CN110629059A - A kind of heterogeneous high entropy alloy material and preparation method thereof - Google Patents
A kind of heterogeneous high entropy alloy material and preparation method thereof Download PDFInfo
- Publication number
- CN110629059A CN110629059A CN201810657004.5A CN201810657004A CN110629059A CN 110629059 A CN110629059 A CN 110629059A CN 201810657004 A CN201810657004 A CN 201810657004A CN 110629059 A CN110629059 A CN 110629059A
- Authority
- CN
- China
- Prior art keywords
- entropy alloy
- heterogeneous
- alloy material
- chips
- preparation
- 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
- 239000000956 alloy Substances 0.000 title claims abstract description 64
- 238000002360 preparation method Methods 0.000 title claims abstract description 17
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 50
- 238000000034 method Methods 0.000 claims abstract description 19
- 238000000137 annealing Methods 0.000 claims abstract description 16
- 238000002156 mixing Methods 0.000 claims abstract description 15
- 238000010438 heat treatment Methods 0.000 claims abstract description 11
- 238000005056 compaction Methods 0.000 claims abstract description 6
- 230000000694 effects Effects 0.000 claims abstract description 6
- 238000005728 strengthening Methods 0.000 claims abstract description 4
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 28
- 229910052786 argon Inorganic materials 0.000 claims description 14
- 238000003801 milling Methods 0.000 claims description 14
- 238000005096 rolling process Methods 0.000 claims description 13
- 238000003825 pressing Methods 0.000 claims description 11
- 239000012298 atmosphere Substances 0.000 claims description 7
- 238000001125 extrusion Methods 0.000 claims description 7
- 239000011261 inert gas Substances 0.000 claims description 5
- 238000003756 stirring Methods 0.000 claims description 5
- 230000007547 defect Effects 0.000 claims description 2
- 239000007789 gas Substances 0.000 claims description 2
- 239000013078 crystal Substances 0.000 abstract description 2
- 238000005551 mechanical alloying Methods 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 13
- 239000011805 ball Substances 0.000 description 6
- 239000002131 composite material Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 229910000733 Li alloy Inorganic materials 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 239000001989 lithium alloy Substances 0.000 description 4
- GCICAPWZNUIIDV-UHFFFAOYSA-N lithium magnesium Chemical compound [Li].[Mg] GCICAPWZNUIIDV-UHFFFAOYSA-N 0.000 description 4
- 239000007769 metal material Substances 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000012300 argon atmosphere Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000011806 microball Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 239000002440 industrial waste Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 241000446313 Lamella Species 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000013590 bulk material Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000013332 literature search Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002905 metal composite material Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/02—Changing 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
本发明公开了一种异构高熵合金材料及其制备方法,包含:制屑、混屑和预压实、塑性变形处理、退火处理四步工序,选择两种或两种以上具有不同晶粒细化效果的单相和双相结构高熵合金,充分混合它们的碎屑后进行塑性变形,通过高温、高应变使碎屑完全机械合金化,获得致密、多成分混合的异构高熵合金块体坯料。通过后续的退火热处理,形成多尺度晶粒混合的异质结构。本发明软硬结合的异质结构在变形过程中会形成显著的背应力强化,从而制备得高强韧性的异构高熵合金。
The invention discloses a heterogeneous high-entropy alloy material and a preparation method thereof, comprising four steps of chip making, chip mixing and pre-compaction, plastic deformation treatment, and annealing treatment, and selecting two or more types with different crystal grains Single-phase and dual-phase structure high-entropy alloys with refinement effect, plastic deformation after fully mixing their debris, and complete mechanical alloying of debris through high temperature and high strain, to obtain dense, multi-component mixed heterogeneous high-entropy alloys block blanks. After subsequent annealing heat treatment, a heterogeneous structure with mixed multi-scale grains is formed. The soft-hard combined heterogeneous structure of the present invention can form significant back stress strengthening during the deformation process, thereby preparing a heterogeneous high-entropy alloy with high strength and toughness.
Description
技术领域technical field
本发明涉及的是一种异构高熵合金材料及其制备方法,属于金属材料制备领域。The invention relates to a heterogeneous high-entropy alloy material and a preparation method thereof, belonging to the field of metal material preparation.
