CN115747742A - A preparation method of high-hardness high-entropy alloy film with grain size gradient - Google Patents
A preparation method of high-hardness high-entropy alloy film with grain size gradient Download PDFInfo
- Publication number
- CN115747742A CN115747742A CN202211518524.0A CN202211518524A CN115747742A CN 115747742 A CN115747742 A CN 115747742A CN 202211518524 A CN202211518524 A CN 202211518524A CN 115747742 A CN115747742 A CN 115747742A
- Authority
- CN
- China
- Prior art keywords
- grain size
- preparation
- power
- hardness
- sputtering
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Physical Vapour Deposition (AREA)
Abstract
Description
技术领域technical field
本发明属于合金材料领域,具体涉及到在一种具有晶粒尺寸梯度的高硬度高熵合金薄膜的制备方法。The invention belongs to the field of alloy materials, and in particular relates to a preparation method of a high-hardness high-entropy alloy thin film with a grain size gradient.
背景技术Background technique
2004年,高熵合金的概念一经提出,就吸引了众多学者的目光,其打破了传统合金的设计限制,舍弃了合金中溶剂-溶质的区分,具有多主元的结构特征。其中,具有稳定的FCC单相结构特征的CrMnFeCoNi系高熵合金因其优异的低温性能和高抗蠕变性能等优异的综合力学性能而被广泛研究,但是仍然不可避免的具有强塑性冲突,即高塑性但是低强度的特征。例如,CrMnFeCoNi延性在60-70%,并且断裂韧性超过200MPa/m,但是,其在室温下的强度需要进一步改善提高。In 2004, once the concept of high-entropy alloys was proposed, it attracted the attention of many scholars. It broke the design restrictions of traditional alloys, abandoned the distinction between solvent and solute in alloys, and has the structural characteristics of multiple principal elements. Among them, CrMnFeCoNi high-entropy alloys with stable FCC single-phase structure characteristics have been widely studied because of their excellent comprehensive mechanical properties such as excellent low-temperature performance and high creep resistance, but they still inevitably have strong plasticity conflicts, namely Characteristic of high plasticity but low strength. For example, the ductility of CrMnFeCoNi is 60-70%, and the fracture toughness exceeds 200MPa/m, but its strength at room temperature needs to be further improved.
对于FCC单相金属而言,想要提高其强度并且不损失其延性,甚至同步提高延性达到强度以及延性的协同效果,需要对其进行结构设计。合理的结构设计是打破FCC单相强塑性冲突的有效手段。其中,晶粒尺寸梯度被认为是一种有效的结构设计,合理的梯度结构设计可以兼顾强度和塑性。对于块体材料而言,可以采用多种表面机械处理,例如喷丸、高压扭转等,使表面结构纳米化,进而得到表面纳米晶过渡到内部粗晶晶粒尺寸梯度结构。纳米晶强度和粗晶塑性的良好结合,可以使FCC相结构材料强度提升,又不会过早失效。但是薄膜体系材料厚度一般为微米级,晶粒尺寸多为纳米级,结构硬且脆,很难通过机械处理进行结构梯度设计。所以针对薄膜体系的研究多为结构复合(多层膜)或是成分设计(元素添加),但是梯度结构设计仍存在困难。如何在高熵合金薄膜体系中实现可行的晶粒尺寸梯度结构设计并有效提高FCC单相合金的强度是具有挑战性的。For FCC single-phase metals, in order to increase its strength without losing its ductility, or even simultaneously improve the ductility to achieve the synergistic effect of strength and ductility, it is necessary to carry out structural design. Reasonable structural design is an effective means to break the single-phase strong-plastic conflict of FCC. Among them, the grain size gradient is considered to be an effective structure design, and a reasonable gradient structure design can take both strength and plasticity into account. For bulk materials, a variety of surface mechanical treatments, such as shot peening, high-pressure torsion, etc., can be used to make the surface structure nanoscale, and then obtain the transition from surface nanocrystals to internal coarse grain size gradient structure. The good combination of nanocrystalline strength and macrocrystalline plasticity can improve the strength of FCC phase structure materials without premature failure. However, the material thickness of the thin film system is generally micron-scale, the grain size is mostly nano-scale, and the structure is hard and brittle, so it is difficult to design structural gradients through mechanical processing. Therefore, the research on thin film systems is mostly structural composite (multilayer film) or composition design (element addition), but there are still difficulties in gradient structure design. How to achieve feasible grain size gradient structure design and effectively improve the strength of FCC single-phase alloys in high-entropy alloy thin film systems is challenging.
