CN114480921A - Heat-resistant aluminum alloy monofilament material for overhead conductor and preparation method thereof - Google Patents
Heat-resistant aluminum alloy monofilament material for overhead conductor and preparation method thereof Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 67
- 239000004020 conductor Substances 0.000 title claims abstract description 29
- 239000000463 material Substances 0.000 title claims abstract description 26
- 238000002360 preparation method Methods 0.000 title claims abstract description 10
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 61
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 61
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 46
- 229910052738 indium Inorganic materials 0.000 claims abstract description 39
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 claims abstract description 39
- 229910052691 Erbium Inorganic materials 0.000 claims abstract description 25
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052742 iron Inorganic materials 0.000 claims abstract description 23
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 19
- 239000010703 silicon Substances 0.000 claims abstract description 19
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 16
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 16
- 239000011651 chromium Substances 0.000 claims abstract description 16
- 239000012535 impurity Substances 0.000 claims abstract description 16
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 16
- 239000010936 titanium Substances 0.000 claims abstract description 16
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 16
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 15
- 229910052796 boron Inorganic materials 0.000 claims abstract description 15
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 12
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims abstract description 11
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 11
- 239000011572 manganese Substances 0.000 claims abstract description 11
- 238000005096 rolling process Methods 0.000 claims abstract description 11
- 238000003723 Smelting Methods 0.000 claims abstract description 9
- 238000007670 refining Methods 0.000 claims abstract description 9
- 238000005266 casting Methods 0.000 claims abstract description 8
- 239000002994 raw material Substances 0.000 claims abstract description 4
- 229910000846 In alloy Inorganic materials 0.000 claims abstract description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract 9
- 229910045601 alloy Inorganic materials 0.000 claims description 31
- 239000000956 alloy Substances 0.000 claims description 31
- -1 manganese-aluminum-boron-erbium-indium-iron-silicon-vanadium-titanium-chromium-manganese Chemical compound 0.000 claims description 15
- 238000005275 alloying Methods 0.000 claims description 11
- DJPURDPSZFLWGC-UHFFFAOYSA-N alumanylidyneborane Chemical compound [Al]#B DJPURDPSZFLWGC-UHFFFAOYSA-N 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 9
- 238000001125 extrusion Methods 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 5
- 230000008018 melting Effects 0.000 claims description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 238000004321 preservation Methods 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 230000008569 process Effects 0.000 claims description 3
- 238000007664 blowing Methods 0.000 claims description 2
- 238000007872 degassing Methods 0.000 claims description 2
- VHHHONWQHHHLTI-UHFFFAOYSA-N hexachloroethane Chemical compound ClC(Cl)(Cl)C(Cl)(Cl)Cl VHHHONWQHHHLTI-UHFFFAOYSA-N 0.000 claims description 2
- 239000007788 liquid Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 229910052757 nitrogen Inorganic materials 0.000 claims description 2
- 238000003756 stirring Methods 0.000 claims description 2
- 238000005271 boronizing Methods 0.000 claims 1
- 239000000203 mixture Substances 0.000 abstract description 9
- 230000032683 aging Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 3
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 7
- 230000005540 biological transmission Effects 0.000 description 6
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 4
- 239000002245 particle Substances 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 230000001627 detrimental effect Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052761 rare earth metal Inorganic materials 0.000 description 2
- 150000002910 rare earth metals Chemical class 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 238000009835 boiling Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000002772 conduction electron Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000001808 coupling effect Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000003574 free electron Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
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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
