US20030098090A1 - Surface coatings - Google Patents

Surface coatings Download PDF

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Publication number
US20030098090A1
US20030098090A1 US09/988,666 US98866601A US2003098090A1 US 20030098090 A1 US20030098090 A1 US 20030098090A1 US 98866601 A US98866601 A US 98866601A US 2003098090 A1 US2003098090 A1 US 2003098090A1
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weight
metallic material
powdered metallic
substrate
iron
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US09/988,666
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Hans Hallen
Lars Nilsson
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Hoganas AB
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Hoganas AB
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Publication of US20030098090A1 publication Critical patent/US20030098090A1/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0052Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based alloys
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • 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
    • C23C26/00Coating not provided for in groups C23C2/00 - C23C24/00
    • C23C26/02Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
    • 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/60Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using solids, e.g. powders, pastes
    • C23C8/62Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using solids, e.g. powders, pastes only one element being applied
    • C23C8/64Carburising

Definitions

  • the present invention relates to protective coatings. Specifically the invention concerns hard, ductile, corrosion, wear and oxidation resistant surface coatings which can applied on substrates by thermal coating.
  • the base element of the powdered material is frequently nickel and a common alloy system used is nickel alloyed with silicon and boron.
  • the powdered material may include phosphorous as is disclosed in the U.S. Pat. Nos. 4,231,793 and 5,234,510.
  • powdered materials including less than 5% have a beneficial effect on the viscosity of the molten powder whereas copper additions above 5% by weight markedly deteriorates the appearance of the surface coating which is unacceptable.
  • An essential feature of the present invention is also the inclusion of carbide forming elements in the powdered material.
  • carbide forming elements will make the final coating more ductile which is believed to depend on a phenomenon generally referred to as grain size refinement. With higher amounts of carbide forming element it is also possible to get coatings having improved hardness.
  • the present invention thus concerns a nickel based powdered metallic material comprising in addition to nickel, less than 5% by weight of copper, less than 5.0% by weight of iron, a carbide forming element, boron, silicon, phosphorus carbon and inevitable impurities.
  • the present invention concerns a nickel based powdered metallic material comprising, in addition to nickel, 0-4.5% by weight of copper, 0-5.0% by weight of iron, whereby the total amount of copper and iron is at least 2.5% by weight, 0.05-5.0% by weight of a carbide forming element, 0.5-2.0% by weight of boron, 1.0-4.0% by weight of silicon, 0.5-4.0% by weight of phosphorus, 0.01-0.5% by weight of C and less than 2% by weight of inevitable impurities.
  • the amount of Cu is less than 2.5 percent effect on the viscosity has shown to be too low, resulting in great demands on the skill of the person applying the powder to the substrate.
  • the amount of copper is larger than 4.5% the appearance of the surface coating will deteriorate, which makes it difficult to apply several layers.
  • the viscosity is still too low i.e. with the addition of 4.5% of Cu
  • iron may be added in order to increase the viscosity and thus make it possible to obtain uniform layers without deteriorating the appearance of the final surface coating layer.
  • the amount of iron should be less than 5.0 percent and preferably less than 3.0 percent.
  • the copper could be replaced by iron.
  • the total amount of copper and iron should not be less than 2.5% in order to reach the beneficial effects on the viscosity.
  • carbide forming elements may be selected from the group consisting of chromium, tungsten, molybdenum, vanadium, tantalum, niobium, titanium and zirconium and manganese. Without being bound to any specific theory it is believed that small amounts of these elements, such as 0.05-1.0% results in grain size refinement of the structure of the final coating.
  • the key feature of inoculation is related to the nucleation during solidification.
  • the inoculants consist of the precipitated carbides.
  • the obtained structure will be finer which is advantageous as the obtained coating will have a high ductility. This will also slightly increase the hardness.
  • carbide forming elements such as between 1.0-5.0% by weight, will increase the hardness and wear resistance but this will also make the machinablity of the applied surface coating more difficult.
  • amount of carbide forming element should vary between 0.05-5.0% by weight.
  • the carbides may be formed in situ, i.e. the formation of carbides occurs by picking up carbon from the substrate.
  • the carbide forming element reacts with the carbon in the substrate resulting in the formation of carbide, by way of example chromium carbide.
  • the powdered material to be applied on the substrate includes a metal such as those listed above which have an high affinity to the carbon of the cast iron substrate. This must be taken into account when designing the metal powder due to the fact that cast iron is frequently used and comparatively inexpensive.
  • the amount and type of carbides formed during the application process depends on the temperature provided, since the amount of carbon that is set free during the application depends on the temperature conditions on the substrate. The higher temperature, the more carbon is set free, and accordingly a larger amount of carbide is formed.
  • other parameters also influencing the carbide formation are, by way of example, the time that the substrate is being heated during the application and the distance between the heating source and the substrate surface.
  • the preferred temperature depends of the carbide forming element used. By way of example, if chromium is used, the preferred temperature at the heating source, i.e. the fusing temperature is 850-910° C. Accordingly, it is essential for the invention that the amount of carbide and thus the hardness of the coating can be controlled by not only the choice and amount of carbide forming element but also the fusing temperature provided during the application.
  • the carbon is used in amounts between 0.01-0.5% by weight. Carbon together with the carbide forming element precipitates as carbides in the surface coating. The amount of carbides is related to the amount of carbon and carbide forming elements.
  • the addition of boron and silicon is used for increasing the wettability but also for lowering the melting point. Also, the combination of boron and silicon works as a fluxing agent. Further the addition of silicon adds oxidation resistance to the coating.
  • the amount of boron is 0.5-2.0, preferably 0.6-1.6% by weight of the composition.
  • the amount of silicon is 1.0-4.0, preferably 1.6-3.5% by weight.
  • the amount of phosphorous is 0.5-4.0, more preferably 1.5-3.0 percent.
  • the main purpose of the addition of phosphorous is lowering the melting point of the powdered metallic material.
  • the amount is preferably sufficient for achieving a melting temperature affordable for the coating to be applicable by means of conventional methods such as powder welding.
  • the present composition of the powdered metallic material has shown to provide a melting temperature of around 850° C. which can be compared with around 1050° C. without phosphorous. Before applying the powdered material onto the substrate it is preferred to preheat the substrate to a temperature in the range of 300-800° C.
  • the surface coatings are generally applied to the substrate on a specific wear exposed area or over an entire surface.
  • the coating is thereafter machined for supplying a true gauge surface or a desired texture.
  • the coating although providing the desired hardness can be machined using conventional equipment.
  • the application of the surface coating can be performed manually or be automatized, and irrespective of method chosen it is a generally known problem that there sometimes are problems when building layers of large thickness as the viscosity in the weld pool might be to low.
  • the low viscosity results in dripping effects which makes high demands on the skill of the person performing the application.
  • the viscosity in the weld pool is too high it is difficult applying even layers.
  • the melting temperature of the used powdered metallic material must in addition not be too high, since the available maximum fusing temperature with conventional equipment is limited and the melting temperature of the substrate must also be taken into account.
  • the melting temperature is also important since a reasonable melting temperature provides the possibility of speeding up the application process.
  • the powder composition also includes carbon.
  • the amount of carbon is decided by the required properties of the final coating. Thus if the substrate is cast iron carbon from this substrate may diffuse from the cast iron into the coating and the prealloyed carbon will be set lower.
  • the powdered metallic material is manufactured by conventional methods such as water atomization or gas atomization.
  • the particle size is adapted to the application method being used. By way of example, if the powder is applied by powder welding the particle size is often in the range of 20-106 ⁇ m. On the other hand, if the powder is applied by PTA, the particle size is often in the range of 45-150 ⁇ m.
  • the substrate is preheated before application of the powdered material.
  • the preheating is preferably uniform throughout the thickness of the substrate and is thus suitable performed in an oven.
  • the temperature can be varied depending on e.g. the purpose of the coating and available equipment. Generally the temperature interval is 300-800° C.
  • the preheating reduces the affordable application time since the melting of the applied powder on the substrate surface occurs faster.
  • the affordable time can also be reduced by e.g. increasing the fusing temperature.
  • a powdered metallic material of the composition according to table 1 below was prepared by gas atomization and applied on a cast iron substrate containing 3.2% by weight of carbon and also on a substrate of mild steel having a carbon content of about 0.1% by weight.
  • the hardness KV30 of the coating on the cast iron substrate was 299, whereas the hardness of the coating on the mild steel substrate was 280.
  • the higher hardness of the coating on the cast iron substrate results from the carbon pick up from the cast iron.
  • the powdered material having the above composition could be applied at high temperature without problems because of the relatively high viscosity.
  • the wettablilty to the substrates, cast iron and mild iron, was without remark. Also the appearance of the final coatings was acceptable.
  • a powdered material having the composition according to table 2 was prepared. TABLE 2 Composition % by weight Cu 1.7 Fe 1.5 Cr 4.9 B 1.2 Si 3.1 P 1.9 C 0.17 Ni Bal. Impurities ⁇ 1
  • this powder was prepared by gas atomization.
  • the hardness HV30 of the coating on the cast iron substrate was 402, whereas the hardness of the coating on the mild steel substrate was 380.
  • the powder was applied at high temperature and the viscosity was sufficiently high for applying the coating without problems.
  • the wettablity to both the substrates was quite acceptable as was the machinability of the coatings.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention concerns a nickel based powdered metallic material comprising in addition to nickel 0-4.5 wt % of copper, 0-5.0% by weight of iron, whereby the total amount of copper and iron is at least 2.5% by weight, 0.05-5.0% by weight of a carbide forming element 0.5-2.0% by weight of boron, 1.0-4.0% by weight of silicon, 0.5-4.0% by weight of phosphorus, 0.01-0.5% by weight of C and less than 2% by weight of inevitable impurities.

Description

    TECHNICAL FIELD
  • The present invention relates to protective coatings. Specifically the invention concerns hard, ductile, corrosion, wear and oxidation resistant surface coatings which can applied on substrates by thermal coating. [0001]
  • BACKGROUND OF THE INVENTION
  • It is generally known to provide surfaces subjected to harsh conditions such as excessive wear, corrosive environment etc with protective coatings. The coatings are applied in the form of powdered materials by methods such as thermal spraying and plasma arc welding etc. Depending on the final use of the coated substrate a large variety of powdered metallic materials have been developed. [0002]
  • The base element of the powdered material is frequently nickel and a common alloy system used is nickel alloyed with silicon and boron. In order to make the powder melt at a lower temperature the powdered material may include phosphorous as is disclosed in the U.S. Pat. Nos. 4,231,793 and 5,234,510. [0003]
  • A problem with these powders, especially when it is desired to apply the coating rapidly using a high energy input, is that the molten powder, when applied to the substrate, has too low viscosity which in turn results in difficulties to restrict the melt on a specific surface area of the substrate. According to the present invention it has been now found that this problem may be minimized or even eliminated by adding controlled amounts of copper or iron to the powdered material which is to be applied on the substrate. [0004]
  • The use of copper in connection with protective coatings intended for copper based substrates is disclosed in U.S. Pat. No. 5,496,391. According to this patent the copper should be added in amounts above 5% by weight and even up to 30% by weight in order to avoid problems related to poor wettability of the copper containing substrate and poor machinability. [0005]
  • According to the present invention it has been found that powdered materials including less than 5% have a beneficial effect on the viscosity of the molten powder whereas copper additions above 5% by weight markedly deteriorates the appearance of the surface coating which is unacceptable. [0006]
  • An essential feature of the present invention is also the inclusion of carbide forming elements in the powdered material. The inclusion of small amounts of such elements will make the final coating more ductile which is believed to depend on a phenomenon generally referred to as grain size refinement. With higher amounts of carbide forming element it is also possible to get coatings having improved hardness. [0007]
  • SUMMARY OF THE INVENTION
  • In brief the present invention thus concerns a nickel based powdered metallic material comprising in addition to nickel, less than 5% by weight of copper, less than 5.0% by weight of iron, a carbide forming element, boron, silicon, phosphorus carbon and inevitable impurities. [0008]
  • DETAILED DESCRIPTION OF THE INVENTION
  • Specifically the present invention concerns a nickel based powdered metallic material comprising, in addition to nickel, 0-4.5% by weight of copper, 0-5.0% by weight of iron, whereby the total amount of copper and iron is at least 2.5% by weight, 0.05-5.0% by weight of a carbide forming element, 0.5-2.0% by weight of boron, 1.0-4.0% by weight of silicon, 0.5-4.0% by weight of phosphorus, 0.01-0.5% by weight of C and less than 2% by weight of inevitable impurities. [0009]
  • Effect of Copper and Iron [0010]
  • It the amount of Cu is less than 2.5 percent effect on the viscosity has shown to be too low, resulting in great demands on the skill of the person applying the powder to the substrate. On the other hand, if the amount of copper is larger than 4.5% the appearance of the surface coating will deteriorate, which makes it difficult to apply several layers. If the viscosity is still too low i.e. with the addition of 4.5% of Cu we have found that iron may be added in order to increase the viscosity and thus make it possible to obtain uniform layers without deteriorating the appearance of the final surface coating layer. In such a case the amount of iron should be less than 5.0 percent and preferably less than 3.0 percent. It has also been found that the copper could be replaced by iron. However the total amount of copper and iron should not be less than 2.5% in order to reach the beneficial effects on the viscosity. [0011]
  • Effect of Carbide Forming Elements [0012]
  • Another essential feature of the powder according to the present invention is the presence of carbide forming elements. These carbide forming elements may be selected from the group consisting of chromium, tungsten, molybdenum, vanadium, tantalum, niobium, titanium and zirconium and manganese. Without being bound to any specific theory it is believed that small amounts of these elements, such as 0.05-1.0% results in grain size refinement of the structure of the final coating. The key feature of inoculation is related to the nucleation during solidification. The inoculants consist of the precipitated carbides. The obtained structure will be finer which is advantageous as the obtained coating will have a high ductility. This will also slightly increase the hardness. Comparatively high additions of carbide forming elements, such as between 1.0-5.0% by weight, will increase the hardness and wear resistance but this will also make the machinablity of the applied surface coating more difficult. Thus the amount of carbide forming element should vary between 0.05-5.0% by weight. [0013]
  • In the event that the substrate to be provided with the surface coating is cast iron, the carbides may be formed in situ, i.e. the formation of carbides occurs by picking up carbon from the substrate. Thus, when the powdered metallic material is applied to the cast iron substrate surface, the carbide forming element reacts with the carbon in the substrate resulting in the formation of carbide, by way of example chromium carbide. In this case the powdered material to be applied on the substrate includes a metal such as those listed above which have an high affinity to the carbon of the cast iron substrate. This must be taken into account when designing the metal powder due to the fact that cast iron is frequently used and comparatively inexpensive. [0014]
  • Furthermore, in the case that the substrate is cast iron the amount and type of carbides formed during the application process depends on the temperature provided, since the amount of carbon that is set free during the application depends on the temperature conditions on the substrate. The higher temperature, the more carbon is set free, and accordingly a larger amount of carbide is formed. It should be understood that other parameters also influencing the carbide formation are, by way of example, the time that the substrate is being heated during the application and the distance between the heating source and the substrate surface. Further, the preferred temperature depends of the carbide forming element used. By way of example, if chromium is used, the preferred temperature at the heating source, i.e. the fusing temperature is 850-910° C. Accordingly, it is essential for the invention that the amount of carbide and thus the hardness of the coating can be controlled by not only the choice and amount of carbide forming element but also the fusing temperature provided during the application. [0015]
  • Effect of Carbon [0016]
  • The carbon is used in amounts between 0.01-0.5% by weight. Carbon together with the carbide forming element precipitates as carbides in the surface coating. The amount of carbides is related to the amount of carbon and carbide forming elements. [0017]
  • Effect of Boron and Silicon [0018]
  • The addition of boron and silicon is used for increasing the wettability but also for lowering the melting point. Also, the combination of boron and silicon works as a fluxing agent. Further the addition of silicon adds oxidation resistance to the coating. The amount of boron is 0.5-2.0, preferably 0.6-1.6% by weight of the composition. The amount of silicon is 1.0-4.0, preferably 1.6-3.5% by weight. [0019]
  • Effect of Phosphorous [0020]
  • The amount of phosphorous is 0.5-4.0, more preferably 1.5-3.0 percent. The main purpose of the addition of phosphorous is lowering the melting point of the powdered metallic material. The amount is preferably sufficient for achieving a melting temperature affordable for the coating to be applicable by means of conventional methods such as powder welding. The present composition of the powdered metallic material has shown to provide a melting temperature of around 850° C. which can be compared with around 1050° C. without phosphorous. Before applying the powdered material onto the substrate it is preferred to preheat the substrate to a temperature in the range of 300-800° C. [0021]
  • The surface coatings are generally applied to the substrate on a specific wear exposed area or over an entire surface. The coating is thereafter machined for supplying a true gauge surface or a desired texture. Thus, it is of great importance that the coating although providing the desired hardness can be machined using conventional equipment. [0022]
  • The application of the surface coating can be performed manually or be automatized, and irrespective of method chosen it is a generally known problem that there sometimes are problems when building layers of large thickness as the viscosity in the weld pool might be to low. The low viscosity results in dripping effects which makes high demands on the skill of the person performing the application. On the other hand, if the viscosity in the weld pool is too high it is difficult applying even layers. [0023]
  • The melting temperature of the used powdered metallic material must in addition not be too high, since the available maximum fusing temperature with conventional equipment is limited and the melting temperature of the substrate must also be taken into account. The melting temperature is also important since a reasonable melting temperature provides the possibility of speeding up the application process. [0024]
  • When the carbide forming element is present in the upper part of the above range a coating that is machinable but still provides sufficient hardness to withstand the harsh conditions prevailing in e.g. glass moulds. [0025]
  • The powder composition also includes carbon. The amount of carbon is decided by the required properties of the final coating. Thus if the substrate is cast iron carbon from this substrate may diffuse from the cast iron into the coating and the prealloyed carbon will be set lower. [0026]
  • The powdered metallic material is manufactured by conventional methods such as water atomization or gas atomization. The particle size is adapted to the application method being used. By way of example, if the powder is applied by powder welding the particle size is often in the range of 20-106 μm. On the other hand, if the powder is applied by PTA, the particle size is often in the range of 45-150 μm. [0027]
  • To enhance the wettability and to better control the formation of carbides the substrate is preheated before application of the powdered material. The preheating is preferably uniform throughout the thickness of the substrate and is thus suitable performed in an oven. The temperature can be varied depending on e.g. the purpose of the coating and available equipment. Generally the temperature interval is 300-800° C. The preheating reduces the affordable application time since the melting of the applied powder on the substrate surface occurs faster. On the other hand, the affordable time can also be reduced by e.g. increasing the fusing temperature.[0028]
  • EXAMPLES
  • The invention is further illustrated by, but should not be limited to, the following preparations and examples. [0029]
  • Example 1
  • A powdered metallic material of the composition according to table 1 below was prepared by gas atomization and applied on a cast iron substrate containing 3.2% by weight of carbon and also on a substrate of mild steel having a carbon content of about 0.1% by weight. The hardness KV30 of the coating on the cast iron substrate was 299, whereas the hardness of the coating on the mild steel substrate was 280. The higher hardness of the coating on the cast iron substrate results from the carbon pick up from the cast iron. [0030]
    TABLE 1
    Composition % by weight
    Cu 3.9
    Fe 0.1
    Cr 0.2
    B 0.9
    Si 2.2
    P 2.1
    C 0.03
    Ni Bal
    Impurities <1.0
  • Additionally the powdered material having the above composition could be applied at high temperature without problems because of the relatively high viscosity. The wettablilty to the substrates, cast iron and mild iron, was without remark. Also the appearance of the final coatings was acceptable. [0031]
  • Example 2
  • A powdered material having the composition according to table 2 was prepared. [0032]
    TABLE 2
    Composition % by weight
    Cu 1.7
    Fe 1.5
    Cr 4.9
    B 1.2
    Si 3.1
    P 1.9
    C 0.17
    Ni Bal.
    Impurities <1
  • Also this powder was prepared by gas atomization. The hardness HV30 of the coating on the cast iron substrate was 402, whereas the hardness of the coating on the mild steel substrate was 380. Thus also in this case an effect of the pick up of carbon from the cast iron substrate could be observed. Furthermore, as in the previous example, the powder was applied at high temperature and the viscosity was sufficiently high for applying the coating without problems. The wettablity to both the substrates was quite acceptable as was the machinability of the coatings. [0033]

Claims (14)

1. A nickel based powdered metallic material comprising in addition to nickel 0-4.5% by weight of copper, 0-5.0% by weight of iron, whereby the total amount of copper and iron is at least 2.5% by weight, 0.05-5.0% by weight of a carbide forming element, 0.5-2.0% by weight of boron, 1.0-4.0% by weight of silicon, 0.5-4.0% by weight of phosphorus, 0.01-0.5% by weight of C and less than 2% by weight of inevitable impurities.
2. Material according to claim 1, including copper in an amount of 2.5-4.5% by weight
3. Material according to claim 1 or 2 claim, wherein the powdered metallic material comprises less than 3.0 wt % iron.
4. Material according to claim 1 wherein the carbide forming element is selected from the group consisting of chromium, tungsten, molybdenum, vanadium, tantalum, niobium, titanium and zirconium.
5. Material according to any of the preceding claims, wherein the powdered metallic material preferably comprises 0.05-1.0% by weight of a carbide forming element.
6. Material according to any of the preceding claims, wherein the powdered metallic material preferably comprises 1.0-5.0% by weight of carbide forming element.
7. Material according to any of the preceding claims, wherein the powdered metallic material preferably comprises 0.6-1.6% boron and 1.6-3.5% silicon.
8. Material according to any of the preceding claims, wherein the powdered metallic material preferably comprises 1.5-3.0 wt % phosphorous.
9. Material according to any of the preceding claims, wherein the powdered metallic material preferably comprises 0.01-0.5% by weight of carbon and preferably less than 0.3% by weight.
10. Material according to any of the preceding claims, wherein the powdered metallic material is a homogenous alloy.
11. Material according to any of the preceding claims, wherein the powdered metallic material is a gas atomized powder or a water atomized powder.
12. A method of forming a wear resistant surface coating on a cast iron substrate, comprising the steps of
providing a nickel based powdered metallic material comprising in addition to nickel 0-4.5% by weight of copper, 0-5.0% by weight of iron, whereby the total amount of copper and iron is at least 2.5% by weight, 0.05-5.0% by weight of a carbide forming element, 0.5-2.0% by weight of boron, 1.0-4.0% by weight of silicon, 0.5-4.0% by weight of phosphorus, 0.01-0.5% by weight of C and less than 2% by weight of inevitable impurities,
optionally preheating the substrate to a temperature in the range of 300-800° C.; and
applying and melting at least one layer of the powdered metallic material onto the substrate by means of thermal coating, whereby formation of carbide occurs on the surface of the substrate.
13. The method according to claim 12, wherein thermal coating includes the use of powder welding or plasma transferred arc welding.
14. The method according to claim 1, wherein thermal coating includes the use of a equipment providing a fusing temperature of 850-910° C.
US09/988,666 2001-11-20 2001-11-20 Surface coatings Abandoned US20030098090A1 (en)

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US20110200838A1 (en) * 2010-02-18 2011-08-18 Clover Industries, Inc. Laser clad metal matrix composite compositions and methods
US20120077058A1 (en) * 2010-09-28 2012-03-29 Kennametal Inc. Corrosion and wear-resistant claddings
CN104226976A (en) * 2013-06-20 2014-12-24 沈阳大陆激光技术有限公司 Laser repair nickel-based alloy powder for gas inlet housings of superchargers of internal combustion engines
US20200208242A1 (en) * 2018-12-28 2020-07-02 Industrial Technology Research Institute Multicomponent alloy coating
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EP3834960A1 (en) 2019-12-13 2021-06-16 Etablissements Chpolansky Laser recharging powder, associated manufacturing method and mould
KR20220012902A (en) * 2019-05-23 2022-02-04 도요세이칸 그룹 홀딩스 가부시키가이샤 A member for glass manufacturing using a Ni-based self-soluble alloy, a Ni-based self-soluble alloy, and a member for conveying a mold and a glass lump using a member for glass manufacturing

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Publication number Priority date Publication date Assignee Title
US20110200838A1 (en) * 2010-02-18 2011-08-18 Clover Industries, Inc. Laser clad metal matrix composite compositions and methods
US20120077058A1 (en) * 2010-09-28 2012-03-29 Kennametal Inc. Corrosion and wear-resistant claddings
US8445117B2 (en) * 2010-09-28 2013-05-21 Kennametal Inc. Corrosion and wear-resistant claddings
CN104226976A (en) * 2013-06-20 2014-12-24 沈阳大陆激光技术有限公司 Laser repair nickel-based alloy powder for gas inlet housings of superchargers of internal combustion engines
US20200208242A1 (en) * 2018-12-28 2020-07-02 Industrial Technology Research Institute Multicomponent alloy coating
US11624104B2 (en) * 2018-12-28 2023-04-11 Industrial Technology Research Institute Multicomponent alloy coating
KR20220012902A (en) * 2019-05-23 2022-02-04 도요세이칸 그룹 홀딩스 가부시키가이샤 A member for glass manufacturing using a Ni-based self-soluble alloy, a Ni-based self-soluble alloy, and a member for conveying a mold and a glass lump using a member for glass manufacturing
EP3974552A4 (en) * 2019-05-23 2023-08-09 Toyo Seikan Group Holdings, Ltd. Ni-based self-fluxing alloy, glass production member using ni-based self-fluxing alloy, and mold and glass mass transport member each using glass production member
KR102650768B1 (en) * 2019-05-23 2024-03-25 도요세이칸 그룹 홀딩스 가부시키가이샤 Ni-based self-soluble alloy, glass manufacturing member using Ni-based self-soluble alloy, mold using glass manufacturing member, and member for transporting glass lumps
FR3104615A1 (en) * 2019-12-13 2021-06-18 Etablissements Chpolansky Laser reloading powder, manufacturing process and mold and related
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