发明内容Contents of the invention
基于上述讨论,本发明旨在提出一种具有晶粒尺寸梯度的高硬度高熵合金薄膜的制备方法。Based on the above discussion, the present invention aims to propose a method for preparing a high-hardness high-entropy alloy film with a grain size gradient.
为达到上述目的,本发明采用如下技术方案:To achieve the above object, the present invention adopts the following technical solutions:
一种具有晶粒尺寸梯度的高硬度高熵合金薄膜的制备方法,采用磁控溅射共溅射得到薄膜并通过低温退火调控得到沿厚度方向晶粒尺寸连续变化的高熵合金薄膜。A method for preparing a high-hardness high-entropy alloy thin film with a grain size gradient. The thin film is obtained by magnetron sputtering and co-sputtering, and the high-entropy alloy thin film whose grain size continuously changes along the thickness direction is obtained through low-temperature annealing control.
本发明所采用的方法,具体包括如下步骤:The method adopted in the present invention specifically comprises the following steps:
1)将在酒精内超声清洗5-10min后的单面抛光单晶硅基片与底托对角固定好后水平插入(抛光面朝上)超高真空磁控溅射设备中;1) After ultrasonic cleaning in alcohol for 5-10 minutes, the single-sided polished single-crystal silicon substrate and the bottom bracket are fixed diagonally, and then inserted horizontally (polished side up) into the ultra-high vacuum magnetron sputtering equipment;
2)将需要溅射的合金靶材与纯金属靶材分别固定在射频和直流电源上;2) Fix the alloy target to be sputtered and the pure metal target on the RF and DC power sources respectively;
3)在利用机械泵和分子泵组合抽至所需的高真空条件后,通入高纯氩气作为主要离化气体进行辉光放电;3) After the combination of mechanical pump and molecular pump is used to pump to the required high vacuum condition, high-purity argon gas is introduced as the main ionized gas for glow discharge;
4)确认气体通入之后,调节两个电源控制器至所需功率后打开电源,开始预溅射20-30min去除靶材表面杂质;4) After confirming the gas flow, adjust the two power controllers to the required power, turn on the power, and start pre-sputtering for 20-30 minutes to remove impurities on the target surface;
5)预溅射结束后,利用控制杆翻转基片(抛光面朝下)开始正式共溅射,并打开360°旋转控制开关确保溅射均匀性;5) After the pre-sputtering is over, use the control lever to flip the substrate (polished side down) to start formal co-sputtering, and turn on the 360°rotation control switch to ensure sputtering uniformity;
6)将沉积得到的合金薄膜置于真空退火炉中,在395-405℃后时保温60min,然后关闭加热使样品冷却。6) Place the deposited alloy film in a vacuum annealing furnace, keep it at 395-405°C for 60 minutes, and then turn off the heating to cool the sample.
所述高真空是指真空度需要低至7x10-4Pa以下。The high vacuum means that the degree of vacuum needs to be as low as 7x10 -4 Pa or below.
所述高纯氩气的纯度≥99.999%。The purity of the high-purity argon gas is ≥99.999%.
所述溅射过程中,射频电源功率固定(>100W),而直流电源的功率从大到小变化(0-30W)。During the sputtering process, the power of the RF power supply is fixed (>100W), while the power of the DC power supply varies from large to small (0-30W).
进一步地,步骤6)退火过程中计时开始在温度显示器至400℃开始。冷却前期需要控制冷却速度为10℃/min,至200℃后开始随炉冷却。Further, during step 6) during the annealing process, the timing starts when the temperature display reaches 400°C. In the early stage of cooling, it is necessary to control the cooling rate to 10°C/min, and start cooling with the furnace after reaching 200°C.
本发明具有以下优点:The present invention has the following advantages:
1.利用此种方法得到沿高熵合金薄膜厚度方向纳米晶晶粒尺寸梯度变化的样品。1. Using this method to obtain samples with gradient changes in the size of nanocrystalline grains along the thickness direction of the high-entropy alloy film.
2.晶粒尺寸梯度变化的结构设计使具有FCC单相结构的CrMnFeCoNi系高熵合金硬度达到13.52GPa。2. The structural design of the gradient change in grain size makes the hardness of CrMnFeCoNi high-entropy alloy with FCC single-phase structure reach 13.52GPa.
附图说明Description of drawings
图1是薄膜的截面TEM结构图;Figure 1 is a cross-sectional TEM structure diagram of the film;
(a)TEM样品整体截面图(薄区)。(a) The overall cross-sectional view (thin area) of the TEM sample.