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
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Abstract
一种架空导线用耐热铝合金单丝材料,其特征在于:成分体系包括铝、硼、铒、铟合金元素以及铁、硅、钒、钛、铬、锰原材料中的杂质元素;各质量分数的含量分别为:硼:0.01~0.02%,铒:0.08~0.12%,铟:0.05~0.1%,硅:0.03~0.06%,铁:0.08~1.2%,(钒+钛+铬+锰)≤0.005%,其余为铝的含量和不可避免的其它微量杂质。一种架空导线用耐热铝合金单丝材料的其制备方法,冶炼,精炼,浇铸,轧制,拉拔:的铝合金圆杆经过10‑15道次拉拔,获得铝合金单丝;时效处理。本发明的优点:提高耐热铝合金单丝导电率的同时对强度和耐热性均有有益作用;优化了制备工艺参数,由此制备出的耐热铝合金单丝可以在保证力学性能和耐热性能的前提下显著提高导电率至61.8%IACS。A heat-resistant aluminum alloy monofilament material for overhead conductors, characterized in that the composition system includes aluminum, boron, erbium, indium alloy elements and impurity elements in the raw materials of iron, silicon, vanadium, titanium, chromium, and manganese; The content of the iron is as follows: boron: 0.01~0.02%, erbium: 0.08~0.12%, indium: 0.05~0.1%, silicon: 0.03~0.06%, iron: 0.08~1.2%, (vanadium + titanium + chromium + manganese) ≤ 0.005%, the rest is the content of aluminum and other unavoidable trace impurities. A preparation method of a heat-resistant aluminum alloy monofilament material for overhead conductors, smelting, refining, casting, rolling, and drawing: After 10-15 passes of drawing, the aluminum alloy round rod obtained Aluminum alloy monofilament; aging treatment. The advantages of the invention are: while improving the electrical conductivity of the heat-resistant aluminum alloy monofilament, it has beneficial effects on strength and heat resistance; the preparation process parameters are optimized, and the heat-resistant aluminum alloy monofilament prepared thereby can ensure mechanical properties and On the premise of heat resistance, the electrical conductivity is significantly improved to 61.8% IACS.
Description
技术领域technical field
本发明属于电工导体材料技术领域,涉及发明架空导线用耐热铝合金单丝材料及其制备方法。The invention belongs to the technical field of electrical conductor materials, and relates to the invention of a heat-resistant aluminum alloy monofilament material for overhead wires and a preparation method thereof.
背景技术Background technique
目前,对电网的节能环保需要被重视,亟需开发和应用低损耗、高安全可靠性的高导电率铝合金导线。At present, the energy saving and environmental protection of the power grid needs to be paid attention to, and it is urgent to develop and apply high-conductivity aluminum alloy wires with low loss and high safety and reliability.
现役的钢芯铝绞线采用硬铝导体材料,耐热性差,载流量低,对于城网及农网改造工程而言,为扩大输电系统,采用现有的钢芯铝绞线必须增大导线截面,需要更换全部杆塔,重新建造,这对位于居民密集区的线路来说很难实现。因此,使用耐热铝合金导线,以更换相同截面积增容导线的方式加大传输容量成为有效的技术之一。The active steel-cored aluminum stranded wire is made of hard aluminum conductor material, which has poor heat resistance and low current-carrying capacity. For urban and rural power grid reconstruction projects, in order to expand the transmission system, the existing steel-cored aluminum stranded wire must increase the number of conductors. Section, need to replace all towers, rebuild, which is difficult to achieve for lines located in densely populated areas. Therefore, using heat-resistant aluminum alloy wires to increase the transmission capacity by replacing the same cross-sectional area capacity-enhancing wires has become one of the effective technologies.
耐热铝合金导线是一种性能良好的特种增容导线,采用大容量耐热铝合金导线进行现有线路增容改造,在尽量不更换杆塔的原则下,不但能提高线路的输送能力,并且能降低工程的整体造价。目前国内外市场中耐热铝合金导线产品主要以60%IACS耐热铝合金导线为主,61%IACS耐热铝合金导线应用相对较少,导线的的导电率低、输电线损高,难以满足远距离、大容量输电线路建设工程及电网增容改造工程的绿色发展需求。因此,在保证较高载流量的同时,如何提高耐热铝合金的导电率,减少输电线损,成为目前耐热铝导线最为迫切的技术需求。The heat-resistant aluminum alloy wire is a special capacity-enhancing wire with good performance. The large-capacity heat-resistant aluminum alloy wire is used to increase the capacity of the existing line. Under the principle of not replacing the tower as much as possible, it can not only improve the transmission capacity of the line, but also Can reduce the overall cost of the project. At present, the heat-resistant aluminum alloy wire products in the domestic and foreign markets are mainly 60% IACS heat-resistant aluminum alloy wires. The application of 61% IACS heat-resistant aluminum alloy wires is relatively small. Meet the green development needs of long-distance, large-capacity transmission line construction projects and power grid capacity expansion and reconstruction projects. Therefore, how to improve the electrical conductivity of heat-resistant aluminum alloy and reduce the loss of transmission lines while ensuring a high current carrying capacity has become the most urgent technical demand for heat-resistant aluminum wire.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于以纯度为99.7%的工业铝锭为原材料,开发出一种铝-铒-铟-硼耐热铝合金单丝材料,解决现有耐热铝合金单丝及导线产品导电率低、输电线损高的技术难题。The purpose of the present invention is to develop an aluminum-erbium-indium-boron heat-resistant aluminum alloy monofilament material using industrial aluminum ingots with a purity of 99.7% as a raw material, so as to solve the problem of the electrical conductivity of the existing heat-resistant aluminum alloy monofilament and wire products. The technical problems of low and high transmission line losses.