背景技术Background technique
高熵合金是由五种或五种以上的元素以等原子比或者近似等原子比的方式混合在一起的新型金属材料,其中每种元素的原子含量百分比在5%~35%之间。通过合理优化元素种类及配比,高熵合金可以形成单一的体心立方、面心立方、两相混合等固溶体结构,从而表现出一些优异的性能,例如良好的耐腐蚀性、抗辐照性、热稳定性,以及较高的强度、硬度和耐磨性。但是和传统金属材料一样,高熵合金的强度和韧性这对矛盾体依旧存在,其特点是质地硬而脆、或者软而韧。如何同时提高高熵合金的强度和韧性,制备高强韧性的材料,是目前金属材料领域的研究热点。A high-entropy alloy is a new type of metal material that is mixed with five or more elements in an equiatomic or approximately equiatomic ratio, where the atomic content of each element is between 5% and 35%. By rationally optimizing the types and proportions of elements, high-entropy alloys can form solid solution structures such as body-centered cubic, face-centered cubic, and two-phase mixtures, thereby exhibiting some excellent properties, such as good corrosion resistance and radiation resistance. , thermal stability, and high strength, hardness and wear resistance. However, like traditional metal materials, the contradiction between strength and toughness of high-entropy alloys still exists, and its characteristics are hard and brittle, or soft and tough. How to simultaneously improve the strength and toughness of high-entropy alloys and prepare high-strength and tough materials is currently a research hotspot in the field of metal materials.
经对现有技术的文献检索发现,X.L.Wu等人在《Proceedings of the NationalAcademy of Science of the United States of America》美国科学院院报,2015,112(47):14501-14505上发表的“Heterogeneous lamella structure unites ultrafine-grain strength with coarse-grain ductility”(高强高韧粗细晶混合层片状结构材料)一文中,通过轧制变形技术和热处理工艺,制备出强度接近1GPa,均匀延伸率10%左右的高强高韧纯钛板材。这种纯钛材料具有硬的超细晶与软的粗晶混合层片状结构,通过软硬相异质结构变形协调诱发的背应力强化,能够在一定程度上兼得超细晶的高强度和粗晶的高韧性,从而大幅提升纯钛的力学性能。但是,该技术制备的混晶纯钛材料组元较为单一,而且热稳定性较差。Through literature search to prior art, X.L.Wu et al published "Heterogeneous lamella" in "Proceedings of the National Academy of Science of the United States of America" Proceedings of the American Academy of Sciences, 2015, 112 (47): 14501-14505 In the article "structure units ultrafine-grain strength with coarse-grain ductility" (high-strength, high-toughness coarse-fine-grain mixed layer sheet structure material), through rolling deformation technology and heat treatment process, the strength is close to 1GPa, and the uniform elongation is about 10%. High-strength and high-toughness pure titanium plate. This pure titanium material has a hard ultra-fine grain and soft coarse-grain mixed layer lamellar structure, and the back stress strengthening induced by the coordination of deformation of the soft-hard phase heterogeneous structure can achieve both the high strength of the ultra-fine grain to a certain extent. And the high toughness of coarse grains, thus greatly improving the mechanical properties of pure titanium. However, the mixed crystal pure titanium material prepared by this technology has relatively single components and poor thermal stability.
压力加工复合法是制备高强韧金属复合材料的另一种有效方法,进一步检索发现,中国发明专利CN106064504A介绍了一种高强韧性镁锂合金层状复合材料的制备方法,其原理是通过累积叠轧和退火处理工艺,将强度较高的α-Mg单相镁锂合金板材和塑韧性良好的β-Li单相镁锂合金板材结合在一起,从而制备出α/β交替的镁锂合金层状复合材料,复合板材兼具高强度和良好塑性。同时,利用α-Mg相和β-Li相之间的塑性变形能力差异实现“搓轧区”的形成,复合板材的界面结合效果良好。但是,这种方法的局限性在于复合板材制备的过程较为繁琐,用于轧制的板材需要进行多次裁剪、打磨、固定、加热,生产效率较低。The pressure processing composite method is another effective method for preparing high-strength and tough metal composite materials. Further search found that Chinese invention patent CN106064504A introduced a preparation method of high-strength and toughness magnesium-lithium alloy layered composite materials. and annealing process, the α-Mg single-phase magnesium-lithium alloy sheet with high strength and the β-Li single-phase magnesium-lithium alloy sheet with good plasticity and toughness are combined to prepare an α/β alternating magnesium-lithium alloy layer Composite materials, composite panels have both high strength and good plasticity. At the same time, the difference in plastic deformation ability between the α-Mg phase and the β-Li phase is used to realize the formation of the "rolling zone", and the interface bonding effect of the composite plate is good. However, the limitation of this method is that the preparation process of the composite sheet is relatively cumbersome, and the sheet for rolling needs to be cut, polished, fixed, and heated multiple times, and the production efficiency is low.
发明内容Contents of the invention
本发明目的在于针对现有技术存在的上述不足,提供一种异构高熵合金材料及其制备方法。The object of the present invention is to provide a heterogeneous high-entropy alloy material and a preparation method thereof in view of the above-mentioned deficiencies in the prior art.