(b)图(a)中“1”处高分辨微观结构图(b) High-resolution microstructure at "1" in Figure (a)
(c)图(a)中“2”处高分辨微观结构图(c) High-resolution microstructure at "2" in Figure (a)
(d)图(a)中“3”处高分辨微观结构图(d) High-resolution microstructure at "3" in Figure (a)
图2是高熵合金薄膜TEM选区衍射图及标定结果。Figure 2 is the TEM selected area diffraction pattern and calibration results of the high-entropy alloy thin film.
图3是CrMnFeCoNi系FCC相纳米晶硬度对比图。Fig. 3 is a comparative diagram of hardness of CrMnFeCoNi-based FCC phase nanocrystals.
具体实施方式Detailed ways
下面将结合具体实例以及附图来详细说明本发明,但并不作为对本发明的限定。The present invention will be described in detail below in conjunction with specific examples and accompanying drawings, but it is not intended to limit the present invention.
参照图1所示,图(a)显示了高熵合金薄膜TEM制样后薄区整体截面图,显示了薄膜的厚度约1.8微米,图(b-d)显示了不同区域的微观结构放大图,虚线显示了晶粒大小的变化,即从大于30nm到约5nm的晶粒尺寸过渡。“1”处是近表面处。Referring to Figure 1, Figure (a) shows the overall cross-sectional view of the thin area after TEM sample preparation of the high-entropy alloy thin film, showing that the thickness of the film is about 1.8 microns, and Figures (b-d) show enlarged views of the microstructure of different areas, dotted lines A change in grain size is shown, ie a grain size transition from greater than 30 nm to about 5 nm. "1" is near the surface.
参照图2所示,衍射图中显示薄膜相结构仍标定显示为FCC单相纳米多晶。Referring to Figure 2, the thin film phase structure shown in the diffraction pattern is still labeled as FCC single-phase nano-polycrystalline.
参照图3所示,当将薄膜硬度与其他CrMnFeCoNi系的FCC单相纳米晶硬度进行对比,此薄膜硬度具有明显的优势。Referring to Figure 3, when the hardness of the film is compared with that of other CrMnFeCoNi-based FCC single-phase nanocrystals, the hardness of this film has obvious advantages.
实施例1Example 1
采用磁控共溅射的方式制备成分为CrMnFeCoNi的5元非等原子比高熵合金薄膜。近等原子比的CrMnFeCoNi高熵合金靶材和纯锰金属靶材进行共溅射,分别放置在射频电源以及直流电源上,其中射频电源功率稳定在120W,直流电源从30W均匀变化至0W,溅射总时长为4个小时。然后在真空退火炉中400℃退火60min,保温结束后,控制冷却速度为10℃/min。A 5-element non-isoatomic ratio high-entropy alloy thin film composed of CrMnFeCoNi was prepared by magnetron co-sputtering. CrMnFeCoNi high-entropy alloy target and pure manganese metal target with near-equal atomic ratio were co-sputtered and placed on the RF power supply and DC power supply respectively. The total shooting time is 4 hours. Then anneal at 400°C for 60min in a vacuum annealing furnace, and control the cooling rate to 10°C/min after the heat preservation is over.
所得高熵合金薄膜TEM表征结果如图1所示,结果表明薄膜的结构出现了纳米晶晶粒尺寸梯度,表面晶粒尺寸大于30nm,随着厚度增加,晶粒尺寸一直过渡到内部的约5nm。相结构仍然保持为FCC单相(如图2所示)。相对比于其他高熵合金薄膜,本发明制备的薄膜具有突出的高硬度(13.52GPa),相较于其他单一尺寸的FCC单相纳米晶薄膜硬度突出。The TEM characterization results of the obtained high-entropy alloy thin film are shown in Figure 1. The results show that the structure of the thin film has a nanocrystalline grain size gradient, and the grain size on the surface is greater than 30nm. As the thickness increases, the grain size transitions to about 5nm in the interior. . The phase structure remains as FCC single phase (as shown in Figure 2). Compared with other high-entropy alloy films, the film prepared by the present invention has outstanding high hardness (13.52GPa), and compared with other single-size FCC single-phase nanocrystalline films, the hardness is outstanding.
