[go: up one dir, main page]

US3762884A - Nickel aluminide coated low alloy stainless steel - Google Patents

Nickel aluminide coated low alloy stainless steel Download PDF

Info

Publication number
US3762884A
US3762884A US00190316A US3762884DA US3762884A US 3762884 A US3762884 A US 3762884A US 00190316 A US00190316 A US 00190316A US 3762884D A US3762884D A US 3762884DA US 3762884 A US3762884 A US 3762884A
Authority
US
United States
Prior art keywords
percent
aluminum
nickel
stainless steel
chromium
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
Application number
US00190316A
Inventor
S Grisaffe
E Klechke
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Aeronautics and Space Administration NASA
Original Assignee
National Aeronautics and Space Administration NASA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by National Aeronautics and Space Administration NASA filed Critical National Aeronautics and Space Administration NASA
Application granted granted Critical
Publication of US3762884A publication Critical patent/US3762884A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/16Selection of particular materials
    • 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/02Pretreatment of the material to be coated
    • 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/36Embedding in a powder mixture, i.e. pack cementation only one element being diffused
    • C23C10/48Aluminising
    • C23C10/50Aluminising of ferrous surfaces
    • 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/18After-treatment
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/923Physical dimension
    • Y10S428/924Composite
    • Y10S428/926Thickness of individual layer specified
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/937Sprayed metal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/938Vapor deposition or gas diffusion
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12458All metal or with adjacent metals having composition, density, or hardness gradient
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12937Co- or Ni-base component next to Fe-base component

Definitions

  • ABSTRACT Low alloy austenitic stainless steel is protected from oxidative corrosion and erosion at high temperatures in the presence of exhaust gases from internal combustion engines by flame-spraying a layer between about 0.003 inches and about 0.007 inches thick of an alloy of 80 percent nickel and 20 percent chromium on the steel base, and thereafter converting the layer to an intermetallic chromium containing nickel aluminide coating by a low temperature aluminum cementation process.
  • a cementation pack comprising 96 percent aluminum oxidc, 2 percent aluminum, l percent sodium chloride, and 1 percent ammonium bifluoride is placed on the nickel-chromium layer in an inert atmosphere for a period between four hours and 24 hours at l400F to 1600F to form an intermetallic chromium containing nickel aluminide coating containing 40 to 60 atomic percent aluminum.
  • the coated steel is highly resistant to oxidation corrosion and erosion by high temperature exhaust gases from internal combustion engines. It is particularly useful in the construction of thermal reactors'for exhaust systems in automobiles for the control of pollution from exhausts.
  • This invention relates to a coating for low alloy austenitic stainless steel to render the steel highly resistant to oxidation corrosion and erosion from exhaust gases in internal combustion engines.
  • the engine exhaust of automotive internal combustion engines contains carbon monoxide, carbon dioxide, nitrogen dioxide, unburned hydrocarbons, sulfur compounds, and other corrosive products which are exhausted into the atmosphere in the absence of means for controlling such emissions.
  • Recently federal regulations have been imposed which set progressively lower allowable engine exhaust levels for such combustion products. Minor adjustments in carburetion and spark control and the like are no longer satisfactory in meeting such requirements.
  • One way such engine emissions can be reduced further in the future in order to meet the requirements of controlling agencies is by the utilization of thermal exhaust converters or reactors. Such thermal reactors replace the exhaust manifold.
  • thermal exhaust reactors are required in large quantities, for example, up to fifteen million units a year at the present automotive industry production rate, it is essential that such thermal reactors be capable of being produced at the minimum possible cost.
  • One approach to avoid utilization of expensive components is to use protective coatings on the metal materi als used in such thermal reactors.
  • U.S. Pat. No. 3,338,733, Rowady discloses metallic surface coatings resistant to corrosion and wear such as that to which internal combustion valves are exposed.
  • a steel base is first preheated to 1300 to l800F and a nickel-chromium alloy is applied by flame-spraying.
  • the coated object is then subjected to a first diffusion step at temperatures of l800 to 2250F to promote alloying between the coated alloy and the base metal.
  • the coating subsequently may be coated with an aluminum layer by first preheating the coated base to l200 to l400F and then thereafter dipping the article in a molten bath of aluminum or applying the aluminum by a flame-spraying technique. After the aluminum coating has been applied, the object is then heated to 1500F to 2l00F to diffuse and alloy the aluminum into the nickel-chromium alloy.
  • the present invention provides a low alloy austenitic stainless steel article highly resistant to oxidation corrosion and erosion by a coating which comprises a chromium containing nickel aluminid-e applied by the process of this invention.
  • Low alloy stainless steel material I coated according to this invention exhibits oxidation resistance equal to or better than the oxidation resistance obtained on many highly allloyed steels either uncoated, or coated with expensive alloys and other compounds, many applied by complex processes.
  • a relatively low cost stock article suitable for use in constructing thermal exhaust reactors is provided by this invention by using low alloy austenitic stainless steel. It provides resistance to corrosion using steels having only a relatively small amount of nickel.
  • an oxidation corrosion and erosion resistant article is provided by depositing on a low nickel alloy austenitic stainless steel basea layer between about 0.003 to 0.007 inch, preferably 0.005 inch, thick of a nickel-chromium alloy such as 80 percent nickel-20 percent chromium, by means of flame-spraying or plasma spraying, then converting the nickel-chromium alloy layer to one comprising an intermetallic compound, as opposed to an alloy.
  • a low tem' perature aluminum pack cemcntation process at l400 l600F for four to 24 hours which in a single process step also serves to diffusion bond the coating to the steel substrate.
  • the chromium-containing nickel aluminide coating contains from about 40 to about atomic percent of aluminum.
  • test specimens of austenitic 304 stainless steel (Fel8Cr8Ni0.008C) were cut from 1/16 inch thick sheet stock. One set were inch X Ht: inches, and an other were 1 inch X 2 inches. Prior to coating according to this invention the specimens were ball milled in a ceramic mill with no. 36 alumina grit and water and thereafter vapor blasted with l mesh alumina, degreased, and then ultrasonically cleaned in trichloroethylene.
  • the samples are then coated with a 0.005 inch layer of 80 percent nickel-20 percent chromium by flamespraying, using a conventional spray gun adapted for spraying nickel-chromium alloy fed in wire form.
  • the thickness of the layer can be between 0.003 and 0.007 inches. Layers having thicknesses at the lower end of the range have less stresses while the thicker layers have longer lives.
  • the nickel-chromium layer is then converted to a chromium containing nickel aluminide intermetallic compound by a pack cementation step by treating the layer with a high activity aluminum pack.
  • the pack employed comprises 96 percent aluminum oxide, 2 percent aluminum, 1 percent sodium chloride, and l percent ammonium bifluoride.
  • the coating is treated in a furnace under an inert atmosphere such as argon for from four to 24 hours, preferably for 16 hours, at l600F.
  • the process deposits approximately mg. of aluminum per square centimeter which reacts to form a chromium enriched nickel aluminide intermetallic protective layer on the low alloy austenitic stainless steel and at the same time forms a diffusion bond between the coating and the substrate.
  • the inch X 1% inches samples are then placed in a horizontal multitube furnace on high purity recrystallized alumina boats. Air is passed over the specimens at the rate of two cubic feet per hour. One set of specimens is heated for 100 hours at 2000F, with cycling to room temperature. The cycles consist of hours at test temperature followed by cooling to room temperature. At room temperature the specimens are lightly brushed to remove any oxide scale and weighed to 0.05 mg. per square centimeter accuracy. A second set of specimens is similarly cycled for 600 hours at l800F. Excellent resistance to oxidation corrosion and erosion was evident from visual examination, x-ray diffraction, microscopic and metallographic analysis.
  • the specimens gain about 3 mg. per square centimeter after 600 hours exposure to the l800F cycling tests.
  • the metal temperature is measured by thermocouples which are mounted on adjacent uncoated specimens.
  • An article of manufacture resistant to oxidative corrosion and erosion at high temperatures comprising an austenitic stainless steel base having a nickelchromium alloy coating with a thickness of about 0.005 inch forming a diffused modified bonded junction with the stainless steel base, said alloy coating having aluminum diffused thercinto to form nickel aluminide which increases from the base surface to the outer surface so that said outer surface comprises substantially all nickel aluminide and chromium.
  • An austenitic stainless steel substrate having a flame sprayed alloy coating of 80 percent nickel and 20 percent chromium with a minimum thickness of 0.003 inch, said alloy coating having aluminum diffused thercinto to form nickel aluminide which increases from the stainless steel surface to the outer surface thereof so that said outer surface comprises substantially all nickel aluminide and chromium, said coating forming a diffused modified bonded junction with the stainless steel substrate.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

Low alloy austenitic stainless steel is protected from oxidative corrosion and erosion at high temperatures in the presence of exhaust gases from internal combustion engines by flame-spraying a layer between about 0.003 inches and about 0.007 inches thick of an alloy of 80 percent nickel and 20 percent chromium on the steel base, and thereafter converting the layer to an intermetallic chromium containing nickel aluminide coating by a low temperature aluminum cementation process. A cementation pack comprising 96 percent aluminum oxide, 2 percent aluminum, 1 percent sodium chloride, and 1 percent ammonium bifluoride is placed on the nickel-chromium layer in an inert atmosphere for a period between four hours and 24 hours at 1400*F to 1600*F to form an intermetallic chromium containing nickel aluminide coating containing 40 to 60 atomic percent aluminum. The coated steel is highly resistant to oxidation corrosion and erosion by high temperature exhaust gases from internal combustion engines. It is particularly useful in the construction of thermal reactors for exhaust systems in automobiles for the control of pollution from exhausts.

Description

United States Patent 1 Grisaffe et al.
[ 1 Oct. 2, 1973 [75] Inventors: Salvatore J. Grisaife, Rocky River;
Ernest W. Klechke, Fairview Park, both of Ohio [73] Assignee: The United States of America as represented by the National Aeronautics and Space Administration, Washington, DC.
22 Filed: Oct. 18, 1971 211 Appl. No.: 190,316
3,505,028 4/l970 Douthit 1. 29/1962 3,597,l72 8/]971 Blingardt 29/l96.2 3,640,755 2/1972 Barth 29/1962 3,653,852 4/l972 Seller 1. 29/196!) Primary Examiner-Hyland Bizot Attorney-N. T. Musial et al.
[57] ABSTRACT Low alloy austenitic stainless steel is protected from oxidative corrosion and erosion at high temperatures in the presence of exhaust gases from internal combustion engines by flame-spraying a layer between about 0.003 inches and about 0.007 inches thick of an alloy of 80 percent nickel and 20 percent chromium on the steel base, and thereafter converting the layer to an intermetallic chromium containing nickel aluminide coating by a low temperature aluminum cementation process. A cementation pack comprising 96 percent aluminum oxidc, 2 percent aluminum, l percent sodium chloride, and 1 percent ammonium bifluoride is placed on the nickel-chromium layer in an inert atmosphere for a period between four hours and 24 hours at l400F to 1600F to form an intermetallic chromium containing nickel aluminide coating containing 40 to 60 atomic percent aluminum.
The coated steel is highly resistant to oxidation corrosion and erosion by high temperature exhaust gases from internal combustion engines. It is particularly useful in the construction of thermal reactors'for exhaust systems in automobiles for the control of pollution from exhausts.
6 Claims, No Drawings NICKEL ALUMINIDE COATED LOW ALLOY STAINLESS STEEL ORIGIN OF THE INVENTION The invention described herein was made by employees of the United States Government and may be manufactured and used by or for the Government for governmental purposes without the payment of any royalties thereon or therefor.
BACKGROUND OF THE INVENTION Field of the Invention This invention relates to a coating for low alloy austenitic stainless steel to render the steel highly resistant to oxidation corrosion and erosion from exhaust gases in internal combustion engines.
The engine exhaust of automotive internal combustion engines contains carbon monoxide, carbon dioxide, nitrogen dioxide, unburned hydrocarbons, sulfur compounds, and other corrosive products which are exhausted into the atmosphere in the absence of means for controlling such emissions. Recently federal regulations have been imposed which set progressively lower allowable engine exhaust levels for such combustion products. Minor adjustments in carburetion and spark control and the like are no longer satisfactory in meeting such requirements. One way such engine emissions can be reduced further in the future in order to meet the requirements of controlling agencies is by the utilization of thermal exhaust converters or reactors. Such thermal reactors replace the exhaust manifold.
In some reactors, secondary air is introduced into the reactor in order to promote the complete combustion of unburned hydrocarbons and carbon monoxide. In order to achieve the desired ends, many components of the thermal reactor must operate at temperatures on the order of 1900F with the possibility that if the ignition means fails, the temperature may increase up to 2300F.
It is a practical requirement of the automobile industry that such reactors have useful lives of 2000 hours or more, which translates to 50,000 miles of driving at an average speed of 25 miles per hour. Under such stringent conditions of severe temperatures, exhaust atmosphere, and term of life requirements, the oxidation corrosion and erosion as well as the chemical attack by lead and sulfur compounds on unprotected steel components are very significant.
Since such thermal exhaust reactors are required in large quantities, for example, up to fifteen million units a year at the present automotive industry production rate, it is essential that such thermal reactors be capable of being produced at the minimum possible cost. One approach to avoid utilization of expensive components is to use protective coatings on the metal materi als used in such thermal reactors.
