum or aluminum alloy powder and a chloride base flux carried in suspension in a liquid vehicle. Auxiliary components of the slip are a suspending agent and a binder. Small amounts of a refractory oxide, iron, nickel or a mixture thereof may also be included in the slip for purposes which will be described hereinafter. Table I shows the general constituency of slips according to my invention:
Of great importance is the fact that the aluminum powder may vary considerably in both chemical composition and physical properties with no deleterious effect on the final protective coating. In general pure aluminum or silicon-aluminum alloys are preferred since these exhibit the most satisfactory resistance to corrosion and oxidation. I do not, however, wish to limit the scope of this invention to these two aluminum materials, since other aluminum alloys containing substantial copper, magnesium, manganese, and other metals, have proved'useful for providing highly satisfactory protective coatings.
Although a grain size of minus 100 mesh plus 400 mesh is preferred when standard dip and spray techniques are used, in general any grain size is useful in my process. The size used is governed by the requirements of the specific application. Also, both atomized aluminum powder and flake aluminum can be successfully used in my process, although atomized powder is the preferred material.
The fluxing agent is a critical factor in the production of satisfactory coatings as pointed out above. My new improved fiuxing agent is a chloride base flux consisting of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists essentially of lithium fluoride and cryolite. Examples of flux compositions I have found satisfactory are listed in Table II.
Compositions 1 through 6 inclusive function satisfactorily on steels having less than about 15 points of carbon, and composition 7 functions satisfactorily on alloys of both low and high carbon content. Since compositions 1 through 6 are the more water soluble they are preferably used where applicable, because they can be readily removed by inexpensive non-deleterious water wash.
The melting point of the flux may be varied by varying the ratio of KCl to NaCl. For example, I find that when pure aluminum or such alloys as copper-aluminum and manganese-aluminum are used as the coating ingredient, the ratio of KCl to NaCl should not be less than 1:1.2 and is preferably about 1:1. However, when a high silicon-aluminum alloy or a magnesium-aluminum alloy is utilized, it is preferred to lower the melting point of the flux by increasing the ratio of KCl to'NaCl to approximately 1.3:1. Of course, the ratio may be varied to obtain the desired melting point for each alloy. In my experience, the most satisfactory flux composition has an aggregate chloride content of from 70% to 88% by weight of the total, the chlorides being present in a potassium chloride-sodium chloride ratio between 1.3:1 and 121.2.
The aggregate fluoride content is preferably 12% to 3 0% by weight of the total, with the lithium fluoride rang ing from 3.5% to 20%, the cryolite from 8.5% to 20%, and aluminum fluoride from 0 to 20% of the total. I have found that this combination of lithium fluoride, cryo lite, and aluminum fluoride is more satisfactory than any of the fluoride components singly. The fluorides, which are the active constituents of the flux, promote the wetting and flotation of the basis metal oxides (which will be iron oxides if the basis metal is ferrous) and the aluminum oxides.
The flux is formulated to clean the surface of the basis metal prior to the melting of the aluminum. Otherwise, agglomeration of the aluminum powder will pre vent complete coverage of the work piece. The flux compositions of Table II provide this necessary cleaning action. Being the first constituent of the bisque to melt, the flux first washes the surface of the basis metal free of the oxides existing or formed on the basis metal prior to the fusion of the flux. Further oxidation is prevented by the flux cover. Then, as the aluminum melts, the flux dissolves and washes away the aluminum oxide on the aluminum powder. When both basis metal and aluminum are free of oxide, the aluminum flows evenly over and wets the surface of the basis metal to form a diffused layer of aluminum in solid solution with the basis metal topped by a layer of pure aluminum or aluminum alloy. The fluorides, which are the active constituents of the flux, promote the dissolution, wetting and flotation of the basis metal oxides and the oxides of aluminum.
The liquid vehicle selected will vary with requirements of the specific application. Although I prefer to use an organic solvent such, for example, as methyl alcohol,
butyl' Cellosolve or Stoddard solvent, I have achieved useful results with water as the slip vehicle. However, i
drogen reaction and corrosion- Ammonium chromate has been found to be a satisfactory inhibitor. However, the coating cycleshould be completed within 30 minutes when water is the vehicle,- or there will be a strong possibility of reaction with the finely divided aluminum powder and the water with possibly dangerous hydrogen generation. Any organic solvent, such as above noted is superior to water as a vehicle, especially in production where'long life of the slip is essential, and the coating cycle frequently may not be completed within 30 minutes I after the slip is made.
