CN113046585B - Preparation method and application of high-entropy alloy for extremely cold environment - Google Patents
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- 239000000956 alloy Substances 0.000 title claims abstract description 131
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 131
- 238000002360 preparation method Methods 0.000 title claims abstract description 17
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims abstract description 86
- 229910052751 metal Inorganic materials 0.000 claims abstract description 63
- 239000002184 metal Substances 0.000 claims abstract description 63
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 44
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 44
- 229910052786 argon Inorganic materials 0.000 claims abstract description 43
- 239000007789 gas Substances 0.000 claims abstract description 40
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 33
- 239000000843 powder Substances 0.000 claims abstract description 32
- 238000005121 nitriding Methods 0.000 claims abstract description 29
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims abstract description 23
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 22
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 22
- 239000011651 chromium Substances 0.000 claims abstract description 22
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 22
- 239000010941 cobalt Substances 0.000 claims abstract description 22
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 22
- 229910052742 iron Inorganic materials 0.000 claims abstract description 22
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 22
- 239000011572 manganese Substances 0.000 claims abstract description 22
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 22
- 238000010438 heat treatment Methods 0.000 claims abstract description 20
- 230000008021 deposition Effects 0.000 claims abstract description 19
- 238000001192 hot extrusion Methods 0.000 claims abstract description 18
- 239000000314 lubricant Substances 0.000 claims abstract description 16
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 13
- 238000005553 drilling Methods 0.000 claims abstract description 12
- 238000005065 mining Methods 0.000 claims abstract description 12
- 239000011248 coating agent Substances 0.000 claims abstract description 11
- 238000000576 coating method Methods 0.000 claims abstract description 11
- 238000002844 melting Methods 0.000 claims abstract description 10
- 230000008018 melting Effects 0.000 claims abstract description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 10
- 238000001816 cooling Methods 0.000 claims abstract description 9
- 238000001035 drying Methods 0.000 claims abstract description 8
- 239000011261 inert gas Substances 0.000 claims abstract description 8
- 238000002156 mixing Methods 0.000 claims abstract description 8
- 238000000889 atomisation Methods 0.000 claims abstract 2
- 238000000151 deposition Methods 0.000 claims description 18
- 238000001125 extrusion Methods 0.000 claims description 14
- 238000000265 homogenisation Methods 0.000 claims description 13
- 238000000034 method Methods 0.000 claims description 11
- 238000003723 Smelting Methods 0.000 claims description 10
- 238000009718 spray deposition Methods 0.000 claims description 8
- 229910001873 dinitrogen Inorganic materials 0.000 claims description 7
- 230000001681 protective effect Effects 0.000 claims description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- 229910002804 graphite Inorganic materials 0.000 claims description 5
- 239000010439 graphite Substances 0.000 claims description 5
- 150000004767 nitrides Chemical class 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 239000003973 paint Substances 0.000 claims description 3
- 241001062472 Stokellia anisodon Species 0.000 claims 1
- 239000000126 substance Substances 0.000 claims 1
- 229910000831 Steel Inorganic materials 0.000 description 12
- 239000010959 steel Substances 0.000 description 12
- 239000000203 mixture Substances 0.000 description 7
- 239000007788 liquid Substances 0.000 description 6
- 238000009864 tensile test Methods 0.000 description 5
- 239000003795 chemical substances by application Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
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- 125000004433 nitrogen atom Chemical group N* 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 125000004429 atom Chemical group 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
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- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/24—Nitriding
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Abstract
Description
技术领域technical field
本发明涉及高熵合金技术领域,具体涉及一种极寒环境用高熵合金的制备方法与应用。The invention relates to the technical field of high-entropy alloys, in particular to a preparation method and application of a high-entropy alloy for extremely cold environments.
背景技术Background technique
近年来随着工业化进程不断推进和人口的攀升,对能源需求不断提高,过度对陆地、近海和深海区域能源的开产导致全球能源紧缺。人类对能源的探索范围逐渐向南极和北极圈扩展。北极被科学家确认是贮存未来能源的地带,并且以邻近北极圈的国家为中心已经进行了对石油和天然气资源的开发。极地区域采矿、钻探用的钢材在长时间交变应力作用下,低温下断裂破坏的倾向增大,钢材变脆更容易发生脆性断裂破坏。近年来我国在南极和北极区域大规模展开科研工作,所处环境最低温度已达-80℃。因此,在提高钢材强度的同时,还需保证有一定的低温韧塑性,而现有材料难以有效满足使用要求,亟需一种在极低温下具有韧性和疲劳断裂特性的金属材料。In recent years, with the continuous advancement of industrialization and the increase of population, the demand for energy has continued to increase, and the excessive production of energy in land, offshore and deep sea areas has led to a global energy shortage. The scope of human exploration of energy has gradually expanded to the Antarctic and Arctic circles. The Arctic is recognized by scientists as a place to store future energy, and oil and gas resources have been developed centered on countries adjacent to the Arctic Circle. Under the action of alternating stress for a long time, the steel used for mining and drilling in polar regions has an increased tendency to fracture and failure at low temperature, and the steel becomes brittle and more prone to brittle fracture failure. In recent years, my country has carried out large-scale scientific research work in the Antarctic and Arctic regions, and the minimum temperature of the environment has reached -80 °C. Therefore, while improving the strength of steel, it is also necessary to ensure a certain low temperature toughness and plasticity, and the existing materials are difficult to effectively meet the requirements of use, and a metal material with toughness and fatigue fracture characteristics at extremely low temperature is urgently needed.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种极寒环境用高熵合金的制备方法,通过本发明方法制得的CoCrFeNiMn高熵合金具有高硬度和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。The purpose of the present invention is to provide a preparation method of a high-entropy alloy for extremely cold environments, the CoCrFeNiMn high-entropy alloy prepared by the method of the present invention has high hardness and high low-temperature toughness, and can be used for mining in polar regions and steel for drilling equipment .
本发明是通过如下技术方案实现的:The present invention is achieved through the following technical solutions:
一种极寒环境用高熵合金的制备方法,包括如下步骤:A preparation method of high-entropy alloy for extremely cold environment, comprising the following steps:
(1)配粉:按所述高熵合金的原子百分比将钴、铬、铁、镍、锰单质粉混合,得到混合金属粉末;(1) Mixing powder: mix cobalt, chromium, iron, nickel, manganese elemental powder according to the atomic percentage of the high-entropy alloy to obtain mixed metal powder;
(2)熔炼:将所述混合金属粉末熔化,得到金属液;(2) smelting: melting the mixed metal powder to obtain molten metal;
(3)涂润滑剂:在沉积腔体中工作台上的圆形模具内涂覆润滑剂,干燥后通入惰性气体形成保护气氛;(3) Apply lubricant: apply lubricant in the circular mold on the worktable in the deposition cavity, and after drying, introduce an inert gas to form a protective atmosphere;
(4)沉积:将所述金属液加注到金属液包中并通入惰性气体,将金属液雾化沉积在所述模具内,获得CoCrFeNiMn高熵合金锭;(4) deposition: the molten metal is injected into the molten metal bag and an inert gas is introduced, and the molten metal is atomized and deposited in the mold to obtain a CoCrFeNiMn high-entropy alloy ingot;
(5)均质化处理:将所述CoCrFeNiMn高熵合金锭置于真空加热炉中进行热处理,然后水冷;(5) homogenization treatment: the CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace for heat treatment, and then water-cooled;
(6)热挤压:将均质化处理后的所述CoCrFeNiMn高熵合金锭进行热挤压,得到CoCrFeNiMn高熵合金棒材;(6) hot extrusion: the CoCrFeNiMn high-entropy alloy ingot after the homogenization treatment is hot-extruded to obtain a CoCrFeNiMn high-entropy alloy rod;
(7)去氧化皮:去除所述CoCrFeNiMn高熵合金棒材表面氧化皮;(7) descaling: remove the oxide scale on the surface of the CoCrFeNiMn high-entropy alloy bar;
(8)渗氮处理:将去氧化皮后的所述CoCrFeNiMn高熵合金棒材置于真空渗氮装置中,并通入氩气和氮气混合气体进行高温渗氮处理,在所述CoCrFeNiMn高熵合金棒材表面形成氮化层,即获得极寒环境用CoCrFeNiMn高熵合金。(8) Nitriding treatment: place the descaled CoCrFeNiMn high-entropy alloy bar in a vacuum nitriding device, and introduce a mixed gas of argon and nitrogen for high-temperature nitriding treatment. A nitrided layer is formed on the surface of the alloy bar, that is, a CoCrFeNiMn high-entropy alloy for extremely cold environments is obtained.
进一步地,步骤(1)中所述钴、所述铬、所述铁、所述镍和所述锰的原子百分比为1:1:1:1:1;所述钴、所述铬、所述铁、所述镍和所述锰的纯度为99.9%。Further, in step (1), the atomic percentages of the cobalt, the chromium, the iron, the nickel and the manganese are 1:1:1:1:1; the cobalt, the chromium, the The purity of the iron, the nickel and the manganese was 99.9%.
进一步地,步骤(2)熔炼:将所述混合金属粉末加注到喷射沉积设备的坩埚熔炼炉中在1500-1600℃下熔化,得到金属液。Further, step (2) smelting: adding the mixed metal powder into the crucible smelting furnace of the spray deposition equipment and melting at 1500-1600° C. to obtain molten metal.
进一步地,步骤(3)中所述的润滑剂为水剂胶体石墨、DFY-1型脂基涂料或锭子油;所述的惰性气体为氩气,且所述氩气的流量为80-100sccm。Further, the lubricant described in step (3) is water-based colloidal graphite, DFY-1 type fat-based paint or spindle oil; the inert gas is argon, and the flow rate of the argon is 80-100sccm .
进一步地,步骤(4)沉积:将所述金属液加注到金属液包中并通入0.9-1.2MPa的氩气,将金属液通过直径为φ3±0.05mm的喷嘴进行雾化,将金属液雾化沉积在圆形模具内,获得尺寸为φ50cm×80cm的CoCrFeNiMn高熵合金锭。Further, step (4) deposition: the molten metal is injected into the molten metal bag and argon gas of 0.9-1.2 MPa is passed in, the molten metal is atomized through a nozzle with a diameter of φ3±0.05mm, and the metal The liquid was atomized and deposited in a circular mold to obtain CoCrFeNiMn high-entropy alloy ingots with a size of φ50cm×80cm.
进一步地,步骤(5)均质化处理:将所述CoCrFeNiMn高熵合金锭置于900-1100℃的真空加热炉中热处理6-12小时;所述水冷的温度0-20℃。Further, step (5) homogenization treatment: the CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace at 900-1100°C for heat treatment for 6-12 hours; the water cooling temperature is 0-20°C.
进一步地,步骤(6)热挤压:将均质化处理后的所述CoCrFeNiMn高熵合金锭在800-900℃下预热8-10小时,然后进行热挤压,挤压比为10-20,挤压速度为1-3mm/s;获得CoCrFeNiMn高熵合金棒材。Further, step (6) hot extrusion: the homogenized CoCrFeNiMn high-entropy alloy ingot is preheated at 800-900 ° C for 8-10 hours, and then hot extrusion is performed, and the extrusion ratio is 10- 20, the extrusion speed is 1-3mm/s; the CoCrFeNiMn high-entropy alloy rod is obtained.
进一步地,步骤(7)去氧化皮:通过数控车床去除CoCrFeNiMn高熵合金棒材表面氧化皮1-1.5mm。Further, step (7) descaling: remove 1-1.5mm of oxide scale on the surface of the CoCrFeNiMn high-entropy alloy bar by a numerically controlled lathe.
进一步地,步骤(8)渗氮处理的温度为500-1000℃,渗氮处理时间为2-12小时;所述氩气流量为40-100sccm,所述氩气与所述氮气流量比为1:(0.2-1);所述氮化层的厚度为2-3mm。Further, the temperature of the nitriding treatment in step (8) is 500-1000 ° C, and the nitriding treatment time is 2-12 hours; the flow rate of the argon gas is 40-100 sccm, and the flow ratio of the argon gas to the nitrogen gas is 1 : (0.2-1); the thickness of the nitride layer is 2-3mm.
一种极寒环境用高熵合金的应用,将上述的制备方法制得的高熵合金用作极地区域采矿、钻探装备用的钢材。An application of high-entropy alloys for extremely cold environments, the high-entropy alloys prepared by the above preparation method are used as steel materials for mining and drilling equipment in polar regions.
本发明的有益效果:Beneficial effects of the present invention:
本发明的方法制备的极寒环境用CoCrFeNiMn高熵合金组织均匀、致密,晶粒细小粒径约20-30μm,晶粒细化后晶界密度增大,晶界能有效阻碍位错运动,并且组织致密缺陷少,因此所制备的CoCrFeNiMn高熵合金具有高的抗拉强度。另外,低温条件下CoCrFeNiMn的层错能随着温度降低,合金的变形机制发生了转变,由位错滑移转变为孪生的过程,避免了由于位错塞积造成冷脆断裂的发生,因此具有高的低温韧性。本发明的制备方法通过喷射成形和渗氮技术完成,该方法生产效率高,有利于规模化生产可获得大尺寸合金坯锭,制备的高熵合金棒材具有高硬度的表面和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。本发明的制备方法在渗氮处理前,对CoCrFeNiMn高熵合金棒材表面车削量较大去除氧化层,有利于氮原子固溶到合金中;另外本发明的高熵合金成分中含有较高原子百分比的锰元素,锰元素也有利于氮原子固溶到合金中,因此可以形成较厚的氮化层,进一步提升了所得合金的硬度和低温韧性。The CoCrFeNiMn high-entropy alloy for extremely cold environment prepared by the method of the invention has a uniform and dense structure, and the small grain size is about 20-30 μm. The dense structure has few defects, so the prepared CoCrFeNiMn high-entropy alloy has high tensile strength. In addition, at low temperature, the stacking fault energy of CoCrFeNiMn decreases with the temperature, and the deformation mechanism of the alloy changes, from dislocation slip to twinning process, which avoids the occurrence of cold brittle fracture due to dislocation plugging. High low temperature toughness. The preparation method of the invention is completed by spray forming and nitriding technology, the method has high production efficiency, is conducive to large-scale production to obtain large-sized alloy ingots, and the prepared high-entropy alloy bar has a high-hardness surface and high low-temperature toughness. , which can be used as steel for mining and drilling equipment in polar regions. In the preparation method of the present invention, before the nitriding treatment, the surface of the CoCrFeNiMn high-entropy alloy bar has a large amount of turning to remove the oxide layer, which is conducive to the solid solution of nitrogen atoms into the alloy; in addition, the high-entropy alloy composition of the present invention contains relatively high atoms. The percentage of manganese element is also conducive to the solid solution of nitrogen atoms into the alloy, so a thicker nitride layer can be formed, which further improves the hardness and low temperature toughness of the obtained alloy.
具体实施方式Detailed ways
下面将结合具体的实施例,对本发明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的一部分实施例,而不是全部的实施例。以下对至少一个示例性实施例的描述实际上仅仅是说明性的,决不作为对本发明及其应用或使用的任何限制。基于本发明中的实施例,本领域普通技术人员在没有作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 technical solutions of the present invention will be clearly and completely described below with reference to specific embodiments. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
实施例1Example 1
一种极寒环境用高熵合金的制备方法,包括如下步骤:A preparation method of high-entropy alloy for extremely cold environment, comprising the following steps:
(1)配粉:按所述高熵合金的原子百分比将钴、铬、铁、镍、锰单质粉混合均匀,得到混合金属粉末;所述钴、所述铬、所述铁、所述镍和所述锰的原子百分比为1:1:1:1:1;所述钴、所述铬、所述铁、所述镍和所述锰的纯度为99.9%;(1) Mixing powder: uniformly mix cobalt, chromium, iron, nickel, and manganese elemental powder according to the atomic percentage of the high-entropy alloy to obtain mixed metal powder; the cobalt, the chromium, the iron, the nickel and the atomic percentage of the manganese is 1:1:1:1:1; the purity of the cobalt, the chromium, the iron, the nickel and the manganese is 99.9%;
(2)熔炼:将上述混合金属粉末加注到喷射沉积设备的坩埚熔炼炉中在1500℃下熔化,得到金属液;(2) smelting: the above mixed metal powder is poured into the crucible melting furnace of the spray deposition equipment and melted at 1500 ° C to obtain molten metal;
(3)涂润滑剂:在沉积腔体中工作台上的圆形模具内涂覆水剂胶体石墨润滑剂,干燥后通入高纯氩气形成保护气氛;且所述氩气流量为100sccm;(3) Coating lubricant: coating water-agent colloidal graphite lubricant in the circular mold on the worktable in the deposition cavity, and feeding high-purity argon gas after drying to form a protective atmosphere; and the argon gas flow rate is 100sccm;
(4)沉积:将上述金属液加注到金属液包中并通入1.2MPa的高纯氩气,将金属液通过直径为φ3mm的喷嘴进行雾化,将金属液雾化沉积在圆形模具内,获得尺寸为φ50cm×80cm的CoCrFeNiMn高熵合金锭;(4) Deposition: The above-mentioned molten metal is injected into the molten metal bag and high-purity argon gas of 1.2 MPa is passed in, the molten metal is atomized through a nozzle with a diameter of φ3mm, and the molten metal is atomized and deposited on a circular mold Inside, a CoCrFeNiMn high-entropy alloy ingot with a size of φ50cm×80cm was obtained;
(5)均质化处理:将所得CoCrFeNiMn高熵合金锭置于1000℃的真空加热炉中热处理12小时,然后放入20℃水中冷却;(5) homogenization treatment: the obtained CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace at 1000 ° C for heat treatment for 12 hours, and then placed in 20 ° C of water for cooling;
(6)热挤压:将经过均质化处理后的CoCrFeNiMn高熵合金锭在800℃下预热8小时,然后进行热挤压,挤压比为10,挤压速度为3mm/s;即获得CoCrFeNiMn高熵合金棒材;(6) Hot extrusion: Preheat the homogenized CoCrFeNiMn high-entropy alloy ingot at 800 °C for 8 hours, and then perform hot extrusion, the extrusion ratio is 10, and the extrusion speed is 3 mm/s; Obtain CoCrFeNiMn high-entropy alloy rods;
(7)去氧化皮:通过数控车床去除所述CoCrFeNiMn高熵合金棒材表面1.0mm厚的氧化皮;(7) Descale: remove the 1.0mm-thick scale on the surface of the CoCrFeNiMn high-entropy alloy bar by a numerically controlled lathe;
(8)渗氮处理:将去氧化皮后的所述CoCrFeNiMn高熵合金棒材置于真空渗氮装置中,并通入氩气和氮气混合气体在600℃下进行氮化处理12小时,在所述CoCrFeNiMn高熵合金棒材表面形成氮化层,获得极寒环境用CoCrFeNiMn高熵合金;且通入的氩气流量为40sccm,氩气与氮气的流量比为1:0.2。(8) Nitriding treatment: the CoCrFeNiMn high-entropy alloy bar after descaling was placed in a vacuum nitriding device, and a mixed gas of argon and nitrogen was introduced for nitriding treatment at 600° C. for 12 hours. A nitrided layer is formed on the surface of the CoCrFeNiMn high-entropy alloy bar to obtain a CoCrFeNiMn high-entropy alloy for extremely cold environments; and the flow rate of argon gas introduced is 40sccm, and the flow ratio of argon gas to nitrogen gas is 1:0.2.
测试:通过硬度计测量上述实施例1所得极寒环境用CoCrFeNiMn高熵合金表面硬度为8GPa;通过在液氮(-196℃)拉伸试验测量抗拉强度为802MPa、延伸率为68%;可见本发明所制得的高熵合金在极低温度下的延伸率较好,表面了其低温韧性好。Test: The surface hardness of the CoCrFeNiMn high-entropy alloy for extreme cold environment obtained in the above-mentioned Example 1 was measured by a hardness tester to be 8GPa; the tensile strength measured by the tensile test in liquid nitrogen (-196°C) was 802MPa, and the elongation was 68%; it can be seen that The high-entropy alloy prepared by the invention has good elongation at extremely low temperature and good low-temperature toughness on the surface.
应用:本发明制备的CoCrFeNiMn高熵合金具有高硬度的表面和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。Application: The CoCrFeNiMn high-entropy alloy prepared by the present invention has a high hardness surface and high low temperature toughness, and can be used as steel for mining and drilling equipment in polar regions.
实施例2Example 2
一种极寒环境用高熵合金的制备方法,包括如下步骤:A preparation method of high-entropy alloy for extremely cold environment, comprising the following steps:
(1)配粉:按所述高熵合金的原子百分比将钴、铬、铁、镍、锰单质粉混合均匀,得到混合金属粉末;所述钴、所述铬、所述铁、所述镍和所述锰的原子百分比为1:1:1:1:1;所述钴、所述铬、所述铁、所述镍和所述锰的纯度为99.9%;(1) Mixing powder: uniformly mix cobalt, chromium, iron, nickel, and manganese elemental powder according to the atomic percentage of the high-entropy alloy to obtain mixed metal powder; the cobalt, the chromium, the iron, the nickel and the atomic percentage of the manganese is 1:1:1:1:1; the purity of the cobalt, the chromium, the iron, the nickel and the manganese is 99.9%;
(2)熔炼:将上述混合金属粉末加注到喷射沉积设备的坩埚熔炼炉中在1550℃下熔化,得到金属液;(2) smelting: the above mixed metal powder is poured into the crucible melting furnace of the spray deposition equipment and melted at 1550 ° C to obtain molten metal;
(3)涂润滑剂:在沉积腔体中工作台上的圆形模具内涂覆水剂胶体石墨润滑剂,干燥后通入高纯氩气形成保护气氛;且所述氩气流量为80sccm;(3) coating lubricant: coating water-agent colloidal graphite lubricant in the circular mold on the worktable in the deposition cavity, and feeding high-purity argon gas after drying to form a protective atmosphere; and the flow rate of the argon gas is 80sccm;
(4)沉积:将上述金属液加注到金属液包中并通入1.1MPa的高纯氩气,将金属液通过直径为φ3.05mm的喷嘴进行雾化,将金属液雾化沉积在圆形模具内,获得尺寸为φ50cm×80cm的CoCrFeNiMn高熵合金锭;(4) Deposition: The above-mentioned molten metal is poured into the molten metal bag, and high-purity argon gas of 1.1 MPa is passed in, and the molten metal is atomized through a nozzle with a diameter of φ3.05 mm, and the molten metal is atomized and deposited on a circle. In the mold, a CoCrFeNiMn high-entropy alloy ingot with a size of φ50cm×80cm was obtained;
(5)均质化处理:将所得CoCrFeNiMn高熵合金锭置于950℃的真空加热炉中热处理10小时,然后放入15℃水中冷却;(5) Homogenization treatment: the obtained CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace at 950 ° C for heat treatment for 10 hours, and then placed in 15 ° C of water for cooling;
(6)热挤压:将经过均质化处理后的CoCrFeNiMn高熵合金锭在900℃下预热8小时,然后进行热挤压,挤压比为15,挤压速度为2mm/s;即获得CoCrFeNiMn高熵合金棒材;(6) Hot extrusion: preheat the CoCrFeNiMn high-entropy alloy ingot after homogenization treatment at 900 ° C for 8 hours, and then perform hot extrusion, the extrusion ratio is 15, and the extrusion speed is 2 mm/s; Obtain CoCrFeNiMn high-entropy alloy rods;
(7)去氧化皮:通过数控车床去除所述CoCrFeNiMn高熵合金棒材表面1.2mm厚的氧化皮;(7) Descale: remove the 1.2mm-thick scale on the surface of the CoCrFeNiMn high-entropy alloy bar by a numerically controlled lathe;
(8)渗氮处理:将去氧化皮后的所述CoCrFeNiMn高熵合金棒材置于真空渗氮装置中,并通入氩气和氮气混合气体在500℃下进行氮化处理8小时,在所述CoCrFeNiMn高熵合金棒材表面形成氮化层,获得极寒环境用CoCrFeNiMn高熵合金;且通入的氩气流量为60sccm,氩气与氮气的流量比为1:0.4。(8) Nitriding treatment: the CoCrFeNiMn high-entropy alloy bar after descaling was placed in a vacuum nitriding device, and a mixed gas of argon and nitrogen was introduced for nitriding treatment at 500° C. for 8 hours. A nitrided layer is formed on the surface of the CoCrFeNiMn high-entropy alloy bar to obtain a CoCrFeNiMn high-entropy alloy for extremely cold environments; the flow rate of argon gas introduced is 60sccm, and the flow ratio of argon gas to nitrogen gas is 1:0.4.
测试:通过硬度计测量上述实施例2所得极寒环境用CoCrFeNiMn高熵合金表面硬度为10.2GPa;通过在液氮(-196℃)拉伸试验测量抗拉强度为799MPa、延伸率为70%;可见本发明所制得的高熵合金在极低温度下的延伸率较好,表面了其低温韧性好。Test: The surface hardness of the CoCrFeNiMn high-entropy alloy for extremely cold environments obtained in the above-mentioned Example 2 was measured by a hardness tester to be 10.2GPa; the tensile strength measured by the tensile test in liquid nitrogen (-196°C) was 799MPa, and the elongation was 70%; It can be seen that the high-entropy alloy prepared by the present invention has better elongation at extremely low temperature, and has good low-temperature toughness on the surface.
应用:本发明制备的CoCrFeNiMn高熵合金具有高硬度的表面和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。Application: The CoCrFeNiMn high-entropy alloy prepared by the present invention has a high hardness surface and high low temperature toughness, and can be used as steel for mining and drilling equipment in polar regions.
实施例3Example 3
一种极寒环境用高熵合金的制备方法,包括如下步骤:A preparation method of high-entropy alloy for extremely cold environment, comprising the following steps:
(1)配粉:按所述高熵合金的原子百分比将钴、铬、铁、镍、锰单质粉混合均匀,得到混合金属粉末;所述钴、所述铬、所述铁、所述镍和所述锰的原子百分比为1:1:1:1:1;所述钴、所述铬、所述铁、所述镍和所述锰的纯度为99.9%;(1) Mixing powder: uniformly mix cobalt, chromium, iron, nickel, and manganese elemental powder according to the atomic percentage of the high-entropy alloy to obtain mixed metal powder; the cobalt, the chromium, the iron, the nickel and the atomic percentage of the manganese is 1:1:1:1:1; the purity of the cobalt, the chromium, the iron, the nickel and the manganese is 99.9%;
(2)熔炼:将上述混合金属粉末加注到喷射沉积设备的坩埚熔炼炉中在1580℃下熔化,得到金属液;(2) Smelting: adding the mixed metal powder to the crucible melting furnace of the spray deposition equipment and melting at 1580 ° C to obtain molten metal;
(3)涂润滑剂:在沉积腔体中工作台上的圆形模具内涂覆DFY-1型脂基涂料润滑剂,干燥后通入高纯氩气形成保护气氛;且所述氩气流量为100sccm;(3) Apply lubricant: apply DFY-1 grease-based paint lubricant in the circular mold on the worktable in the deposition cavity, and after drying, pass high-purity argon gas to form a protective atmosphere; and the argon gas flow rate is 100sccm;
(4)沉积:将上述金属液加注到金属液包中并通入0.9MPa的高纯氩气,将金属液通过直径为φ2.95mm的喷嘴进行雾化,将金属液雾化沉积在圆形模具内,获得尺寸为φ50cm×80cm的CoCrFeNiMn高熵合金锭;(4) Deposition: The above-mentioned molten metal is poured into the molten metal bag, and high-purity argon gas of 0.9 MPa is passed through. In the mold, a CoCrFeNiMn high-entropy alloy ingot with a size of φ50cm×80cm was obtained;
(5)均质化处理:将所得CoCrFeNiMn高熵合金锭置于900℃的真空加热炉中热处理8小时,然后放入10℃水中冷却;(5) Homogenization treatment: the obtained CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace at 900 ° C for heat treatment for 8 hours, and then placed in 10 ° C of water for cooling;
(6)热挤压:将经过均质化处理后的CoCrFeNiMn高熵合金锭在850℃下预热8小时,然后进行热挤压,挤压比为20,挤压速度为2mm/s;即获得CoCrFeNiMn高熵合金棒材;(6) Hot extrusion: Preheat the CoCrFeNiMn high-entropy alloy ingot after homogenization treatment at 850 ° C for 8 hours, and then perform hot extrusion, the extrusion ratio is 20, and the extrusion speed is 2 mm/s; Obtain CoCrFeNiMn high-entropy alloy rods;
(7)去氧化皮:通过数控车床去除所述CoCrFeNiMn高熵合金棒材表面1.5mm厚的氧化皮;(7) Descale: remove the 1.5mm thick scale on the surface of the CoCrFeNiMn high-entropy alloy bar by a numerically controlled lathe;
(8)渗氮处理:将去氧化皮后的所述CoCrFeNiMn高熵合金棒材置于真空渗氮装置中,并通入氩气和氮气混合气体在1000℃下进行氮化处理2小时,在所述CoCrFeNiMn高熵合金棒材表面形成氮化层,获得极寒环境用CoCrFeNiMn高熵合金;且通入的氩气流量为80sccm,氩气与氮气的流量比为1:0.6。(8) Nitriding treatment: the CoCrFeNiMn high-entropy alloy bar after descaling was placed in a vacuum nitriding device, and a mixed gas of argon and nitrogen was introduced to carry out nitriding treatment at 1000° C. for 2 hours. A nitrided layer is formed on the surface of the CoCrFeNiMn high-entropy alloy bar to obtain a CoCrFeNiMn high-entropy alloy for extremely cold environments; and the flow rate of argon gas introduced is 80sccm, and the flow ratio of argon gas to nitrogen gas is 1:0.6.
测试:通过硬度计测量上述实施例3所得极寒环境用CoCrFeNiMn高熵合金表面硬度为11.98GPa;通过在液氮(-196℃)拉伸试验测量抗拉强度为801MPa、延伸率为68%;可见本发明所制得的高熵合金在极低温度下的延伸率较好,表面了其低温韧性好。Test: The surface hardness of the CoCrFeNiMn high-entropy alloy for extreme cold environment obtained in the above-mentioned Example 3 was measured by a hardness tester to be 11.98GPa; the tensile strength measured by the tensile test in liquid nitrogen (-196°C) was 801MPa, and the elongation was 68%; It can be seen that the high-entropy alloy prepared by the present invention has better elongation at extremely low temperature, and has good low-temperature toughness on the surface.
应用:本发明制备的CoCrFeNiMn高熵合金具有高硬度的表面和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。Application: The CoCrFeNiMn high-entropy alloy prepared by the present invention has a high hardness surface and high low temperature toughness, and can be used as steel for mining and drilling equipment in polar regions.
实施例4Example 4
一种极寒环境用高熵合金的制备方法,包括如下步骤:A preparation method of high-entropy alloy for extremely cold environment, comprising the following steps:
(1)配粉:按所述高熵合金的原子百分比将钴、铬、铁、镍、锰单质粉混合均匀,得到混合金属粉末;所述钴、所述铬、所述铁、所述镍和所述锰的原子百分比为1:1:1:1:1;所述钴、所述铬、所述铁、所述镍和所述锰的纯度为99.9%;(1) Mixing powder: uniformly mix cobalt, chromium, iron, nickel, and manganese elemental powder according to the atomic percentage of the high-entropy alloy to obtain mixed metal powder; the cobalt, the chromium, the iron, the nickel and the atomic percentage of the manganese is 1:1:1:1:1; the purity of the cobalt, the chromium, the iron, the nickel and the manganese is 99.9%;
(2)熔炼:将上述混合金属粉末加注到喷射沉积设备的坩埚熔炼炉中在1600℃下熔化,得到金属液;(2) Smelting: the above-mentioned mixed metal powder is poured into the crucible melting furnace of the spray deposition equipment and melted at 1600 ° C to obtain molten metal;
(3)涂润滑剂:在沉积腔体中工作台上的圆形模具内涂覆锭子油,干燥后通入高纯氩气形成保护气氛;且所述氩气流量为90sccm;(3) coating lubricant: coating spindle oil in the circular mold on the worktable in the deposition cavity, and feeding high-purity argon gas after drying to form a protective atmosphere; and the argon gas flow rate is 90sccm;
(4)沉积:将上述金属液加注到金属液包中并通入1.0MPa的高纯氩气,将金属液通过直径为φ3.0mm的喷嘴进行雾化,将金属液雾化沉积在圆形模具内,即可获得尺寸为φ50cm×80cm的CoCrFeNiMn高熵合金锭;(4) Deposition: Add the above-mentioned molten metal into the molten metal bag and pass high-purity argon gas of 1.0 MPa, atomize the molten metal through a nozzle with a diameter of φ3.0 mm, and atomically deposit the molten metal on a circular A CoCrFeNiMn high-entropy alloy ingot with a size of φ50cm×80cm can be obtained in the mold;
(5)均质化处理:将所得CoCrFeNiMn高熵合金锭置于1100℃的真空加热炉中热处理6小时,然后放入5℃水中冷却;(5) Homogenization treatment: the obtained CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace at 1100 ° C for heat treatment for 6 hours, and then placed in 5 ° C of water for cooling;
(6)热挤压:将经过均质化处理后的CoCrFeNiMn高熵合金锭在900℃下预热8小时,然后进行热挤压,挤压比为10,挤压速度为3mm/s;即获得CoCrFeNiMn高熵合金棒材;(6) Hot extrusion: preheat the CoCrFeNiMn high-entropy alloy ingot after homogenization treatment at 900 ° C for 8 hours, and then perform hot extrusion, the extrusion ratio is 10, and the extrusion speed is 3 mm/s; Obtain CoCrFeNiMn high-entropy alloy rods;
(7)去氧化皮:通过数控车床去除所述CoCrFeNiMn高熵合金棒材表面1.3mm厚的氧化皮;(7) Descale: remove the 1.3mm thick scale on the surface of the CoCrFeNiMn high-entropy alloy bar by a CNC lathe;
(8)渗氮处理:将去氧化皮后的所述CoCrFeNiMn高熵合金棒材置于真空渗氮装置中,并通入氩气和氮气混合气体在800℃下进行氮化处理5小时,在所述CoCrFeNiMn高熵合金棒材表面形成氮化层,获得极寒环境用CoCrFeNiMn高熵合金;且通入的氩气流量为100sccm,氩气与氮气的流量比为1:0.8。(8) Nitriding treatment: place the CoCrFeNiMn high-entropy alloy bar after descaling in a vacuum nitriding device, and introduce a mixed gas of argon and nitrogen for nitriding treatment at 800° C. for 5 hours. A nitrided layer is formed on the surface of the CoCrFeNiMn high-entropy alloy rod to obtain a CoCrFeNiMn high-entropy alloy for extremely cold environments; and the flow rate of argon gas introduced is 100sccm, and the flow ratio of argon gas to nitrogen gas is 1:0.8.
测试:通过硬度计测量上述实施例4所得极寒环境用CoCrFeNiMn高熵合金表面硬度为12.2GPa;通过在液氮(-196℃)拉伸试验测量抗拉强度为804MPa、延伸率为69%;可见本发明所制得的高熵合金在极低温度下的延伸率较好,表面了其低温韧性好。Test: The surface hardness of the CoCrFeNiMn high-entropy alloy for extreme cold environments obtained in Example 4 was measured by a hardness tester, and the surface hardness was 12.2GPa; the tensile strength measured by the tensile test in liquid nitrogen (-196°C) was 804MPa, and the elongation was 69%; It can be seen that the high-entropy alloy prepared by the present invention has better elongation at extremely low temperature, and has good low-temperature toughness on the surface.
应用:本发明制备的CoCrFeNiMn高熵合金具有高硬度的表面和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。Application: The CoCrFeNiMn high-entropy alloy prepared by the present invention has a high hardness surface and high low temperature toughness, and can be used as steel for mining and drilling equipment in polar regions.
实施例5Example 5
一种极寒环境用高熵合金的制备方法,包括如下步骤:A preparation method of high-entropy alloy for extremely cold environment, comprising the following steps:
(1)配粉:按所述高熵合金的原子百分比将钴、铬、铁、镍、锰单质粉混合均匀,得到混合金属粉末;所述钴、所述铬、所述铁、所述镍和所述锰的原子百分比为1:1:1:1:1;所述钴、所述铬、所述铁、所述镍和所述锰的纯度为99.9%;(1) Mixing powder: uniformly mix cobalt, chromium, iron, nickel, and manganese elemental powder according to the atomic percentage of the high-entropy alloy to obtain mixed metal powder; the cobalt, the chromium, the iron, the nickel and the atomic percentage of the manganese is 1:1:1:1:1; the purity of the cobalt, the chromium, the iron, the nickel and the manganese is 99.9%;
(2)熔炼:将上述混合金属粉末加注到喷射沉积设备的坩埚熔炼炉中在1500℃下熔化,得到金属液;(2) smelting: the above mixed metal powder is poured into the crucible melting furnace of the spray deposition equipment and melted at 1500 ° C to obtain molten metal;
(3)涂润滑剂:在沉积腔体中工作台上的圆形模具内涂覆水剂胶体石墨润滑剂,干燥后通入高纯氩气形成保护气氛;且所述氩气流量为100sccm;(3) Coating lubricant: coating water-agent colloidal graphite lubricant in the circular mold on the worktable in the deposition cavity, and feeding high-purity argon gas after drying to form a protective atmosphere; and the argon gas flow rate is 100sccm;
(4)沉积:将上述金属液加注到金属液包中并通入1.2MPa的高纯氩气,将金属液通过直径为φ3.0mm的喷嘴进行雾化,将金属液雾化沉积在圆形模具内,即可获得尺寸为φ50cm×80cm的CoCrFeNiMn高熵合金锭;(4) Deposition: The above-mentioned molten metal is injected into the molten metal bag and the high-purity argon gas of 1.2MPa is passed in, the molten metal is atomized through a nozzle with a diameter of φ3.0mm, and the molten metal is atomized and deposited on the circular A CoCrFeNiMn high-entropy alloy ingot with a size of φ50cm×80cm can be obtained in the mold;
(5)均质化处理:将所得CoCrFeNiMn高熵合金锭置于1050℃的真空加热炉中热处理9小时,然后放入20℃水中冷却;(5) homogenization treatment: the obtained CoCrFeNiMn high-entropy alloy ingot is placed in a vacuum heating furnace at 1050 ° C for heat treatment for 9 hours, and then placed in 20 ° C of water for cooling;
(6)热挤压:将经过均质化处理后的CoCrFeNiMn高熵合金锭在800℃下预热9小时,然后进行热挤压,挤压比为10,挤压速度为3mm/s;即获得CoCrFeNiMn高熵合金棒材;(6) Hot extrusion: Preheat the CoCrFeNiMn high-entropy alloy ingot after homogenization treatment at 800 ° C for 9 hours, and then perform hot extrusion, the extrusion ratio is 10, and the extrusion speed is 3 mm/s; Obtain CoCrFeNiMn high-entropy alloy rods;
(7)去氧化皮:通过数控车床去除所述CoCrFeNiMn高熵合金棒材表面1.1mm厚的氧化皮;(7) Descale: remove the 1.1mm thick oxide scale on the surface of the CoCrFeNiMn high-entropy alloy bar by a numerically controlled lathe;
(8)渗氮处理:将去氧化皮后的所述CoCrFeNiMn高熵合金棒材置于真空渗氮装置中,并通入氩气和氮气混合气体在700℃下进行氮化处理8小时,在所述CoCrFeNiMn高熵合金棒材表面形成氮化层,获得极寒环境用CoCrFeNiMn高熵合金;且通入的氩气流量为50sccm,氩气与氮气的流量比为1:1。(8) Nitriding treatment: the CoCrFeNiMn high-entropy alloy bar after descaling was placed in a vacuum nitriding device, and a mixed gas of argon and nitrogen was introduced for nitriding treatment at 700° C. for 8 hours. A nitrided layer is formed on the surface of the CoCrFeNiMn high-entropy alloy bar to obtain a CoCrFeNiMn high-entropy alloy for extremely cold environments; and the flow rate of argon gas introduced is 50 sccm, and the flow ratio of argon gas to nitrogen gas is 1:1.
测试:通过硬度计测量上述实施例5所得极寒环境用CoCrFeNiMn高熵合金表面硬度为12.1GPa;通过在液氮(-196℃)拉伸试验测量抗拉强度为805MPa、延伸率为70%;可见本发明所制得的高熵合金在极低温度下的延伸率较好,表面了其低温韧性好。Test: The surface hardness of the CoCrFeNiMn high-entropy alloy for extreme cold environment obtained in Example 5 was measured by a hardness tester, and the surface hardness was 12.1GPa; the tensile strength measured by the tensile test in liquid nitrogen (-196°C) was 805MPa, and the elongation was 70%; It can be seen that the high-entropy alloy prepared by the present invention has better elongation at extremely low temperature, and has good low-temperature toughness on the surface.
应用:本发明制备的CoCrFeNiMn高熵合金具有高硬度的表面和高的低温韧性,可用于极地区域采矿、钻探装备用的钢材。Application: The CoCrFeNiMn high-entropy alloy prepared by the present invention has a surface with high hardness and high low temperature toughness, and can be used as steel for mining and drilling equipment in polar regions.
从上述实施例1-5的测试结果可以看出,通过本发明的制备方法方法制得的CoCrFeNiMn高熵合金,其具有优异的硬度、抗拉强度以及低温韧性等力学性能,可用于极地区域采矿、钻探装备用的钢材。上述为本发明的较佳实施例仅用于解释本发明,并不用于限定本发明。凡由本发明的技术方案所引伸出的显而易见的变化或变动仍处于本发明的保护范围之中。It can be seen from the test results of the above examples 1-5 that the CoCrFeNiMn high-entropy alloy prepared by the preparation method of the present invention has excellent mechanical properties such as hardness, tensile strength and low temperature toughness, and can be used for mining in polar regions , Steel for drilling equipment. The above-mentioned preferred embodiments of the present invention are only used to explain the present invention, and are not intended to limit the present invention. Any obvious changes or changes derived from the technical solutions of the present invention are still within the protection scope of the present invention.
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