DESCRIPTION OF THE PRIOR ART It is known, of course, that materials such as extremely high alloy steels are resistant to oxidation corrosion and erosion and thus fulfill the technical requirements for materials in such thermal exhaust reactors. The use of high alloy steels would be extremely expen- 'sive for such applications, however, because of the vast amounts of metal such as nickel that are required. It is known that low alloy steels possess moderately high temperature strengths but that they are not resistant to degradation by the environmental conditions in the thermal exhaust reactors.
In US. Pat. No. 3,481,715, Whalen et al., there is disclosed a sealing member which is moderately resistant to oxidation at high temperatures in which the steel base is coated with an intermediate layer of an alloy-of nickel with aluminum or chromium appliep by a plasma gun, to which a surface layer of material comprising nickel oxide and calcium fluoride is applied-using a plasma gun. The nickel with aluminum or chromium layer serves to improve the adhesion of the oxide surface layer.
U.S. Pat. No. 3,338,733, Rowady, discloses metallic surface coatings resistant to corrosion and wear such as that to which internal combustion valves are exposed. In this case a steel base is first preheated to 1300 to l800F and a nickel-chromium alloy is applied by flame-spraying. The coated object is then subjected to a first diffusion step at temperatures of l800 to 2250F to promote alloying between the coated alloy and the base metal. The coating subsequently may be coated with an aluminum layer by first preheating the coated base to l200 to l400F and then thereafter dipping the article in a molten bath of aluminum or applying the aluminum by a flame-spraying technique. After the aluminum coating has been applied, the object is then heated to 1500F to 2l00F to diffuse and alloy the aluminum into the nickel-chromium alloy.
SUMMARY OF THE INVENTION The present invention provides a low alloy austenitic stainless steel article highly resistant to oxidation corrosion and erosion by a coating which comprises a chromium containing nickel aluminid-e applied by the process of this invention. Low alloy stainless steel material I coated according to this invention exhibits oxidation resistance equal to or better than the oxidation resistance obtained on many highly allloyed steels either uncoated, or coated with expensive alloys and other compounds, many applied by complex processes.
A relatively low cost stock article suitable for use in constructing thermal exhaust reactors is provided by this invention by using low alloy austenitic stainless steel. It provides resistance to corrosion using steels having only a relatively small amount of nickel.
According to this invention, an oxidation corrosion and erosion resistant article is provided by depositing on a low nickel alloy austenitic stainless steel basea layer between about 0.003 to 0.007 inch, preferably 0.005 inch, thick ofa nickel-chromium alloy such as 80 percent nickel-20 percent chromium, by means of flame-spraying or plasma spraying, then converting the nickel-chromium alloy layer to one comprising an intermetallic compound, as opposed to an alloy. of chromium-containing nickel aluminide by a low tem' perature aluminum pack cemcntation process at l400 l600F for four to 24 hours which in a single process step also serves to diffusion bond the coating to the steel substrate. The chromium-containing nickel aluminide coating contains from about 40 to about atomic percent of aluminum.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Test specimens of austenitic 304 stainless steel (Fel8Cr8Ni0.008C) were cut from 1/16 inch thick sheet stock. One set were inch X Ht: inches, and an other were 1 inch X 2 inches. Prior to coating according to this invention the specimens were ball milled in a ceramic mill with no. 36 alumina grit and water and thereafter vapor blasted with l mesh alumina, degreased, and then ultrasonically cleaned in trichloroethylene.
The samples are then coated with a 0.005 inch layer of 80 percent nickel-20 percent chromium by flamespraying, using a conventional spray gun adapted for spraying nickel-chromium alloy fed in wire form. The thickness of the layer can be between 0.003 and 0.007 inches. Layers having thicknesses at the lower end of the range have less stresses while the thicker layers have longer lives.
The nickel-chromium layer is then converted to a chromium containing nickel aluminide intermetallic compound by a pack cementation step by treating the layer with a high activity aluminum pack. The pack employed comprises 96 percent aluminum oxide, 2 percent aluminum, 1 percent sodium chloride, and l percent ammonium bifluoride. The coating is treated in a furnace under an inert atmosphere such as argon for from four to 24 hours, preferably for 16 hours, at l600F. The process deposits approximately mg. of aluminum per square centimeter which reacts to form a chromium enriched nickel aluminide intermetallic protective layer on the low alloy austenitic stainless steel and at the same time forms a diffusion bond between the coating and the substrate.
Essentially no diffusion bonding takes place during the flame-spraying application of the nickel-chromium layer. The bond between the alloy layer and the steel base at this stage is itself primarily a mechanical bond. Following the aluminum cementation, the chromiumnickel alloy layer has been converted to a chromiumcontaining nickel aluminide intermetallic compound coating which is diffusion bonded to the steel substrate.
The inch X 1% inches samples are then placed in a horizontal multitube furnace on high purity recrystallized alumina boats. Air is passed over the specimens at the rate of two cubic feet per hour. One set of specimens is heated for 100 hours at 2000F, with cycling to room temperature. The cycles consist of hours at test temperature followed by cooling to room temperature. At room temperature the specimens are lightly brushed to remove any oxide scale and weighed to 0.05 mg. per square centimeter accuracy. A second set of specimens is similarly cycled for 600 hours at l800F. Excellent resistance to oxidation corrosion and erosion was evident from visual examination, x-ray diffraction, microscopic and metallographic analysis. Furthermore, there was no loss of weight of the samples, but a slight weight gain, for example, the specimens gain about 3 mg. per square centimeter after 600 hours exposure to the l800F cycling tests. During all of the tests, the metal temperature is measured by thermocouples which are mounted on adjacent uncoated specimens.
The 1 inch X 2 inches coated specimens are tested in an experimental automotive thermal reactor connected to a high performance 472 cubic inch V-8 automobile engine with air injection and carburetion. Leaded gasoline is used as a fuel and the engine is operated to provide test specimen cycles of IO minutes at l900F, 5 minutes at 1200F, and repeat. After l70 cycles, the specimens exhibit no significant deterioration and gain approximately 0.l gram. All coatings after testing exhibit excellent weight stability, coating preservation and metallographic stability. The specimens when examined visually appear almost unchanged from the as coated condition.
The coatings obtained according to the process ofthe present invention impart excellent high temperature corrosion and erosion resistance to low alloy austenitic stainless steel. The protection of the low alloy austenitic stainless steel is achieved by a process which involves primarily only two steps as opposed to other methods of applying different oxidation resistant coatings which are often quite complex. The invention is particularly advantageous in providing an article suitable for utilization in automotive thermal reactors which are necessary to reduce exhaust pollution in automobiles. Significantly the present invention provides an excellent material for such reactors at relatively low cost and a low consumption of expensive nickel metal. By way of illustration, in order to provide 15 million thermal exhaust reactors annually utilizing a high alloy stainless steel such as aluminum coated lnco 800 containing 32 percent nickel, about 15 percent of the total nickel consumed annually in the United States would be required, whereas utilizing material according'to the present invention about 7 percent of the nickel consumed annually would be required. This is based upon the use of 4% square feet of material 1.5 mm. thick for a typical thermal core reactor.
While the invention has been explained by a detailed description of a specific embodiment, it is understood that various modifications and substitutions can be made within the scope of the appended claims which are intended to include equivalents of such embodiments.
What is claimed is:
1. An article of manufacture resistant to oxidative corrosion and erosion at high temperatures comprising an austenitic stainless steel base having a nickelchromium alloy coating with a thickness of about 0.005 inch forming a diffused modified bonded junction with the stainless steel base, said alloy coating having aluminum diffused thercinto to form nickel aluminide which increases from the base surface to the outer surface so that said outer surface comprises substantially all nickel aluminide and chromium.
2. An article of manufacture as claimed in claim 1 wherein said coating is produced by applying aluminum by means of low temperature pack cementation to a flame-sprayed layer between about 0.003 inch and about 0.007 inch thick of percent nickel-20 percent chromium alloy on said base, said'aluminum reacting with said layer to form said nickel aluminide.
3. An article of manufacture as claimed in claim 2 wherein said austenitic stainless steel is a low nickel alloy stainless steel, and said aluminum is applied from a cementation pack comprising 96 percent aluminum oxide, 2 percent aluminum, 1 percent sodium chloride, and 1 percent ammonium bifluoride.
4. An article of manufacture as claimed in claim 2 wherein said aluminum is applied in an inert atmosphere at about l400 to 1600F.
5. An austenitic stainless steel substrate having a flame sprayed alloy coating of 80 percent nickel and 20 percent chromium with a minimum thickness of 0.003 inch, said alloy coating having aluminum diffused thercinto to form nickel aluminide which increases from the stainless steel surface to the outer surface thereof so that said outer surface comprises substantially all nickel aluminide and chromium, said coating forming a diffused modified bonded junction with the stainless steel substrate.
6. An article as claimed in claim 5 wherein said flame-sprayed layer is about 0.005 inch thick.

Claims (5)

  1. 2. An article of manufacture as claimed in claim 1 wherein said coating is produced by applying aluminum by means of low temperature pack cementation to a flame-sprayed layer between about 0.003 inch and about 0.007 inch thick of 80 percent nickel-20 percent chromium alloy on said base, said aluminum reacting with said layer to form said nickel aluminide.
  2. 3. An article of manufacture as claimed in claim 2 wherein said austenitic stainless steel is a low nickel alloy stainless steel, and said aluminum is applied from a cementation pack comprising 96 percent aluminum oxide, 2 percent aluminum, 1 percent sodium chloride, and 1 percent ammonium bifluoride.
  3. 4. An article of manufacture as claimed in claim 2 wherein said aluminum is applied in an inert atmosphere at about 1400* to 1600*F.
  4. 5. An austenitic stainless steel substrate having a flame sprayed alloy coating of 80 percent nickel and 20 percent chromium with a minimum thickness of 0.003 inch, said alloy coating having aluminum diffused thereinto to form nickel aluminide which increases from the stainless steel surface to the outer surface thereof so that said outer surface comprises substantially all nickel aluminide and chromium, said coating forming a diffused modified bonded junction with the stainless steel substrate.
  5. 6. An article as claimed in claim 5 wherein said flame-sprayed layer is about 0.005 inch thick.
US00190316A 1971-10-18 1971-10-18 Nickel aluminide coated low alloy stainless steel Expired - Lifetime US3762884A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US19031671A 1971-10-18 1971-10-18

Publications (1)

Publication Number Publication Date
US3762884A true US3762884A (en) 1973-10-02

Family

ID=22700840

Family Applications (1)

Application Number Title Priority Date Filing Date
US00190316A Expired - Lifetime US3762884A (en) 1971-10-18 1971-10-18 Nickel aluminide coated low alloy stainless steel

Country Status (1)

Country Link
US (1) US3762884A (en)

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859061A (en) * 1973-04-23 1975-01-07 Chromalloy American Corp Corrosion resistant coating system for ferrous metal articles having brazed joints
US4071659A (en) * 1975-11-13 1978-01-31 Texas Instruments Incorporated Solar absorption surface panel
FR2429271A1 (en) * 1978-06-23 1980-01-18 Gen Electric Corrosion resistant coating for steel - obtd. by diffusing chromium into steel, and used esp. on sulphur containers in sodium-sulphur batteries
JPS56273A (en) * 1979-06-14 1981-01-06 Mitsubishi Heavy Ind Ltd Diffusion-penetration method of alloy
DE3922265A1 (en) * 1988-07-06 1990-02-01 Usui Kokusai Sangyo Kk SUPPORT BODY MADE FROM METAL FOR AN EXHAUST GAS PURIFICATION CATALYST AND METHOD FOR THE PRODUCTION THEREOF
US5015535A (en) * 1987-07-30 1991-05-14 Intevep, S.A. Article formed from a low carbon iron alloy having a corrosion resistant diffusion coating thereon
WO1993011934A1 (en) * 1991-12-19 1993-06-24 Emitec Gesellschaft Für Emissionstechnologie Mbh Plated steel sheet
US5409748A (en) * 1990-12-31 1995-04-25 Pohang Iron & Steel Co., Ltd. Heat radiating tube for annealing furnace, with ceramic coated on the inside thereof
US5411162A (en) * 1992-07-31 1995-05-02 Allen-Bradley Company, Inc. V-band coupling for an explosion-proof enclosure
US6613452B2 (en) 2001-01-16 2003-09-02 Northrop Grumman Corporation Corrosion resistant coating system and method
US6653608B1 (en) 2001-10-24 2003-11-25 The Boeing Company Oxidation protected susceptor
WO2005106064A1 (en) * 2004-04-28 2005-11-10 Diffusion Alloys Limited Coatings for turbine blades
US20130140829A1 (en) * 2011-12-02 2013-06-06 Gamesa Innovation & Technology., S.L., Nacelle thermal conditioning system for off-shore wind turbines
DE102012002637A1 (en) 2012-02-10 2013-08-14 Faurecia Emissions Control Technologies, Germany Gmbh exhaust system
US8557397B2 (en) * 2011-12-29 2013-10-15 Arcanum Alloy Design Inc. Metallurgically bonded stainless steel
US8628861B2 (en) * 2011-12-29 2014-01-14 Arcanum Alloy Design Inc. Metallurgically bonded stainless steel
US8790790B2 (en) * 2011-12-29 2014-07-29 Arcanum Alloy Design, Inc. Metallurgically bonded stainless steel
US20150240343A1 (en) * 2014-02-26 2015-08-27 Endurance Technologies, Inc. Coating compositions, methods and articles produced thereby
US10876198B2 (en) 2015-02-10 2020-12-29 Arcanum Alloys, Inc. Methods and systems for slurry coating
US11261516B2 (en) 2016-05-20 2022-03-01 Public Joint Stock Company “Severstal” Methods and systems for coating a steel substrate

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859061A (en) * 1973-04-23 1975-01-07 Chromalloy American Corp Corrosion resistant coating system for ferrous metal articles having brazed joints
US4071659A (en) * 1975-11-13 1978-01-31 Texas Instruments Incorporated Solar absorption surface panel
FR2429271A1 (en) * 1978-06-23 1980-01-18 Gen Electric Corrosion resistant coating for steel - obtd. by diffusing chromium into steel, and used esp. on sulphur containers in sodium-sulphur batteries
JPS56273A (en) * 1979-06-14 1981-01-06 Mitsubishi Heavy Ind Ltd Diffusion-penetration method of alloy
JPS5710182B2 (en) * 1979-06-14 1982-02-25
US5015535A (en) * 1987-07-30 1991-05-14 Intevep, S.A. Article formed from a low carbon iron alloy having a corrosion resistant diffusion coating thereon
DE3922265A1 (en) * 1988-07-06 1990-02-01 Usui Kokusai Sangyo Kk SUPPORT BODY MADE FROM METAL FOR AN EXHAUST GAS PURIFICATION CATALYST AND METHOD FOR THE PRODUCTION THEREOF
US5049206A (en) * 1988-07-06 1991-09-17 Usui Kokusai Sangyo Kabushiki Kaisha Metal-made carrier body for exhaust gas cleaning catalyst and production of the carrier body
US5409748A (en) * 1990-12-31 1995-04-25 Pohang Iron & Steel Co., Ltd. Heat radiating tube for annealing furnace, with ceramic coated on the inside thereof
WO1993011934A1 (en) * 1991-12-19 1993-06-24 Emitec Gesellschaft Für Emissionstechnologie Mbh Plated steel sheet
US5514348A (en) * 1991-12-19 1996-05-07 Emitec Gesellschaft Fuer Emissionstechnologie Mbh Plated steel sheet and housing including the sheet
US5411162A (en) * 1992-07-31 1995-05-02 Allen-Bradley Company, Inc. V-band coupling for an explosion-proof enclosure
US6613452B2 (en) 2001-01-16 2003-09-02 Northrop Grumman Corporation Corrosion resistant coating system and method
US6653608B1 (en) 2001-10-24 2003-11-25 The Boeing Company Oxidation protected susceptor
WO2005106064A1 (en) * 2004-04-28 2005-11-10 Diffusion Alloys Limited Coatings for turbine blades
US20080057189A1 (en) * 2004-04-28 2008-03-06 John Smith Coatings For Turbine Blades
US7824738B2 (en) 2004-04-28 2010-11-02 Diffusion Alloys Limited Coatings for turbine blades
US20130140829A1 (en) * 2011-12-02 2013-06-06 Gamesa Innovation & Technology., S.L., Nacelle thermal conditioning system for off-shore wind turbines
US9062659B2 (en) * 2011-12-02 2015-06-23 Gamesa Innovation & Technology, S.L. Nacelle thermal conditioning system for off-shore wind turbines
US8628861B2 (en) * 2011-12-29 2014-01-14 Arcanum Alloy Design Inc. Metallurgically bonded stainless steel
US8557397B2 (en) * 2011-12-29 2013-10-15 Arcanum Alloy Design Inc. Metallurgically bonded stainless steel
US8784997B2 (en) * 2011-12-29 2014-07-22 Arcanum Alloy Design, Inc. Metallurgically bonded stainless steel
US8790790B2 (en) * 2011-12-29 2014-07-29 Arcanum Alloy Design, Inc. Metallurgically bonded stainless steel
DE102012002637B4 (en) * 2012-02-10 2014-01-02 Faurecia Emissions Control Technologies, Germany Gmbh exhaust system
DE102012002637A1 (en) 2012-02-10 2013-08-14 Faurecia Emissions Control Technologies, Germany Gmbh exhaust system
US20150240343A1 (en) * 2014-02-26 2015-08-27 Endurance Technologies, Inc. Coating compositions, methods and articles produced thereby
US9957599B2 (en) * 2014-02-26 2018-05-01 Endurance Technologies, Inc. Coating compositions, methods and articles produced thereby
US10801099B2 (en) 2014-02-26 2020-10-13 Endurance Technologies, Inc. Coating compositions, methods and articles produced thereby
US10876198B2 (en) 2015-02-10 2020-12-29 Arcanum Alloys, Inc. Methods and systems for slurry coating
US11261516B2 (en) 2016-05-20 2022-03-01 Public Joint Stock Company “Severstal” Methods and systems for coating a steel substrate

Similar Documents

Publication Publication Date Title
US3762884A (en) Nickel aluminide coated low alloy stainless steel
CA1117828A (en) Process for producing elevated temperature corrosion resistant metal articles
US5547770A (en) Multiplex aluminide-silicide coating
US4326011A (en) Hot corrosion resistant coatings
US4248940A (en) Thermal barrier coating for nickel and cobalt base super alloys
US3649225A (en) Composite coating for the superalloys
USRE31339E (en) Process for producing elevated temperature corrosion resistant metal articles
US4639399A (en) Nickel oxide, ceramic insulated, high temperature coating
US4867116A (en) Aircraft exhaust valves
US3505028A (en) Material of construction for exhaust manifold reactor inner chamber
US3748110A (en) Ductile corrosion resistant coating for nickel base alloy articles
GB2130249A (en) Diffusion coating of metals
JPS6013056B2 (en) coated superalloy
US4371570A (en) Hot corrosion resistant coatings
US4374183A (en) Silicon-slurry/aluminide coating
JPH09324278A (en) Thermal insulation coating containing improved base film and member coated with the same thermal insulation coating
US4451496A (en) Coating with overlay metallic-cermet alloy systems
Kircher et al. Performance of a silicon-modified aluminide coating in high temperature hot corrosion test conditions
US4241113A (en) Process for producing protective coatings on metals and metal alloys for use at high temperatures
US4310574A (en) Method of protecting a surface with a silicon-slurry/aluminide coating
Wang Corrosion behavior of chromized and/or aluminized 214Cr-1Mo steel in medium-BTU coal gasifier environments
Rani et al. Characterization and hot corrosion behavior of D-gun sprayed Cr2O3-75% Al2O3 coated ASTM-SA210-A1 boiler steel in molten salt environment
GB2159838A (en) Surface strengthening of overlay coatings
US4929473A (en) Corrosion resistance of low carbon steels in a vanadium, sulfur and sodium environment at high temperatures
US3859079A (en) High temperature oxidation resistant alloy