The present invention relates to the technical field of metal powder processing, in particular to a preparation process of multi-component spherical alloy powder.
Refractory metals and their compounds, such as tungsten, molybdenum, tantalum, niobium, rhenium, tungsten carbide, tantalum carbide and the like, are widely used in many key fields such as aerospace, national defense and military industry, energy electronics and nuclear industry due to their unique high temperature resistance, corrosion resistance, high density, wear resistance and other special properties. With the development and application of powder metallurgy technology and 3D printing technology, the demand for multi-component spherical powder containing refractory metals or compounds thereof is growing. Spherical powder has the characteristics of good fluidity and high tap density and is good in wettability. After being added as an additive particle, the spherical powder has good bondability with surrounding tissues, and stress concentration is not liable to occur. It is difficult to prepare spherical powder by traditional physical and chemical methods. Powder prepared by the plasma rotation electrode process (PREP) method has a sphericity of up to 95%, is low in content of oxygen and other impurities and excellent in comprehensive performance, and is an ideal material for powder metallurgy and 3D printing. According to the PREP method, a round bar is used as the base material, and the base material is heated and melted by an ultra-high temperature plasma gun, and the molten liquid is centrifugally atomized into spherical powder. For a single refractory metal or compound thereof, it is difficult to smelt and make a rod due to its high melting point and high hardness, which makes it difficult to prepare powder by the PREP method. The present invention solves the problem of difficulty in preparing rods from a single refractory metal or compound thereof by prefabricating a multi-component base material in advance, and can directly prepare the multi-component spherical alloy powder containing the refractory metals or compound thereof by the PREP method.
Therefore, based on the above background, the present invention provides a preparation process of multi-component spherical alloy powder containing a refractory metal or compound thereof, which adopts the PREP method to prepare the multi-component spherical alloy powder to meet the application requirements.
The present invention is achieved through the following technical solutions:
a preparation process of multi-component spherical alloy powder adopts a PREP method to prepare multi-component spherical alloy powder, the multi-component alloy includes at least one of refractory metals and compounds thereof, specifically including tungsten, molybdenum, tantalum, niobium, rhenium, tungsten carbide, tantalum carbide and the like.
To further describe the present invention, the preparation method thereof is as follows:
To further describe the present invention, a spatial structure meshing method is adopted to prepare the multi-component alloy rod in step 2.1, and the preparation method thereof is as follows:
To further describe the present invention, a direct element mixing method is adopted to prepare the multi-component alloy rod in step 2.1, and the preparation method thereof is as follows:
To further describe the present invention, before the powder material is put into the graphite mold in step 4.2, the graphite is treated as follows: the surface of the graphite mold in contact with the powder is sprayed with a boron nitride spray, and after the boron nitride spray is air-dried, the ball-milled powder material is put into the graphite mold under the protection of argon.
To further describe the present invention, hot pressed sintering in step 4.3 includes three stages, which are:
To further describe the present invention, a porous framework method is adopted to prepare the multi-component alloy rod in step 2.1, and the preparation method thereof is as follows:
To further describe the present invention, stearic acid or urea is used as the pore-forming agent.
By adopting the above technical solutions, the beneficial effects are as follows:
In order to explain the embodiments of the present invention or the technical solutions in the prior art, more clearly, the accompanying drawings that necessarily used in the description of the embodiments or the prior art are briefly introduced below. Apparently, the accompanying drawings in the following description are only some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained according to these accompanying drawings without creative efforts.
Wherein: 1—multi-component alloy rod; 2—mesh; 3—filler metal particles; 4—multi-component alloy rod; 5—framework of a refractory metal or compound thereof; and 6—pouring metal.