实施例2Example 2
通过磁控溅射,同时控制射频电源和直流电源对近等原子比的CrMnFeCoNi高熵合金靶材和纯锰金属靶材进行溅射,其中射频电源功率仍稳定在120W,直流电源的功率从4W变化到30W,溅射总时长为4个小时。然后在真空退火炉中400℃退火60min,保温结束后,控制冷却速度为10℃/min。Through magnetron sputtering, control the RF power supply and DC power supply at the same time to sputter CrMnFeCoNi high-entropy alloy targets and pure manganese metal targets with nearly equiatomic ratio. The power of RF power supply is still stable at 120W, and the power of DC power supply is from 4W Change to 30W for a total sputtering time of 4 hours. Then anneal at 400°C for 60min in a vacuum annealing furnace, and control the cooling rate to 10°C/min after the heat preservation is over.
所得高熵合金薄膜在经过纳米压入硬度表征后显示为13.37GPa。但是结构中没有显示出晶粒尺寸的变化,呈现出了晶体/非晶相的复合结构。The resulting high-entropy alloy film was characterized by nano-indentation hardness of 13.37GPa. However, there is no change in grain size in the structure, showing a composite structure of crystalline/amorphous phases.
实施例3Example 3
通过磁控溅射,同时控制射频电源和直流电源对近等原子比的CrMnFeCoNi高熵合金靶材和纯锰金属靶材进行溅射,其中射频电源功率稳定在120W,直流电源的功率控制在10W,溅射总时长为4个小时。然后在真空退火炉中400℃退火60min,保温结束后,控制冷却速度为10℃/min。Through magnetron sputtering, the RF power supply and the DC power supply are simultaneously controlled to sputter CrMnFeCoNi high-entropy alloy targets and pure manganese metal targets with near equiatomic ratios. The power of the RF power supply is stable at 120W, and the power of the DC power supply is controlled at 10W. , the total sputtering time is 4 hours. Then anneal at 400°C for 60min in a vacuum annealing furnace, and control the cooling rate to 10°C/min after the heat preservation is over.
所得高熵合金薄膜在经过纳米压入硬度表征后显示为8.008GPa。但是结构中没有显示出晶粒尺寸的变化,呈现出了晶体/非晶相的复合结构。The resulting high-entropy alloy film was characterized by nano-indentation hardness of 8.008GPa. However, there is no change in grain size in the structure, showing a composite structure of crystalline/amorphous phases.
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211518524.0A CN115747742B (en) | 2022-11-29 | 2022-11-29 | A method for preparing a high-hardness high-entropy alloy film with a grain size gradient |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211518524.0A CN115747742B (en) | 2022-11-29 | 2022-11-29 | A method for preparing a high-hardness high-entropy alloy film with a grain size gradient |
Publications (2)
Publication Number | Publication Date |
---|---|
CN115747742A true CN115747742A (en) | 2023-03-07 |
CN115747742B CN115747742B (en) | 2025-06-03 |
Family
ID=85340981
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202211518524.0A Active CN115747742B (en) | 2022-11-29 | 2022-11-29 | A method for preparing a high-hardness high-entropy alloy film with a grain size gradient |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115747742B (en) |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02192403A (en) * | 1989-01-19 | 1990-07-30 | Fujitsu Ltd | Method for manufacturing superconducting thin film |
CN105132874A (en) * | 2015-08-31 | 2015-12-09 | 辽宁工业大学 | Method for preparing high-concentration gradient AZO monocrystalline conductive thin film by direct current/radio frequency co-sputtering process |
CN107641790A (en) * | 2017-09-18 | 2018-01-30 | 南京大学 | A kind of preparation method for having high intensity and high ductility metal film concurrently |
CN107779834A (en) * | 2017-11-08 | 2018-03-09 | 重庆交通大学 | A kind of method that rf magnetron sputtering prepares nanometer aluminium film |
CN108359953A (en) * | 2018-04-16 | 2018-08-03 | 山东建筑大学 | A kind of Cu-Ni gradient films material and preparation method thereof |
CN110029320A (en) * | 2019-05-14 | 2019-07-19 | 天津师范大学 | Magnetron sputtering method prepares titanium diboride/zirconium dioxide gradient nano structural membrane and its application |
CN113737135A (en) * | 2021-08-27 | 2021-12-03 | 西安交通大学 | High-entropy alloy film capable of quantitatively controlling element content gradient change and preparation method thereof |
CN114150203A (en) * | 2021-11-10 | 2022-03-08 | 青岛理工大学 | Laser cladding in-situ self-generated high-entropy alloy gradient coating and preparation method thereof |
CN115074685A (en) * | 2022-06-27 | 2022-09-20 | 商丘市鸿大光电有限公司 | Preparation process of high-temperature-resistant TaVNb/TaVNbHfZr composite gradient barrier layer for purifying hydrogen catalyzed by tantalum/palladium |