本发明是通过以下技术方案来实现的,包括以下步骤:The present invention is achieved through the following technical solutions, comprising the following steps:
第一步,制屑:根据高熵合金的力学性能差异,在FCC(面心立方)单相结构和FCC+BCC(面心立方+体心立方)双相结构的高熵合金中至少各选择一种;满足高熵合金在后续变形及热处理过程中分别具有不同的晶粒细化效果。The first step, shavings: According to the difference in mechanical properties of high-entropy alloys, at least each of the high-entropy alloys with FCC (face-centered cubic) single-phase structure and FCC+BCC (face-centered cubic + body-centered cubic) dual-phase structure is selected. One: the high-entropy alloy has different grain refinement effects in subsequent deformation and heat treatment processes.
对高熵合金铸锭进行碎屑铣制,切屑的进给量控制在0.01至0.5mm之间;对铣制后的粗屑进行精细破碎,从而进一步减小碎屑大小,使碎屑尺寸更加均匀。Chip milling is carried out on high-entropy alloy ingots, and the feed rate of chips is controlled between 0.01 and 0.5mm; the coarse chips after milling are finely broken, so as to further reduce the size of chips and make the size of chips more accurate. uniform.
进一步的,采用微型立式铣床进行碎屑铣制,然后采用微型破碎机进行精细破碎。Further, a micro vertical milling machine is used for chip milling, and then a micro crusher is used for fine crushing.
为了避免高熵合金碎屑氧化引起材料界面结合性差等问题,因此在隔氧的惰性气体(氩气)氛围中,在惰性气体(氩气)保护箱内,进行高熵合金制屑工艺。In order to avoid problems such as poor material interface bonding caused by the oxidation of high-entropy alloy debris, the high-entropy alloy chip-making process is carried out in an oxygen-insulated inert gas (argon) atmosphere and in an inert gas (argon) protective box.
第二步,混屑和预压实:在隔氧的惰性气体(氩气)氛围中,通过球磨机对异种高熵合金切屑进行充分的搅拌混合;混屑时间控制在0.5至2小时之间,球磨机振动搅拌的频率设置为10-300赫兹;混屑工艺完成后,将混合细屑的装入模具并置于压力机上,压制成初始的混合细屑预制块。The second step, chip mixing and pre-compacting: in an oxygen-barrier inert gas (argon) atmosphere, the dissimilar high-entropy alloy chips are fully stirred and mixed by a ball mill; the chip mixing time is controlled between 0.5 and 2 hours, The frequency of vibration and agitation of the ball mill is set at 10-300 Hz; after the chip mixing process is completed, the mixed fine chips are put into a mold and placed on a press to be pressed into an initial mixed fine chip prefabricated block.
进一步的,压力机的工作压强为100-3000兆帕,压制温度为25-300℃,保压时间控制在10至60分钟之间,获得的预制块致密度在80%-98%之间。Further, the working pressure of the press is 100-3000 MPa, the pressing temperature is 25-300° C., the holding time is controlled between 10 and 60 minutes, and the density of the obtained prefabricated blocks is between 80% and 98%.
进一步的,预制块压制完成后,对样品进行真空封装,然后从氩气保护箱内取出备用。Further, after the prefabricated block is pressed, the sample is vacuum-packaged, and then taken out of the argon gas protection box for use.
进一步的,采用高能球磨机对异种高熵合金切屑进行充分的搅拌混合。Further, a high-energy ball mill is used to fully stir and mix the dissimilar high-entropy alloy chips.
第三步,塑性变形处理:变形处理分为常规挤压和室温轧制两步进行;首先在真空炉中对预压坯料进行预热处理,预热温度设置为400-600℃,预热时间控制在10至60分钟之间;然后对预压坯料进行挤压变形,挤压比为5:1至50:1;最后对挤压所得板材进行室温轧制,轧制变形量为50%-90%。The third step is plastic deformation treatment: the deformation treatment is divided into two steps: conventional extrusion and room temperature rolling; The control is between 10 and 60 minutes; then the pre-pressed billet is extruded and deformed, and the extrusion ratio is 5:1 to 50:1; finally, the extruded sheet is rolled at room temperature, and the rolling deformation is 50%- 90%.
第四步,退火处理:对轧制后的样品进行退火处理,退火温度设置为700-750℃,退火时间为60-90分钟。消除变形过程中产生的缺陷,同时在块体材料内形成不同细晶强化效果的软硬相异质结构。The fourth step, annealing treatment: perform annealing treatment on the rolled sample, the annealing temperature is set at 700-750° C., and the annealing time is 60-90 minutes. Eliminate the defects generated during the deformation process, and at the same time form a soft and hard phase heterogeneous structure with different fine-grain strengthening effects in the bulk material.