In order to make the purposes, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Apparently, the described embodiments are some embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
Embodiments of the present invention are described in detail below, and examples of which are illustrated in the accompanying drawings, wherein the same or similar reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. In the description of the present invention, it should be understood that the orientation or positional relationship indicated by the terms such as “upper”, “lower”, “front”, “rear”, “left”, “right”, “inner”, “outer”, “vertical” and “circumferential” is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the indicated device or element must have a specific orientation or constructed and operated in a specific orientation, and therefore should not be construed as limiting the invention.
In the description of the present invention, “first feature” and “second feature” may include one or more of the features. In addition, the terms “first” and “second” are only used for descriptive purposes, and should not be construed as indicating or implying relative importance or implying the number of indicated technical features. Thus, a feature defined as “first” or “second” may expressly or implicitly include one or more of that features.
The present invention will be further described below with reference to
Embodiment 1: a preparation process of multi-component spherical alloy powder adopts the PREP method to prepare multi-component spherical alloy powder, the multi-component alloy includes at least one of refractory metals and compounds thereof, specifically including tungsten, molybdenum, tantalum, niobium, rhenium, tungsten carbide, tantalum carbide and the like.
The specific preparation method is as follows:
In the present embodiment, a spatial structure meshing method is adopted to prepare the multi-component alloy rod, and the specific preparation method thereof is as follows:
Embodiment 2: a preparation process of multi-component spherical alloy powder adopts the PREP method to prepare multi-component spherical alloy, multi-components include at least one of refractory metals and compounds thereof, specifically including tungsten, molybdenum, tantalum, niobium, rhenium, tungsten carbide, tantalum carbide and the like. The specific preparation method is as follows:
In the present embodiment, a direct element mixing method is adopted to prepare the multi-component alloy rod, and the specific preparation method is as follows:
In this step, before the powder material is put into the graphite mold, the graphite is treated as follows: the surface of the graphite mold in contact with the powder is sprayed with a boron nitride spray, on the one hand, the powder is prevented from diffusing and reacting with the graphite mold during the sintering process, and on the other hand, it is beneficial to demolding a sintered block after sintering; and after the boron nitride spray is air-dried, the ball-milled powder material is put into the graphite mold under the protection of argon.
In this step, hot pressed sintering includes three stages, which are:
Embodiment 3: a preparation process of multi-component spherical alloy powder adopts the PREP method to prepare a multi-component spherical alloy, multi-components include at least one of refractory metals and compounds thereof, specifically including tungsten, molybdenum, tantalum, niobium, rhenium, tungsten carbide, tantalum carbide and the like. The specific preparation method is as follows:
In the present embodiment, a porous framework method is adopted to prepare the multi-component alloy rod, and the specific preparation method is as follows:
In this step, the spherical pore-forming agent is used to ensure the isotropy of pores, and in order to avoid the segregation of the pore-forming agent, the raw material and the pore-forming agent are put into the mixer for mixing.
In this step, in order to reduce the friction between the mold wall and the powder, so as to maintain the integrity of the green body during the demolding process after pressing, a zinc stearate alcohol solution is applied to the mold wall as a lubricant before pressing.
The present invention and the embodiments have been described above, and the description is not restrictive. What is shown in the accompanying drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In a word, if those of ordinary skill in the art are inspired by it and design structure modes and embodiments similar to the technical solution without creativity and departing from the purpose of the present invention, the structure modes and embodiments should fall within the protection scope of the present invention.
Number | Date | Country | Kind |
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202210027237.3 | Jan 2022 | CN | national |
Number | Name | Date | Kind |
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4562039 | Koehler | Dec 1985 | A |
20180236138 | Ye | Aug 2018 | A1 |
Entry |
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Yin et al. (“Titanium-tantalum alloy powder produced by the plasma rotating electrode process (PREP).” Key Engineering Materials 770 (2018): 18-22.) (Year: 2018). |
Number | Date | Country | |
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20230219133 A1 | Jul 2023 | US |
Number | Date | Country | |
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Parent | PCT/CN2022/072870 | Jan 2022 | US |
Child | 17669865 | US |