通过加入微量铒、铟、硼元素改善合金微观组织与综合性能,开发出导电率不低于61.8%IACS(20℃)、抗拉强度不低于160MPa、延伸率不低于2%、长期耐热温度为150℃(230℃保温1小时后的室温强度残存率≥90%)的架空导线用耐热铝合金导单丝。By adding trace amounts of erbium, indium, and boron to improve the microstructure and comprehensive properties of the alloy, a new product with a conductivity of not less than 61.8% IACS (20°C), a tensile strength of not less than 160MPa, an elongation of not less than 2%, and a long-term resistance Heat-resistant aluminum alloy monofilament for overhead conductors with a thermal temperature of 150°C (residual rate of room temperature strength after 230°C heat preservation for 1 hour ≥ 90%).
本发明提供了一种架空导线用耐热铝合金单丝材料,其特征在于:成分体系包括铝、硼、铒、铟合金元素以及铁、硅、钒、钛、铬、锰原材料中的杂质元素。The invention provides a heat-resistant aluminum alloy monofilament material for overhead wires, which is characterized in that the composition system includes aluminum, boron, erbium, indium alloy elements and impurity elements in the raw materials of iron, silicon, vanadium, titanium, chromium and manganese. .
各质量分数的含量分别为:硼:0.01~0.02%,铒:0.08~0.12%,铟:0.05~0.1%,硅:0.03~0.06%,铁:0.08~1.2%,(钒+钛+铬+锰)≤0.005%,其余为铝的含量和不可避免的其它微量杂质。The content of each mass fraction is: boron: 0.01-0.02%, erbium: 0.08-0.12%, indium: 0.05-0.1%, silicon: 0.03-0.06%, iron: 0.08-1.2%, (vanadium + titanium + chromium + Manganese)≤0.005%, the rest is the content of aluminum and other unavoidable trace impurities.
一种架空导线用耐热铝合金单丝材料的其制备方法,其特征在于:具体制备工艺如下:A preparation method of a heat-resistant aluminum alloy monofilament material for overhead wires, characterized in that: the specific preparation process is as follows:
(1)冶炼:纯度≥99.7%的工业纯铝锭加入熔炼炉中,熔炼温度为730~750℃;待纯铝完全熔化后,730~750℃加入铝-硼中间合金进行硼化处理;730~750℃加入铝-铒中间合金和纯铟锭,完全熔化后搅拌10~15m铟,静置20~30m铟。(1) Smelting: industrial pure aluminum ingots with a purity of ≥99.7% are added to the melting furnace, and the melting temperature is 730-750 ° C; Add aluminum-erbium intermediate alloy and pure indium ingot at ~750°C, stir 10-15m indium after complete melting, and let stand for 20-30m indium.
(2)精炼:710~730℃吹入氮气,吹气时间5~15m铟,或加入0.3%-0.5%的六氯乙烷进行除气精炼,静置10-20m铟后扒渣。(2) Refining: Blow in nitrogen at 710-730°C, blowing time 5-15m indium, or add 0.3%-0.5% hexachloroethane for degassing refining, let stand for 10-20m indium and then remove slag.
