CN116815009A - A multi-component complex coherent precipitation strengthened Cu-Ni-Al-Cr-Ti high temperature resistant copper alloy and its preparation method - Google Patents
A multi-component complex coherent precipitation strengthened Cu-Ni-Al-Cr-Ti high temperature resistant copper alloy and its preparation method Download PDFInfo
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- CN116815009A CN116815009A CN202310511357.5A CN202310511357A CN116815009A CN 116815009 A CN116815009 A CN 116815009A CN 202310511357 A CN202310511357 A CN 202310511357A CN 116815009 A CN116815009 A CN 116815009A
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- 229910000881 Cu alloy Inorganic materials 0.000 title claims abstract description 18
- 230000001427 coherent effect Effects 0.000 title claims abstract description 17
- 238000001556 precipitation Methods 0.000 title claims abstract description 11
- 238000002360 preparation method Methods 0.000 title abstract description 5
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 47
- 239000000956 alloy Substances 0.000 claims abstract description 47
- 238000005728 strengthening Methods 0.000 claims abstract description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 6
- 239000002994 raw material Substances 0.000 claims description 6
- 230000032683 aging Effects 0.000 claims description 5
- 238000002844 melting Methods 0.000 claims description 4
- 230000008018 melting Effects 0.000 claims description 4
- 229910052786 argon Inorganic materials 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 238000000034 method Methods 0.000 claims description 2
- 239000010949 copper Substances 0.000 abstract description 9
- 239000000203 mixture Substances 0.000 abstract description 5
- 229910052759 nickel Inorganic materials 0.000 abstract description 3
- 238000009864 tensile test Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 229910017813 Cu—Cr Inorganic materials 0.000 description 2
- 241001062472 Stokellia anisodon Species 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000739 chaotic effect Effects 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 238000007086 side reaction Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000004154 testing of material Methods 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C9/00—Alloys based on copper
- C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
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- 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
- C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
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Abstract
一种多组元复杂共格析出强化Cu‑Ni‑Al‑Cr‑Ti耐高温铜合金及其制备方法,其属于耐高温铜合金领域。该铜合金的质量百分比组成为Cu:58.67~64.85wt%,Ni:26.18~28.94%,Al:4.51~4.99 wt%,Cr:2.60~2.88wt%,Ti:3.03~3.35wt%。该合金始终具有多组元复杂共格析出组织,合金室温拉伸强度不低于760MPa,800℃下拉伸强度不低于200MPa。采用多种高温共格析出强化相的组合,可以在宽温区提升铜合金的高温性能。
A multi-component complex coherent precipitation-strengthened Cu‑Ni‑Al‑Cr‑Ti high-temperature resistant copper alloy and a preparation method thereof, which belongs to the field of high-temperature resistant copper alloys. The mass percentage composition of the copper alloy is Cu: 58.67~64.85wt%, Ni: 26.18~28.94%, Al: 4.51~4.99wt%, Cr: 2.60~2.88wt%, and Ti: 3.03~3.35wt%. This alloy always has a multi-component complex coherent precipitation structure. The tensile strength of the alloy at room temperature is not less than 760MPa, and the tensile strength at 800°C is not less than 200MPa. Using a combination of multiple high-temperature coherent precipitation strengthening phases can improve the high-temperature properties of copper alloys in a wide temperature range.
Description
技术领域Technical field
本发明涉及一种多组元复杂共格析出强化Cu-Ni-Al-Cr-Ti耐高温合金及其制备方法,其属于耐高温铜合金领域。The invention relates to a multi-component complex coherent precipitation-strengthened Cu-Ni-Al-Cr-Ti high-temperature resistant alloy and a preparation method thereof, which belongs to the field of high-temperature resistant copper alloys.
背景技术Background technique
高性能铜合金是应用于高铁接触线、电磁炮、火箭发动机燃烧室的关键材料。目前的耐高温铜合金主要为弥散强化型和析出强化型。氧化物(Al2O3)弥散强化Cu合金,其软化温度可达930℃,但由于氧化物颗粒与Cu熔体的润湿性很差、比重相差较大,易偏聚,难均匀弥散分布,以及副反应夹杂物等问题,导致其加工性极差,因而氧化物添加量有限,其硬度不高于160HV。典型的析出强化型Cu-Cr合金,由于Cr析出相在高温下会快速粗化,导致合金的抗软化能力下降。且随着工业化发展需求,对材料的耐温性能提出了更高的要求,服役材料需要具备良好的高温强度及高温稳定性。由于Cu和Ni的混乱占位问题,现有单一形态立方共格析出强化铜合金中的γ′相稳定性下降,高温下易回溶。High-performance copper alloys are key materials used in high-speed rail contact wires, electromagnetic guns, and rocket engine combustion chambers. The current high-temperature resistant copper alloys are mainly dispersion-strengthened and precipitation-strengthened. Oxide (Al 2 O 3 ) dispersion-strengthened Cu alloy has a softening temperature of up to 930°C. However, due to the poor wettability of the oxide particles and the Cu melt and the large difference in specific gravity, it is easy to segregate and difficult to disperse uniformly. , as well as side reaction inclusions and other problems, resulting in extremely poor processability, so the amount of oxide added is limited, and its hardness is not higher than 160HV. In typical precipitation-strengthened Cu-Cr alloys, the Cr precipitation phase will coarsen rapidly at high temperatures, resulting in a decrease in the softening resistance of the alloy. And with the development needs of industrialization, higher requirements have been placed on the temperature resistance of materials. Service materials need to have good high-temperature strength and high-temperature stability. Due to the chaotic space occupation problem of Cu and Ni, the stability of the γ' phase in the existing single-form cubic coherent precipitation-strengthened copper alloy decreases and is easy to redissolve at high temperatures.
发明内容Contents of the invention
为解决现有合金中存在的问题,本发明拟制备具有良好高温性能的多组元复杂共格析出强化铜合金。Ti元素在γ'相中的固溶可提升γ'相的高温稳定性,而单质Cr相可提升合金中低温强度,并可在高温下提升合金抗氧化性能。In order to solve the problems existing in existing alloys, the present invention intends to prepare a multi-component complex coherent precipitation-strengthened copper alloy with good high-temperature properties. The solid solution of Ti element in the γ' phase can improve the high-temperature stability of the γ' phase, while the elemental Cr phase can improve the low-temperature strength of the alloy and improve the oxidation resistance of the alloy at high temperatures.
本发明的技术方案为:一种多组元复杂共格析出强化Cu-Ni-Al-Cr-Ti耐高温铜合金,所述铜合金中包括组分的质量百分比为Cu:58.67~64.85wt%,Ni:26.18~28.94%,Al:4.51~4.99wt%,Cr:2.60~2.88wt%,Ti:3.03~3.35wt%。该合金始终具有多组元复杂共格析出组织,合金室温拉伸强度不低于760MPa,800℃下拉伸强度不低于200MPa。The technical solution of the present invention is: a multi-component complex coherent precipitation-strengthened Cu-Ni-Al-Cr-Ti high-temperature resistant copper alloy. The mass percentage of the components included in the copper alloy is Cu: 58.67~64.85wt% , Ni: 26.18~28.94%, Al: 4.51~4.99wt%, Cr: 2.60~2.88wt%, Ti: 3.03~3.35wt%. This alloy always has a multi-component complex coherent precipitation structure. The tensile strength of the alloy at room temperature is not less than 760MPa, and the tensile strength at 800°C is not less than 200MPa.
所述的一种多组元复杂共格析出强化Cu-Ni-Al-Cr-Ti耐高温合金的制备方法:The preparation method of the multi-component complex coherent precipitation-strengthened Cu-Ni-Al-Cr-Ti high temperature resistant alloy:
按合金的上述成分,使用4N以上高纯度金属为原料配制合金;采用非自耗真空电弧熔炼炉,通入高纯氩气保护,对配制好的合金原料进行反复熔炼,最终得到成分均匀的合金锭;将熔炼好的合金锭进行热处理:先进行固溶处理,在1100℃下恒温保持6h,随后在炉中冷却到室温;再进行时效处理,在450℃下恒温保持4h,随后在炉中冷却到室温,获得多组元复杂共格析出强化Cu-Ni-Al-Cr-Ti耐高温合金。利用万能试验机对合金进行高温拉伸测试。According to the above composition of the alloy, use high-purity metals above 4N as raw materials to prepare the alloy; use a non-consumable vacuum arc melting furnace, pass in high-purity argon gas for protection, and repeatedly smelt the prepared alloy raw materials to finally obtain an alloy with uniform composition. Ingot; perform heat treatment on the smelted alloy ingot: first perform solution treatment, maintain at a constant temperature of 1100°C for 6 hours, and then cool to room temperature in the furnace; then perform aging treatment, maintain at a constant temperature of 450°C for 4 hours, and then in the furnace After cooling to room temperature, a multi-component complex coherent precipitation-strengthened Cu-Ni-Al-Cr-Ti high temperature resistant alloy is obtained. The alloy was subjected to high-temperature tensile testing using a universal testing machine.
本发明的有益效果为:The beneficial effects of the present invention are:
1、Ti元素在γ'相中的固溶可提升γ'相的高温稳定性。单质Cr相与基体和γ'相完全共格,可提升合金中低温强度,可降低Cu-Cr合金中元素的扩散速率,抑制析出相的粗化,从而提高合金的抗软化能力,并可在高温下提升合金抗氧化性能。1. The solid solution of Ti element in the γ' phase can improve the high temperature stability of the γ' phase. The elemental Cr phase is completely consistent with the matrix and γ' phase, which can improve the low-temperature strength of the alloy, reduce the diffusion rate of elements in the Cu-Cr alloy, inhibit the coarsening of the precipitated phase, thereby improving the alloy's resistance to softening, and can Improve the oxidation resistance of alloys at high temperatures.
2、利用多组元复杂共格析出(~500nm的γ'相+~500nm的单质Cr相)提高了合金的高温强度,该合金常温强度高于760MPa,在800℃下,合金强度不低于200Mpa,远高于现役耐热铜合金。采用多种高温共格析出强化相的组合,可以在宽温区提升铜合金的高温性能。2. The high-temperature strength of the alloy is improved by using the complex coherent precipitation of multiple components (~500nm γ' phase + ~500nm elemental Cr phase). The normal temperature strength of the alloy is higher than 760MPa. At 800°C, the alloy strength is not less than 200Mpa, much higher than existing heat-resistant copper alloys. Using a combination of multiple high-temperature coherent precipitation strengthening phases can improve the high-temperature properties of copper alloys in a wide temperature range.
附图说明Description of the drawings
图1是时效处理后Cu61.76Ni27.56Al4.75Cr2.74Ti3.19(wt.%)合金的SEM二次电子图像。图2是时效处理后Cu61.76Ni27.56Al4.75Cr2.74Ti3.19(wt.%)合金的室温和800℃下的工程应力-应变曲线。Figure 1 is the SEM secondary electron image of Cu 61.76 Ni 27.56 Al 4.75 Cr 2.74 Ti 3.19 (wt.%) alloy after aging treatment. Figure 2 is the engineering stress-strain curve of Cu 61.76 Ni 27.56 Al 4.75 Cr 2.74 Ti 3.19 (wt.%) alloy at room temperature and 800°C after aging treatment.
具体实施方式Detailed ways
下面结合技术方案详细叙述本发明的具体实施例。Specific embodiments of the present invention are described in detail below in conjunction with technical solutions.
实施例1:Cu61.76Ni27.56Al4.75Cr2.74Ti3.19(wt.%)合金Example 1: Cu 61.76 Ni 27.56 Al 4.75 Cr 2.74 Ti 3.19 (wt.%) alloy
步骤一:合金制备Step 1: Alloy Preparation
根据合金成分Cu61.76Ni27.56Al4.75Cr2.74Ti3.19(wt.%),使用纯度为5N的Cu和Al、纯度为4N的Ni、Cr、Ti原料配制合金;采用非自耗真空电弧熔炼炉,通入高纯氩气保护,对配制好的合金原料进行反复熔炼5次,最终得到成分均匀的合金锭;随后将熔炼好的合金锭进行热处理(固溶处理:在1100℃下保温6h,随后在炉中冷却到室温;时效处理:在450℃下保温4h,随后在炉中冷却到室温)。According to the alloy composition Cu 61.76 Ni 27.56 Al 4.75 Cr 2.74 Ti 3.19 (wt.%), the alloy is prepared using raw materials of Cu and Al with a purity of 5N and Ni, Cr and Ti with a purity of 4N; a non-consumable vacuum arc melting furnace is used. Pass high-purity argon gas for protection, and repeatedly smelt the prepared alloy raw materials 5 times to finally obtain an alloy ingot with uniform composition; then the smelted alloy ingot is heat treated (solid solution treatment: heat preservation at 1100°C for 6 hours, and then Cool to room temperature in the furnace; aging treatment: hold at 450°C for 4 hours, then cool to room temperature in the furnace).
步骤二:合金结构和性能表征Step 2: Alloy structure and performance characterization
采用德国布鲁克D8 FOCUS X射线衍射仪和JSM-7900F型场发射扫描电子显微镜对合金进行组织和结构分析,可以确定合金中含有多尺度多相,其显微组织形貌如图1所示。采用中国深圳生产的UTM5504材料测试系统对合金样品在室温和800℃下分别进行了名义应变速率为1×10-4/s的拉伸试验。室温及高温拉伸试验根据金属材料室温及高温拉伸试验国家标准进行(GB/T 228.1-2010及GB/T 228.2-2015)。结果显示,合金室温拉伸强度不低于760MPa,800℃下拉伸强度不低于200MPa,如图2所示。The German Bruker D8 FOCUS X-ray diffractometer and JSM-7900F field emission scanning electron microscope were used to analyze the structure and structure of the alloy. It can be determined that the alloy contains multi-scale multi-phases, and its microstructure morphology is shown in Figure 1. The UTM5504 material testing system produced in Shenzhen, China, was used to conduct tensile tests on the alloy samples at room temperature and 800°C with a nominal strain rate of 1×10 -4 /s. The room temperature and high temperature tensile tests were conducted according to the national standards for room temperature and high temperature tensile tests of metal materials (GB/T 228.1-2010 and GB/T 228.2-2015). The results show that the tensile strength of the alloy at room temperature is not less than 760MPa, and the tensile strength at 800°C is not less than 200MPa, as shown in Figure 2.
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| CN117535553A (en) * | 2023-11-14 | 2024-02-09 | 安徽工程大学 | High-temperature oxidation resistant and high-temperature softening resistant high-strength Cu alloy and preparation method thereof |
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| CN103328665A (en) * | 2010-12-13 | 2013-09-25 | 日本精线株式会社 | Copper alloy and method for producing copper alloy |
| CN112210693A (en) * | 2020-09-30 | 2021-01-12 | 大连理工大学 | A kind of Cu-Ni-Al alloy with high temperature self-lubricating properties and preparation method thereof |
| CN115735017A (en) * | 2020-07-29 | 2023-03-03 | 同和金属技术有限公司 | Cu-Ni-Al-based copper alloy sheet material, manufacturing method thereof, and conductive spring member |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103328665A (en) * | 2010-12-13 | 2013-09-25 | 日本精线株式会社 | Copper alloy and method for producing copper alloy |
| CN115735017A (en) * | 2020-07-29 | 2023-03-03 | 同和金属技术有限公司 | Cu-Ni-Al-based copper alloy sheet material, manufacturing method thereof, and conductive spring member |
| CN112210693A (en) * | 2020-09-30 | 2021-01-12 | 大连理工大学 | A kind of Cu-Ni-Al alloy with high temperature self-lubricating properties and preparation method thereof |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN117535553A (en) * | 2023-11-14 | 2024-02-09 | 安徽工程大学 | High-temperature oxidation resistant and high-temperature softening resistant high-strength Cu alloy and preparation method thereof |
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