CN111996484A - AlCrSi slurry permeating agent on surface of nickel-based superalloy and preparation method thereof - Google Patents
AlCrSi slurry permeating agent on surface of nickel-based superalloy and preparation method thereof Download PDFInfo
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- 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
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- C23C10/20—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions only one element being diffused
Abstract
The invention discloses an AlCrSi slurry permeating agent for a nickel-based superalloy surface and a preparation method thereof, wherein the AlCrSi slurry permeating agent comprises 3 components, 18-30% of a liquid component A, 35-60% of a liquid component B and the balance of a solid component C in percentage by mass. The aluminized slurry provided by the invention is reasonable in compatibility, moderate in aluminum content and various in addition forms, the infiltration speed and the infiltration layer thickness of aluminum are improved, the toughness of the infiltration layer is ensured, and the mechanical property is improved. The activator, the adhesive and the like all participate or promote the reaction in the high-temperature aluminizing process, no harmful residue is generated, the purity of an aluminized layer is ensured, and the service life of the aluminized coating is prolonged. The aluminum-chromium-silicon slurry prepared by the method greatly improves the sulfur corrosion resistance, the oxygen corrosion resistance, the thermal stability and the coating service life of the aluminum-chromium-silicon coating; meanwhile, the defects of uneven coating thickness, surface nodulation, local aluminum enrichment and the like in the traditional aluminum penetrating agent preparation are overcome.
Description
Technical Field
The invention belongs to the technical field of metal material surface treatment, and particularly relates to an AlCrSi slurry permeating agent for a nickel-based superalloy surface and a preparation method thereof.
Background
The updating of the aerospace field requires more advanced and high thrust-weight turbine engines, and therefore also increasingly higher requirements are placed on the materials. The demand for aircraft engines is closely linked to the development of high temperature alloys. At present, the temperature of a gas inlet of an advanced gas turbine can reach 1600 ℃, the working temperature of a blade can reach 1000-1200 ℃, and a high-temperature part of a turbine engine is not only required to bear thermal cycle and mechanical load, but also required to be corroded by corrosive particles such as sulfate generated by fuel oil combustion. The nickel-based high-temperature alloy has good high-temperature oxidation resistance and hot corrosion resistance, and also has high-temperature creep strength and rupture strength, so that the nickel-based high-temperature alloy is widely applied to the fields of turbine engine blades and the like. The research trend of the current blade materials is to reduce the chromium content in the alloy to improve the high-temperature strength of the alloy, and the side effect is that the alloy generates more serious problems of high-temperature oxidation and gas hot corrosion when in use. Designs that rely solely on superalloy compositions have not been able to meet industry needs. Therefore, surface treatment techniques must be used to improve the performance of the superalloy to achieve higher operating temperatures. Therefore, it is necessary to find a protective coating with excellent high temperature oxidation resistance and high temperature corrosion resistance. Among the high performance aluminized coatings, the liquid (slurry) aluminizing process and the solid aluminizing process are the most mature and widely used processes. In a high-temperature oxidation environment, a compact alumina film is generated on the surface of the material by the aluminized coating, so that an external corrosion medium is prevented from further reacting with the matrix, and the matrix is effectively protected from external corrosion. However, the solid penetrating agent is easy to cause environmental pollution, the uniformity of a penetrating layer is difficult to control, nodules are easy to generate, local aluminum enrichment and the like, the liquid slurry is the best choice, and local aluminizing can be realized, but the aluminizing slurry of the traditional formula has the following problems: (1) the coating prepared by the traditional AlNi slurry permeating agent has insufficient high-temperature oxidation resistance and corrosion resistance; (2) the viscosity and the pH value of the traditional slurry are not appropriate, and the problems of local unevenness, tumor saving and the like appear after the surfaces of parts such as high-temperature alloy blades and the like are dried.
Disclosure of Invention
The invention aims to provide an AlCrSi slurry penetrant on the surface of a nickel-based high-temperature alloy, which is resistant to corrosion in an oxygen and sulfur atmosphere and uniform in coating property, and a preparation method thereof.