-
2022
- 2022-11-29 CN CN202211518524.0A patent/CN115747742B/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02192403A (en) * | 1989-01-19 | 1990-07-30 | Fujitsu Ltd | Method for manufacturing superconducting thin film |
CN105132874A (en) * | 2015-08-31 | 2015-12-09 | 辽宁工业大学 | Method for preparing high-concentration gradient AZO monocrystalline conductive thin film by direct current/radio frequency co-sputtering process |
CN107641790A (en) * | 2017-09-18 | 2018-01-30 | 南京大学 | A kind of preparation method for having high intensity and high ductility metal film concurrently |
CN107779834A (en) * | 2017-11-08 | 2018-03-09 | 重庆交通大学 | A kind of method that rf magnetron sputtering prepares nanometer aluminium film |
CN108359953A (en) * | 2018-04-16 | 2018-08-03 | 山东建筑大学 | A kind of Cu-Ni gradient films material and preparation method thereof |
CN110029320A (en) * | 2019-05-14 | 2019-07-19 | 天津师范大学 | Magnetron sputtering method prepares titanium diboride/zirconium dioxide gradient nano structural membrane and its application |
CN113737135A (en) * | 2021-08-27 | 2021-12-03 | 西安交通大学 | High-entropy alloy film capable of quantitatively controlling element content gradient change and preparation method thereof |
CN114150203A (en) * | 2021-11-10 | 2022-03-08 | 青岛理工大学 | Laser cladding in-situ self-generated high-entropy alloy gradient coating and preparation method thereof |
CN115074685A (en) * | 2022-06-27 | 2022-09-20 | 商丘市鸿大光电有限公司 | Preparation process of high-temperature-resistant TaVNb/TaVNbHfZr composite gradient barrier layer for purifying hydrogen catalyzed by tantalum/palladium |
Also Published As
Publication number | Publication date |
---|---|
CN115747742B (en) | 2025-06-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN113789503B (en) | An In Situ Synthesis of High-Entropy Silicide Thin Films with Antioxidant Properties | |
CN113151795A (en) | NbMoTaWAl refractory high-entropy alloy film and preparation method thereof | |
TW200532035A (en) | Co-Cr-Pt-B based alloy sputtering target | |
JP2024530077A (en) | Molybdenum alloy target material, its preparation method and application | |
JP2025507240A (en) | Method for preparing molybdenum alloy tube target material, molybdenum alloy tube target material and its use | |
CN114921757A (en) | A kind of amorphous high-entropy alloy thick film preparation equipment and preparation method | |
CN114672778A (en) | Nanocrystalline NbMoTaWTi refractory high-entropy alloy coating and preparation method thereof | |
CN108588646B (en) | Method for preparing amorphous/amorphous nano multilayer film with improved plasticity | |
CN110129732B (en) | High-resistivity high-entropy alloy film and preparation method thereof | |
TW201821627A (en) | Aluminum alloy sputtering target | |
EP2002027B1 (en) | Ternary aluminum alloy films and targets | |
CN101696481A (en) | Ultrahigh recovery stress Ti-Ni-Cu shape memory alloy thin film and preparation method thereof | |
CN104630727B (en) | Method for controlling phase structures of metallic nano Cu/Ru multilayer film | |
CN109988998A (en) | A kind of preparation method of multi-element high-entropy alloy thin film | |
CN115747742A (en) | A preparation method of high-hardness high-entropy alloy film with grain size gradient | |
CN113802100A (en) | Method for regulating and controlling processing hardening capacity of amorphous/amorphous nano multilayer film | |
CN110512181B (en) | A kind of nanocrystalline Al-Zr alloy film and preparation method thereof | |
CN103266304B (en) | A kind of preparation method of Cu(Ru) alloy material without diffusion barrier layer with high thermal stability | |
CN103898456B (en) | NbVN hard nanometer film and preparation method | |
CN109023278B (en) | Method for preparing high-strength copper-aluminum alloy | |
WO2007141988A1 (en) | HIGH-POWER Ti-Ni-Cu SHAPE MEMORY ALLOY AND PROCESS FOR PRODUCING THE SAME | |
CN116180025A (en) | TaCo binary amorphous alloy film and preparation method thereof | |
JP2004520492A (en) | Physical vapor deposition target containing Ti and Zr and method of use | |
CN117467939B (en) | Ag-Cu-Al alloy film and preparation method thereof | |
CN116240474B (en) | A method for preparing high-purity copper target material |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |