CN116516228A - A superhard wear-resistant refractory high-entropy alloy film and its preparation method - Google Patents
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- 238000002360 preparation method Methods 0.000 title claims abstract description 15
- 239000010408 film Substances 0.000 claims abstract description 50
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- 229910052710 silicon Inorganic materials 0.000 claims abstract description 24
- 239000010703 silicon Substances 0.000 claims abstract description 24
- 239000010409 thin film Substances 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims abstract description 18
- 238000001755 magnetron sputter deposition Methods 0.000 claims abstract description 15
- 229910052715 tantalum Inorganic materials 0.000 claims abstract description 11
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 11
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 9
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 9
- 229910052751 metal Inorganic materials 0.000 claims abstract description 7
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- 239000000843 powder Substances 0.000 claims abstract description 6
- 238000005245 sintering Methods 0.000 claims abstract description 6
- 238000005477 sputtering target Methods 0.000 claims abstract description 6
- 238000004544 sputter deposition Methods 0.000 claims description 23
- 238000005516 engineering process Methods 0.000 claims description 15
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 claims description 10
- 238000000354 decomposition reaction Methods 0.000 claims description 7
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- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 5
- 238000000713 high-energy ball milling Methods 0.000 claims description 5
- 238000007373 indentation Methods 0.000 claims description 3
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- 238000001035 drying Methods 0.000 claims 1
- 239000013078 crystal Substances 0.000 abstract description 4
- 239000002159 nanocrystal Substances 0.000 abstract description 3
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- 229910052720 vanadium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/045—Alloys based on refractory metals
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
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- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/14—Metallic material, boron or silicon
- C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
- C23C14/165—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon by cathodic sputtering
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/3407—Cathode assembly for sputtering apparatus, e.g. Target
- C23C14/3414—Metallurgical or chemical aspects of target preparation, e.g. casting, powder metallurgy
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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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- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
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- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
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Abstract
本发明属于耐磨合金材料技术领域,涉及一种超硬耐磨难熔高熵合金薄膜及其制备方法。所述的超硬耐磨难熔高熵合金薄膜具有超细纳米晶、硬度耐磨性能超常等特征。所述的制备方法包括以下步骤:制备NbMoWTa难熔高熵合金靶材;所述的溅射靶材是通过Nb、Mo、W、Ta金属粉末球磨混合后,在高温下进行等离子体烧结而成;采用磁控溅射法将所得到的难熔高熵合金靶材在硅基底上溅射成膜,得到超硬耐磨难熔高熵合金薄膜。本发明制备工艺简单、稳定可控;所得到的产品晶粒细小均一、力学性能和耐磨性优异。这为实现难熔高熵合金在极端工程应用提供了必要条件。
The invention belongs to the technical field of wear-resistant alloy materials, and relates to a superhard wear-resistant refractory high-entropy alloy film and a preparation method thereof. The super-hard wear-resistant refractory high-entropy alloy thin film has the characteristics of ultra-fine nanocrystals, extraordinary hardness and wear resistance, and the like. The preparation method includes the following steps: preparing a NbMoWTa refractory high-entropy alloy target; the sputtering target is formed by ball milling and mixing Nb, Mo, W, and Ta metal powders, and then plasma sintering at high temperature ; Using the magnetron sputtering method to sputter the obtained refractory high-entropy alloy target on the silicon substrate to form a film to obtain a superhard wear-resistant refractory high-entropy alloy film. The preparation process of the invention is simple, stable and controllable; the obtained product has fine and uniform crystal grains, excellent mechanical properties and wear resistance. This provides the necessary conditions for the realization of refractory high-entropy alloys in extreme engineering applications.
Description
技术领域technical field
本发明涉及耐磨合金材料技术领域,具体为一种超硬耐磨难熔高熵合金薄膜及其制备方法。The invention relates to the technical field of wear-resistant alloy materials, in particular to a superhard wear-resistant refractory high-entropy alloy film and a preparation method thereof.
背景技术Background technique
高熵合金是由四种或四种以上的合金元素以等摩尔比或近等摩尔比混合而成的,其多组元将导致其混合熵较高,在热力学上呈现出高熵效应,往往形成单相固溶体结构,而不是脆性的金属间化合物,因此相较于传统合金而言,高熵合金表现出高强度、抗辐照性、耐腐蚀性能等优异的力学及物理化学性能。难熔高熵合金则是由四种或四种以上难熔金属元素(如Nb、Mo、W、Ta、V、Zr、Hf)以等原子比或近等原子比混合而成的一类高熵合金,由于组元都具有高熔点等特点,因此相比于传统的镍基、钴基高温合金,难熔高熵合金具有更高的回火抗力和抗高温软化性能,有望在航空、航天、核能等高温苛刻工况下应用。High-entropy alloys are composed of four or more alloying elements mixed in an equimolar ratio or nearly equimolar ratio, and its multi-components will lead to a high mixing entropy, showing a high-entropy effect in thermodynamics, often A single-phase solid solution structure is formed instead of a brittle intermetallic compound. Therefore, compared with traditional alloys, high-entropy alloys exhibit excellent mechanical and physical and chemical properties such as high strength, radiation resistance, and corrosion resistance. Refractory high-entropy alloys are a class of high-entropy alloys that are mixed with four or more refractory metal elements (such as Nb, Mo, W, Ta, V, Zr, Hf) in equal or nearly equal atomic ratios. Entropy alloys, because the components have high melting points, etc., compared with traditional nickel-based and cobalt-based superalloys, refractory high-entropy alloys have higher tempering resistance and high-temperature softening resistance, and are expected to be used in aviation and aerospace. , Nuclear energy and other high temperature and harsh working conditions.
然而,由于难熔高熵合金的高熔点,采用传统的电弧熔炼法和粉末冶金法难以满足制备出具有组织均匀、单相结构的难熔高熵合金,制约了难熔高熵合金的发展;其次,块体难熔高熵合金成本过于高昂,难以将其推向规模化应用,因此将难熔高熵合金薄膜涂覆于现有的零部件表面或具有更大的经济效益。However, due to the high melting point of refractory high-entropy alloys, it is difficult to prepare refractory high-entropy alloys with uniform structure and single-phase structure by traditional arc melting and powder metallurgy methods, which restricts the development of refractory high-entropy alloys; Secondly, the cost of bulk refractory high-entropy alloys is too high to push them into large-scale applications. Therefore, coating refractory high-entropy alloy thin films on the surface of existing parts may have greater economic benefits.
目前,薄膜的制备方法主要有磁控溅射法、激光熔覆法、等离子喷涂法等工艺方法。其中,磁控溅射技术具有沉积速度快、可在各类基底上沉积,所得到的薄膜纯度高、均匀致密、能够精确调控厚度等优点,是将其推向实际生产应用的理想工艺技术;另一方面,该技术仅涉及靶材的物理溅射过程,无需将其加热熔化,因此十分适合制备难熔高熵合金体系薄膜。At present, the preparation methods of thin films mainly include magnetron sputtering, laser cladding, and plasma spraying. Among them, the magnetron sputtering technology has the advantages of fast deposition speed, can be deposited on various substrates, and the obtained thin film is high in purity, uniform and dense, and can accurately control the thickness. It is an ideal technology to push it to practical production applications; On the other hand, this technology only involves the physical sputtering process of the target without heating and melting it, so it is very suitable for the preparation of refractory high-entropy alloy thin films.
此外,由于难熔高熵合金多组元间迥异的元素性质,通过磁控溅射工艺的合理调控有望制备得到具有特殊结构的涂层材料,从而获得非凡的力学及摩擦性能。In addition, due to the very different element properties among the multi-components of refractory high-entropy alloys, coating materials with special structures are expected to be prepared through reasonable regulation of the magnetron sputtering process, so as to obtain extraordinary mechanical and friction properties.
发明内容Contents of the invention
本发明的目的在于提供一种超硬耐磨难熔高熵合金薄膜及其制备方法,以实现上述背景技术中提出的技术效果。The purpose of the present invention is to provide a superhard wear-resistant refractory high-entropy alloy thin film and a preparation method thereof, so as to realize the technical effects proposed in the background art above.
为实现上述目的,发明提供如下技术方案:一种超硬耐磨难熔高熵合金薄膜,包括以下等原子百分比的合金组分:Nb、Mo、W、Ta。In order to achieve the above object, the invention provides the following technical solution: a superhard wear-resistant refractory high-entropy alloy thin film, including the following alloy components with equal atomic percentages: Nb, Mo, W, Ta.
优选的,所述超硬耐磨难熔高熵合金薄膜具有单相BCC固溶体结构,晶粒尺寸不高于25nm,薄膜厚度在3.0~3.5μm。Preferably, the superhard wear-resistant refractory high-entropy alloy film has a single-phase BCC solid solution structure, the grain size is not higher than 25 nm, and the film thickness is 3.0-3.5 μm.
优选的,所述超硬耐磨难熔高熵合金薄膜的原始组织表现出周期性为5~10nm的调幅层状分解亚结构。Preferably, the original structure of the superhard wear-resistant refractory high-entropy alloy thin film exhibits an amplitude-modulated layered decomposition substructure with a periodicity of 5-10 nm.
优选的,所述超硬耐磨难熔高熵合金薄膜的纳米压入硬度在20~25GPa,磨损率在1.0×10-5~1.4×10-5mm3/(N·m)。Preferably, the nano-indentation hardness of the superhard wear-resistant refractory high-entropy alloy film is 20-25 GPa, and the wear rate is 1.0×10 -5 -1.4×10 -5 mm 3 /(N·m).
一种超硬耐磨难熔高熵合金薄膜的制备方法,具体包括以下步骤:A method for preparing a superhard wear-resistant refractory high-entropy alloy film, specifically comprising the following steps:
步骤一:溅射靶材的制备:将各单质元素Nb、Mo、W、Ta金属粉末按照等摩尔比例使用高能球磨法混合24~30h,随后在1500~1700℃下采用等离子体烧结技术制备出具有等原子比的NbMoWTa难熔高熵合金靶材;Step 1: Preparation of sputtering target: Mix metal powders of elemental elements Nb, Mo, W, and Ta in equimolar proportions using high-energy ball milling for 24-30 hours, and then use plasma sintering technology at 1500-1700°C to prepare NbMoWTa refractory high-entropy alloy target with equiatomic ratio;
步骤二:薄膜沉积:通过磁控溅射技术将步骤一所得到的合金靶材在硅基底上溅射成膜,溅射功率为100~120W,偏置电压为-80~-100V,得到超硬耐磨难熔高熵合金薄膜。Step 2: Thin film deposition: The alloy target obtained in step 1 is sputtered on the silicon substrate to form a film by magnetron sputtering technology, the sputtering power is 100~120W, the bias voltage is -80~-100V, and super Hard and wear-resistant refractory high-entropy alloy thin films.
优选的,所述硅基底采用经丙酮、无水乙醇清洗并吹干后的单面抛光单晶硅基片。Preferably, the silicon substrate is a single-sided polished single-crystal silicon substrate cleaned with acetone and absolute ethanol and dried.
优选的,所述的磁控溅射技术中沉积速率为0.19~0.22nm/s。Preferably, the deposition rate in the magnetron sputtering technique is 0.19-0.22 nm/s.
优选的,所述的磁控溅射技术采用直流电源溅射。Preferably, the magnetron sputtering technology uses DC power sputtering.
优选的,所述的磁控溅射技术是采用纯度高达99.99%的Ar作为离化气体。Preferably, the magnetron sputtering technology uses Ar with a purity as high as 99.99% as the ionized gas.
与现有技术相比,发明的有益效果是:Compared with the prior art, the beneficial effects of the invention are:
1、该超硬耐磨难熔高熵合金薄膜及其制备方法,提供的超硬耐磨难熔高熵合金薄膜的制备方法具有沉积速度快、工艺易于调控、薄膜厚度精确可控、经济效益高等优点。1. The ultra-hard wear-resistant refractory high-entropy alloy thin film and its preparation method, the preparation method of the ultra-hard wear-resistant refractory high-entropy alloy thin film provided has the advantages of fast deposition speed, easy process control, precise and controllable film thickness, and economic benefits Advanced advantages.
2、该超硬耐磨难熔高熵合金薄膜及其制备方法,所制备的超硬耐磨难熔高熵合金薄膜表面光滑、结构致密,晶粒尺寸不高于25nm,具有超细纳米晶的特征,薄膜厚度在3.0~3.5μm,膜基结合力好,可直接满足关键耐磨零部件的服役要求;此外,通过工艺调控,采用特定的工作气压、电源功率、沉积速率、基体旋转、基底偏压、沉积后的离化气体保护等方式,使难熔合金元素中的W、Ta元素发生偏析,致使形成周期性为5~10nm的调幅层状分解亚结构,为实现难熔高熵合金超硬和超常耐磨性能提供结构基础。2. The ultra-hard wear-resistant refractory high-entropy alloy film and its preparation method. The prepared super-hard wear-resistant refractory high-entropy alloy film has a smooth surface, a dense structure, a grain size of no higher than 25nm, and ultrafine nanocrystalline The film thickness is 3.0-3.5μm, and the film-base bonding force is good, which can directly meet the service requirements of key wear-resistant parts; in addition, through process regulation, specific working air pressure, power supply, deposition rate, substrate rotation, Substrate bias, ionized gas protection after deposition, etc., segregate the W and Ta elements in the refractory alloy elements, resulting in the formation of an amplitude-modulated layered decomposition substructure with a periodicity of 5-10nm, in order to achieve refractory high entropy Alloy superhard and super wear resistance provide structural basis.
3、该超硬耐磨难熔高熵合金薄膜及其制备方法,所制备的超硬耐磨难熔高熵合金薄膜的纳米压入硬度在20~25GPa,磨损率在1.0×10-5~1.4×10-5mm3/(N·m),其中多主元的固溶强化、超细纳米晶强化效应、独特的调幅分解层状结构强化效应以及柱状晶边界强化的叠加效应导致其获得超高硬度;此外,较高的基底偏压会导致薄膜在成型过程中受到更多的离子轰击,使薄膜内应力增加,进而导致薄膜的高硬度。本发明所制备的薄膜均高于现阶段研究的同体系难熔高熵合金薄膜,具有广阔的应用前景。3. The super-hard wear-resistant refractory high-entropy alloy film and its preparation method, the nano-indentation hardness of the prepared super-hard wear-resistant refractory high-entropy alloy film is 20-25GPa, and the wear rate is 1.0× 10-5 ~ 1.4×10 -5 mm 3 /(N m), in which the multi-principal solid solution strengthening, ultrafine nanocrystalline strengthening effect, unique amplitude modulation decomposition layered structure strengthening effect and the superposition effect of columnar grain boundary strengthening lead to its Ultra-high hardness; in addition, a higher substrate bias will cause the film to be bombarded by more ions during the forming process, which will increase the internal stress of the film and lead to high hardness of the film. The films prepared by the invention are all higher than the refractory high-entropy alloy films of the same system studied at the present stage, and have broad application prospects.
附图说明Description of drawings
图1是本发明制备的NbMoWTa难熔高熵合金薄膜的XRD图谱;Fig. 1 is the XRD spectrum of the NbMoWTa refractory high-entropy alloy film prepared by the present invention;
图2是本发明制备的NbMoWTa难熔高熵合金薄膜的截面图像;(a)扫描电子显微镜;(b)透射电子显微镜;Fig. 2 is the cross-sectional image of the NbMoWTa refractory high-entropy alloy film prepared by the present invention; (a) scanning electron microscope; (b) transmission electron microscope;
图3是本发明制备的NbMoWTa难熔高熵合金薄膜的亚结构元素分布图像;Fig. 3 is the substructural element distribution image of the NbMoWTa refractory high-entropy alloy film prepared by the present invention;
图4是本发明制备的NbMoWTa难熔高熵合金薄膜与现阶段研究的难熔金属单质、难熔高熵合金的硬度与耐磨性能的对比图:(a)硬度对比;(b)磨损率对比。Fig. 4 is a comparison diagram of the hardness and wear resistance of the NbMoWTa refractory high-entropy alloy film prepared by the present invention and the refractory metal single substance and refractory high-entropy alloy studied at the present stage: (a) hardness comparison; (b) wear rate Compared.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
实施例1:Example 1:
一种超硬耐磨难熔高熵合金薄膜的制备方法,包括以下步骤:A method for preparing a superhard wear-resistant refractory high-entropy alloy film, comprising the following steps:
1)将各单质元素Nb、Mo、W、Ta金属粉末按照等摩尔比例使用高能球磨法混合24h,随后在1700℃下采用等离子体烧结技术制备出具有等摩尔比的NbMoWTa难熔高熵合金靶材;1) The metal powders of elemental elements Nb, Mo, W, and Ta were mixed in equimolar proportions using high-energy ball milling for 24 hours, and then NbMoWTa refractory high-entropy alloy targets with equimolar ratios were prepared by plasma sintering technology at 1700°C material;
2)将硅基底依次在丙酮、无水乙醇中超声清洗20min,随后使用电吹风将其烘干,以保证去除硅基底表面的油污及水分;2) The silicon substrate was ultrasonically cleaned in acetone and absolute ethanol for 20 minutes, and then dried with a hair dryer to ensure the removal of oil and water on the surface of the silicon substrate;
3)将硅基底与合金靶材分别置入磁控溅射炉内的基片台与溅射靶台,调整溅射角度为30~45°后固定,以保证溅射原子可击中硅片正中央,依次启动机械泵和分子泵,将溅射炉内抽真空至4×10-5Pa,准备镀膜;3) Put the silicon substrate and the alloy target into the substrate stage and the sputtering target stage in the magnetron sputtering furnace respectively, adjust the sputtering angle to 30-45° and then fix it to ensure that the sputtered atoms can hit the silicon wafer In the center, start the mechanical pump and the molecular pump in turn, and vacuum the sputtering furnace to 4×10 -5 Pa to prepare for coating;
4)通入高纯Ar气,保证炉内气压在0.2Pa,以保证正常的辉光放电和良好的镀膜质量,将靶台接入设备电源,设置溅射功率为100W,偏置电压为-80V,启动电源并开始预溅射10min;4) Introduce high-purity Ar gas to ensure that the pressure in the furnace is 0.2Pa to ensure normal glow discharge and good coating quality. Connect the target platform to the power supply of the equipment, set the sputtering power to 100W, and the bias voltage to - 80V, start the power supply and start pre-sputtering for 10 minutes;
5)打开靶材挡板和基片台旋转,开始溅射,溅射4h后,依次关闭靶材挡板、电源、偏置电压,保持通入Ar气,使薄膜成品与硅基底在Ar气氛中冷却1.5h,避免薄膜表面应力过大导致碎裂,随后停止通气,退真空后即可取出,得到一块在硅基底上沉积的超硬耐磨难熔高熵合金薄膜。5) Turn on the target baffle and the substrate table to rotate, and start sputtering. After 4 hours of sputtering, turn off the target baffle, power supply, and bias voltage in sequence, and keep feeding Ar gas, so that the finished film and the silicon substrate are in the Ar atmosphere. Cool in medium for 1.5 hours to avoid cracking due to excessive surface stress of the film, then stop the ventilation, and take it out after the vacuum is turned off to obtain a superhard wear-resistant refractory high-entropy alloy film deposited on a silicon substrate.
实施例2:Example 2:
一种超硬耐磨难熔高熵合金薄膜的制备方法,包括以下步骤:A method for preparing a superhard wear-resistant refractory high-entropy alloy film, comprising the following steps:
1)将各单质元素Nb、Mo、W、Ta金属粉末按照等摩尔比例使用高能球磨法混合24h,随后在1700℃下采用等离子体烧结技术制备出具有等摩尔比的NbMoWTa难熔高熵合金靶材;1) The metal powders of elemental elements Nb, Mo, W, and Ta were mixed in equimolar proportions using high-energy ball milling for 24 hours, and then NbMoWTa refractory high-entropy alloy targets with equimolar ratios were prepared by plasma sintering technology at 1700°C material;
2)将硅基底依次在丙酮、无水乙醇中超声清洗20min,随后使用电吹风将其烘干,以保证去除硅基底表面的油污及水分;2) The silicon substrate was ultrasonically cleaned in acetone and absolute ethanol for 20 minutes, and then dried with a hair dryer to ensure the removal of oil and water on the surface of the silicon substrate;
3)将硅基底与合金靶材分别置入磁控溅射炉内的基片台与溅射靶台,调整溅射角度为30~45°后固定,以保证溅射原子可击中硅片正中央,依次启动机械泵和分子泵,将溅射炉内抽真空至4×10-5Pa,准备镀膜;3) Put the silicon substrate and the alloy target into the substrate stage and the sputtering target stage in the magnetron sputtering furnace respectively, adjust the sputtering angle to 30-45° and then fix it to ensure that the sputtered atoms can hit the silicon wafer In the center, start the mechanical pump and the molecular pump in turn, and vacuum the sputtering furnace to 4×10 -5 Pa to prepare for coating;
4)通入高纯Ar气,保证炉内气压在0.3Pa,以保证正常的辉光放电和良好的镀膜质量,将靶台接入设备电源,设置溅射功率为110W,偏置电压为-90V,启动电源并开始预溅射10min;4) Introduce high-purity Ar gas to ensure that the pressure in the furnace is 0.3Pa to ensure normal glow discharge and good coating quality. Connect the target platform to the power supply of the equipment, set the sputtering power to 110W, and the bias voltage to - 90V, start the power supply and start pre-sputtering for 10 minutes;
5)打开靶材挡板和基片台旋转,开始溅射,溅射4h后,依次关闭靶材挡板、电源、偏置电压,保持通入Ar气,使薄膜成品与硅基底在Ar气氛中冷却1.5h,避免薄膜表面应力过大导致碎裂,随后停止通气,退真空后即可取出,得到一块在硅基底上沉积的超硬耐磨难熔高熵合金薄膜。5) Turn on the target baffle and the substrate table to rotate, and start sputtering. After 4 hours of sputtering, turn off the target baffle, power supply, and bias voltage in sequence, and keep feeding Ar gas, so that the finished film and the silicon substrate are in the Ar atmosphere. Cool in medium for 1.5 hours to avoid cracking due to excessive surface stress of the film, then stop the ventilation, and take it out after the vacuum is turned off to obtain a superhard wear-resistant refractory high-entropy alloy film deposited on a silicon substrate.
实施例3:Example 3:
一种超硬耐磨难熔高熵合金薄膜的制备方法,包括以下步骤:A method for preparing a superhard wear-resistant refractory high-entropy alloy film, comprising the following steps:
1)将各单质元素Nb、Mo、W、Ta金属粉末按照等摩尔比例使用高能球磨法混合24h,随后在1700℃下采用等离子体烧结技术制备出具有等摩尔比的NbMoWTa难熔高熵合金靶材;1) The metal powders of elemental elements Nb, Mo, W, and Ta were mixed in equimolar proportions using high-energy ball milling for 24 hours, and then NbMoWTa refractory high-entropy alloy targets with equimolar ratios were prepared by plasma sintering technology at 1700°C material;
2)将硅基底依次在丙酮、无水乙醇中超声清洗20min,随后使用电吹风将其烘干,以保证去除硅基底表面的油污及水分;2) The silicon substrate was ultrasonically cleaned in acetone and absolute ethanol for 20 minutes, and then dried with a hair dryer to ensure the removal of oil and water on the surface of the silicon substrate;
3)将硅基底与合金靶材分别置入磁控溅射炉内的基片台与溅射靶台,调整溅射角度为30~45°后固定,以保证溅射原子可击中硅片正中央,依次启动机械泵和分子泵,将溅射炉内抽真空至4×10-5Pa,准备镀膜;3) Put the silicon substrate and the alloy target into the substrate stage and the sputtering target stage in the magnetron sputtering furnace respectively, adjust the sputtering angle to 30-45° and then fix it to ensure that the sputtered atoms can hit the silicon wafer In the center, start the mechanical pump and the molecular pump in turn, and vacuum the sputtering furnace to 4×10 -5 Pa to prepare for coating;
4)通入高纯Ar气,保证炉内气压在0.2Pa,以保证正常的辉光放电和良好的镀膜质量,将靶台接入设备电源,设置溅射功率为120W,偏置电压为-100V,启动电源并开始预溅射10min;4) Introduce high-purity Ar gas to ensure that the pressure in the furnace is 0.2Pa to ensure normal glow discharge and good coating quality. Connect the target platform to the equipment power supply, set the sputtering power to 120W, and the bias voltage to - 100V, start the power supply and start pre-sputtering for 10 minutes;
5)打开靶材挡板和基片台旋转,开始溅射,溅射4h后,依次关闭靶材挡板、电源、偏置电压,保持通入Ar气,使薄膜成品与硅基底在Ar气氛中冷却1.5h,避免薄膜表面应力过大导致碎裂,随后停止通气,退真空后即可取出,得到一块在硅基底上沉积的超硬耐磨难熔高熵合金薄膜。5) Turn on the target baffle and the substrate table to rotate, and start sputtering. After 4 hours of sputtering, turn off the target baffle, power supply, and bias voltage in sequence, and keep feeding Ar gas, so that the finished film and the silicon substrate are in the Ar atmosphere. Cool in medium for 1.5 hours to avoid cracking due to excessive surface stress of the film, then stop the ventilation, and take it out after the vacuum is turned off to obtain a superhard wear-resistant refractory high-entropy alloy film deposited on a silicon substrate.
由于实施例1-3制备得到的超硬耐磨难熔高熵合金薄膜的性能基本相同,故以下仅以实施例1制备得到的超硬耐磨难熔高熵合金薄膜为例进行效果说明。Since the performances of the superhard wear-resistant refractory high-entropy alloy thin films prepared in Examples 1-3 are basically the same, the effects of the superhard wear-resistant refractory high-entropy alloy thin films prepared in Example 1 are taken as an example below.
图1是通过本发明制备的NbMoWTa难熔高熵合金薄膜的XRD图谱,可以看出该薄膜表现出单一的体心立方固溶体结构,且具有(110)晶面的择优取向,衍射峰强度较弱归结于其内部细小的晶粒。Fig. 1 is the XRD spectrum of the NbMoWTa refractory high-entropy alloy thin film prepared by the present invention, it can be seen that the thin film shows a single body-centered cubic solid solution structure, and has a preferred orientation of (110) crystal plane, and the diffraction peak intensity is relatively weak It is due to the fine grains inside it.
图2是通过本发明制备的NbMoWTa难熔高熵合金薄膜的截面扫描电子显微镜和透射电子显微镜图像,可以看出该晶粒垂直于硅基底呈柱状生长;通过放大倍数更高的透射电子显微镜可以看出,其晶粒尺寸极小,平均尺寸不超过25nm。Fig. 2 is the cross-sectional scanning electron microscope and the transmission electron microscope image of the NbMoWTa refractory high-entropy alloy thin film prepared by the present invention, it can be seen that the crystal grains grow in a columnar shape perpendicular to the silicon substrate; through a higher magnification transmission electron microscope can It can be seen that the crystal grain size is extremely small, and the average size does not exceed 25 nm.
图3是通过本发明制备的NbMoWTa难熔高熵合金的亚结构元素分布图像,可以看出其中W、Ta元素分布并不均匀,其表现出周期性为5~10nm的调幅分解亚结构。超细纳米晶与合金元素的调幅分解为薄膜优异的机械与耐磨性能提供结构基础。Fig. 3 is the substructure element distribution image of the NbMoWTa refractory high-entropy alloy prepared by the present invention. It can be seen that the distribution of W and Ta elements is not uniform, and it shows an amplitude-modulated decomposition substructure with a periodicity of 5-10 nm. The amplitude-modulated decomposition of ultrafine nanocrystals and alloying elements provides the structural basis for the excellent mechanical and wear resistance properties of the film.
图4是通过本发明制备的NbMoWTa难熔高熵合金薄膜与现阶段研究难熔金属单质、难熔高熵合金的硬度及耐磨性能的对比图,可以看出通过本发明制备的NbMoWTa难熔高熵合金薄膜的硬度超过20GPa,均优于目前文献1-4所报道的NbMoWTa系难熔高熵合金和难熔金属单质,表现出超硬特征;其耐磨性能均大幅优于TiZrHfNb系、TiZrHfNbTa系以及块体NbMoWTa系难熔高熵合金,磨损率水平位于1.0×10-5~1.4×10-5mm3/(N·m),表现出超耐磨特征。Figure 4 is a comparison chart of the hardness and wear resistance of the NbMoWTa refractory high-entropy alloy film prepared by the present invention and the current research on the refractory metal single substance and refractory high-entropy alloy. It can be seen that the NbMoWTa refractory prepared by the present invention The hardness of the high-entropy alloy film exceeds 20GPa, which is better than that of the NbMoWTa series refractory high-entropy alloy and refractory metal element reported in the current literature 1-4, showing superhard characteristics; its wear resistance is much better than that of TiZrHfNb series, TiZrHfNbTa series and bulk NbMoWTa series refractory high-entropy alloys have wear rates ranging from 1.0×10 -5 to 1.4×10 -5 mm 3 /(N·m), showing super wear resistance.
多主元的固溶强化、超细纳米晶强化效应、独特的调幅分解亚结构强化效应以及柱状晶边界强化的叠加效应导致薄膜获得超高的硬度;此外,较高的基底偏压会导致薄膜在成型过程中受到更多的离子轰击,使薄膜内应力增加,是导致薄膜高硬耐磨的原因之一。The multi-principal solid solution strengthening, ultrafine nanocrystal strengthening effect, unique amplitude modulation decomposition substructure strengthening effect, and the superimposed effect of columnar grain boundary strengthening lead to the ultra-high hardness of the film; in addition, a higher substrate bias will lead to the thin film During the forming process, more ion bombardment increases the internal stress of the film, which is one of the reasons for the high hardness and wear resistance of the film.
显然,本领域的技术人员可以对本发明进行各种改动和变型而不脱离本发明的精神和范围。这样,倘若本发明的这些修改和变型属于本发明权利要求及其等同技术的范围之内,则本发明也意图包含这些改动和变型在内。Obviously, those skilled in the art can make various changes and modifications to the present invention without departing from the spirit and scope of the present invention. Thus, if these modifications and variations of the present invention fall within the scope of the claims of the present invention and their equivalent technologies, the present invention also intends to include these modifications and variations.
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