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CN116411235B - Method for preparing in-situ self-generated nano precipitated phase enhanced high-entropy alloy coating by plasma spraying - Google Patents

Method for preparing in-situ self-generated nano precipitated phase enhanced high-entropy alloy coating by plasma spraying Download PDF

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CN116411235B
CN116411235B CN202310356129.5A CN202310356129A CN116411235B CN 116411235 B CN116411235 B CN 116411235B CN 202310356129 A CN202310356129 A CN 202310356129A CN 116411235 B CN116411235 B CN 116411235B
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entropy alloy
coating
plasma spraying
spraying
alloy coating
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CN116411235A (en
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贾延东
廖洁
王刚
孙康
穆永坤
易军
柯海波
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SHANGHAI UNIVERSITY
Songshan Lake Materials Laboratory
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/134Plasma spraying
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/002Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/02Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/08Metallic material containing only metal elements
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/18After-treatment

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

Abstract

The invention discloses a method for preparing an in-situ self-generated nano precipitated phase enhanced high-entropy alloy coating by plasma spraying, and belongs to the technical field of high-entropy alloy coatings. High-entropy alloy powder Fe by plasma spraying 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 Spraying on a substrate, and carrying out vacuum heat treatment and solution treatment on the obtained coating to obtain an in-situ authigenic nano precipitated phase enhanced high-entropy alloy coating; the parameters in the plasma spraying process are set as follows: the distance between the plasma spray gun and the substrate is 140mm, the spraying voltage is 72.5V, the spraying current is 620A, the powder feeding rate is 35g/min, the argon flow is 30Slpm, and the hydrogen flow is 8Slpm. The method has low cost, further expands the application range of the high-entropy alloy, and has good interlayer combination, compact structure and excellent wear resistance.

Description

一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层 的方法A kind of plasma spraying preparation of in-situ self-generated nano-precipitated phase-enhanced high-entropy alloy coating Methods

技术领域Technical field

本发明属于高熵合金涂层技术领域,尤其涉及一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法。The invention belongs to the technical field of high-entropy alloy coatings, and in particular relates to a method for preparing in-situ self-generated nano-precipitated phase-enhanced high-entropy alloy coatings by plasma spraying.

背景技术Background technique

传统合金的发展经验认为,组成合金的金属元素多了之后,会形成诸多结构复杂的脆性金属间化合物,恶化合金性能。然而近年来,研究者们发现,将5种及5种以上的金属元素按照等摩尔比或近等摩尔比混合到一起,不区分主要元素,熔炼得到的合金具有显微结构简化、不倾向于出现金属间化合物、具有纳米析出物与非晶结构等结构特征,具有高强度、高硬度、耐回火软化、耐磨等性能特性。这类合金最初由叶均蔚等人率先定义为多主元合金或高熵合金。现有传统合金还没有哪种合金可以同时具备以上优异性能,因此高熵合金具有广阔的应用前景,可大幅度应用于制作高强度、耐高温、耐腐蚀的刀具、模具及机件,是切入高性能、高附加值特殊合金材料领域的良好契机。The development experience of traditional alloys believes that when there are too many metal elements making up an alloy, many brittle intermetallic compounds with complex structures will be formed, which will deteriorate the alloy properties. However, in recent years, researchers have discovered that if five or more metal elements are mixed together in an equimolar or nearly equimolar ratio without distinguishing the main elements, the alloy obtained by smelting will have a simplified microstructure and will not tend to It has structural characteristics such as intermetallic compounds, nano-precipitates and amorphous structure, and has performance characteristics such as high strength, high hardness, resistance to tempering and softening, and wear resistance. This type of alloy was first defined as multi-principal alloy or high-entropy alloy by Ye Junwei and others. There is no existing traditional alloy that can possess the above excellent properties at the same time. Therefore, high-entropy alloys have broad application prospects and can be widely used in the production of high-strength, high-temperature-resistant, and corrosion-resistant cutting tools, molds, and machine parts. Good opportunities in the field of high-performance, high-value-added special alloy materials.