When water is the vehicle, sodium carboxyethyl cellulose, sodium alginate and a number of alginic acid derivatives provide a satisfactory suspending agent. With organic solvent vehicles, ethyl cellulose, aluminum stearates, and aluminum octoates are good suspending agents. In either case. the suspension agent acts in part as a binder, providing a hard bisque when the slip is dried so that the article coated can be more readily handled. The binding action may be enhanced by addition of any of the coumarone-indene type resins.
Methyl alcohol (methanol) has proven to be an unexpectedly especially good solvent for the aluminizing processes of this invention. It is the only slip vehicle discovered to date which does not require an auxiliary binder to obtain a hard bisque that can be handled after drying. Crystallization on drying provides the necessary dry bisque strength for handling the parts. Hence, the use of methanol obviates the addition of a hydrocarbon binder, such as coumarone-indene resins, which must be burned out in the firing cycle. Higher quality coatings can be obtained with a methanol vehicle for this reason.
I have found that the addition of small amounts (up to parts by weight) of a finely divided refractory oxide such as alumina to the slip will decrease the fluidity of the flux during the firing cycle, thereby inhibiting it from flowing away from the particles of aluminum and result in a superior cleaning action on the aluminum powder.
The thickness of the finished coating may readily be controlled to within one-thousandth of an inch by varying the amount of aluminum powder applied to each unit area of the surface being coated. This may be done either by varying the thickness of the layer of slip deposited on the surface or by varying the concentrate of aluminum powder in the slip. If, however, the aluminum powder is supplied in too great amount, as for the purpose of obtaining an extremely thick coating, it may tend to flow too freely about on the surface when melted during the firing cycle. This may cause the coating alloy to drip from the surface edges or accumulate at low points on the surface of the article, causing the finished coating to be non-uniform in thickness. I have found that this difficulty may be obviated in heavier coatings, and uniform thickness obtained, by adding small amounts up to parts by weight of iron or nickel or a mixture of these metal powders to the slip. These additives increase the viscosity and limit fiowout of the molten aluminum so that a thicker layer will remain in place on the surface during the firing cycle.
It has been found that a coating which adds 1 to 3 mils to the surface thickness will provide excellent oxidation protection. Low alloy steels are usually coated with 3 mils of aluminum, while the higher alloys of chromium and nickel and chromium-nickel-iron and cobaltnickel-chromium-iron, withother alloying elements, usually require only approximately 1 mil of aluminum. Low alloy parts coated to 3 mils thickness have been tested in air at furnace temperatures of 1500 F. for more than 1000 hours with no measurable oxidation. The 18-8 stainless steels have been tested for 20 hours at 2400 F. with no change in the original thickness of the sample through oxidation. Other results with various metals and alloys have been equally satisfactory.
In Table III are listed seven slips I have found satisfactory, although it should be understood many variations may be made without departing from the spirit of the invention:
TABLE III (Solids shown in grams, liquids in milliliters) Ingredient 1 2 3 4 5 6 7 Aluminum Powder 33. 3 50 50 50 100 100 Flux 66. 7 50 50 50 100 100 100 Ooumarone-Indene Resin 2 0 0 1 0 2 So'lium Alginate 0. 25 Stoddard Solvent 50 50 50 50 0 100 H2O 75 Ammonium Ohrornate ((NBQzCl'OQ 0.4
lumina (-325 Mesh ubular) 0 5 0 0 0 0 Aluminum Stearate 0.5 0. 75 0.75 0 0 0 Aluminum Oetoate--. 0 0 0 0. 13 0 0 Iron and/or niclrel (A gregate) 2. 5 4 Methyl Alcohol (methanol) 100 1 Any organic solvent that will not react with aluminum.
A preferred coating cycle, which may be varied to suit various specific applications without departing from the spirit of my invention, would be as follows:
The part to be aluminized may be degreased, then cleaned by such methods as light pickle or light sandblast. It should be understood that, where in many prior art processes, a heavy pickle and sandblast are required to develop a rough surface to improve adherence, I have found that my process will develop a superior bond equally well on a smooth surface, for example, a No. 4 finish stainless steel, which is classed as a mirror finish. The absence of any need for roughening the surface of the part preparatory to application of my coatings presents many advantages, among which are the saving in time and cost of preparing the surface for coating, and the ability to coat thin sheet material such as metal foil and the like which cannot withstand the extensive treatment required for surface roughening. A further advantage is presentedwhere a relatively thin coating is to be applied to a smooth surface. Since the surface need not be roughened prior to being coated, the coating may be made very thin without sacrifice of appearance due to the inability of such a coating to hide surface roughness.