(3)浇铸:700~720℃将铝合金液浇入250~300℃预热的金属型模具,浇铸成横截面为边长20~25mm的铝锭。(3) Casting: pour the aluminum alloy liquid into a metal mold preheated at 250-300°C at 700-720°C, and cast it into an aluminum ingot with a side length of 20-25mm in cross section.
(4)轧制:将铝锭置于480~510℃保温3~6小时后进行轧制,经过6道次轧制成的铝合金圆杆,并喷水快速冷却。(4) Rolling: The aluminum ingot is placed at 480-510°C for 3-6 hours and then rolled, and rolled for 6 passes. Aluminum alloy round rod, and spray water for rapid cooling.
(5)拉拔:的铝合金圆杆经过10-15道次拉拔,获得铝合金单丝。(5) Drawing: After 10-15 passes of drawing, the aluminum alloy round rod is obtained. Aluminium alloy monofilament.
(6)时效:单丝在90~120℃下保温0.5~2小时。(6) Aging: The monofilament is kept at 90-120°C for 0.5-2 hours.
所述的步骤(4)也能通过挤压的方式实现,具体工艺为:将铝锭置于480~510℃保温3~6小时后进行轧制,经过挤压制成的铝合金圆杆,并喷水快速冷却。The step (4) can also be realized by extrusion, and the specific process is as follows: the aluminum ingot is placed at 480-510° C. for 3-6 hours and then rolled for 3-6 hours. Aluminum alloy round rod, and spray water for rapid cooling.
本发明的优点:Advantages of the present invention:
本发明所述的架空导线用耐热铝合金单丝材料及其制备方法,通过铒元和铟元素的复合添加,在一定的制备工艺下生成了铝3铒相和铟粒子,经过二者的耦合作用,在保证强度和耐热性的基础之上提高了导电率。The heat-resistant aluminum alloy monofilament material for overhead wires and the preparation method thereof of the present invention, through the compound addition of erbium element and indium element, under a certain preparation process, Al3 - erbium phase and indium particles are generated, and after the combination of the two elements The coupling effect improves electrical conductivity on the basis of ensuring strength and heat resistance.
由于在耐热合金中添加微量稀土铒元素,通过在轧制前的热处理可生成铝3铒相,该铝3铒相具有较好的高温稳定性,能够提高耐热铝合金单丝的强度和耐热性能,且铒元素可与铁、硅元素反应生成第二相,从铁、硅元素从溶质原子转变为第二相,降低了晶格畸变,提高耐热铝合金单丝导电率的同时对强度和耐热性均有有益作用;添加微量铟元素,经过时效后可析出铟粒子,提高耐热铝合金单丝的强度。在此合金成分配方基础之上,优化了制备工艺参数,由此制备出的耐热铝合金单丝可以在保证力学性能和耐热性能的前提下显著提高导电率至61.8%IACS(20℃)。Due to the addition of a trace amount of rare earth erbium element in the heat-resistant alloy, the aluminum 3 erbium phase can be generated by heat treatment before rolling. The aluminum 3 erbium phase has good high temperature stability, which can improve the strength and strength of the heat-resistant aluminum alloy monofilament. Heat resistance, and erbium element can react with iron and silicon elements to form a second phase, from iron and silicon elements from solute atoms to the second phase, which reduces lattice distortion and improves the conductivity of heat-resistant aluminum alloy monofilaments. It has beneficial effects on strength and heat resistance; adding trace indium elements can precipitate indium particles after aging, and improve the strength of heat-resistant aluminum alloy monofilaments. On the basis of this alloy composition formula, the preparation process parameters are optimized, and the heat-resistant aluminum alloy monofilament prepared from this can significantly increase the electrical conductivity to 61.8%IACS (20℃) on the premise of ensuring the mechanical properties and heat-resistant properties. .
