US3617359A - Process for the vapor deposition of metals - Google Patents
Process for the vapor deposition of metals Download PDFInfo
- Publication number
- US3617359A US3617359A US817591*A US3617359DA US3617359A US 3617359 A US3617359 A US 3617359A US 3617359D A US3617359D A US 3617359DA US 3617359 A US3617359 A US 3617359A
- Authority
- US
- United States
- Prior art keywords
- titanium
- chromium
- substrate
- hydrogen
- halides
- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/06—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of metallic material
- C23C16/08—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of metallic material from metal halides
Definitions
- Hassell and Harold Levine ABSTRACT A method of vapor depositing metal on a substrate by reducing titanium and chromium halides with hydrogen under controlled conditions to chemically vapor deposit titanium and chromium alloys on the substrate. Best results are obtained when the halides are introduced into the deposition chamber as a gaseous mixture with an inert gas carner.
- This invention relates to the deposition of metals upon a substrate by the reductionof the halides of the metals with hydrogen.
- alloy deposits of titanium and chromium for example, are 'chemi cally vapor deposited upon a substrate from controlled mixtures of titanium and chromium halides-by reduction with hydrogen.
- one or more metals are deposited upon a surface of a substrate by the reduction of halides of one or more metals with hydrogen diffused through the substrate.
- Refractory metals such as tantalum, molybdenum, columbium (niobium) and tungsten by way of examples, are especially desirable for applications requiring high strength at elevated temperature, particularly where ease'of fabrication and ductility are needed. However, before any of these metals can satisfy a wide range of requirements, they must receive an oxidation resistant coating. Titanium and chromium, being metallurgicallycompatible with refractory metals, form a good base coating which, when alloyed with silicon, will protect them against oxidation.
- objects of the present invention are to provide a method for the simultaneous production of titanium and chromium halides for the codeposition of titanium and chromium upon a substrate; to provide a method of controlling the composition of the gas stream containing said metal halides; to provide a method for obtaining a uniform mixture of the two halide gas streams; to eliminate the presence of hydrogen chloride in the reactant mixture; to provide a method for controlling the rate of reaction and thickness of a chemically vapor deposited metal upon a substrate by diffusing hydrogen through the substrate, and to provide a method for forming uniform coatings of a chemically vapor deposited metal upon a substrate.
- controlled uniform mixtures of titanium and chromium halides are obtained by flowing an appropriate titanium halide in an inert gas stream over heated chromium and titanium metals, contained in separate compartments within a generating chamber.
- the relative concentration of halides obtained from the chamber can be controlled by regulating the amount of titanium halide gas entering each compartment, and by regulating the composition of the metals in each chamber.
- the process of the present invention is operationally convenient because, in contrast with the prior art in which the flow rate of hydrogen chloride must be controlled, only the flow of titanium halide must be controlled since no hydrogen chloride is used, The possibility of unreacted hydrogen chloride being present to inhibit the subsequent reduction of the metals is also eliminated which resultsin higher deposition rates. Furthermore, the method of the present invention does not require that hydroscopic halides of either titanium or chromium be handled in the solid state. Also the equipment and materials contained in the halide generating chamber can be heated under vacuum, if necessary, to remove any absorbed impurity gases without harming the subsequent deposition process. This is not usually possible when halide materials are contained in the reactor itself.
- FIGS. 1 and 2 illustrate suitable apparatus for the generation of controlled mixtures of titanium. and chromium halides and the simultaneous codeposition of titanium and chromium metals from these halides upon asubstrate;
- FIG. 3 is a plot of the composition of the coating against the composition of the reactant gas phase.
- FIGS. 4 and 5 illustrate suitable apparatus for controlling the rate of reaction and thickness of chemically vapor deposited metals upon a substrate by diffusing hydrogen through the substrate.
- FIG. 1 depicts a coating reactor for the reduction of metallic halides with hydrogen.
- the reactor is comprised of a furnace 1 containing a resistance heaters (not shown), a halide inlet 2 at the top of the reactor, areducing hydrogen inlet 3 at the upper part of one side of the reactor, a substrate 4 to be coated and located directly beneath the furnace l, a substrate support 5, a substrate heater 14 mounted below the substrate upon the substrate support and an exhaust outlet 6 at the bottom of the reactor.
- a halide generating chamber comprised of a quartz chamber 7 which is divided into two compartments 8 and 9, containing, for example, titanium metal 10 and chromium metal 11, respectively.
- a divider plate 12 is located at one end of the chamber and an exit 13 is provided at the other end for the impingement of the mixture of gases upon the substrate 4.
- Controlled mixtures of titanium trichloride (TiCl,) and chromium dichloride (CrCl may be obtained by flowing titanium tetrachloride (TiCL) in a stream of inert gas such as argon or helium over heated chromium and titanium metals contained in the compartments 8 and 9 within the chamber 7. The following reactions are believed to occur:
- the metals are preferably maintained at a temperature between 750 C. and 900 C.
- the preferred manner of controlling the relative concentration of chlorides obtained from the chamber 7 is by regulating the amount of titanium tetrachloride gas (TiCL) entering each compartment. This may be accomplished by varying the size and number of holes in the divider plate 12, and by regulating the composition of the metals in each chamber, by which is meant that the same metal, chromium or titanium, is placed in both chambers, that chromium is placed in one chamber and titanium in the other, or that a mixture of titanium and chromium is placed in one chamber and either titanium or chromium is placed in the other.
- TiCL titanium tetrachloride gas
- This control of the ratio of titanium chloride to chromium chloride in the reactant gas stream allows control of the composition of the alloy deposited upon the substrate.
- Hydrogen gas in excess of the stoichiometric amount which passes from inlet 3 downward through the reactor along the outside walls of the chloride generating chamber 7, then mixes into the stream of chlorides in the proximity of the heated substrate 4 to reduce the chlorides and produce pure titanium and chromium according to the following equation:
- the relative concentration of halides in the reactant gas stream may also be controlled by the use of a single compartment generating chamber containing alloys of titanium and chromium, as shown in FIG. 2.
- the composition of the alloy placed in the chamber determines the composition of the alloy deposited upon the substrate.
- FIG. 2 depicts a single compartment halide generating chamber comprised of a quartz chamber 21 which contains an alloy of titanium and chromium 22, the rest of the apparatus being the same as shown in FIG. 1.
- a titanium halide in an inert carrier gas stream is admitted through inlet 23 and reduced by the metals in the alloy to form a stream of reactant gases which exits through outlet 24.
- a titanium-chromium alloy 22 composed of 75% titanium and 25% chromium is placed in the chamber 21.
- variation of the proportion of the titanium tetrachloride gas passed through each of the compartments and the selection of the metals placed in either compartment determine the composition of the alloy deposited upon the substrate 4.
- titanium is placed in one compartment and chromium in the other.
- Variation of the ratio of the amount of tetrachloride gas passed through the chromium compartment to the amount passed through the titanium compartment further varies the ratio of chromium to titanium in the alloy deposit.
- Alloys of high chromium metal concentration for example 90 to 95% chromium and to 5% titanium, have been obtained by placing only chromium metal in the chloride generating chamber. (A high concentration of chromium results because chromium is more readily reduced by the hydrogen gas). Alloys of high titanium concentration have been produced by substituting a mixture of titanium and chromium metal in the chromium compartment 9, which is then reacted with the titanium tetrachloride. The alloys deposited utilizing this chloride source are about 95% titanium and 5% chromium, which is the result of the preferential formation of titanium chloride over chromium chloride in the gas phase, causing the chromium concentration in the alloy to be correspondingly low.
- the graph in FIG. 3 expresses the composition of the coating deposit to be expected from any particular ratio of titanium trichloride to chromium dichloride in the reactant gas mixture over a range from near zero to about l9.
- the coating method of the present invention also offers a practical solution to the problem of corrosion through the application of a corrosion resistant protective layer by chemical vapor deposition to a cheaper, stronger material such as low carbon steel. Application of these materials may be carried out following formation into the final desired shape.
- hydrogen may be passed through the iron to form a coating by reaction of the outward difi'using hydrogen with a gaseous halide of one or more metals at the surface of the permeable substrate to be coated.
- the reaction thus occurs at the interface of the solid containing hydrogen and the gas phase containing the reducible metal halides.
- the hydrogen is contained on the inside of the tube and the gaseous metal halides are maintained on the exterior of the tube.
- gaseous metal halides are contained within the tube and the hydrogen is introduced from the exterior.
- a liquid or a fused salt solution containing a reducible metal halide is substituted for the gaseous metal halides.
- the reaction occurs at the interface of the solid and the liquid containing the reducible metal halide.
- the thickness of the metal coating is controlled inherently since the thicker portions of the coating tend to produce a slower rate of diffusion. Thus a leveling effect is produced.
- the state of absorbed hydrogen at the metal surface is atomic rather than molecular.
- Atomic hydrogen is a better reducing agent than molecular hydrogen by approximately 50 K- cal/mole, the energy necessary to separate the hydrogen atoms. This permits reaction at temperatures and rates which are impossible with molecular hydrogen. such as the reduction of titanium chloride at 700 to 800 C.
- FIG. 4 illustrates suitable apparatus for practicing an embodiment of the difi'usion coating method described above, wherein the interior or exterior surface of a hydrogen permeable tube may be coated by the reaction of hydrogen and a gaseous metal halide by way of example.
- the coating reactor comprises a furnace 41 provided with heating coils 42 which maintain the furnace at the appropriate deposition temperature. lnlets 43 and 44 are located at the top of the reactor.
- the substrate to be coated consists of a tube 45 which is attached to inlet 44 within the chamber 46. Exhaust outlet 47 at the end of tube 45 and exhaust outlet 48 at the bottom of the chamber 46 are for the exit of the spent gasses.
- hydrogen is introduced through inlet 44 and gaseous metal halides through inlet 43.
- gaseous metal halides are introduced through the inlet 44 and hydrogen through inlet 43.
- EXAMPLE Ill The reactor was first brought to an operating temperature of 1000 C.
- An argon carrier gas stream containing 1.7 atomic titanium trichloride (Ticl was admitted through inlet 44 and passed through a steel tube 45 having a wall thickness of 32 mils.
- Hydrogen gas was admitted through inlet 43 and allowed to purge the chamber 46 of atmospheric gases. Thereafter, the exhaust valve 48-was closed and the hydrogen gas was maintained in chamber46 at a pressure of 25 p.s.i.
- An operating time of 30 minutes produced a coating of titanium on the interior of the tube on the order of l mil in thickness.
- FIG. 5 illustrates suitable apparatus for practicing another embodiment of the diffusion coating method of the invention, wherein a flat hydrogen-permeable sheet may be coated by the reaction of hydrogen and a reducible metal halide containcd in a fused salt solution.
- FIG. 5 depicts a flat iron plate 51 to be coated on its upper surface, mounted between a hydrogen chamber 52 provided with heating coils 53 and a fused salt chamber 54 also provided with heating coils 55. These coils are shown separate but they need not be.
- Hydrogen chamber 52 is further provided with an inlet 56 near the top of one side of said chamber and an outlet 57 near the bottom of the other side.
- the invention supplied a method for the simultaneous production of titanium and chromium halides for the codeposition of titanium and chromium upon a substrate which advantageously provides a control of the composition of the gas stream containing said metal halides, and results in uniform mixtures of the two halide gas streams.
- a further advantage of the invention is the elimination of hydrogen chloride from the reactant mixture, thus favoring sition of titanium.
- the invention also provides a metho for controlling the rate of reaction and thickness of a chemically vapor deposited metal upon a substrate by the diffusion of hydrogen through the substrate, thereby forming uniform coatings.
- a method of forming an alloy deposit of chromium and titanium upon a heated substrate the process of simultaneously reducing halides of chromium and titanium with hydrogen in a gaseous steam at a surface of said substrate, including the step of passing a mixture consisting essentially of an inert gas and a titanium halide gas through a heated chamber, said chamber containing chromium or an alloy of chromium and titanium, to produce the gaseous mixture of the halides of titanium and chromium.
- gaseous mixture of halides comprises titanium trichloride and chromium dichloride.
- said heated chamber comprises two compartments and one of said compartments contains titanium or a titanium-chromium alloy and the other compartment contains chromium or a chromiumtitanium alloy.
- a method according to claim 3 wherein the amount of titanium halide gas entering each of said compartments is regulated by varying the size and number of holes in a divider plate located at the entrance to said two compartments.
- one compartment of said heated chamber contains a mixture of titanium and chromium or an alloy of titanium and chromium and the other compartment contains titanium or a titanium-chromium.
Landscapes
- Chemical & Material Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Vapour Deposition (AREA)
Abstract
A method of vapor depositing metal on a substrate by reducing titanium and chromium halides with hydrogen under controlled conditions to chemically vapor deposit titanium and chromium alloys on the substrate. Best results are obtained when the halides are introduced into the deposition chamber as a gaseous mixture with an inert gas carrier.
Description
United States Patent Inventor Gene F. Wakefield [56] References Cited Ri h r T UNITED STATES PATENTS Q 5 3 2,885,310 5/1959 Olson etal 117/107.2x 1 7 9 6 966 2,887,407 5/1959 Koch 117/1072 ,1 3,188,230 6/1965 Bakish m1. 117/107.2x Pat-1033281607- 3,190,771 6/1965 McLean etal.... 117/107x Patented Nov-2,1971 3,252,823 5/1966 Jacobsen etal... 117/107.2x Asslsnee Texlnmumenslnmmmed 3265 521 8/1966 Spacil 117/1072 Dallas, Tex.
PROCESS FOR THE VAPOR DEPOSITION OF METALS 6 Claims, 5 Drawing Figs.
US. Cl. ..ll7/l07.2R
Int. Cl C23c 11/02 Field of Search 1 17/1072,
Primary Examiner-Alfred L. Leavitt Assistant Examiner-Wm. E. Hall Attorneys-Samuel M. Mims, Jr., James 0. Dixon, Andrew M.
Hassell and Harold Levine ABSTRACT: A method of vapor depositing metal on a substrate by reducing titanium and chromium halides with hydrogen under controlled conditions to chemically vapor deposit titanium and chromium alloys on the substrate. Best results are obtained when the halides are introduced into the deposition chamber as a gaseous mixture with an inert gas carner.
TICI +ARGON,Z
HYDR 0GEN,3
FURNACE,/
DIVIDER PLATE 1? QUARTZ CHAMBER] TITANIUM COMPARTMENT,8
CHROMIUM COMPARTMENT,9 TITANIUM METAL,/0
CHROMIUM METAL,
SUBSTRATE, 4 SUBSTRATE HEATER,/4
SUBSTRATE SUPPORT,5
lNVEN'lOR EXHAUST,6 Gene Wakefield PROCESS FOR THE VAPOR DEPOSITION OF METALS This is a division of application serial number 579,963 tiled Sept. 16, 1966 now U.S. Pat. No. 3,428,607.
This invention relates to the deposition of metals upon a substrate by the reductionof the halides of the metals with hydrogen. According to one aspect of the invention, alloy deposits of titanium and chromium, for example, are 'chemi cally vapor deposited upon a substrate from controlled mixtures of titanium and chromium halides-by reduction with hydrogen. According to another aspect of the invention, one or more metals are deposited upon a surface of a substrate by the reduction of halides of one or more metals with hydrogen diffused through the substrate.
Refractory metals, such as tantalum, molybdenum, columbium (niobium) and tungsten by way of examples, are especially desirable for applications requiring high strength at elevated temperature, particularly where ease'of fabrication and ductility are needed. However, before any of these metals can satisfy a wide range of requirements, they must receive an oxidation resistant coating. Titanium and chromium, being metallurgicallycompatible with refractory metals, form a good base coating which, when alloyed with silicon, will protect them against oxidation.
While many techniques can be employed to prepare coatings of titanium and chromium, several features make the vapor streaming technique of chemical vapor deposition especially desirable. Process parameters may beindividually and accurately controlled, allowing high reproducibility. Also, the chemical vapor deposition process possesses the inherent ability to form an overlay coating, that is, a coating which can be applied to a substrate with minimum interaction.
Attempts to coreduce titanium and chromium halides produced separately and individually introduced into a deposition chamber fail to yield satisfactory codeposits of titanium and chromium alloys upon a substrate, because of nonuniform mixing of the two halide gas streams and inadequate control of the composition of the reactant gas stream. Furthermore, in the separate production of, for example, the chlorides of the metals by the reaction of hydrogen chloride gas with the individual metals, 'the unreacted hydrogen chloride gas tends to inhibit the deposition of titanium metal.
Accordingly, objects of the present invention are to provide a method for the simultaneous production of titanium and chromium halides for the codeposition of titanium and chromium upon a substrate; to provide a method of controlling the composition of the gas stream containing said metal halides; to provide a method for obtaining a uniform mixture of the two halide gas streams; to eliminate the presence of hydrogen chloride in the reactant mixture; to provide a method for controlling the rate of reaction and thickness of a chemically vapor deposited metal upon a substrate by diffusing hydrogen through the substrate, and to provide a method for forming uniform coatings of a chemically vapor deposited metal upon a substrate.
in the preferred embodiment of the present invention, controlled uniform mixtures of titanium and chromium halides are obtained by flowing an appropriate titanium halide in an inert gas stream over heated chromium and titanium metals, contained in separate compartments within a generating chamber. The relative concentration of halides obtained from the chamber can be controlled by regulating the amount of titanium halide gas entering each compartment, and by regulating the composition of the metals in each chamber.
The process of the present invention is operationally convenient because, in contrast with the prior art in which the flow rate of hydrogen chloride must be controlled, only the flow of titanium halide must be controlled since no hydrogen chloride is used, The possibility of unreacted hydrogen chloride being present to inhibit the subsequent reduction of the metals is also eliminated which resultsin higher deposition rates. Furthermore, the method of the present invention does not require that hydroscopic halides of either titanium or chromium be handled in the solid state. Also the equipment and materials contained in the halide generating chamber can be heated under vacuum, if necessary, to remove any absorbed impurity gases without harming the subsequent deposition process. This is not usually possible when halide materials are contained in the reactor itself.
Other objects, features and advantages of the invention will become more readily understood from the following detailed description taken in conjunction with the appended claims and attached drawings in which:
FIGS. 1 and 2 illustrate suitable apparatus for the generation of controlled mixtures of titanium. and chromium halides and the simultaneous codeposition of titanium and chromium metals from these halides upon asubstrate;
FIG. 3 is a plot of the composition of the coating against the composition of the reactant gas phase; and
FIGS. 4 and 5 illustrate suitable apparatus for controlling the rate of reaction and thickness of chemically vapor deposited metals upon a substrate by diffusing hydrogen through the substrate.
Referring now to the FIGS. in detail, FIG. 1 depicts a coating reactor for the reduction of metallic halides with hydrogen. The reactor is comprised of a furnace 1 containing a resistance heaters (not shown), a halide inlet 2 at the top of the reactor, areducing hydrogen inlet 3 at the upper part of one side of the reactor, a substrate 4 to be coated and located directly beneath the furnace l, a substrate support 5, a substrate heater 14 mounted below the substrate upon the substrate support and an exhaust outlet 6 at the bottom of the reactor.
Mounted within the furnace l is a halide generating chamber comprised of a quartz chamber 7 which is divided into two compartments 8 and 9, containing, for example, titanium metal 10 and chromium metal 11, respectively. A divider plate 12 is located at one end of the chamber and an exit 13 is provided at the other end for the impingement of the mixture of gases upon the substrate 4.
Although the method of the present invention is described with reference to titanium and chromium chlorides, it is to be understood that other halides of titanium and chromium may also be utilized in accordance with the principles of the inven-. tion by selection of the appropriate apparatus, reactants, flow rates and temperatures. Accordingly, the detailed description given hereinafter is to be taken as exemplary.
Controlled mixtures of titanium trichloride (TiCl,) and chromium dichloride (CrCl may be obtained by flowing titanium tetrachloride (TiCL) in a stream of inert gas such as argon or helium over heated chromium and titanium metals contained in the compartments 8 and 9 within the chamber 7. The following reactions are believed to occur:
The metals are preferably maintained at a temperature between 750 C. and 900 C.
The preferred manner of controlling the relative concentration of chlorides obtained from the chamber 7 is by regulating the amount of titanium tetrachloride gas (TiCL) entering each compartment. This may be accomplished by varying the size and number of holes in the divider plate 12, and by regulating the composition of the metals in each chamber, by which is meant that the same metal, chromium or titanium, is placed in both chambers, that chromium is placed in one chamber and titanium in the other, or that a mixture of titanium and chromium is placed in one chamber and either titanium or chromium is placed in the other. Thus, for example, to deposit an alloy of nearly equal concentration of titanium and chromium, titanium is placed in one compartment 8 and chromium in the other compartment 9. The incoming gaseous titanium tetrachloride from inlet 2, carried in a stream of argon for example, is divided by the plate 12, one part flowing through compartment 8 and the other part flowing through compartment 9. Leaving the individual compartments after severally passing through the metals therewithin, the gases reunite in a common gas stream 13 at the base of the reactor. This control of the ratio of titanium chloride to chromium chloride in the reactant gas stream allows control of the composition of the alloy deposited upon the substrate.
Hydrogen gas in excess of the stoichiometric amount, which passes from inlet 3 downward through the reactor along the outside walls of the chloride generating chamber 7, then mixes into the stream of chlorides in the proximity of the heated substrate 4 to reduce the chlorides and produce pure titanium and chromium according to the following equation:
1350 C. ZTiClg SCrC]; 6H: 2T1 30: 121101 The pure titanium and chromium then deposit in alloy form upon the substrate 4, the HCl gas and other spent gases exit through exhaust 6. The temperature of deposition, which is preferably maintained from about 1,250 C. to about l,375 C. by the substrate heater 14, which is heated by any suitable means (not shown) to the indicated temperature, also affects the ratio of metals in the deposit, higher temperatures favoring titanium reduction; lower temperatures favoring chromium reduction. Coatings formed by the utilization of the abovedescribed chloride source and deposition process are uniform in appearance and thickness.
The relative concentration of halides in the reactant gas stream may also be controlled by the use of a single compartment generating chamber containing alloys of titanium and chromium, as shown in FIG. 2. The composition of the alloy placed in the chamber determines the composition of the alloy deposited upon the substrate.
FIG. 2 depicts a single compartment halide generating chamber comprised of a quartz chamber 21 which contains an alloy of titanium and chromium 22, the rest of the apparatus being the same as shown in FIG. 1. A titanium halide in an inert carrier gas stream is admitted through inlet 23 and reduced by the metals in the alloy to form a stream of reactant gases which exits through outlet 24.
To deposit an alloy of nearly equal concentration of titanium and chromium by way of example, a titanium-chromium alloy 22 composed of 75% titanium and 25% chromium is placed in the chamber 21. The incoming gaseous titanium tetrachloride from inlet 23, carried in a stream of argon for example, is reduced by the titanium and chromium in the alloy to form a mixture of titanium trichloride and chromium dichloride which exits through outlet 24 leading to the deposition site.
In the use of the two compartment halide generating chamber as illustrated in FIG. 1, variation of the proportion of the titanium tetrachloride gas passed through each of the compartments and the selection of the metals placed in either compartment determine the composition of the alloy deposited upon the substrate 4. As described above, to deposit an alloy of nearly equal concentration of titanium and chromiurn, titanium is placed in one compartment and chromium in the other. Variation of the ratio of the amount of tetrachloride gas passed through the chromium compartment to the amount passed through the titanium compartment further varies the ratio of chromium to titanium in the alloy deposit. Alloys of high chromium metal concentration, for example 90 to 95% chromium and to 5% titanium, have been obtained by placing only chromium metal in the chloride generating chamber. (A high concentration of chromium results because chromium is more readily reduced by the hydrogen gas). Alloys of high titanium concentration have been produced by substituting a mixture of titanium and chromium metal in the chromium compartment 9, which is then reacted with the titanium tetrachloride. The alloys deposited utilizing this chloride source are about 95% titanium and 5% chromium, which is the result of the preferential formation of titanium chloride over chromium chloride in the gas phase, causing the chromium concentration in the alloy to be correspondingly low.
The following examples further serve to illustrate typical applications of the basic principles of the invention to the simultaneous codeposition of chromium and titanium within a deposition unit of the type illustrated by FIG. 1.
EXAMPLE I To prepare an alloy deposit of the composition 45% titanium and 55% chromium metal, one compartment of the chloride generating chamber was appropriately filled with titanium, the other with chromium. A helium carrier gas stream containing 0.6 mole titanium tetrachloride was passed into the chloride generating chamber at the rate of 7 liters/min. The divider plate contained 10 holes on the titanium side and two holes on the chromium side, the holes being 40 mils in diameter. The ratio of titanium trichloride (TiCl,) to chromium dichloride (CrCl,) in the reactant gas mixture was 13 to l. The rate of flow of the reducing hydrogen stream was 7 liters/min. The resulting mixture of gases was reacted at the deposition site at the temperature of [370 C. The above conditions produced a deposition rate of l mg./cm.'/min.
EXAMPLE II To prepare an alloy deposit of the composition 93% chromium and 7% titanium metal, both compartments of the chloride generating chamber were appropriately filled with chromium. An argon carrier gas stream containing 1.4 mole titanium tetrachloride was passed into the chloride generating chamber at the rate of 5 liters/min. The ratio of titanium trichloride to chromium dichloride in the reactant gas mixture was about 2 to l. The rate of flow of the reducing hydrogen stream was 4 liters/min. The resulting mixture of gases was reacted at the deposition site at a temperature of l,350 C. The above conditions produced a deposition rate of ZmflcmF/min.
The graph in FIG. 3 expresses the composition of the coating deposit to be expected from any particular ratio of titanium trichloride to chromium dichloride in the reactant gas mixture over a range from near zero to about l9.
The coating method of the present invention also offers a practical solution to the problem of corrosion through the application of a corrosion resistant protective layer by chemical vapor deposition to a cheaper, stronger material such as low carbon steel. Application of these materials may be carried out following formation into the final desired shape.
For coating metals which have a high permeability to hydrogen, such as iron, hydrogen may be passed through the iron to form a coating by reaction of the outward difi'using hydrogen with a gaseous halide of one or more metals at the surface of the permeable substrate to be coated. The reaction thus occurs at the interface of the solid containing hydrogen and the gas phase containing the reducible metal halides. For coating the outside of objects such as tubes, the hydrogen is contained on the inside of the tube and the gaseous metal halides are maintained on the exterior of the tube. To coat the interior of the tube, gaseous metal halides are contained within the tube and the hydrogen is introduced from the exterior.
In another embodiment of this diffusion coating technique, a liquid or a fused salt solution containing a reducible metal halide is substituted for the gaseous metal halides. In this case the reaction occurs at the interface of the solid and the liquid containing the reducible metal halide.
Two advantages are obtained by utilizing the diffusion coating method: (1) the thickness of the metal coating is controlled inherently since the thicker portions of the coating tend to produce a slower rate of diffusion. Thus a leveling effect is produced. (2) According to the prevailing view, the state of absorbed hydrogen at the metal surface is atomic rather than molecular. Atomic hydrogen is a better reducing agent than molecular hydrogen by approximately 50 K- cal/mole, the energy necessary to separate the hydrogen atoms. This permits reaction at temperatures and rates which are impossible with molecular hydrogen. such as the reduction of titanium chloride at 700 to 800 C. However, applicant does not wish to be bound by the accuracy of the above stated prevailing view.
FIG. 4 illustrates suitable apparatus for practicing an embodiment of the difi'usion coating method described above, wherein the interior or exterior surface of a hydrogen permeable tube may be coated by the reaction of hydrogen and a gaseous metal halide by way of example. The coating reactor comprises a furnace 41 provided with heating coils 42 which maintain the furnace at the appropriate deposition temperature. lnlets 43 and 44 are located at the top of the reactor. The substrate to be coated consists of a tube 45 which is attached to inlet 44 within the chamber 46. Exhaust outlet 47 at the end of tube 45 and exhaust outlet 48 at the bottom of the chamber 46 are for the exit of the spent gasses. To coat the outside of the tube 45, hydrogen is introduced through inlet 44 and gaseous metal halides through inlet 43. To coat the inside of tube 45, gaseous metal halides are introduced through the inlet 44 and hydrogen through inlet 43.
The following example illustrates a typical application of the basic principles of the diffusion coating method of the invention within a deposition unit of the type illustrated by FIG. 4.
EXAMPLE Ill The reactor was first brought to an operating temperature of 1000 C. An argon carrier gas stream containing 1.7 atomic titanium trichloride (Ticl was admitted through inlet 44 and passed through a steel tube 45 having a wall thickness of 32 mils. Hydrogen gas was admitted through inlet 43 and allowed to purge the chamber 46 of atmospheric gases. Thereafter, the exhaust valve 48-was closed and the hydrogen gas was maintained in chamber46 at a pressure of 25 p.s.i. An operating time of 30 minutes produced a coating of titanium on the interior of the tube on the order of l mil in thickness.
FIG. 5 illustrates suitable apparatus for practicing another embodiment of the diffusion coating method of the invention, wherein a flat hydrogen-permeable sheet may be coated by the reaction of hydrogen and a reducible metal halide containcd in a fused salt solution. FIG. 5 depicts a flat iron plate 51 to be coated on its upper surface, mounted between a hydrogen chamber 52 provided with heating coils 53 and a fused salt chamber 54 also provided with heating coils 55. These coils are shown separate but they need not be. Hydrogen chamber 52 is further provided with an inlet 56 near the top of one side of said chamber and an outlet 57 near the bottom of the other side.
The following example illustrates a typical application of the basic principles of the diffusion coating method of the invention within a deposition unit of the type illustrated by FIG. 5.
EXAMPLE IV To coat a flat iron plate 5 mils thick, a mixture of 5 to atomic chromium trichloride (CrCl in a potassium chloride, lithium chloride liquid eutectic was maintained in the de chamber 54. l-Iydrogen gas was admitted through inlet 56 and allowed to purge the chamber 52 of atmospheric gases. Thereafter, the exhaust valve 57 was closed and the hydrogen gas maintained in chamber 52 at a pressure of 25 p.s.i. The apparatus was operated at 850 C. for 30 minutes to produce a crystalline deposit of chromium 0.5 mil thick on the upper surface of the flat iron plate.
Thus it may be seen that the invention supplied a method for the simultaneous production of titanium and chromium halides for the codeposition of titanium and chromium upon a substrate which advantageously provides a control of the composition of the gas stream containing said metal halides, and results in uniform mixtures of the two halide gas streams. A further advantage of the invention is the elimination of hydrogen chloride from the reactant mixture, thus favoring sition of titanium. The invention also provides a metho for controlling the rate of reaction and thickness of a chemically vapor deposited metal upon a substrate by the diffusion of hydrogen through the substrate, thereby forming uniform coatings.
It is to be understood that the above-described embodiments of the invention are merely illustrative of its principles. The apparatus shown and described may be modified to coat substrates of varying configurations using reducible metal halides contained in either a gaseous stream or a fused salt solution. Various other modifications may be devised by those skilled in the art to fit the character of the substrate to be coated without departing from the spirit and scope of the invention as defined by the appended claims.
What is claimed is:
1. In a method of forming an alloy deposit of chromium and titanium upon a heated substrate, the process of simultaneously reducing halides of chromium and titanium with hydrogen in a gaseous steam at a surface of said substrate, including the step of passing a mixture consisting essentially of an inert gas and a titanium halide gas through a heated chamber, said chamber containing chromium or an alloy of chromium and titanium, to produce the gaseous mixture of the halides of titanium and chromium.
2. The method of claim 1 wherein said gaseous mixture of halides comprises titanium trichloride and chromium dichloride.
3. A method according to claim 1 wherein said heated chamber comprises two compartments and one of said compartments contains titanium or a titanium-chromium alloy and the other compartment contains chromium or a chromiumtitanium alloy.
4. A method according to claim 3 wherein the amount of titanium halide gas entering each of said compartments is regulated by varying the size and number of holes in a divider plate located at the entrance to said two compartments.
5. The method of claim 3 wherein said titanium halide is titanium tetrachloride.
6. The method of claim 3 wherein one compartment of said heated chamber contains a mixture of titanium and chromium or an alloy of titanium and chromium and the other compartment contains titanium or a titanium-chromium.
Claims (5)
- 2. The method of claim 1 wherein said gaseous mixture of halides comprises titanium trichloride and chromium dichloride.
- 3. A method according to claim 1 wherein said heated chamber comprises two compartments and one of said compartments contains titanium or a titanium-chromium alloy and the other compartment contains chromium or a chromium-titanium alloy.
- 4. A method according to claim 3 wherein the amount of titanium halide gas entering each of said compartments is regulated by varying the size and number of holes in a divider plate located at the entrance to said two compartments.
- 5. The method of claim 3 wherein said titanium halide is titanium tetrachloride.
- 6. The method of claim 3 wherein one compartment of said heated chamber contains a mixture of titanium and chromium or an alloy of titanium and chromium and the other compartment contains titanium or a titanium-chromium.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US81759169A | 1969-01-13 | 1969-01-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3617359A true US3617359A (en) | 1971-11-02 |
Family
ID=25223421
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US817591*A Expired - Lifetime US3617359A (en) | 1969-01-13 | 1969-01-13 | Process for the vapor deposition of metals |
Country Status (1)
Country | Link |
---|---|
US (1) | US3617359A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3996400A (en) * | 1973-04-25 | 1976-12-07 | Centre Stephanois De Recherches Mecaniques Hydromecanique Et Frottement | Method for surface coating ferrous alloy parts |
US4343836A (en) * | 1979-07-26 | 1982-08-10 | United States Of America As Represented By The United States Department Of Energy | One-directional uniformly coated fibers, method of preparation, and uses therefor |
FR2577944A1 (en) * | 1985-02-22 | 1986-08-29 | Procedyne Corp | HARD SURFACE COATINGS OF METALS IN FLUIDIZED BEDS |
US4699082A (en) * | 1983-02-25 | 1987-10-13 | Liburdi Engineering Limited | Apparatus for chemical vapor deposition |
US5575902A (en) * | 1994-01-04 | 1996-11-19 | Chevron Chemical Company | Cracking processes |
US5593571A (en) * | 1993-01-04 | 1997-01-14 | Chevron Chemical Company | Treating oxidized steels in low-sulfur reforming processes |
US5723707A (en) * | 1993-01-04 | 1998-03-03 | Chevron Chemical Company | Dehydrogenation processes, equipment and catalyst loads therefor |
US5849969A (en) * | 1993-01-04 | 1998-12-15 | Chevron Chemical Company | Hydrodealkylation processes |
US5989733A (en) * | 1996-07-23 | 1999-11-23 | Howmet Research Corporation | Active element modified platinum aluminide diffusion coating and CVD coating method |
US6258256B1 (en) * | 1994-01-04 | 2001-07-10 | Chevron Phillips Chemical Company Lp | Cracking processes |
US6274113B1 (en) | 1994-01-04 | 2001-08-14 | Chevron Phillips Chemical Company Lp | Increasing production in hydrocarbon conversion processes |
US6419986B1 (en) | 1997-01-10 | 2002-07-16 | Chevron Phillips Chemical Company Ip | Method for removing reactive metal from a reactor system |
US6548030B2 (en) | 1991-03-08 | 2003-04-15 | Chevron Phillips Chemical Company Lp | Apparatus for hydrocarbon processing |
USRE38532E1 (en) | 1993-01-04 | 2004-06-08 | Chevron Phillips Chemical Company Lp | Hydrodealkylation processes |
US20050097991A1 (en) * | 2003-09-19 | 2005-05-12 | Angel Sanjurjo | Methods and apparatuses for producing metallic compositions via reduction of metal halides |
US20080050608A1 (en) * | 2006-08-25 | 2008-02-28 | Mcfaul Surry D | Metal coating process and product |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2885310A (en) * | 1954-09-13 | 1959-05-05 | Ohmite Mfg Company | Method and apparatus for making film resistors |
US2887407A (en) * | 1957-08-05 | 1959-05-19 | Manufacturers Chemical Corp | Preparation of diffusion coatings on metals |
US3188230A (en) * | 1961-03-16 | 1965-06-08 | Alloyd Corp | Vapor deposition process and device |
US3190771A (en) * | 1962-01-11 | 1965-06-22 | Electra Mfg Company | Filament for vacuum deposition apparatus and method of making it |
US3252823A (en) * | 1961-10-17 | 1966-05-24 | Du Pont | Process for aluminum reduction of metal halides in preparing alloys and coatings |
US3265521A (en) * | 1963-01-02 | 1966-08-09 | Gen Electric | Method of forming a composite member with a metallic coating |
-
1969
- 1969-01-13 US US817591*A patent/US3617359A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2885310A (en) * | 1954-09-13 | 1959-05-05 | Ohmite Mfg Company | Method and apparatus for making film resistors |
US2887407A (en) * | 1957-08-05 | 1959-05-19 | Manufacturers Chemical Corp | Preparation of diffusion coatings on metals |