After the part has been cleaned it is spray, brush, or dip coated with aluminizing slip and the slip dried, preferably, but not necessarily, in an oven. The part may then be fired to cause the flux and aluminum powder to melt and the aluminum to alloy with the basis metal. Firing should be just long enough to bring the part to heat and hold it approximately 5 minutes. The time at temperature is determined by the extent of diffusion desired. I have found, for example, that for many parts fabricated of .050-.078 sheet, the firing cycle is completed in from 5 to 10 minutes at a temperature range of l220-l500 F. The temperature'is determined by the thickness of the article, the diffusion desired, and the need to melt the flux before excessive oxidationof the basis metal develops. Depending upon the article and complexities of design higher temperatures may be used. For coating of thin sheets a temperature range of 1300" F. to 1400 F. is preferred, and on thicker articles in general it is preferred to maintain temperatures below 1509 :F. Where feasible it is preferable on low alloy steels to fire below the transition points of the basis metal to minimize distortions. The best coating temperature in each specific application can be readily determined by test.
Following air cool, the flux residue may be removed in a hot water wash. A passivating treatment in dilute nitric acid may follow to produce a clean, white surface.
It has been found advantageous to use an inert atmosphere in the firing of these aluminum coatings, especially for parts of large cross-section, which can. be heated only slowly in the furnace. Such large parts may oxidize excessively before the flux is molten, unless an inert atmosphere is used, and a heavy oxide will preclude a uniform aluminum coating. Therefore, I have found that it is very desirable to use an inert atmosphere, preferably nitrogen, for firing of these large parts. Also, firing in an inert atmosphere rather than in air makes it possible to obtain better wetting by the aluminum powder when the basis metal article is made certain of the highly alloyed steels and super alloys, like Inconel, Inconel X, and L-605.
' Subsequent heat treatment of the thus-coated article may be utilized to improve the oxidation and corrosion resistance of the protective coating layer by causing further diffusion of the aluminum or aluminum alloy into the basis metal. For the mild steels and other low alloys, this heat treatment may be carried out in a temperature range of 15001750 F. for about one hour; for the stainless steels and other high alloys, a temperature in the range of 1750-2150" F. is desirable if the time is limited to one hour. However, in either case, the temperature and time are related, and a lower temperature may be successfully employed if the time is extended. To an extent, this further diifusion and adequate protection develop automatically when the protected part is subjected to service temperatures above900 F. for an extends period of time. Excellent results are obtained, however, without diffusion, and the use of a diffusion cycle is generally applicable to the stainless steels and super alloys to develop an erosion resistance as well as the oxidation and corrosion resistance.
-It has been found that removal of the oxidation product after diffusion, by a'hydroblast or similar process using 220 mesh or finerfrit, greatly improves the durability of the coating, especially if service is about 1500 F.
Following are two typical specific coating treatments A and B which are illustrative of my preferred powdermetal suspension coating process employing slips using methanol asthe vehicle. Example A employs the preferred step of firing in an inert atmosphere, followed by diffusion treatment which gives better results with a super alloy like L 605.
A. Typical treatment of L-605 alloy 1) Slip composition (No. 7 in Table III above).
100 parts by weight atomized aluminum powder, preferably Alcoa atomized aluminum Type 101.
100 parts by Weight flux composition No. 7 in flux composition Table II, above.
4 parts by weight iron powder325 mesh.
100 ml. methyl alcohol.
('2) Cycle of operation: vapor degrease, light sandblast, apply slip by spraying approximately 7 mils bisque; fire in a nitrogen atmosphere minutes at 1300 F.; rinse off flux in hot water; dip in hot nitric acid solution 140 F. for 1 minute to remove last traces of flux; diffuse in air 3 hours at 1850 F.; vapor blast with 220 grit sand for satin finish, if desired.
B. Typical treatment of mild steel screen 1) Use same slip as outlined above.
(2) Cycle of operation: vapor degrease; pickle in 50 percent inhibited muriatic acid; neutralize in percent sodium carbonate solution at 200 F apply slip by spraying to a uniform 8 mil bisque; fire in air at 1300 F. for 2 minutes; soak in hot water for 2 minutes to remove flux; air-water blast to remove last of flux.
It will be appreciated that these are only two examples of a great variety of possible applications, in accordance has been damaged, I have found that the coating may be easily repaired by cleaning the affected area, brushing or spraying a layer of the slip over the area, and torch or furnace firing at the correct temperature. However, the part may be stripped of the coating and reprocessed, if desired.
My improved processes employing cold dipped or sprayed aluminum powder slips are particularly adapted to uses in which the part to be aluminized is of complex geometry or very large size, and to uses in which the aluminum coating must be relatively thicker of very uniform thickness to meet close dimensional tolerances. As applied to such uses, these processes present many advantages over hot dip processes which are, in general, restricted to use with articles which are of such shape as to permit excess aluminum to be easily drained or shaken therefrom while the aluminum is still in the molten state.