迄今,虽然很多学者采用各种方法制备了高熵合金块体材料,并取得了一定的研究成果,但是块体材料的制备存在材料浪费以及成分偏析、缩孔等不可避免的缺陷。通过涂层技术将高熵合金材料用作涂层,可以大大降低制作成本并加速其工业化。So far, although many scholars have used various methods to prepare high-entropy alloy bulk materials and achieved certain research results, the preparation of bulk materials has inevitable defects such as material waste, component segregation, and shrinkage cavities. Using high-entropy alloy materials as coatings through coating technology can greatly reduce production costs and accelerate its industrialization.

目前已有一些方法用于制备高熵合金涂层,如激光熔覆、磁控溅射、热压烧结等,但这些方法具有较高的制备成本并且很难应用到工业中。There are currently some methods used to prepare high-entropy alloy coatings, such as laser cladding, magnetron sputtering, hot press sintering, etc., but these methods have high preparation costs and are difficult to apply in industry.

发明内容Contents of the invention

针对上述现有技术中存在的问题,本发明提出了一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法。采用大气等离子喷涂工艺在不锈钢基体表面制备耐磨涂层,通过调整喷涂参数,实现对涂层微观形貌的最大程度优化,得到涂层耐磨性能最佳的喷涂参数。该方法成本较低,并且进一步扩大了高熵合金的应用范围,该涂层层间结合良好,组织致密,耐磨性能极佳。In view of the problems existing in the above-mentioned prior art, the present invention proposes a method for preparing an in-situ self-generated nano-precipitated phase-enhanced high-entropy alloy coating by plasma spraying. The atmospheric plasma spraying process is used to prepare a wear-resistant coating on the surface of a stainless steel substrate. By adjusting the spraying parameters, the micromorphology of the coating is optimized to the greatest extent, and the spraying parameters with the best wear-resistant performance of the coating are obtained. This method is low-cost and further expands the application scope of high-entropy alloys. The coating has good interlayer bonding, dense structure, and excellent wear resistance.

为实现上述目的,本发明提供如下技术方案:In order to achieve the above objects, the present invention provides the following technical solutions:

一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,通过等离子喷涂的方式将高熵合金粉末喷涂在基体上,对得到的涂层进行真空热处理和固溶处理,即得到原位自生纳米析出相增强高熵合金涂层;A method for preparing an in-situ self-generated nanoprecipitated phase-enhanced high-entropy alloy coating by plasma spraying. The high-entropy alloy powder is sprayed on the substrate by plasma spraying, and the obtained coating is subjected to vacuum heat treatment and solid solution treatment, thereby obtaining In-situ self-generated nano-precipitated phase enhanced high-entropy alloy coating;

所述高熵合金粉末为Fe28.0Co29.5Ni27.5Al8.5Ti6.5The high-entropy alloy powder is Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 ;

所述等离子喷涂过程中的参数设定为:等离子喷枪与基体的距离设为140mm,喷涂电压为72.5V,喷涂电流为620A,送粉速率为35g/min,氩气流量30Slpm,氢气流量为8Slpm。The parameters during the plasma spraying process are set as follows: the distance between the plasma spray gun and the substrate is set to 140mm, the spraying voltage is 72.5V, the spraying current is 620A, the powder feeding rate is 35g/min, the argon flow rate is 30Slpm, and the hydrogen flow rate is 8Slpm. .

所述基体为304不锈钢,在喷涂之前,对基体表面进行油污清除,然后喷砂毛化处理,达到表面粗糙度均匀、无反光;最后置于90℃下干燥2h后进行等离子喷涂。The substrate is made of 304 stainless steel. Before spraying, the surface of the substrate is cleaned of oil and then sandblasted and textured to achieve uniform surface roughness and no reflection. Finally, it is dried at 90°C for 2 hours and then plasma sprayed.

进一步地,所述高熵合金涂层粉末的粒径为53-150μm。Further, the particle size of the high-entropy alloy coating powder is 53-150 μm.

进一步地,所述真空热处理的参数为:温度780±50℃,时间3-5h;所述固溶处理的淬火温度为15-25℃。Further, the parameters of the vacuum heat treatment are: temperature 780±50°C, time 3-5h; the quenching temperature of the solid solution treatment is 15-25°C.

本发明还提供一种利用上述方法制备得到的原位自生纳米析出相增强高熵合金涂层。The invention also provides an in-situ self-generated nano-precipitated phase-reinforced high-entropy alloy coating prepared by the above method.

与现有技术相比,本发明具有如下优点和技术效果:Compared with the existing technology, the present invention has the following advantages and technical effects:

1)本发明提出了一种用大气等离子方法制备Fe28.0Co29.5Ni27.5Al8.5Ti6.5高熵合金涂层的可行性;在本发明中,采用等离子喷涂技术制备高熵合金涂层,通过改变H2流量以控制焰流温度,使得高熵合金粉末在沉积过程中充分融化,增强扁平化颗粒之间界面结构,降低涂层的孔隙率并抑制裂纹的生成,得到Fe28.0Co29.5Ni27.5Al8.5Ti6.5高熵合金涂层法的最佳喷涂参数。1) The present invention proposes the feasibility of using atmospheric plasma method to prepare Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 high-entropy alloy coating; in the present invention, plasma spraying technology is used to prepare high-entropy alloy coating, by changing The H 2 flow is used to control the flame temperature, so that the high-entropy alloy powder is fully melted during the deposition process, enhancing the interface structure between flattened particles, reducing the porosity of the coating and inhibiting the generation of cracks, obtaining Fe 28.0 Co 29.5 Ni 27.5 Al Optimal spraying parameters for 8.5 Ti 6.5 high-entropy alloy coating method.

2)本发明采取商业气雾化高熵合金粉末,粉末球形度好,在喷涂过程中保证粉末的良好流动性;由于高熵合金有扩散迟滞效应,在过饱和的固溶体中,易析出第二相,从而起到弥散强化作用。2) The present invention uses commercial gas atomized high-entropy alloy powder. The powder has good sphericity and ensures good fluidity of the powder during the spraying process. Since the high-entropy alloy has a diffusion hysteresis effect, it is easy to precipitate the second component in a supersaturated solid solution. phase, thus playing a dispersion strengthening effect.

3)本发明采用的方法制备工艺简单,易于制备,成本较低,能够实现工业化。制备的Fe28.0Co29.5Ni27.5Al8.5Ti6.5高熵合金涂层具有高硬度、耐磨性等特点,经过后续热处理强化,涂层的硬度和耐磨性又有了大幅的提高。3) The method used in the present invention has a simple preparation process, is easy to prepare, has low cost, and can be industrialized. The prepared Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 high-entropy alloy coating has the characteristics of high hardness and wear resistance. After subsequent heat treatment strengthening, the hardness and wear resistance of the coating have been greatly improved.

4)本发明采用的方法对基体影响较小,制备的涂层均匀,涂层厚度可控。4) The method adopted in the present invention has little impact on the substrate, the prepared coating is uniform, and the thickness of the coating is controllable.

附图说明Description of the drawings

构成本申请的一部分的附图用来提供对本申请的进一步理解,本申请的示意性实施例及其说明用于解释本申请,并不构成对本申请的不当限定。在附图中:The drawings that form a part of this application are used to provide a further understanding of this application. The illustrative embodiments and descriptions of this application are used to explain this application and do not constitute an improper limitation of this application. In the attached picture:

图1为Fe28.0Co29.5Ni27.5Al8.5Ti6.5粉末的形貌,(a)低倍粉末形貌,(b)高倍粉末形貌;Figure 1 shows the morphology of Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 powder, (a) low magnification powder morphology, (b) high magnification powder morphology;

图2为Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层的表面及截面形貌,(a)涂层表面形貌,(b)涂层截面形貌;Figure 2 shows the surface and cross-sectional morphology of Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating. (a) Coating surface morphology, (b) Coating cross-sectional morphology;

图3本发明制备的喷涂态Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层和热处理态Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层的X射线衍射图;Figure 3 X-ray diffraction patterns of the sprayed Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating and the heat-treated Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating prepared by the present invention;

图4为本发明制备的原位自生纳米析出相增强高熵合金涂层热处理前后的维氏硬度图;Figure 4 is a Vickers hardness diagram before and after heat treatment of the in-situ autogenous nano-precipitated phase-reinforced high-entropy alloy coating prepared by the present invention;

图5为本发明制备的喷涂态Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层和热处理态Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层的磨损系数图。Figure 5 is a graph of the wear coefficient of the sprayed Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating and the heat-treated Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating prepared by the present invention.

具体实施方式Detailed ways

现详细说明本发明的多种示例性实施方式,该详细说明不应认为是对本发明的限制,而应理解为是对本发明的某些方面、特性和实施方案的更详细的描述。Various exemplary embodiments of the invention will now be described in detail. This detailed description should not be construed as limitations of the invention, but rather as a more detailed description of certain aspects, features and embodiments of the invention.

应理解本发明中所述的术语仅仅是为描述特别的实施方式,并非用于限制本发明。另外,对于本发明中的数值范围,应理解为还具体公开了该范围的上限和下限之间的每个中间值。在任何陈述值或陈述范围内的中间值以及任何其他陈述值或在所述范围内的中间值之间的每个较小的范围也包括在本发明内。这些较小范围的上限和下限可独立地包括或排除在范围内。It should be understood that the terms used in the present invention are only used to describe particular embodiments and are not intended to limit the present invention. In addition, for numerical ranges in the present invention, it should be understood that every intermediate value between the upper and lower limits of the range is also specifically disclosed. Every smaller range between any stated value or value intermediate within a stated range and any other stated value or value intermediate within a stated range is also included within the invention. The upper and lower limits of these smaller ranges may independently be included or excluded from the range.

除非另有说明,否则本文使用的所有技术和科学术语具有本发明所述领域的常规技术人员通常理解的相同含义。虽然本发明仅描述了优选的方法和材料,但是在本发明的实施或测试中也可以使用与本文所述相似或等同的任何方法和材料。本说明书中提到的所有文献通过引用并入,用以公开和描述与所述文献相关的方法和/或材料。在与任何并入的文献冲突时,以本说明书的内容为准。Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. Although only the preferred methods and materials are described herein, any methods and materials similar or equivalent to those described herein can be used in the practice or testing of the invention. All documents mentioned in this specification are incorporated by reference to disclose and describe the methods and/or materials in connection with which the documents relate. In the event of conflict with any incorporated document, the contents of this specification shall prevail.

在不背离本发明的范围或精神的情况下,可对本发明说明书的具体实施方式做多种改进和变化,这对本领域技术人员而言是显而易见的。由本发明的说明书得到的其他实施方式对技术人员而言是显而易见的。本申请说明书和实施例仅是示例性的。It will be apparent to those skilled in the art that various modifications and changes can be made to the specific embodiments described herein without departing from the scope or spirit of the invention. Other embodiments will be apparent to the skilled person from the description of the invention. The specification and examples are intended to be illustrative only.

关于本文中所使用的“包含”、“包括”、“具有”、“含有”等等,均为开放性的用语,即意指包含但不限于。The words "includes", "includes", "has", "contains", etc. used in this article are all open terms, which mean including but not limited to.

本发明公开了一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,在304不锈钢表面采用等离子热喷涂在氩气、氢气保护下加热预置合金粉(高熵合金涂层粉末),经高温喷涂(等离子喷涂火焰温度高达几千摄氏度)及快速冷却(等离子喷涂时间非常短,只在表面停留几秒钟,因此涂层从几千摄氏度迅速回到室温会经历一个快速冷却的过程,这是由于等离子喷涂工艺带来的)后形成高熵合金涂层,对其固溶处理后可获得耐磨涂层。本发明制备的高熵合金涂层层间结合良好,组织致密,耐磨性能极佳。测试后发现涂层耐磨性能好,由FCC相、L12相一些氧化物相构成。经过热处理后,涂层由FCC相和L21相以及氧化物相构成,涂层耐磨性能进一步提高。本发明提供的涂层经过测试室温磨损系数为0.35。具体技术方案如下:The invention discloses a method for preparing an in-situ self-generated nano-precipitated phase-enhanced high-entropy alloy coating by plasma spraying. Plasma thermal spraying is used on the surface of 304 stainless steel to heat pre-set alloy powder (high-entropy alloy coating) under the protection of argon and hydrogen. powder), after high-temperature spraying (the plasma spray flame temperature is as high as several thousand degrees Celsius) and rapid cooling (the plasma spraying time is very short and only stays on the surface for a few seconds, so the coating will quickly return to room temperature from several thousand degrees Celsius and will experience a rapid cooling process (this is due to the plasma spraying process), a high-entropy alloy coating is formed, and a wear-resistant coating can be obtained after solid solution treatment. The high-entropy alloy coating prepared by the invention has good interlayer bonding, dense structure and excellent wear resistance. After testing, it was found that the coating has good wear resistance and is composed of FCC phase, L12 phase and some oxide phases. After heat treatment, the coating is composed of FCC phase, L21 phase and oxide phase, and the wear resistance of the coating is further improved. The coating provided by the invention has a room temperature wear coefficient of 0.35 after testing. The specific technical solutions are as follows:

一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,通过等离子喷涂的方式将高熵合金粉末喷涂在基体上,对得到的涂层进行真空热处理和固溶处理,即得到原位自生纳米析出相增强高熵合金涂层;A method for preparing an in-situ self-generated nanoprecipitated phase-enhanced high-entropy alloy coating by plasma spraying. The high-entropy alloy powder is sprayed on the substrate by plasma spraying, and the obtained coating is subjected to vacuum heat treatment and solid solution treatment, thereby obtaining In-situ self-generated nano-precipitated phase enhanced high-entropy alloy coating;

所述高熵合金粉末为Fe28.0Co29.5Ni27.5Al8.5Ti6.5The high-entropy alloy powder is Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 ;

所述等离子喷涂过程中的参数设定为:等离子喷枪与基体的距离设为140mm,喷涂电压为72.5V,喷涂电流为620A,送粉速率为35g/min,氩气流量30Slpm,氢气流量为8Slpm。The parameters during the plasma spraying process are set as follows: the distance between the plasma spray gun and the substrate is set to 140mm, the spraying voltage is 72.5V, the spraying current is 620A, the powder feeding rate is 35g/min, the argon flow rate is 30Slpm, and the hydrogen flow rate is 8Slpm. .

所述等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的具体方法如下:The specific method for preparing in-situ self-generated nano-precipitated phase-enhanced high-entropy alloy coatings by plasma spraying is as follows:

1)喷涂前对基体进行处理;1) Treat the substrate before spraying;

2)将基体固定在喷涂架上;2) Fix the substrate on the spray frame;

3)将喷涂用的高熵合金粉末放置于送粉器中;3) Place the high-entropy alloy powder for spraying in the powder feeder;

4)调整喷涂距离,确定喷枪的运行轨迹;4) Adjust the spraying distance and determine the running trajectory of the spray gun;

5)采用等离子喷涂方法制备高熵合金涂层;5) Use plasma spraying method to prepare high-entropy alloy coating;

6)对制备的高熵合金涂层进行真空热处理和固溶处理,即可获得所述高熵合金涂层。6) Subject the prepared high-entropy alloy coating to vacuum heat treatment and solid solution treatment to obtain the high-entropy alloy coating.

在本发明的一些实施例中,所述基体不做具体限制,但是作为优选,在本发明中所述基体为304不锈钢,在喷涂之前,对基体表面进行油污清除,然后喷砂毛化处理,达到表面粗糙度均匀、无反光;最后置于90℃下干燥2h后进行等离子喷涂。In some embodiments of the present invention, the base body is not specifically limited, but preferably, the base body in the present invention is 304 stainless steel. Before spraying, the surface of the base body is cleaned of oil stains and then sandblasted and textured. Achieve uniform surface roughness and no reflection; finally dry it at 90°C for 2 hours before plasma spraying.

作为优选,在本发明的一些实施例中,所述高熵合金涂层粉末的粒径为53-150μm,因为该粒径范围可以保证粉末流动性好的情况下,易于熔化。低于该范围会不利于流动性,以及容易造成过烧,从而在涂层中留下大量孔洞且粉末容易被等离子火焰吹散,很难沉积到基材上面从而导致沉积效率低。高于该范围会提高熔化难度,会造成粉末熔化不均匀涂层气孔会比较多。Preferably, in some embodiments of the present invention, the particle size of the high-entropy alloy coating powder is 53-150 μm, because this particle size range can ensure that the powder has good fluidity and is easy to melt. Below this range, it will be detrimental to fluidity and easily cause over-burning, leaving a large number of holes in the coating and the powder is easily blown away by the plasma flame, making it difficult to deposit onto the substrate, resulting in low deposition efficiency. Higher than this range will increase the difficulty of melting, resulting in uneven powder melting and more pores in the coating.

作为优选,在本发明的一些实施例中,所述真空热处理的参数为:温度780±50℃,时间3-5h;低于该温度第二相析出尺寸小,数量少,高于该温度第二相会长大且数量减少。Preferably, in some embodiments of the present invention, the parameters of the vacuum heat treatment are: temperature 780±50°C, time 3-5h; below this temperature, the second phase precipitates in small size and quantity, and above this temperature, the second phase precipitates Phase II will grow larger and decrease in number.

作为优选,在本发明的一些实施例中,所述固溶处理的淬火温度为15-25℃,时间为4h。在该温度下进行固溶可以使涂层中的合金元素发生充分扩散,析出纳米强化相,从而提高涂层的硬度。低于该温度析出相数量较少,析出强化效果差,高于该温度会析出相尺寸会长大且数量减少。Preferably, in some embodiments of the present invention, the quenching temperature of the solid solution treatment is 15-25°C and the time is 4 hours. Solid solution at this temperature can fully diffuse the alloy elements in the coating and precipitate nano-strengthening phases, thereby improving the hardness of the coating. Below this temperature, the number of precipitated phases is small and the precipitation strengthening effect is poor. Above this temperature, the size of the precipitated phases will grow and their number will decrease.

本发明还提供一种利用上述方法制备得到的原位自生纳米析出相增强高熵合金涂层。The invention also provides an in-situ self-generated nano-precipitated phase-reinforced high-entropy alloy coating prepared by the above method.

本发明以下实施例所用原料是由宁波众远新材料科技有限公司采用气雾化法制备的。The raw materials used in the following examples of the present invention were prepared by Ningbo Zhongyuan New Material Technology Co., Ltd. using the aerosolization method.

以下实施例作为本发明技术方案的进一步说明。The following examples serve as further explanations of the technical solutions of the present invention.

实施例1Example 1

步骤一、选取304不锈钢工件,用乙醇超声对其表面进行油污清除,然后喷砂毛化处理,达到表面粗糙度均匀,无反光;最后置于90℃下干燥2h,备用。Step 1: Select the 304 stainless steel workpiece, use ethanol ultrasonic to remove oil stains on its surface, and then sandblast and texturize it to achieve uniform surface roughness and no reflection; finally, dry it at 90°C for 2 hours and set aside.

步骤二、以Fe28.0Co29.5Ni27.5Al8.5Ti6.5(见图1)为涂层原料,粒径为53-150μm,通过大气等离子喷涂设备在喷砂粗化处理后的基体表面上进行喷涂,获得Fe28.0Co29.5Ni27.5Al8.5Ti6.5高熵合金涂层的厚度为400μm。喷涂参数为:等离子喷枪与基体的距离设为140mm,喷涂电压为72.5V,喷涂电流为620A,送粉速率为35g/min,氩气流量30Slpm,氢气流量为8Slpm。Step 2: Use Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 (see Figure 1) as the coating raw material, with a particle size of 53-150 μm, and spray it on the surface of the substrate after sandblasting and roughening through atmospheric plasma spraying equipment. The thickness of the Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 high-entropy alloy coating was obtained to be 400 μm. The spraying parameters are: the distance between the plasma spray gun and the substrate is set to 140mm, the spraying voltage is 72.5V, the spraying current is 620A, the powder feeding rate is 35g/min, the argon gas flow rate is 30Slpm, and the hydrogen gas flow rate is 8Slpm.

步骤三、将制备好的高熵合金涂层在真空热处理炉中780℃下热处理4h,随后淬火(淬火温度为15-25℃,时间为4h),得到原位自生纳米析出相增强高熵合金涂层。Step 3: Heat the prepared high-entropy alloy coating in a vacuum heat treatment furnace at 780°C for 4 hours, and then quench (quenching temperature is 15-25°C, time is 4 hours) to obtain an in-situ autogenous nano-precipitated phase-reinforced high-entropy alloy. coating.

图1为Fe28.0Co29.5Ni27.5Al8.5Ti6.5粉末形貌图,从图中可以看出,高熵合金粉末的球形度良好,可以保证在喷涂过程中可以保证良好的流动性。Figure 1 shows the morphology of Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 powder. It can be seen from the figure that the sphericity of the high-entropy alloy powder is good, which can ensure good fluidity during the spraying process.

图2为本实施例制备的原位自生纳米析出相增强高熵合金涂层表面及截面的SEM图,从图中可以看出,层间结合良好,硬质相分布均匀。Figure 2 is an SEM image of the surface and cross-section of the in-situ self-generated nanoprecipitated phase-reinforced high-entropy alloy coating prepared in this embodiment. It can be seen from the image that the interlayer combination is good and the hard phase is evenly distributed.

图3为本实施例制备的原位自生纳米析出相增强高熵合金涂层热处理前后的X射线衍射图,从图中可以看出,Fe28.0Co29.5Ni27.5Al8.5Ti6.5高熵合金涂层在热处理过程中发生了相的转变,涂层由FCC相和L21相以及氧化物相构成,提高了涂层性能。Figure 3 is the X-ray diffraction pattern of the in-situ autogenous nano-precipitated phase-enhanced high-entropy alloy coating prepared in this example before and after heat treatment. It can be seen from the figure that Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 high-entropy alloy coating During the heat treatment process, a phase transformation occurred, and the coating was composed of FCC phase, L21 phase and oxide phase, which improved the coating performance.

图4为本实施例制备的原位自生纳米析出相增强高熵合金涂层热处理前后的维氏硬度图,从图中可以看出,喷涂态Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层的硬度为250HV左右,热处理后涂层的硬度为500HV左右。Figure 4 is a Vickers hardness diagram of the in-situ autogenous nano-precipitated phase-reinforced high-entropy alloy coating prepared in this example before and after heat treatment. It can be seen from the figure that the sprayed Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating has The hardness is about 250HV, and the hardness of the coating after heat treatment is about 500HV.

对所制备涂层进行球盘往复摩擦磨损实验,摩球为硬质合金球、载荷5N、速度220mm/s、总滑动距离576m。图5为本实施例制备的原位自生纳米析出相增强高熵合金涂层热处理前后的磨损系数图,从图中可以看出,喷涂态Fe28.0Co29.5Ni27.5Al8.5Ti6.5涂层的磨损系数为0.8左右,热处理后涂层的磨损系数为0.35左右。A ball-disc reciprocating friction and wear experiment was conducted on the prepared coating. The friction ball was a cemented carbide ball, the load was 5N, the speed was 220mm/s, and the total sliding distance was 576m. Figure 5 is a graph of the wear coefficient before and after heat treatment of the in-situ autogenous nanoprecipitated phase-enhanced high-entropy alloy coating prepared in this example. It can be seen from the figure that the wear of the sprayed Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 coating The coefficient is about 0.8, and the wear coefficient of the coating after heat treatment is about 0.35.

对比例1Comparative example 1

同实施例1,区别在于,喷涂参数为:等离子喷枪与基体的距离设为120mm,喷涂电压为71V,喷涂电流为600A,送粉速率为29g/min,氩气流量30Slpm,氢气流量为7Slpm。Same as Example 1, except that the spraying parameters are: the distance between the plasma spray gun and the substrate is set to 120mm, the spraying voltage is 71V, the spraying current is 600A, the powder feeding rate is 29g/min, the argon flow rate is 30Slpm, and the hydrogen flow rate is 7Slpm.

结果发现,利用本对比例制备的涂层维氏硬度值为220HV左右,磨损系数为1.2左右。It was found that the Vickers hardness value of the coating prepared using this comparative example was about 220HV, and the wear coefficient was about 1.2.

对比例2Comparative example 2

同实施例1,区别在于,热处理温度选择900℃;Same as Example 1, except that the heat treatment temperature is 900°C;

结果发现,利用本对比例制备的涂层维氏硬度值为400HV左右,磨损系数为0.6左右。The results show that the Vickers hardness value of the coating prepared using this comparative example is about 400HV, and the wear coefficient is about 0.6.

以上,仅为本申请较佳的具体实施方式,但本申请的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本申请揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本申请的保护范围之内。因此,本申请的保护范围应该以权利要求的保护范围为准。The above are only preferred specific implementations of the present application, but the protection scope of the present application is not limited thereto. Any person familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application. All are covered by the protection scope of this application. Therefore, the protection scope of this application should be subject to the protection scope of the claims.

Claims (5)

1.一种等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,其特征在于,通过等离子喷涂的方式将高熵合金粉末喷涂在基体上,对得到的涂层进行真空热处理和固溶处理,即得到原位自生纳米析出相增强高熵合金涂层;1. A method for preparing an in-situ autogenous nano-precipitated phase-enhanced high-entropy alloy coating by plasma spraying, which is characterized in that high-entropy alloy powder is sprayed on the substrate by plasma spraying, and the obtained coating is subjected to vacuum heat treatment and Solid solution treatment is used to obtain an in-situ self-generated nano-precipitated phase-enhanced high-entropy alloy coating; 所述高熵合金粉末为Fe28.0Co29.5Ni27.5Al8.5Ti6.5The high-entropy alloy powder is Fe 28.0 Co 29.5 Ni 27.5 Al 8.5 Ti 6.5 ; 所述等离子喷涂过程中的参数设定为:等离子喷枪与基体的距离设为140mm,喷涂电压为72.5V,喷涂电流为620A,送粉速率为35g/min,氩气流量30Slpm,氢气流量为8Slpm;The parameters during the plasma spraying process are set as follows: the distance between the plasma spray gun and the substrate is set to 140mm, the spraying voltage is 72.5V, the spraying current is 620A, the powder feeding rate is 35g/min, the argon flow rate is 30Slpm, and the hydrogen flow rate is 8Slpm. ; 所述真空热处理的参数为:温度780±50℃,时间3-5h。The parameters of the vacuum heat treatment are: temperature 780±50°C, time 3-5h. 2.根据权利要求1所述的等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,其特征在于,所述高熵合金涂层粉末的粒径为53-150μm。2. The method for preparing in-situ self-generated nanoprecipitated phase-enhanced high-entropy alloy coating by plasma spraying according to claim 1, characterized in that the particle size of the high-entropy alloy coating powder is 53-150 μm. 3.根据权利要求1所述的等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,其特征在于,在等离子喷涂之前还包括对基体进行预处理的过程,所述预处理方法如下:对基体表面清除油污,然后喷砂毛化处理至表面粗糙度均匀,无反光;最后置于90℃下干燥2小时。3. The method for preparing in-situ self-generated nanoprecipitated phase-enhanced high-entropy alloy coatings by plasma spraying according to claim 1, characterized in that, before plasma spraying, it also includes a process of pretreating the substrate, and the pretreatment method The steps are as follows: remove oil stains on the surface of the substrate, then sandblast and texture it until the surface roughness is uniform and non-reflective; finally, dry it at 90°C for 2 hours. 4.根据权利要求1所述的等离子喷涂制备原位自生纳米析出相增强高熵合金涂层的方法,其特征在于,所述固溶处理的淬火温度为15-25℃。4. The method for preparing in-situ self-generated nanoprecipitated phase-enhanced high-entropy alloy coating by plasma spraying according to claim 1, characterized in that the quenching temperature of the solid solution treatment is 15-25°C. 5.一种如权利要求1-4任一项所述的方法制备得到的原位自生纳米析出相增强高熵合金涂层。5. An in-situ self-generated nano-precipitated phase-reinforced high-entropy alloy coating prepared by the method of any one of claims 1-4.
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