The AlCrSi slurry permeating agent for the surface of the nickel-based superalloy, disclosed by the invention, comprises 3 components, 18-30% of a liquid component A, 35-60% of a liquid component B and the balance of a solid component C in percentage by mass; wherein:
the liquid component A comprises the following raw materials in percentage by mass: 5-20% of AlCl33.7 to 8.6 percent of NH4Cl and 8-15% of Cr2O3And 16-30% of H3PO4Solution, and the balance of absolute ethyl alcohol;
the liquid component B comprises the following raw materials in percentage by mass: 10-17.5% CrCl325 to 35% of Al2O3And 10-20% of H3PO4Solution, and the balance of absolute ethyl alcohol;
the solid component C is solid powder, and the raw materials comprise, by mass, 50-70% of spherical AlCr powder, 30-50% of Si powder, and the balance of spherical Al powder.
H in the components A and B3PO4The concentration of the solution is 80-90%; the liquid component A needs to be added with proper amount of water to adjust the density to be 1.1-1.5 g/cm3A pH of 0.2 to 1.2 and a viscosity of 3 to 15X 10-3Pas; the liquid component B needs to be added with proper amount of water to adjust the density to be 1.0-1.4 g/cm3A pH of 0.8 to 2.6 and a viscosity of 5 to 12X 10-3Pas; the content of Al in AlCr powder in the component C is 55-70%.
Preferably, the AlCrSi slurry seeping agent for the nickel-based superalloy surface comprises the following raw materials, by mass, 20% of a liquid component A, 40% of a liquid component B, and the balance of a solid component C.
Preferably, the liquid component A consists of the following components in percentage by mass: 6% AlCl36% NH4Cl, 10% Cr2O3And 24% of H3PO4The balance of absolute ethyl alcohol.
Preferably, the liquid component B consists of the following components in percentage by mass: 15% CrCl330% of Al2O3And 15% of H3PO4The balance of absolute ethyl alcohol.
Preferably, the solid component C comprises the following components in percentage by mass: 60% of spherical AlCr powder, 30% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCr powder is 60%.
The preparation method of the AlCrSi slurry permeating agent on the surface of the nickel-based superalloy comprises the following steps:
1) preparation of liquid component A: mixing AlCl3、NH4Cl、Cr2O3、H3PO4The solution and absolute ethyl alcohol are mixed according to the proportion. Then adding a proper amount of water, stirring and uniformly mixing, and adjusting the concentration of the diluted chlorine element to be lower than 10-3mol/L, and adjusting the density, pH and viscosity of the components to the required range; then standing and filtering to obtain a liquid component A;
2) preparation of liquid component B: adding CrCl3、Al2O3、H3PO4Mixing the solution and absolute ethyl alcohol according to a proportion, stirring and uniformly mixing, and then standing; then adding a proper amount of water, and adjusting the density, pH and viscosity of the component to the required range to obtain a liquid component B;
3) preparation of solid component C: ball-milling and mixing AlCr powder, Si powder and Al powder to obtain a solid component C;
4) preparing a slurry penetrating agent: and uniformly mixing the liquid component A and the liquid component B according to the proportion, then adding the solid component C, adding water for dilution after uniform mixing, and then placing in a vacuum drying oven for drying to obtain the slurry penetrant.
In the step 1), the material mixing sequence is as follows: firstly adding AlCl into partial absolute ethyl alcohol solution3、NH4Cl、Cr2O3、H3PO4Uniformly mixing the solution, adding the rest part of absolute ethyl alcohol, and uniformly mixing; the standing time is 60-100 h.
In the step 2), the standing time is 60-100 h.
In the step 4), the water is added for dilution by 9-11 times according to the mass ratio; the vacuum drying temperature is 50-80 ℃, and the heat preservation time is 16-50 h.