本发明相对于现有技术相比具有显著优点:Compared with the prior art, the present invention has significant advantages:
1.本发明专利采用双合金或者多合金碎屑混合机械合金化技术,具有极大的微观结构设计指向性和调控灵活性,可根据需求调整合金选择,制备出一系列软硬相结合的异构高熵合金,制备的合金在一定程度上兼得硬相的高强度和软相的高韧性,从而获得综合性能优异的高强韧性双系或多系异构高熵合金。1. The patent of the present invention adopts the double-alloy or multi-alloy debris mixed mechanical alloying technology, which has great microstructure design directionality and control flexibility. The alloy selection can be adjusted according to the demand, and a series of soft and hard alloys are prepared. High-entropy alloys are constructed, and the prepared alloys have both the high strength of the hard phase and the high toughness of the soft phase to a certain extent, so as to obtain high-strength and toughness dual-system or multi-system heterogeneous high-entropy alloys with excellent comprehensive properties.
2.本发明制备的软硬相结合的异构高熵合金具有良好的热稳定性,且混合多晶粒尺度的微观结构没有明显的方向性,适合在多向受力部件上应用。2. The heterogeneous high-entropy alloy with a combination of soft and hard prepared in the present invention has good thermal stability, and the mixed multi-grain-scale microstructure has no obvious directionality, and is suitable for application on multi-directional stress-bearing parts.
3.本发明可制备大尺寸的高熵合金板材,对设备、模具的要求较低。3. The present invention can prepare large-sized high-entropy alloy plates, and has relatively low requirements for equipment and molds.
4.本发明使用的原材料可选择工业废屑,制备工艺流程简便,成本低,回收率高,安全性高,节能环保。相比于传统工业废屑回收,本发明对废屑提纯和分类等常见难题具有更大的适应性。4. The raw material used in the present invention can be industrial waste, the preparation process is simple, the cost is low, the recovery rate is high, the safety is high, energy saving and environmental protection. Compared with traditional industrial waste recycling, the present invention has greater adaptability to common problems such as waste purification and classification.
附图说明Description of drawings
图1分别为本发明制屑、混屑和流程示意图。Fig. 1 is a schematic diagram of chip making, chip mixing and flow chart of the present invention, respectively.
图2为本发明预压实流程示意图。Fig. 2 is a schematic diagram of the pre-compaction process of the present invention.
图3为本发明塑性变形处理流程示意图.Fig. 3 is the schematic flow chart of plastic deformation processing of the present invention.
图4为本发明制备的材料微观结构示意图。Fig. 4 is a schematic diagram of the microstructure of the material prepared in the present invention.
图5为制备的异构高熵合金材料力学性能图。Figure 5 is a diagram of the mechanical properties of the prepared heterogeneous high-entropy alloy material.
具体实施方式Detailed ways
下面对通过实施例详细说明。The following is a detailed description of the examples.
实施例1Example 1
如图1-4所示,以下实施例包括四步工序,分别为:制屑、混屑和预压实、塑性变形处理、退火处理,其中:As shown in Figures 1-4, the following embodiments include a four-step process, namely: chip making, chip mixing and pre-compaction, plastic deformation treatment, and annealing treatment, wherein:
如图1所示,在充满氩气保护的真空手套箱1中,采用微型立式铣床2对CoCrFeNiMn(面心立方单相结构)和Al0.3CoCrFeNi(面心立方+体心立方的双相结构)两种高熵合金进行碎屑制备,铣削进给量为0.2mm,得到厚度0.2mm左右的粗屑。然后采用微型破碎机3对铣制的粗屑进行精细化破碎,减小并均匀化碎屑长度至0.2-0.3mm备用。As shown in Figure 1, in a vacuum glove box 1 filled with argon protection, a micro vertical milling machine 2 is used to pair CoCrFeNiMn (face-centered cubic single-phase structure) and Al 0.3 CoCrFeNi (face-centered cubic + body-centered cubic dual-phase structure) ) Two high-entropy alloys were used for chip preparation, and the milling feed rate was 0.2 mm, and coarse chips with a thickness of about 0.2 mm were obtained. Then use the micro-crusher 3 to finely crush the milled coarse chips, reduce and uniform the length of the chips to 0.2-0.3mm for later use.
如图2所示,在充满氩气保护的真空手套箱1中,采用微型球磨机4对CoCrFeNiMn和Al0.3CoCrFeNi高熵合金碎屑进行振动、搅拌、摇匀等机械合金化混合,混屑时间为60分钟,球磨机振动搅拌的频率为100赫兹。混屑充分完成后,将碎屑填入钢制压制模具5中,型腔尺寸为50×50mm的方形。使用微型压机6对碎屑进行预压成型,压力机的工作压强为300兆帕,压制温度为250℃,保压时间为30分钟,获得致密度为80%左右的预制块7。压制完成后,对预制样品进行真空封装,取出手套箱备用。As shown in Figure 2, in the vacuum glove box 1 filled with argon protection, the CoCrFeNiMn and Al 0.3 CoCrFeNi high-entropy alloy chips are mechanically alloyed and mixed by using a micro ball mill 4, such as vibration, stirring, and shaking, and the mixing time is For 60 minutes, the vibration frequency of the ball mill was 100 Hz. After the mixed chips are fully completed, the chips are filled into the steel pressing mold 5, and the cavity size is a square of 50×50mm. Use the micro-press 6 to pre-press the debris. The working pressure of the press is 300 MPa, the pressing temperature is 250° C., and the holding time is 30 minutes to obtain a prefabricated block 7 with a density of about 80%. After the pressing is completed, vacuum seal the prefabricated samples and take them out of the glove box for later use.
如图3所示,采用真空炉8对预压混屑高熵合金锭7进行氩气氛围下的预热处理,加热温度为550℃,加热时间为30分钟;然后利用挤压模具9对预压坯料进行50×50mm至30×30mm的常规挤压变形;最后,挤压所得板材在轧机10上进行室温轧制,轧制变形量为90%,从而显著提高材料致密度至99%以上。As shown in Figure 3, the pre-compressed high-entropy alloy ingot 7 is preheated under an argon atmosphere by using a vacuum furnace 8, the heating temperature is 550 ° C, and the heating time is 30 minutes; The compacted material is subjected to conventional extrusion deformation of 50×50mm to 30×30mm; finally, the extruded plate is rolled at room temperature on the rolling mill 10, and the rolling deformation is 90%, thereby significantly increasing the material density to more than 99%.
如图4所示,采用高温真空炉11,在氩气保护氛围下,对轧制后的高熵合金样品进行700℃的退火处理,退火时间为60分钟,获得软硬相结合的异构高熵合金材料,其微观结构示意图如图4b所示。由于CoCrFeNiMn和Al0.3CoCrFeNi高熵合金在700℃退火处理下具有不同的晶粒细化效果,从而形成了这样一种多尺度晶粒混合的微观结构。As shown in Figure 4, the rolled high-entropy alloy sample is annealed at 700°C in an argon protective atmosphere using a high-temperature vacuum furnace 11 for 60 minutes to obtain a heterogeneous high-entropy alloy with a combination of soft and hard. The schematic diagram of the microstructure of the entropy alloy material is shown in Fig. 4b. Due to the different grain refinement effects of CoCrFeNiMn and Al 0.3 CoCrFeNi high-entropy alloys annealed at 700 °C, such a microstructure with mixed multi-scale grains is formed.
实施例2Example 2
如图1-4所示,以下实施例包括四步工序,分别为:制屑、混屑和预压实、塑性变形处理、退火处理,其中:As shown in Figures 1-4, the following embodiments include a four-step process, namely: chip making, chip mixing and pre-compaction, plastic deformation treatment, and annealing treatment, wherein:
如图1所示,在充满氩气保护的真空手套箱1中,采用微型立式铣床2对CoCrFeNiMn(面心立方单相结构)和Al0.3CoCrFeNi(面心立方+体心立方的双相结构)两种高熵合金进行碎屑制备,铣削进给量为0.1mm,得到厚度0.1mm左右的粗屑。然后采用微型破碎机3对铣制的粗屑进行精细化破碎,减小并均匀化碎屑长度至0.1-0.2mm备用。As shown in Figure 1, in a vacuum glove box 1 filled with argon protection, a micro vertical milling machine 2 is used to pair CoCrFeNiMn (face-centered cubic single-phase structure) and Al 0.3 CoCrFeNi (face-centered cubic + body-centered cubic dual-phase structure) ) two high-entropy alloys were used for chip preparation, and the milling feed rate was 0.1 mm, and coarse chips with a thickness of about 0.1 mm were obtained. Then use the micro-crusher 3 to finely crush the milled coarse chips, reduce and uniform the length of the chips to 0.1-0.2mm for later use.
如图2所示,在充满氩气保护的真空手套箱1中,采用微型球磨机4对CoCrFeNiMn和Al0.3CoCrFeNi高熵合金碎屑进行振动、搅拌、摇匀等机械合金化混合,混屑时间为90分钟,球磨机振动搅拌的频率为200赫兹。混屑充分完成后,将碎屑填入钢制压制模具5中,型腔尺寸为50×50mm的方形。使用微型压机6对碎屑进行预压成型,压力机的工作压强为500兆帕,压制温度为250℃,保压时间为60分钟,获得致密度为85%左右的预制块7。压制完成后,对预制样品进行真空封装,取出手套箱备用。As shown in Figure 2, in the vacuum glove box 1 filled with argon protection, the CoCrFeNiMn and Al 0.3 CoCrFeNi high-entropy alloy chips are mechanically alloyed and mixed by using a micro ball mill 4, such as vibration, stirring, and shaking, and the mixing time is For 90 minutes, the vibration frequency of the ball mill was 200 Hz. After the mixed chips are fully completed, the chips are filled into the steel pressing mold 5, and the cavity size is a square of 50×50mm. Use the micro press 6 to pre-press the chips. The working pressure of the press is 500 MPa, the pressing temperature is 250° C., and the holding time is 60 minutes to obtain a prefabricated block 7 with a density of about 85%. After the pressing is completed, vacuum seal the prefabricated samples and take them out of the glove box for later use.
如图3所示,采用真空炉8对预压混屑高熵合金锭7进行氩气氛围下的预热处理,加热温度为550℃,加热时间为60分钟;然后利用挤压模具9对预压坯料进行50×50mm至30×30mm的常规挤压变形;最后,挤压所得板材在轧机10上进行室温轧制,轧制变形量为90%,从而显著提高材料致密度至99%以上。As shown in Figure 3, the pre-compressed high-entropy alloy ingot 7 is preheated under an argon atmosphere by using a vacuum furnace 8, the heating temperature is 550 ° C, and the heating time is 60 minutes; The compacted material is subjected to conventional extrusion deformation of 50×50mm to 30×30mm; finally, the extruded plate is rolled at room temperature on the rolling mill 10, and the rolling deformation is 90%, thereby significantly increasing the material density to more than 99%.
如图4所示,采用高温真空炉11,在氩气保护氛围下,对轧制后的高熵合金样品进行700℃的退火处理,退火时间为90分钟,制备出多尺度晶粒混合的高强韧性异构高熵合金。As shown in Figure 4, the rolled high-entropy alloy sample is annealed at 700°C in an argon protective atmosphere using a high-temperature vacuum furnace 11, and the annealing time is 90 minutes to prepare a high-strength alloy with mixed multi-scale grains. Ductile heterogeneous high-entropy alloys.
实施例3Example 3
如图1-4所示,以下实施例包括四步工序,分别为:制屑、混屑和预压实、塑性变形处理、退火处理,其中:As shown in Figures 1-4, the following embodiments include a four-step process, namely: chip making, chip mixing and pre-compaction, plastic deformation treatment, and annealing treatment, wherein:
如图1所示,在充满氩气保护的真空手套箱1中,采用微型立式铣床2对CoCrFeNiMn(面心立方单相结构)和Al0.3CoCrFeNi(面心立方+体心立方的双相结构)两种高熵合金进行碎屑制备,铣削进给量为0.1mm,得到厚度0.1mm左右的粗屑。然后采用微型破碎机3对铣制的粗屑进行精细化破碎,减小并均匀化碎屑长度至0.1-0.2mm备用。As shown in Figure 1, in a vacuum glove box 1 filled with argon protection, a micro vertical milling machine 2 is used to pair CoCrFeNiMn (face-centered cubic single-phase structure) and Al 0.3 CoCrFeNi (face-centered cubic + body-centered cubic dual-phase structure) ) two high-entropy alloys were used for chip preparation, and the milling feed rate was 0.1 mm, and coarse chips with a thickness of about 0.1 mm were obtained. Then use the micro-crusher 3 to finely crush the milled coarse chips, reduce and uniform the length of the chips to 0.1-0.2mm for later use.
如图2所示,在充满氩气保护的真空手套箱1中,采用微型球磨机4对CoCrFeNiMn和Al0.3CoCrFeNi高熵合金碎屑进行振动、搅拌、摇匀等机械合金化混合,混屑时间为120分钟,球磨机振动搅拌的频率为300赫兹。混屑充分完成后,将碎屑填入钢制压制模具5中,型腔尺寸为50×50mm的方形。使用微型压机6对碎屑进行预压成型,压力机的工作压强为500兆帕,压制温度为300℃,保压时间为60分钟,获得致密度为90%左右的预制块7。压制完成后,对预制样品进行真空封装,取出手套箱备用。As shown in Figure 2, in the vacuum glove box 1 filled with argon protection, the CoCrFeNiMn and Al 0.3 CoCrFeNi high-entropy alloy chips are mechanically alloyed and mixed by using a micro ball mill 4, such as vibration, stirring, and shaking, and the mixing time is 120 minutes, the vibration frequency of the ball mill is 300 Hz. After the mixed chips are fully completed, the chips are filled into the steel pressing mold 5, and the cavity size is a square of 50×50mm. Use the micro press 6 to pre-press the debris. The working pressure of the press is 500 MPa, the pressing temperature is 300° C., and the holding time is 60 minutes to obtain a prefabricated block 7 with a density of about 90%. After the pressing is completed, vacuum seal the prefabricated samples and take them out of the glove box for later use.
如图3所示,采用真空炉8对预压混屑高熵合金锭7进行氩气氛围下的预热处理,加热温度为550℃,加热时间为60分钟;然后利用挤压模具9对预压坯料进行50×50mm至30×30mm的常规挤压变形;最后,挤压所得板材在轧机10上进行室温轧制,轧制变形量为90%,从而显著提高材料致密度至99%以上。As shown in Figure 3, the pre-compressed high-entropy alloy ingot 7 is preheated under an argon atmosphere by using a vacuum furnace 8, the heating temperature is 550 ° C, and the heating time is 60 minutes; The compacted material is subjected to conventional extrusion deformation of 50×50mm to 30×30mm; finally, the extruded plate is rolled at room temperature on the rolling mill 10, and the rolling deformation is 90%, thereby significantly increasing the material density to more than 99%.
如图4所示,采用高温真空炉11,在氩气保护氛围下,对轧制后的高熵合金样品进行725℃的退火处理,退火时间为90分钟,制备出多尺度晶粒混合的高强韧性异构高熵合金。As shown in Figure 4, the rolled high-entropy alloy sample is annealed at 725°C in an argon protective atmosphere using a high-temperature vacuum furnace 11, and the annealing time is 90 minutes to prepare a high-strength alloy with mixed multi-scale grains. Ductile heterogeneous high-entropy alloys.
原始CoCrFeNiMn高熵合金的抗拉强度和断裂延伸率分别为650MPa、40%,特点是强度低、拉伸塑性好;而原始Al0.3CoCrFeNi高熵合金的特点是质地硬而脆,其抗拉强度高达1000MPa,但是断裂延伸率仅为8%。本发明制备的高强韧性异构高熵合金充分结合了上述两种材料的优点,抗拉强度高达950MPa,且断裂延伸率为35%。The tensile strength and elongation at break of the original CoCrFeNiMn high-entropy alloy are 650MPa and 40%, respectively, which are characterized by low strength and good tensile plasticity; while the original Al 0.3 CoCrFeNi high-entropy alloy is characterized by hard and brittle texture, and its tensile strength Up to 1000MPa, but the elongation at break is only 8%. The high-strength toughness heterogeneous high-entropy alloy prepared by the invention fully combines the advantages of the above two materials, the tensile strength is as high as 950MPa, and the fracture elongation is 35%.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810657004.5A CN110629059B (en) | 2018-06-25 | 2018-06-25 | A kind of heterogeneous high entropy alloy material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810657004.5A CN110629059B (en) | 2018-06-25 | 2018-06-25 | A kind of heterogeneous high entropy alloy material and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN110629059A true CN110629059A (en) | 2019-12-31 |
CN110629059B CN110629059B (en) | 2021-02-23 |
Family
ID=68967398
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810657004.5A Active CN110629059B (en) | 2018-06-25 | 2018-06-25 | A kind of heterogeneous high entropy alloy material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110629059B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112143924A (en) * | 2020-09-25 | 2020-12-29 | 西安稀有金属材料研究院有限公司 | Preparation method of multi-scale high-strength high-entropy alloy material for corrosive environment |
CN112547798A (en) * | 2020-10-30 | 2021-03-26 | 南京理工大学 | Method for preparing high-strength heterogeneous high-entropy alloy through accumulative pack rolling |
CN115041702A (en) * | 2022-06-17 | 2022-09-13 | 南京理工大学 | Preparation method of medium/high entropy alloy with isomeric components |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130108502A1 (en) * | 2011-10-27 | 2013-05-02 | Ut-Battelle, Llc | Multi-Component Solid Solution Alloys having High Mixing Entropy |
CN105648297A (en) * | 2016-01-18 | 2016-06-08 | 南京工程学院 | Preparation method for high-entropy alloy composite material with externally-added nanometer ceramic phase reinforced and toughened |
WO2016112210A1 (en) * | 2015-01-09 | 2016-07-14 | Scoperta, Inc. | High entropy alloys with non-high entropy second phases |
CN105861909A (en) * | 2016-06-14 | 2016-08-17 | 济南大学 | FeSiBAlNiCo block high-entropy alloy and preparation method thereof |
EP3173498A1 (en) * | 2014-07-23 | 2017-05-31 | Hitachi, Ltd. | Alloy structure and method for producing alloy structure |
CN107523740A (en) * | 2017-09-20 | 2017-12-29 | 湘潭大学 | CuCrFeNiTi high entropy alloy materials and preparation method thereof |
CN107893184A (en) * | 2017-11-08 | 2018-04-10 | 太原理工大学 | A kind of nanometer Ultra-fine Grained high-entropy alloy and preparation method thereof |
-
2018
- 2018-06-25 CN CN201810657004.5A patent/CN110629059B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130108502A1 (en) * | 2011-10-27 | 2013-05-02 | Ut-Battelle, Llc | Multi-Component Solid Solution Alloys having High Mixing Entropy |
EP3173498A1 (en) * | 2014-07-23 | 2017-05-31 | Hitachi, Ltd. | Alloy structure and method for producing alloy structure |
WO2016112210A1 (en) * | 2015-01-09 | 2016-07-14 | Scoperta, Inc. | High entropy alloys with non-high entropy second phases |
CN105648297A (en) * | 2016-01-18 | 2016-06-08 | 南京工程学院 | Preparation method for high-entropy alloy composite material with externally-added nanometer ceramic phase reinforced and toughened |
CN105861909A (en) * | 2016-06-14 | 2016-08-17 | 济南大学 | FeSiBAlNiCo block high-entropy alloy and preparation method thereof |
CN107523740A (en) * | 2017-09-20 | 2017-12-29 | 湘潭大学 | CuCrFeNiTi high entropy alloy materials and preparation method thereof |
CN107893184A (en) * | 2017-11-08 | 2018-04-10 | 太原理工大学 | A kind of nanometer Ultra-fine Grained high-entropy alloy and preparation method thereof |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112143924A (en) * | 2020-09-25 | 2020-12-29 | 西安稀有金属材料研究院有限公司 | Preparation method of multi-scale high-strength high-entropy alloy material for corrosive environment |
CN112143924B (en) * | 2020-09-25 | 2021-06-25 | 西安稀有金属材料研究院有限公司 | A kind of preparation method of multi-scale high-strength high-entropy alloy material for corrosive environment |
CN112547798A (en) * | 2020-10-30 | 2021-03-26 | 南京理工大学 | Method for preparing high-strength heterogeneous high-entropy alloy through accumulative pack rolling |
CN115041702A (en) * | 2022-06-17 | 2022-09-13 | 南京理工大学 | Preparation method of medium/high entropy alloy with isomeric components |
CN115041702B (en) * | 2022-06-17 | 2024-02-13 | 南京理工大学 | Preparation method of component isomerism medium/high entropy alloy |
Also Published As
Publication number | Publication date |
---|---|
CN110629059B (en) | 2021-02-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Poletti et al. | Production of titanium matrix composites reinforced with SiC particles | |
WO2019085183A1 (en) | Method for fabricating titanium and titanium alloy metallurgical products | |
Liu et al. | Design of powder metallurgy titanium alloys and composites | |
US20130071284A1 (en) | Titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of this powder, and process for production thereof | |
Duz et al. | Industrial application of titanium hydride powder | |
JPH0347903A (en) | Density increase of powder aluminum and aluminum alloy | |
Yang et al. | Feasibility of producing Ti-6Al-4V alloy for engineering application by powder compact extrusion of blended elemental powder mixtures | |
US20090087681A1 (en) | High impact resistant metal alloy plate | |
CN110343886B (en) | A kind of preparation method of multi-grain scale reinforced aluminum alloy material | |
CN110629059A (en) | A kind of heterogeneous high entropy alloy material and preparation method thereof | |
CN110904378B (en) | Preparation method of TiAl-based composite material with high strength-ductility product | |
CN110684937B (en) | Preparation method of layered double-scale magnesium alloy | |
CN102392161A (en) | Aluminum alloy and preparation method thereof | |
US5384087A (en) | Aluminum-silicon carbide composite and process for making the same | |
Yang et al. | Microstructure and mechanical properties of a hot-hydrostatically extruded 93W–4.9 Ni–2.1 Fe alloy | |
CN109868380B (en) | Preparation method of multi-scale precipitation strengthening magnesium alloy material | |
Elsayed et al. | Microstructure and mechanical properties of hot extruded Mg–Al–Mn–Ca alloy produced by rapid solidification powder metallurgy | |
Song et al. | Synthesis of Ti/TiB composites via hydrogen-assisted blended elemental powder metallurgy | |
CN108474064A (en) | Powder metallurgy titanium alloy | |
CN105773074B (en) | A kind of preparation method of molybdenum alloy boat | |
CN109985922B (en) | A kind of preparation method of multi-grain-scale strengthened magnesium alloy material | |
WO2009153895A1 (en) | Process for producing magnesium alloy material | |
CN113798494A (en) | A kind of TiB2 particle reinforced magnesium matrix composite material and preparation method thereof | |
JP5837406B2 (en) | Titanium alloy and manufacturing method thereof | |
Wiewiora et al. | Mechanical properties of solid state recycled 6060 aluminum alloy chips |
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 |