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
  • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
  • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
  • C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
  • C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
  • C22C29/08—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
• • 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
  • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
  • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
  • C23C4/06—Metallic material
  • C23C4/067—Metallic material containing free particles of non-metal elements, e.g. carbon, silicon, boron, phosphorus or arsenic

Definitions

• the present invention relates to wear and corrosion resistant coatings and to a method for producing such coatings. More particularly, the invention relates to a new family of W-Co-Cr-C coatings having improved strength and wear resistance.
• Coatings of W-Co-Cr-C are used in those applications where both superior wear and corrosion resistance are required.
• a typical composition for these coatings comprises about 8 to 10 weight percent cobalt, about 3 to 4 weight percent chromium, about 4.5 to 5.5 weight percent carbon and the balance tungsten.
• These coatings can be successfully applied to various substrates, e.g. iron base alloy substrates, using known thermal spray techniques. Such techniques include, for example, detonation gun (D-Gun) deposition as disclosed in U.S. Patent Nos. 2,714,563 and 2,950,867, plasma arc spray as disclosed in U.S. Patent Nos. 2,858,411 and 3,016,447 and other so- called "high velocity" plasma or "hypersonic" combustion spray processes.
• D-Gun detonation gun
• these coatings derive their wear resistance from the presence of complex carbides of W, Co and Cr. It is also known that the wear resistance of the coating usually increases with any increase in the volume fraction of carbides. Therefore, it has been previously thought by those skilled in the art that a relatively high carbon content is necessary in order to obtain optimum wear resistance.
• a coating composition applied to a substrate by a thermal spray process in accordance with the present invention consists of from 6.5 to 9.0 weight percent cobalt, from 2.0 to 4.0 weight percent chromium, from 3.0 to 4.0 weight percent carbon and the balance tungsten and incidential impurities.
• a method for coating a substrate wherein a powdered coating material is suspended within a high temperature, high velocity gaseous stream and heated to a temperature at least close to the melting point thereof, said gaseous stream being directed against a surface of said substrate to deposit said powdered coating material and form a coating thereon, in conformity with the present invention, is characterized in that a powdered coating material having a composition such that the coating deposited onto said substrate consists of from 6.5 to 9.0 weight percent cobalt, from 2.0 to 4.0 weight percent chromium, from 3.0 to 4.0 weight percent carbon and the balance tungsten and incidential impurities, is used.
• a powdered coating composition for applying a wear and corrosion resistant coating to a substrate by a thermal spray process in accordance with the present invention consists of from 6.5 to 9.0 weight percent cobalt, from 2.0 to 4.0 weight percent chromium, from 3.0 to 4.0 weight percent carbon and the balance tungsten and incidential impurities.
• the coatings of the present invention can be applied to a substrate using any conventional thermal spray technique.
• the preferred method of applying the coating is by detonation gun (D-Gun) deposition.
• D-Gun detonation gun
• a typical D-Gun consists essentially of a water-cooled barrel which is several 30 cm (feet) long with an inside diameter of about 25 mm (1 inch).
• a mixture of oxygen and a fuel gas, e.g., acetylene, in a specified ratio (usually about 1:1) is fed into the barrel along with a charge of powder to be coated.
• the gas is then ignited and the detonation wave accelerates the powder to about 730 m/sec. (2400 ft./sec.) while heating the powder close to or above its melting point.
• a pulse of nitrogen purges the barrel and readies the system for the next detonation. The cycle is then repeated many times a second.
• the D-Gun deposits a circle of coating on the substrate with each detonation.
• the circles of coating are about 25 mm (1 inch) in diameter and a few microns (ten thousandths of an inch) thick.
• Each circle of coating is composed of many overlapping microscopic splats corresponding to the individual powder particles. The overlapping splats interlock and mechanically bond to each other and to the substrate without substantially alloying at the interface thereof.
• the placement of the circles and the coating deposition are closely controlled to build up a smooth coating of uniform thickness and to minimize substrate heating and establishment of residual stresses in the applied coating.
• the powder used in producing the coating of the present invention may be essentially the same powder composition as heretofore employed in depositing W-Co-Cr-C coatings of the prior art.
• the oxygen-fuel gas ratio employed in the D-Gun process is increased from a value of about 1.0 to a value of between about 1.1 and 1.2. Under these conditions, changes during the coating process result in the desired coating composition. It is also possible to use other operating conditions with a D-Gun and still obtain the desired coating composition if the powder composition is adjusted accordingly.
• other powder compositions may be used with other thermal spray coating devices to compensate for changes in composition during deposition and obtain the desired coating composition of this invention.
• the powders used in the D-Gun for applying a coating according to the present invention are preferably sintered products. However, other forms of powder such as cast and crushed powder can also be used. Generally, the size of the powder should be about 0.044 mm or smaller (-325 mesh). Powders produced by other methods of manufacture and with other size distributions may be used according to the present invention with other thermal spray deposition techniques if they are more suited to a particular spray device and/or size.
• This powder composition consists of about 10 weight percent cobalt, about 4 weight percent chromium, about 5 weight percent carbon and the balance tungsten.
• the feed rate of both oxygen and fuel gas e.g., acetylene
• acetylene should be adjusted to provide an oxygen-fuel gas ratio of between about 1.1 and 1.2. This ratio is higher than that usually used heretofore with the same powder composition and provides an oxidizing mixture which reduces the carbon content of the applied coating.
• the conventional powder composition using the D-Gun process will produce coatings having a carbon content of about 3.5 weight percent. Conversely, at oxygen-fuel gas mixtures close to about 1.2, this same powder will produce coatings having a lower carbon content of about 3.1 weight percent.
• the coating of the present invention can be applied to a substrate by plasma arc spray or other thermal spray techniques.
• plasma arc spray process an electric arc is established between a non-consumable electrode and a second non-consumable electrode spaced therefrom.
• a gas is passed in contact with the non-consumable electrode such that it contains the arc.
• the arc-containing gas is constricted by a nozzle and results in a high thermal content effluent.
• Powdered coating material is injected into the high thermal content effluent from the nozzle and is deposited onto the surface to be coated.
• This process which is described in U.S. Patent No. 2,858,411, supra, produces a deposited coating which is sound, dense and adherent to the substrate.
• the applied coating also consists of irregularly shaped microscopic splats or leaves which are interlocked and mechanically bonded to one another and also to the substrate.
• powders fed to the arc torch may have essentially the same composition as the applied coating itself.
• some change in composition is to be expected and, in such cases, the powder composition may be adjusted accordingly to achieve the coating composition of the present invention.
• the coatings of the present invention may be applied to almost any type of substrate, e.g., metallic substrates such as iron or steel or non- metallic substrates such as carbon, graphite and polymers, for instance.
• substrate material used in various environments and admirably suited as substrates for the coatings of the present invention include, for example, steel, stainless steel, iron base alloys, nickel, nickel base alloys, cobalt, cobalt base alloys, chromium, chromium base alloys, titanium, titanium base alloys, aluminum, aluminum base alloys, copper, copper base alloys, refractory metals, and refractory-metal base alloys.
• the composition of the coatings of the present invention may vary within the ranges indicated above, the preferred coating composition consists of from 7.0 to 8.5 weight percent cobalt, from 2.5 to 3.5 weight percent chromium, from 3.0 to 4.0 weight percent carbon and the balance tungsten and incidental impurities.
• Such coatings are ideally suited for industrial valves, mechanical seals, bushings and the like. They are also ideally suited for use in the textile industry as crimper rolls, for example.
• the microstructure of the coatings of the present invention are very complex and not completely understood. However, it is believed that the major portion of the coatings consist essentially of a mixture of WC and (W, Cr, C O ) 2 C with other metal carbides and possibly metallic phases. Despite the lower volume fraction of carbides present as compared to similar coatings of the prior art, the coatings of the present invention surprisingly exhibit improved wear resistance without sacrificing other desirable characteristics such as hardness, toughness, etc. Typical hardness values for coatings of the present invention exceed about 900 DPH 30o .
• Specimens of AISI 1018 steel were cleaned and prepared for coating as follows. The surface on one side of each specimen was ground smooth and parallel to the opposite side. The surface was then grit blasted with 0.25 mm (60 mesh) AI 2 0 3 to a surface roughness of about 3 ⁇ m (120 microinch) RMS. All the specimens were then coated according to the prior art using a detonation gun (D-Gun) and a sintered powder of the following composition: 10 weight percent Co, 4 weight percent Cr, 5.2 weight percent C and the balance W. The size of the powders was about 0.044 mm or smaller (-325 mesh). Acetylene was used as the fuel gas. The oxygen-fuel gas ratio was 0.98.
• a chemica.1 analysis of the coating showed the following composition: 8 weight percent Co, 3.2 weight percent Cr, 4.7 weight percent C and the balance W.
• the chemical analysis was carried out principally by two methods. Carbon was analyzed by a combustion analysis technique using a Leco Carbon Analyzer and volumetric determination of gaseous output. Cobalt and chromium were analyzed by first fusing the sample in Na 2 0 2 and separating the cobalt and chromium, then determining the amount of each potentiometrically.
• Abrasive wear properties of the applied coating were determined using the standard dry sand/ rubber wheel abrasion test described in ASTM Standard G65-80, Procedure A.
• ASTM Standard G65-80, Procedure A the specimen was loaded by means of a lever arm against a rotating wheel with a chlorobutyl rubber rim around the wheel.
• An abrasive i.e. 0.21 mm to 0.30 mm (50-70 mesh) Ottawa Silica Sand
• the wheel was rotated in the direction of abrasive flow.
• the test specimen was weighed before, after and periodically during the test, and its weight loss was recorded. Because of the wide differences in the densities of different materials tested, the mass loss is normally converted to volume loss to evaluate the relative ranking of materials.
• the average volume loss for these specimens (conventional W-Co-Cr-C coating) was 1.7 mm 3 per 1000 revolutions.
• the hardness of these specimens was also measured by standard methods. The average hardness was found to be 1100 DPH 300 .
• the specimens were also easily ground to a smooth finish using the normal method of finishing wear resistant coating with a diamond grinding wheel and an infeed of 13 pm (0.0005 inch) per pass.
• Specimens of AISI 1018 steel were prepared in the same manner as described in Example I. The specimen surfaces were then coated using a D-Gun and the same sintered powder, i.e., 10 weight percent Co, 4 weight percent Cr, 5.2 weight percent C and the balance W. The powder size was also identical, i.e., 0.044 mm or smaller (-325 mesh). Acetylene was also used as the fuel gas. In this instance, however, the oxygen-fuel gas ratio in the D-Gun was 1.1 according to the present invention.
• a chemical analysis of the coating showed the following composition: 7.6 weight percent Co. 2.9 weight percent Cr, 3.5 weight percent C and the balance W.
• the hardness of the specimens was also measured and found to be 1150 DPH 3oo .
• the specimens were also easily ground to a smooth finish using the normal method as in Example I.
• Specimens of AISI 1018 steel were prepared in the same manner as described in Example I. The specimen surfaces were then coated with a D-Gun and the same sintered powder, i.e., 10 weight percent Co, 4 weight percent Cr, 5.2 weight percent C and the balance W. The powder size was also identical, i.e., 0.044 mm or smaller (-325 mesh). Acetylene was also used as the fuel gas. However, the oxygen-fuel gas ratio used in this instance was 1.2 according to the present invention.
• a chemical analysis of the coating showed the following composition: 7.8 weight percent Co, 2.9 weight percent Cr, 3.1 weight percent C and the balance W.
• the hardness of the specimen was also measured and found to be 1080 DPH 300 .
• the specimen was ground to a smooth but somewhat rougher finish using the normal method as in Example I.
• Specimens of AISI 1018 steel were prepared in the same manner as described in Example I. The specimen surfaces were then coated with a D-Gun and the same sintered powder; i.e., 10 weight percent Co, 4 weight percent Cr, 5.2 weight percent C and the balance W. The powder size was also identical,.i.e., 0.044 mm or smaller (-325 mesh). Acetylene was also used as the fuel gas. However, the oxygen-fuel gas mixture used in this instance was 1.3.
• a chemical analysis of the coating showed the following composition: 7.6 weight percent Co, 2.7 weight percent Cr, 2.6 weight percent C and the balance W.
• the hardness of this type of coating is about 1125 DPH 300 .
• Abrasive wear tests were carried out on this coating as in Example I, II, and III with a volume loss of 1.5 mm 3 per revolution. However, attempts to grind the coating to a smooth finish were unsuccessful using the normal method as described in Example I.
• Specimens of AISI 1018 steel were prepared in the same manner as described in Example I. The specimen surfaces were then coated using a plasma spray torch and the same sintered powder; i.e., 10 weight percent Co, 4 weight percent Cr, 5.2 weight percent C and the balance W. The powder size was also 0.044 mm or smaller (-325 mesh).
• a chemical analysis of the coating showed the following composition: 9.2 weight percent Co, 3.5 weight percent Cr, 5.0 weight percent C and the balance W.
• the cobalt and carbon content of this coating was higher than that of the coatings of the present invention.
• the hardness of the specimen was also measured and found to be 687 DPH 30o .
• Specimens of AISI 1018 steel were prepared in the same manner as described in Example I. The specimen surfaces were then coated using a plasma spray torch and a sintered powder of the following composition: 10.9 weight percent Co, 4.3 weight percent Cr, 3.8 weight percent C and the balance W. The powder size was 0.044 mm or smaller (-325 mesh).
• a chemical analysis of the coating showed the following composition: 8.6 weight percent Co, 3.6 weight percent Cr, 3.4 weight percent C and the balance W. This coating composition was within the scope of the present invention.
• the hardness of the coated specimen was also measured and found to be 830 DPH 30o .
• iron is usually the principal impurity in the coating resulting from grinding operations and may be present in amounts up to about 1.5 and in some cases 2.0 weight percent of the composition.

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

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• 1984
  • 1984-10-12 CA CA000465336A patent/CA1229204A/en not_active Expired
  • 1984-10-26 EP EP84112938A patent/EP0143343B1/en not_active Expired
  • 1984-10-26 AU AU34731/84A patent/AU564804B2/en not_active Ceased
  • 1984-10-26 DE DE8484112938T patent/DE3466251D1/de not_active Expired
  • 1984-10-26 JP JP59224277A patent/JPS60128257A/ja active Granted
  • 1984-10-27 IN IN835/DEL/84A patent/IN167503B/en unknown
  • 1984-10-27 KR KR1019840006699A patent/KR890005129B1/ko not_active IP Right Cessation
• 1988
  • 1988-01-14 SG SG51/88A patent/SG5188G/en unknown
  • 1988-05-12 HK HK358/88A patent/HK35888A/xx not_active IP Right Cessation

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