The principle of the invention is as follows:
the solid component C of the invention is added with Al powder which forms an intermediate compound strengthening phase with Ni to generate precipitation strengthening and form compact Al on the surface layer of the coating2O3The film improves the high-temperature creep strength, the fatigue resistance, the oxidation resistance and the hot corrosion resistance of the surface of the nickel-based superalloy; addition of Cr element: form Ni-Cr solid solution with Ni, produce solid solution strengthening, and form Cr2O3、NiCr2O4The composite oxide film improves the high-temperature oxidation resistance and the vulcanization resistance of the surface of the nickel-based high-temperature alloy, and improves the pitting corrosion resistance and the interstitial corrosion resistance. Adding Si powder: the formed dispersion relative coating and the matrix play a role in pinning and blocking, Al inward diffusion and Ni outward diffusion can be prevented, the bonding strength between the coating and the matrix is greatly improved, the service life is greatly prolonged, and Si and Al form an Al-Si inner diffusion layer, so that the surface wear resistance of the nickel-based high-temperature alloy is improved;
the components A and B in the invention adopt absolute ethyl alcohol, so that the metal powder is well wetted, the powder agglomeration can be reduced, and the powder distribution is more uniform.
The invention has the beneficial effects that:
1) the aluminized slurry provided by the invention is reasonable in compatibility, moderate in aluminum content and various in addition forms, the infiltration speed and the infiltration layer thickness of aluminum are improved, the toughness of the infiltration layer is ensured, and the mechanical property is improved. The activator, the adhesive and the like all participate or promote the reaction in the high-temperature aluminizing process, no harmful residue is generated, the purity of an aluminized layer is ensured, and the service life of the aluminized coating is prolonged.
2) The aluminum-chromium-silicon slurry prepared by the method greatly improves the sulfur corrosion resistance, the oxygen corrosion resistance, the thermal stability and the coating service life of the aluminum-chromium-silicon coating; meanwhile, the defects of uneven coating thickness, surface nodulation, local aluminum enrichment and the like in the traditional aluminum penetrating agent preparation are overcome. The aluminizing agent is applied to the aerospace engine blade, and the service life of the aerospace plane engine blade is greatly prolonged.
Drawings
FIG. 1 scanning electron micrographs of coating sections obtained by the preparation of the penetrant slurry of examples 1 and 2; (a) example 1; (b) example 2.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with examples are described in detail below.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be practiced in other ways than those specifically described and will be readily apparent to those of ordinary skill in the art without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Furthermore, reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one implementation of the invention. The appearances of the phrase "in one embodiment" in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments.
Example 1
Firstly, preparing a component A by mass fraction: 20%, component B: 40% and component C: 40% of AlCrSi slurry penetrating agent on the surface of the nickel-based superalloy; wherein, the component A: 6% AlCl36% NH4Cl, 10% Cr2O3And 24% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (B) component: 15% CrCl330% of Al2O3And 15% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (3) component C: 60% of spherical AlCr powder, 30% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCrSi powder is 60%.
The component A is fully mixed, and the mixing sequence is as follows: first-directional part anhydrous secondAdding AlCl into alcoholic solution3、NH4Cl、Cr2O3、H3PO4The solution (concentration 85%) is mixed evenly, and then the rest part of the absolute ethyl alcohol solution is added and mixed evenly. Then adding distilled water for dilution, adjusting the density, pH and viscosity of the components to the required range, standing for 80h, and filtering to obtain liquid component A, wherein the concentration of chlorine element is less than 10-3mol/L, component density of 1.2g/cm3pH 0.3 and viscosity 6X 10-3Pas。
And fully mixing the component B, diluting, and standing for 72 hours to obtain a liquid component B. The density of the component is 1.2g/cm3pH 1.3 and viscosity 7X 10-3Pas。
And mixing the AlCr powder, the Cr powder and the spherical Al powder by using a ball mill to prepare a component C.
And uniformly mixing the component A and the component B, adding the component C, uniformly stirring to obtain a slurry, diluting the slurry and ultrapure water according to the ratio of 1:10, then putting the diluted slurry into a vacuum drying oven for drying, adjusting the temperature to 70 ℃, and preserving the temperature for 20 hours to obtain the AlCrSi slurry penetrant.
The obtained AlCrSi slurry permeating agent is sprayed on the blade of the nickel-based high-temperature aircraft engine according to the conventional method, and the cross section of the coating is shown as figure 1 (a).