US3188230A (en) * | 1961-03-16 | 1965-06-08 | Alloyd Corp | Vapor deposition process and device |
US3252823A (en) * | 1961-10-17 | 1966-05-24 | Du Pont | Process for aluminum reduction of metal halides in preparing alloys and coatings |
US3190771A (en) * | 1962-01-11 | 1965-06-22 | Electra Mfg Company | Filament for vacuum deposition apparatus and method of making it |
US3265521A (en) * | 1963-01-02 | 1966-08-09 | Gen Electric | Method of forming a composite member with a metallic coating |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3996400A (en) * | 1973-04-25 | 1976-12-07 | Centre Stephanois De Recherches Mecaniques Hydromecanique Et Frottement | Method for surface coating ferrous alloy parts |
US4343836A (en) * | 1979-07-26 | 1982-08-10 | United States Of America As Represented By The United States Department Of Energy | One-directional uniformly coated fibers, method of preparation, and uses therefor |
US4699082A (en) * | 1983-02-25 | 1987-10-13 | Liburdi Engineering Limited | Apparatus for chemical vapor deposition |
FR2577944A1 (en) * | 1985-02-22 | 1986-08-29 | Procedyne Corp | HARD SURFACE COATINGS OF METALS IN FLUIDIZED BEDS |
US6548030B2 (en) | 1991-03-08 | 2003-04-15 | Chevron Phillips Chemical Company Lp | Apparatus for hydrocarbon processing |
USRE38532E1 (en) | 1993-01-04 | 2004-06-08 | Chevron Phillips Chemical Company Lp | Hydrodealkylation processes |
US5593571A (en) * | 1993-01-04 | 1997-01-14 | Chevron Chemical Company | Treating oxidized steels in low-sulfur reforming processes |
US5723707A (en) * | 1993-01-04 | 1998-03-03 | Chevron Chemical Company | Dehydrogenation processes, equipment and catalyst loads therefor |
US5849969A (en) * | 1993-01-04 | 1998-12-15 | Chevron Chemical Company | Hydrodealkylation processes |
US5866743A (en) * | 1993-01-04 | 1999-02-02 | Chevron Chemical Company | Hydrodealkylation processes |
US6258256B1 (en) * | 1994-01-04 | 2001-07-10 | Chevron Phillips Chemical Company Lp | Cracking processes |
US6274113B1 (en) | 1994-01-04 | 2001-08-14 | Chevron Phillips Chemical Company Lp | Increasing production in hydrocarbon conversion processes |
US5575902A (en) * | 1994-01-04 | 1996-11-19 | Chevron Chemical Company | Cracking processes |
US6291014B1 (en) | 1996-07-23 | 2001-09-18 | Howmet Research Corporation | Active element modified platinum aluminide diffusion coating and CVD coating method |
US5989733A (en) * | 1996-07-23 | 1999-11-23 | Howmet Research Corporation | Active element modified platinum aluminide diffusion coating and CVD coating method |
US6419986B1 (en) | 1997-01-10 | 2002-07-16 | Chevron Phillips Chemical Company Ip | Method for removing reactive metal from a reactor system |
US6551660B2 (en) | 1997-01-10 | 2003-04-22 | Chevron Phillips Chemical Company Lp | Method for removing reactive metal from a reactor system |
US20050097991A1 (en) * | 2003-09-19 | 2005-05-12 | Angel Sanjurjo | Methods and apparatuses for producing metallic compositions via reduction of metal halides |
US7559969B2 (en) * | 2003-09-19 | 2009-07-14 | Sri International | Methods and apparatuses for producing metallic compositions via reduction of metal halides |
US20080050608A1 (en) * | 2006-08-25 | 2008-02-28 | Mcfaul Surry D | Metal coating process and product |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3617359A (en) | Process for the vapor deposition of metals | |
US4623400A (en) | Hard surface coatings for metals in fluidized beds | |
US4803127A (en) | Vapor deposition of metal compound coating utilizing metal sub-halides and coated metal article | |
US3188230A (en) | Vapor deposition process and device | |
Carlsson et al. | Chemical vapor deposition | |
US4699082A (en) | Apparatus for chemical vapor deposition | |
JP3875491B2 (en) | Chemical properties of precursors for chemical vapor deposition of ruthenium or ruthenium oxide. | |
US3771976A (en) | Metal carbonitride-coated article and method of producing same | |
US3368914A (en) | Process for adherently depositing a metal carbide on a metal substrate | |
US3540920A (en) | Process of simultaneously vapor depositing silicides of chromium and titanium | |
GB2256876A (en) | Aluminium gas diffusion coating using heated aluminium particles | |
US4698244A (en) | Deposition of titanium aluminides | |
US2887407A (en) | Preparation of diffusion coatings on metals | |
US2689807A (en) | Method of coating refractory metal articles | |
US3343979A (en) | Method for depositing a tungsten-rhenium metal alloy on a substrate | |
US2604395A (en) | Method of producing metallic bodies | |
US3061463A (en) | Metallic diffusion | |
US3516850A (en) | Process for metal coating a hydrogen permeable material | |
US3018194A (en) | Metal plating process | |
US5230847A (en) | Method of forming refractory metal free standing shapes | |
US4890574A (en) | Internal reactor for chemical vapor deposition | |
US2815299A (en) | Method of producing an adherent molybdenum coating on a metal substrate | |
US3637422A (en) | Dispersion-hardened tungsten alloy | |
EP0117542A2 (en) | Chemical vapor deposition of metal compound coatings utilizing metal sub-halides | |
US3471321A (en) | Vapor coating aluminum on ironcontaining substrate |