I have found that the same fluxing agents described above with reference to my aluminum powder process may successfully be used in hot dip processes, however, and that these fiuxing agents will yield outstanding results when so employed. In hot dip processes the flux is not mixed with aluminum powder, but is separately applied to the surface of the part being coated, and the surface thus iluxed is then immersed in a bath of molten aluminum. The flux may be applied to the surface of the part in the form of a slurry which is brushed or sprayed onto the surface of the part and permitted to dry thereon, or by melting a quantity of flux to form a liquid bath into which the part is dipped to coat its surface with flux.
Definition: The term aluminum used in the claims is defined as meaning a metal selected from the group consisting of aluminum and aluminum base alloys,
From the above disclosure, it will be seen that I have discovered and developed novel methods of forming highly protective aluminum base coatings on metallic surfaces, which methods have solved the many problems existing in the art. The invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. ments are therefore to be considered in all respects 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:
1. A method of applying a protective aluminum coating to the surface of a metallic article which comprises coating said article at room temperature with a mixture of aluminum in particle form and a Water soluble flux in an organic vehicle, said mixture containing a minimum of 25 percent by weight of said flux, said flux consisting essentially of from 70 to 88 percent by weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio between 1.311 and 1:12, and from 30 to 12 percent by weight in the aggregate of lithium fluoride, cryolite and aluminum fluoride, with the lithinum fluoride ranging from 3.5 to 20 percent, cryolite from 8.5 to 20 percent, and aluminum fluoride 0 to 20 percent of the total, heating said coated article to a temperature above the melting point of said flux and said aluminum powder to cause a layer of aluminum to wet and cover the article, and removing said water soluble flux by leaching in water.
2. The method of applying .to a metallic article a protective metal coating which comprises coating the su face of the article with a composition including as essential ingredients thereof between 75 to 25 parts by weight of aluminum in particle form and 25 to 75 parts by weight of a fiuxing agent consisting essentially of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists of alkali metal fluorides The present embodi-,
and aluminum fluoride, and heating said surface to a temperature at which the aluminum melts and wets and covers the article and alloys with said article.
3. The method of applying a protective metal coating to the surface of a metallic article as defined in claim 2, wherein said first-recited step comprises. coating the surface of the article with a composition that also includes up to parts by weight of alumina for decreasing the fluidity of said fluxing agent in said heating step.
4. A method of applying a protective aluminum coating as defined in claim 3, wherein the recited composition of aluminum, flux and alumina is suspended in a liquid vehicle forming a slip which is applied to said article surface.
5. The method of applying a relatively thick protective metal coating to the surface of a metallic article as defined in claim 2, wherein said first-recited step comprises coating the surface of the article with a composition that also includes up to 5 parts by weight in the aggregate of atleast one metal selected from the group consisting of iron and nickel for inhibiting flow-out of said coating metal in said heating step.
6. A method of applying a protective aluminum coating as defined in claim 5, wherein said composition of aluminum, flux, and last-recited metal is suspended in a liquid vehicle forming a slip which is applied to said article surface.
7. The method of applying a protective metal coating to the surface of a metallic article as defined in claim 2, wherein said balance of the flux consists of lithium fluoride and at least one material from the group consisting of cryolite and aluminum fluoride.
8. The method of applying to the surface of a metallic article a protective metal coating of substantially uniform thickness as defined in claim 7, wherein said firstrecited step comprises covering the surface of the article with a composition that includes a fluxing agent consisting essentially of from 70 to 88 percent by Weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio between 13:1 and 1:1.2 and from 30 to 12 percent by weight in the aggregate of lithium fluoride, cryolite and aluminum fluoride with the lithium fluoride ranging from 3.5 to 20 percent, cryolite from 8.5 to 20 percent, and aluminum I fluoride 0 to 20 percent of the total.
9. The method of claim 2 with the additional step of subjecting the protected metallic article to a subsequent heat treatment to further diffuse the protective aluminum layer into the coated article.
10. A method of coating mild steels and other low alloys as defined in claim 9, wherein the heat treatment consists of subjecting the metallic article to a temperature of from 15001750 F. for at least one hour.
11. A method of coating stainless steels and other high alloys as defined in claim 9, wherein the heat treatment consists of subjecting the metallic article to a temperature of from l850-l950 F. for at least one hour. 7
12. A method of coating stainless steels and other high alloys as defined in claim 9, wherein the heat treatment consists of subjecting the article to a temperature of from 17502150 F. for approximately one hour.
13. The method of claim 9 together with the further step of using a hydroblast to remove the oxidation product resulting from said last-mentioned step.
14. The method of applying a protective aluminum coating as defined in claim 2 wherein said flux is water soluble, further comprising the step of removing said water soluble flux by water wash.
15. The method of applying a protective coating as defined in claim 2, wherein said last-recited step is carried out in an inert atmosphere.
16. The method of claim 2, wherein said last-recited step is performed in a nitrogen atmosphere.
17. A method of applying a protective aluminum coating as defined in claim 2, wherein the recited composition 10 of aluminum and flux is suspended in a liquid vehicle forming a slip which is applied to said article to coat the surface thereof.
18. A method of applying a protective aluminum coating as defined in claim 17, wherein said liquid vehicle is methanol.
19. A method as defined in claim 17, wherein said liquid vehicle is water and the slip also includes a corrosion inhibiting agent and suspension agent.
20. A composition including as essential ingredients between to 25 parts by weight of aluminum in particle form and 25 to 75 parts by weight of a fluxing agent consisting essentially of a metal halide mixture the principal part by weight of which consists of chlorides of sodium and potassium and the balance of which consists of lithium fluoride, and at least one material from the group consisting of cryolite and aluminum fluoride.
21. A composition as claimed in claim 20, wherein said fluxing agent consists esentially of from 70 to 88 percent by weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio betwen 1.3:1 and 1:1.2 and from 3 0 to 12 percent by weight in the aggregate of lithium fluoride, aluminum fluoride, and cryolite, with the lithium fluoride ranging from 3.5 to 20 percent, the cryolite from 8.5 to 20 percent, and aluminum fluoride 0 to 20 percent of the total.
22. An aluminizing slip comprising an aqueous suspension of the composition claimed in claim 20 and containing also a suspension agent and a corrosion inhibiting agent.
23. An aluminizing slip as defined in claim 22, Wherein said suspension agent consists of one or more materials selected from the group consisting of sodium carboxymethylcellulose, sodium alginate and algenic acid derivatives, and said corrosion inhibiting agent is ammonium chromate.
24-. An aluminizing slip consisting essentially of the composition defined in claim 20 in suspension in an organic solvent.
25. An aluminizing slip consisting essentially of the composition as defined in claim 24, further including a suspension agent.
26. An aluminizing composition as defined in claim 20, having as a further constituent up to 5 parts by weight of alumina.
27. An aluminizing composition as defined in claim 20, having as a further constituent up to 5 parts by weight of at least one metal selected from the group consisting of iron and nickel.
28. An aluminizing slip consisting essentially of the composition as defined in claim 20, further including a suspension agent.
29. An aluminizing slip as defined in claim 28, further comprising a binder agent.
30. An aluminizing slip as defined in claim 29, wherein said binder agent is one of the coumarone-indene type resins.
31. An aluminizing slip as defined in claim 28, wherein said suspension agent consists of one or more materials selected from a group consisting of ethyl cellulose, aluminum stearates and aluminum octoates.
32. An aluminizing composition as defined in claim 20, having as a further constituent up to 10 parts by weight in the aggregate of at least one metal selected from the group consisting of iron and nickel.
33. An aluminizing slip consisting essentially of a sus pension of the composition defined in claim 20 in methanol.
34. An aluminizing slip composition as defined in claim 33, having as a further constituent up to 10 parts by weight in the aggregate of at least one metal selected from the group consisting of iron and nickel.
35. An aluminizing slip composition as defined in claim 34, wherein approximate proportions of said ingredients 11 are 1130- parts aluminum powder, 1 part flux, 80 parts methanol and 4 parts iron, in parts by weight.
36. An aluminizing slip as defined in claim 35, further comprising a binder agent.
i 37. An aluminizing slip as defined in claim 36, wherein said binder agent is one of the coumarone-indene type resins.
38. A method of applying a protective aluminum coating to the surface of a metallic article which comprises coating said article with a mixture of aluminum in particle form and a water soluble metal halide flux suspended in a liquid vehicle, said mixture containing a minimum of 25% by weight of said flux, heating said article coated with said mixture to a temperature above the rnelting'point of said liux and said aluminum to cause a layer of aluminum to wet and cover the article, and removing said water soluble flux by leaching in water.
39. A method of applying a protective aluminum coating to the surface of a metallic article as defined in claim 38, wherein said mixture of aluminum and flux includes between 25 to 75% by weight of said flux, and wherein said mixture is applied to said article at room temperature.
40. A method of applying a protective aluminum coating to the surface of a metallic article as defined in claim 39, wherein said article is coated with a mixture of said aluminum and flux in an organic vehicle.
41, A method of applying a protective aluminum coating to the surface of a metallic article which comprises coating .s'aid article at room temperature with a mixture of aluminum in particle form and a water soluble flux in a methanol vehicle, said mixture containing a minimum of 25 percent by weight of said flux, said flux consisting essentially of from 70 to 88 percent by weight in the aggregate of chlorides of potassium and sodium present in a potassium chloride-sodium chloride ratio between 1.321 and 1:12, and from 30 to 12 percent'by Weight in the aggregate of lithium fluoride, cryolite and aluminum fluoride, with the lithium fluoride ranging from 3.5 to 20 percent, cryolite from 8.5 to 20 percent, and aluminum fluoride 0 to 20 percent of the total, and heating said coated article in an inert atmosphere to a temperature of at least about 1220 F. and maintaining the coated article at said temperature a sufiicient time to cause a layer of aluminum to wet and cover and alloy with said metal article.
References Cited in the file of this patent UNITED STATES PATENTS 1,155,947 Van Allen 2.. Oct. 5, 1915 1,565,496 Pfeil Dec. 15, 1925 1,817,888 Lowe Aug. 4, 1931 2,403,706 Bryant July 9, 1946 2,466,971 Shawcross Apr. 12, 1949 2,507,956 Bruno et a1 May 16, 1950 2,541,813 Prise-l1 Feb. 13, 1951 2,569,097 Grange et a1. Sept. 25, 1951 2,641,551 Smith et al. June 9, 1953 2,671,737 Jominy et al Mar. 9, 1954 2,785,084 Lundin Mar. 12, 1957

Claims (1)

1. A METHOD OF APPLYING A PROTECTIVE ALUMINUM COATING TO THE SURFACE OF A METALLIC ARTICLE WHICH COMPRISES COATING SAID ARTICLE AT ROOM TEMPERATURE WITH A MIXTURE OF ALUMINUM IN PARTICLE FROM AND A WATER SOLUBLE FLUX IN AN ORGANIC VEHICLE, SAID MIXTURE CONTAINING A MINIMUM OF 25 PERCENT BY WEIGHT OF SAID FLUX, SAID FLUX CONSISTING ESSENTIALLY OF FROM 70 TO 88 PERCENT BY WEIGHT IN THE AGGREGATE OF CHORIDES OF POTASSIUM AND SODIUM PRESENT IN A POTASSIUM CHLORIDE-SODIUM CHLORIDE RATIO BETWEEN 1.3:1 AND 1:1.2, AND FROM 30 TO 12 PERCENT BY WEIGHT IN THE AGGREGATE OF LITHIUM FLORIDE, CRYLOITE AND ALUMINUM FLUORIDE, WITH THE LITHINUM FLUORIDE RANGING FROM 3.5 TO 20 PERCENT, CRYOLITE FROM 8.5 TO 20 PERCENT, AND ALUMINUM FLUORIDE 0 TO 20 PERCENT OF THE TOTAL, HEATING SAID COATED ARTICLE TO A TEMPERATURE ABOVE THE MELTING POINT OF SAID FLUX AND SAID ALUMINUM POWDER TO CAUSE A LAYER ALUMINUM TO WET AND COVER THE ARTICLE, AND REMOVING SAID WATER SOLUBLE FLUX BY LEACHING IN WATER.
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Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3254969A (en) * 1961-11-24 1966-06-07 Misco Prec Casting Company Method of aluminizing chromium alloys and oxidation resistant article produced thereby
US3345197A (en) * 1963-08-09 1967-10-03 Howmet Corp Aluminizing process and composition
US3478413A (en) * 1966-05-09 1969-11-18 Trw Inc Aluminide coating braze stop-off
US3607369A (en) * 1968-09-11 1971-09-21 Union Carbide Corp Method for forming porous aluminum layer
US3753668A (en) * 1970-04-16 1973-08-21 Api Corp Diffusion coated metallic substrate
US4532152A (en) * 1982-03-05 1985-07-30 Elarde Vito D Fabrication of a printed circuit board with metal-filled channels
US4711666A (en) * 1987-02-02 1987-12-08 Zyp Coatings, Inc. Oxidation prevention coating for graphite
US4769074A (en) * 1987-02-02 1988-09-06 Zyp Coatings, Inc. Binder/suspension composition and method of preparation thereof
US5512382A (en) * 1995-05-08 1996-04-30 Alliedsignal Inc. Porous thermal barrier coating
US5562998A (en) * 1994-11-18 1996-10-08 Alliedsignal Inc. Durable thermal barrier coating
US6103386A (en) * 1994-11-18 2000-08-15 Allied Signal Inc Thermal barrier coating with alumina bond inhibitor
US6482537B1 (en) 2000-03-24 2002-11-19 Honeywell International, Inc. Lower conductivity barrier coating
US6884515B2 (en) 2002-12-20 2005-04-26 General Electric Company Afterburner seals with heat rejection coats
US6884460B2 (en) 2002-12-20 2005-04-26 General Electric Company Combustion liner with heat rejection coats
US6884461B2 (en) 2002-12-20 2005-04-26 General Electric Company Turbine nozzle with heat rejection coats
US20070272334A1 (en) * 2006-05-25 2007-11-29 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
DE102007025602A1 (en) * 2006-12-29 2008-07-03 Hoesch Metallurgie Gmbh Solid metal bath fluxing agent for treating a metal bath comprises at least two separate solid components
US20090014093A1 (en) * 2006-05-25 2009-01-15 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US20090200363A1 (en) * 2008-02-13 2009-08-13 Trane International Inc. Braze Ring
US20100065549A1 (en) * 2006-12-11 2010-03-18 Alan Belohlav System and Method of Brazing Using Non-silver Metals
USRE42329E1 (en) 2002-07-24 2011-05-10 Lucas-Milhaupt, Inc. Flux cored preforms for brazing
US20110123824A1 (en) * 2007-05-25 2011-05-26 Alan Belohlav Brazing material
WO2013178216A1 (en) * 2012-05-30 2013-12-05 Dechema-Forschungsinstitut Method for coating a substrate containing cobalt, nickel and/or iron with a corrosion-resistant layer
US8753455B2 (en) 2005-11-10 2014-06-17 Handy + Harman Brazing material containing a flux
US9157134B2 (en) 2009-10-26 2015-10-13 Lucas-Milhaupt, Inc. Low silver, low nickel brazing material
US20160376693A1 (en) * 2015-06-24 2016-12-29 General Electric Company Diffusion coatings for metal-based substrate and methods of preparation thereof
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Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1155947A (en) * 1914-10-21 1915-10-05 Lloyd M Mills Lock for bottle and jars.
US1565496A (en) * 1925-12-15 Process eor making and combining corrobe-resisting metals
US1817888A (en) * 1927-09-15 1931-08-04 Doherty Res Co Protective coating (alborizing)
US2403706A (en) * 1944-04-06 1946-07-09 Nasa Metallic coating
US2466971A (en) * 1945-02-15 1949-04-12 Aluminum Co Of America Method of chemically coating aluminum
US2507956A (en) * 1947-11-01 1950-05-16 Lithographic Technical Foundat Process of coating aluminum
US2541813A (en) * 1947-11-08 1951-02-13 Gen Electric Calorizing process
US2569097A (en) * 1951-02-20 1951-09-25 Gen Motors Corp Method of coating ferrous metal with aluminum or an aluminum alloy
US2641551A (en) * 1949-07-20 1953-06-09 Gulf Oil Corp Metal coating composition
US2671737A (en) * 1950-10-10 1954-03-09 Chrysler Corp Aluminum coating process and flux
US2785084A (en) * 1952-12-13 1957-03-12 Helen Maric Lundin Coating ferrous metals with aluminum

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1565496A (en) * 1925-12-15 Process eor making and combining corrobe-resisting metals
US1155947A (en) * 1914-10-21 1915-10-05 Lloyd M Mills Lock for bottle and jars.
US1817888A (en) * 1927-09-15 1931-08-04 Doherty Res Co Protective coating (alborizing)
US2403706A (en) * 1944-04-06 1946-07-09 Nasa Metallic coating
US2466971A (en) * 1945-02-15 1949-04-12 Aluminum Co Of America Method of chemically coating aluminum
US2507956A (en) * 1947-11-01 1950-05-16 Lithographic Technical Foundat Process of coating aluminum
US2541813A (en) * 1947-11-08 1951-02-13 Gen Electric Calorizing process
US2641551A (en) * 1949-07-20 1953-06-09 Gulf Oil Corp Metal coating composition
US2671737A (en) * 1950-10-10 1954-03-09 Chrysler Corp Aluminum coating process and flux
US2569097A (en) * 1951-02-20 1951-09-25 Gen Motors Corp Method of coating ferrous metal with aluminum or an aluminum alloy
US2785084A (en) * 1952-12-13 1957-03-12 Helen Maric Lundin Coating ferrous metals with aluminum

Cited By (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3254969A (en) * 1961-11-24 1966-06-07 Misco Prec Casting Company Method of aluminizing chromium alloys and oxidation resistant article produced thereby
US3345197A (en) * 1963-08-09 1967-10-03 Howmet Corp Aluminizing process and composition
US3478413A (en) * 1966-05-09 1969-11-18 Trw Inc Aluminide coating braze stop-off
US3607369A (en) * 1968-09-11 1971-09-21 Union Carbide Corp Method for forming porous aluminum layer
US3753668A (en) * 1970-04-16 1973-08-21 Api Corp Diffusion coated metallic substrate
US4532152A (en) * 1982-03-05 1985-07-30 Elarde Vito D Fabrication of a printed circuit board with metal-filled channels
US4711666A (en) * 1987-02-02 1987-12-08 Zyp Coatings, Inc. Oxidation prevention coating for graphite
US4769074A (en) * 1987-02-02 1988-09-06 Zyp Coatings, Inc. Binder/suspension composition and method of preparation thereof
US5562998A (en) * 1994-11-18 1996-10-08 Alliedsignal Inc. Durable thermal barrier coating
US6103386A (en) * 1994-11-18 2000-08-15 Allied Signal Inc Thermal barrier coating with alumina bond inhibitor
US6395343B1 (en) 1994-11-18 2002-05-28 Alliedsignal Durable thermal barrier coating
US5512382A (en) * 1995-05-08 1996-04-30 Alliedsignal Inc. Porous thermal barrier coating
US5624721A (en) * 1995-05-08 1997-04-29 Alliedsignal Inc. Method of producing a superalloy article
US6482537B1 (en) 2000-03-24 2002-11-19 Honeywell International, Inc. Lower conductivity barrier coating
USRE44343E1 (en) 2002-07-24 2013-07-09 Lucas-Milhaupt, Inc. Flux cored preforms for brazing
USRE42329E1 (en) 2002-07-24 2011-05-10 Lucas-Milhaupt, Inc. Flux cored preforms for brazing
US6884461B2 (en) 2002-12-20 2005-04-26 General Electric Company Turbine nozzle with heat rejection coats
US20050129967A1 (en) * 2002-12-20 2005-06-16 General Electric Company Afterburner seals with heat rejection coats
US7094446B2 (en) * 2002-12-20 2006-08-22 General Electric Company Method for applying a coating system including a heat rejection layer to a substrate surface of a component
US6884460B2 (en) 2002-12-20 2005-04-26 General Electric Company Combustion liner with heat rejection coats
US6884515B2 (en) 2002-12-20 2005-04-26 General Electric Company Afterburner seals with heat rejection coats
US8753455B2 (en) 2005-11-10 2014-06-17 Handy + Harman Brazing material containing a flux
US9095937B2 (en) 2006-05-25 2015-08-04 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US7858204B2 (en) 2006-05-25 2010-12-28 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering
US20110089222A1 (en) * 2006-05-25 2011-04-21 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US20090014093A1 (en) * 2006-05-25 2009-01-15 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US8274014B2 (en) 2006-05-25 2012-09-25 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US20070272334A1 (en) * 2006-05-25 2007-11-29 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US10071445B2 (en) 2006-05-25 2018-09-11 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of making and using same
US20100065549A1 (en) * 2006-12-11 2010-03-18 Alan Belohlav System and Method of Brazing Using Non-silver Metals
US8507833B2 (en) 2006-12-11 2013-08-13 Lucas-Milhaupt, Inc. System and method of brazing using non-silver metals
DE102007025602A1 (en) * 2006-12-29 2008-07-03 Hoesch Metallurgie Gmbh Solid metal bath fluxing agent for treating a metal bath comprises at least two separate solid components
US20110123824A1 (en) * 2007-05-25 2011-05-26 Alan Belohlav Brazing material
US20100219231A1 (en) * 2008-02-13 2010-09-02 Trane International Inc. Braze Ring
US20090200363A1 (en) * 2008-02-13 2009-08-13 Trane International Inc. Braze Ring
US9157134B2 (en) 2009-10-26 2015-10-13 Lucas-Milhaupt, Inc. Low silver, low nickel brazing material
WO2013178216A1 (en) * 2012-05-30 2013-12-05 Dechema-Forschungsinstitut Method for coating a substrate containing cobalt, nickel and/or iron with a corrosion-resistant layer
US9731383B2 (en) 2014-07-09 2017-08-15 Bellman-Melcor Development, Llc Filler metal with flux for brazing and soldering and method of using same
US20160376693A1 (en) * 2015-06-24 2016-12-29 General Electric Company Diffusion coatings for metal-based substrate and methods of preparation thereof
US9909019B2 (en) * 2015-06-24 2018-03-06 General Electric Company Diffusion coatings for metal-based substrate and methods of preparation thereof
US10744601B2 (en) 2015-08-07 2020-08-18 Bellman-Melcor Development, Llc Bonded brazing ring system and method for adhering a brazing ring to a tube

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