Example 2
Firstly, preparing a component A by mass fraction: 20%, component B: 40% and component C: 40% of AlCrSi slurry penetrating agent on the surface of the nickel-based superalloy; wherein, the component A: 6% AlCl37% NH4Cl, 12% Cr2O3And 22% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (B) component: 16% CrCl332% of Al2O3And 12% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (3) component C: 55% of spherical AlCr powder, 32% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCrSi powder is 60%;
the component A is fully mixed, and the mixing sequence is as follows: firstly adding AlCl into partial absolute ethyl alcohol solution3、NH4Cl、Cr2O3、H3PO4The solution (concentration 85%) is mixed evenly and then added with the rest part of absolute ethyl alcohol to be mixed evenly. Diluting with distilled water, adjusting component density, pH and viscosity to desired ranges, standing for 80 hr, and filtering to obtain liquid component A with chlorine concentration lower than 10-3mol/L, component density of 1.2g/cm3pH 0.3 and viscosity 6X 10-3Pas。
And fully mixing the component B, diluting, and standing for 72 hours to obtain a liquid component B. The density of the component is 1.2g/cm3pH 1.3 and viscosity 7X 10-3Pas。
And mixing the AlCr powder, the Cr powder and the spherical Al powder by using a ball mill to prepare a component C.
And uniformly mixing the component A and the component B, adding the component C, uniformly mixing and stirring to obtain slurry, diluting the slurry and ultrapure water according to the ratio of 1:10, then putting the diluted slurry into a vacuum drying oven, drying, adjusting the temperature to 70 ℃, and preserving the temperature for 20 hours to obtain the AlCrSi slurry penetrant.
The AlCrSi slurry infiltration agent is sprayed on the blade of the nickel-based high-temperature aircraft engine according to the conventional method, and the cross section of the coating is shown in figure 1 (b).
Example 3
Firstly, preparing a component A by mass fraction: 20%, component B: 40% and component C: 40% of AlCrSi slurry penetrating agent on the surface of the nickel-based superalloy; wherein, the component A: 7% AlCl38% NH4Cl, 13% Cr2O3And 22% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (B) component: 17% CrCl333% of Al2O3And 12% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (3) component C: 55% of spherical AlCr powder, 32% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCrSi powder is 60%.
The component A is fully mixed, and the mixing sequence is as follows: firstly adding AlCl into partial absolute ethyl alcohol solution3、NH4Cl、Cr2O3、H3PO4The solution (concentration 85%) is mixed evenly and then added with the rest part of absolute ethyl alcohol to be mixed evenly. Diluting with distilled water, adjusting component density, pH and viscosity to desired ranges, standing for 80 hr, and filtering to obtain liquid component A with chlorine concentration lower than 10-3mol/L, component density of 1.2g/cm3pH 0.3 and viscosity 6X 10-3Pas。
And fully mixing the component B, diluting, and standing for 72 hours to obtain a liquid component B. The density of the component is 1.1g/cm3pH 1.3 and viscosity 7X 10-3Pas。
And mixing the AlCr powder, the Cr powder and the spherical Al powder by using a ball mill to prepare a component C.
And uniformly mixing the component A and the component B, adding the component C, uniformly mixing and stirring to obtain slurry, diluting the slurry and ultrapure water according to the ratio of 1:10, then putting the diluted slurry into a vacuum drying oven, drying, adjusting the temperature to 70 ℃, and preserving the temperature for 20 hours to obtain the AlCrSi slurry penetrant.
And finally, spraying the AlCrSi slurry permeating agent on a blade of a nickel-based high-temperature aircraft engine according to a conventional method.
Example 4
Firstly, preparing a component A by mass fraction: 15%, component B: 42% and component C: 43 percent of AlCrSi slurry permeating agent on the surface of the nickel-based superalloy; wherein, the component A: 6% AlCl36% NH4Cl, 10% Cr2O3And 24% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (B) component: 15% CrCl330% of Al2O3And 15% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (3) component C: 60% of spherical AlCr powder, 30% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCrSi powder is 60%.
The component A is fully mixed, and the mixing sequence is as follows: firstly adding AlCl into partial absolute ethyl alcohol solution3、NH4Cl、Cr2O3、H3PO4Solution (concentrated)85 percent), mixing evenly, adding the rest part of absolute ethyl alcohol and mixing evenly. Diluting with distilled water, adjusting component density, pH and viscosity to desired ranges, standing for 80 hr, and filtering to obtain liquid component A with chlorine concentration lower than 10-3mol/L, component density of 1.2g/cm3pH 0.3 and viscosity 7X 10-3Pas。
And fully mixing the component B, diluting, and standing for 72 hours to obtain a liquid component B. The density of the component is 1.2g/cm3pH 1.3 and viscosity 7X 10-3Pas。
And mixing the AlCr powder, the Cr powder and the spherical Al powder by using a ball mill to prepare a component C.
And uniformly mixing the component A and the component B, adding the component C, uniformly mixing and stirring to obtain slurry, diluting the slurry and ultrapure water according to the ratio of 1:10, then putting the diluted slurry into a vacuum drying oven, drying, adjusting the temperature to 70 ℃, and preserving the temperature for 20 hours to obtain the AlCrSi slurry penetrant.
And finally, spraying the AlCrSi slurry permeating agent on the blades of the nickel-based high-temperature aircraft engine according to a conventional method.
Example 5
Firstly, preparing a component A by mass fraction: 20%, component B: 40% and component C: 40% of AlCrSi slurry penetrating agent on the surface of the nickel-based superalloy; wherein, the component A: 6% AlCl36% NH4Cl, 10% Cr2O3And 24% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (B) component: 15% CrCl330% of Al2O3And 15% of H3PO4Solution (concentration 85%), and the balance of absolute ethyl alcohol; and (3) component C: 60% of spherical AlCr powder, 30% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCrSi powder is 60%.
The component A is fully mixed, and the mixing sequence is as follows: firstly adding AlCl into partial absolute ethyl alcohol solution3、NH4Cl、Cr2O3、H3PO4Mixing the solution (concentration 85%), adding the rest anhydrous ethanol, and mixingThen diluting with distilled water to adjust the pH and viscosity, standing for 80h, and filtering to obtain a liquid component A. Wherein the concentration of chlorine is less than 10-3mol/L, component density of 1.0g/cm3pH 1.0 and viscosity 7X 10-3Pas。
And fully mixing the component B, diluting, and standing for 72 hours to obtain a liquid component B. The density of the component is 1.0g/cm3pH 1.4 and viscosity 11X 10-3Pas。
And mixing the AlCr powder, the Cr powder and the spherical Al powder by using a ball mill to prepare a component C.
And uniformly mixing the component A and the component B, adding the component C, uniformly mixing and stirring to obtain slurry, diluting the slurry and ultrapure water according to the ratio of 1:10, then putting the diluted slurry into a vacuum drying oven for drying, adjusting the temperature to 70 ℃, and preserving the temperature for 25 hours to obtain the AlCrSi slurry penetrant.
And finally, spraying the AlCrSi slurry permeating agent on a blade of a nickel-based high-temperature aircraft engine according to a conventional method.
The invention carries out oxidation experiments of different embodiments, the sprayed samples of the embodiments 1-5 are cleaned by alcohol and dried, the weight before oxidation is weighed by a four-digit electronic balance, then the samples are put into a muffle furnace to be heated to 1000 ℃, after 200 hours, the mass change is weighed, and the mass change is compared with the surface area of the sample, thus calculating the mass change of unit area. The experimental result shows that the oxidation resistance of the AlCrSi slurry penetrating agent on the surface of the nickel-based superalloy is greatly improved compared with that of an aluminizing agent prepared by the traditional method (the weight is increased to 1.10mg/cm after 100 hours of the oxidation experiment of the traditional method)2). The mass change after 200h oxidation was: 0.5762mg/cm2、0.6158mg/cm2、0.8704mg/cm2、0.8979mg/cm2、0.9198mg/cm2From the above experimental results, it can be known that the oxidation resistance of the AlCrSi slurry penetrant on the surface of the nickel-based superalloy is significantly improved, and the aluminide coating obtained in example 1 has the best oxidation resistance, which is more than three times of the oxidation resistance of the coating obtained by the conventional method.
FIGS. 1(a) and (b) are sectional scanning electron micrographs of coatings of examples 1 and 2, respectively, of the present invention, and it can be seen from FIG. 1 that the coatings of examples 1 and 2 are relatively uniform, and in particular, the aluminized layer of example 1 has the greatest thickness and the greatest uniformity.
The aluminizing agent prepared by the invention solves the problems of poor oxidation resistance, uneven aluminized layer thickness and the like of the traditional aluminizing agent, is applied to the aerospace engine blade, and greatly prolongs the service life of the aerospace aircraft engine blade.
It should be noted that the above-mentioned embodiments are only for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the claims of the present invention.
Claims (8)
1. The AlCrSi slurry permeating agent for the surface of the nickel-based superalloy is characterized by comprising 3 components, 18-30% of a liquid component A, 35-60% of a liquid component B and the balance of a solid component C, wherein the liquid component A is a solid component;
wherein:
the liquid component A comprises the following raw materials in percentage by mass: 5-20% of AlCl33.7 to 8.6 percent of NH4Cl and 8-15% of Cr2O3And 16-30% of H3PO4Solution, and the balance of absolute ethyl alcohol;
the liquid component B comprises the following raw materials in percentage by mass: 10-17.5% CrCl325 to 35% of Al2O3And 10-20% of H3PO4Solution, and the balance of absolute ethyl alcohol;
the solid component C is solid powder, and the raw materials comprise, by mass, 50-70% of spherical AlCr powder, 30-50% of Si powder, and the balance of spherical Al powder.
2. The AlCrSi slurry infiltration agent for the surface of nickel-based superalloy according to claim 1, wherein the infiltration agent is selected from the group consisting ofH in said components A and B3PO4The concentration of the solution is 80-90%; the liquid component A needs to be added with proper amount of water to adjust the density to be 1.1-1.5 g/cm3A pH of 0.2 to 1.2 and a viscosity of 3 to 15X 10-3Pas; the liquid component B needs to be added with proper amount of water to adjust the density to be 1.0-1.4 g/cm3A pH of 0.8 to 2.6 and a viscosity of 5 to 12X 10-3Pas; the content of Al in AlCr powder in the component C is 55-70%.
3. The AlCrSi slurry infiltration agent for the surface of the nickel-based superalloy as claimed in claim 2, wherein the AlCrSi slurry infiltration agent for the surface of the nickel-based superalloy is composed of, by mass, 20% of a liquid component A, 40% of a liquid component B, and the balance of a solid component C.
4. The AlCrSi slurry infiltration agent for the surface of the nickel-based superalloy according to claim 3, wherein the liquid component A comprises the following components in percentage by mass: 6% AlCl36% NH4Cl, 10% Cr2O3And 24% of H3PO4Solution, and the balance of absolute ethyl alcohol; the liquid component B comprises the following components in percentage by mass: 15% CrCl330% of Al2O3And 15% of H3PO4Solution, and the balance of absolute ethyl alcohol; the solid component C comprises the following components in percentage by mass: 60% of spherical AlCr powder, 30% of Si powder and the balance of spherical Al powder, wherein the content of Al in the AlCr powder is 60%.
5. The preparation method of the AlCrSi slurry permeating agent on the surface of the nickel-based superalloy according to any one of claims 1 to 4, comprising the following steps:
1) preparation of liquid component A: mixing AlCl3、NH4Cl、Cr2O3、H3PO4Mixing the solution and anhydrous ethanol at a certain proportion, stirring, adding appropriate amount of water, adjusting the diluted chlorine elementIs less than 10-3mol/L, adjusting the density, pH and viscosity of the component to the required range, standing and filtering to obtain a liquid component A;
2) preparation of liquid component B: adding CrCl3、Al2O3、H3PO4Mixing the solution and absolute ethyl alcohol according to a proportion, stirring and uniformly mixing, and then standing; then adding a proper amount of water, and adjusting the density, pH and viscosity of the component to the required range to obtain a liquid component B;
3) preparation of solid component C: ball-milling and mixing AlCr powder, Si powder and Al powder to obtain a solid component C;
4) preparing a slurry penetrating agent: and uniformly mixing the liquid component A and the liquid component B according to the proportion, then adding the solid component C, adding water for dilution after uniform mixing, and then placing in a vacuum drying oven for drying to obtain the slurry penetrant.
6. The method for preparing the AlCrSi slurry impregnation agent on the surface of the nickel-based superalloy according to any one of claims 5, wherein in the step 1), the mixing sequence is as follows: firstly adding AlCl into partial absolute ethyl alcohol solution3、NH4Cl、Cr2O3、H3PO4Uniformly mixing the solution, adding the rest part of absolute ethyl alcohol, and uniformly mixing; the standing time is 60-100 h.
7. The preparation method of the AlCrSi slurry infiltration agent on the surface of the nickel-based superalloy according to any one of claims 5, wherein the standing time in the step 2) is 60-100 hours.
8. The method for preparing the AlCrSi slurry penetrant on the surface of the nickel-based superalloy according to any one of claims 5, wherein in the step 4), the dilution with water is 9-11 times by mass; the vacuum heat preservation temperature is 50-80 ℃, and the heat preservation time is 16-50 h.
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Cited By (2)
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| CN113529011A (en) * | 2021-07-21 | 2021-10-22 | 昆明理工大学 | Preparation process of ultra-thick aluminized coating |
| CN115627440A (en) * | 2022-10-21 | 2023-01-20 | 中南大学 | LaB6 enhanced aluminum-chromium-silicon solid powder aluminizing agent and aluminizing method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100392150C (en) * | 2000-09-06 | 2008-06-04 | 通用电气公司 | Method of adopting inorganic seriflux mixture for applicating coating contg aluminium |
| CN101724809A (en) * | 2008-10-22 | 2010-06-09 | 沈阳黎明航空发动机(集团)有限责任公司 | High-temperature preventive coating process |
| US20150064354A1 (en) * | 2012-04-03 | 2015-03-05 | MTU Aero Engines AG | Cr(VI)-FREE CORROSION PROTECTION LAYERS OR ADHESION PROMOTER LAYERS PRODUCED USING A SOLUTION COMPRISING PHOSPHATE IONS AND METAL POWDER, WHEREIN THE METAL POWDER IS COATED AT LEAST PARTLY WITH Si OR Si ALLOYS |
| CN107254659A (en) * | 2009-04-09 | 2017-10-17 | 西门子公司 | Superalloy component and paste compound |
| CN108456842A (en) * | 2017-01-20 | 2018-08-28 | 通用电气公司 | The technique that aluminide covers layer system and is used to form aluminide covering layer system |
| CN108546909A (en) * | 2018-05-11 | 2018-09-18 | 中南大学 | A kind of nickel base superalloy surfaces of aluminum nickel slurry liquid penetration enhancer and preparation method thereof |
-
2020
- 2020-08-24 CN CN202010856849.4A patent/CN111996484B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100392150C (en) * | 2000-09-06 | 2008-06-04 | 通用电气公司 | Method of adopting inorganic seriflux mixture for applicating coating contg aluminium |
| CN101724809A (en) * | 2008-10-22 | 2010-06-09 | 沈阳黎明航空发动机(集团)有限责任公司 | High-temperature preventive coating process |
| CN107254659A (en) * | 2009-04-09 | 2017-10-17 | 西门子公司 | Superalloy component and paste compound |
| US20150064354A1 (en) * | 2012-04-03 | 2015-03-05 | MTU Aero Engines AG | Cr(VI)-FREE CORROSION PROTECTION LAYERS OR ADHESION PROMOTER LAYERS PRODUCED USING A SOLUTION COMPRISING PHOSPHATE IONS AND METAL POWDER, WHEREIN THE METAL POWDER IS COATED AT LEAST PARTLY WITH Si OR Si ALLOYS |
| CN108456842A (en) * | 2017-01-20 | 2018-08-28 | 通用电气公司 | The technique that aluminide covers layer system and is used to form aluminide covering layer system |
| CN108546909A (en) * | 2018-05-11 | 2018-09-18 | 中南大学 | A kind of nickel base superalloy surfaces of aluminum nickel slurry liquid penetration enhancer and preparation method thereof |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113529011A (en) * | 2021-07-21 | 2021-10-22 | 昆明理工大学 | Preparation process of ultra-thick aluminized coating |
| CN113529011B (en) * | 2021-07-21 | 2023-03-31 | 昆明理工大学 | Preparation process of ultra-thick aluminized coating |
| CN115627440A (en) * | 2022-10-21 | 2023-01-20 | 中南大学 | LaB6 enhanced aluminum-chromium-silicon solid powder aluminizing agent and aluminizing method |
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