具体实施方式Detailed ways
各合金元素的作用及机理如下:The role and mechanism of each alloying element are as follows:
硼(硼):在众多的影响因素中,化学成分是影响铝导体电导率最基本的因素,因此降低杂质元素对电导率的影响是提高铝导体电导率的关键之举。杂质元素如果以溶质原子状态存在,对导电性能的影响更大。硼化处理是降低铝合金导体材料有害杂质含量的一种有效方法,即在铝合金中加入一定量的硼元素后,能够和过渡族杂质元素铬、锰、钒、钛发生反应,使之由溶质原子态转变为化合态并沉积于熔体底部,从而提高铝合金的导电性能。Boron (boron): Among the many influencing factors, chemical composition is the most basic factor affecting the conductivity of aluminum conductors. Therefore, reducing the influence of impurity elements on conductivity is the key to improving the conductivity of aluminum conductors. If the impurity element exists in the state of solute atom, it has a greater influence on the electrical conductivity. Boriding treatment is an effective method to reduce the content of harmful impurities in aluminum alloy conductor materials, that is, after adding a certain amount of boron element to the aluminum alloy, it can react with the transition group impurity elements chromium, manganese, vanadium and titanium, so that The atomic state of the solute is transformed into a combined state and deposited at the bottom of the melt, thereby improving the electrical conductivity of the aluminum alloy.
铒(铒):本发明中加入稀土铒能显著提高铝合金的导电率、强度和耐热性。通过热处理铒与铝反应生成铝3铒沉淀相,从而提高合金强度;铝3铒为耐高温相,因此可保证合金的耐热性能;由于铒元素还能与铁、硅杂质元素反应,使杂质元素从溶质原子转变为第二相,降低晶格畸变,从而可提高合金的导电性能。Erbium (Erbium): The addition of rare earth erbium in the present invention can significantly improve the electrical conductivity, strength and heat resistance of the aluminum alloy. Through the heat treatment of erbium and aluminum, the precipitated phase of aluminum 3 erbium is formed, thereby improving the strength of the alloy; aluminum 3 erbium is a high temperature resistant phase, so the heat resistance of the alloy can be guaranteed; because erbium element can also react with iron and silicon impurity elements, making impurities Elements are transformed from solute atoms into second phases, reducing lattice distortion and thus improving the electrical conductivity of the alloy.
铟(铟):铟具有延展性好、可塑性强、熔点低、沸点高、低电阻、抗腐蚀优良特性,且具有较好的导电性能。本发明中加入铟后能够明显的改变合金微观组织和力学性能,通过时效处理铟元素会析出形成铟粒子,从而对铝合金起到强化作用。Indium (Indium): Indium has good ductility, strong plasticity, low melting point, high boiling point, low resistance, excellent corrosion resistance, and good electrical conductivity. In the present invention, the microstructure and mechanical properties of the alloy can be obviously changed after adding indium, and the indium element will be precipitated to form indium particles through aging treatment, thereby strengthening the aluminum alloy.
硅(硅):硅是工业铝中的杂质元素之一,硅可与铝、铁、RE元素反应生成第二相,降低晶格畸变,对铝合金导体材料的导电性能、力学性能和耐热性能起到有益作用。Silicon (silicon): Silicon is one of the impurity elements in industrial aluminum. Silicon can react with aluminum, iron, and RE elements to form a second phase, reduce lattice distortion, and improve the electrical conductivity, mechanical properties and heat resistance of aluminum alloy conductor materials. performance is beneficial.
铁(铁):铝中含有一定量的铁,是工业铝中的一种杂质。铁对铸造铝的力学性能是有害的,因为其通常以粗大的一次晶体出现,或以铝-铁-硅化合物形式存在,它们一定程度上都提高了铝的硬度,但使铝的塑性降低。研究表明,铁能提高铝导体强度,并不显著降低其导电性。但也有资料表明在实际生产中,铝导体中的铁过高则会使其电阻率显著升高,所以也应该注意控制铁的含量。Iron (iron): Aluminum contains a certain amount of iron, which is an impurity in industrial aluminum. Iron is detrimental to the mechanical properties of cast aluminum because it usually occurs as coarse primary crystals, or in the form of aluminum-iron-silicon compounds, which increase the hardness of aluminum to a certain extent, but reduce the plasticity of aluminum. Studies have shown that iron increases the strength of aluminum conductors without significantly reducing their conductivity. However, there are also data that in actual production, too high iron in aluminum conductors will significantly increase the resistivity, so attention should also be paid to controlling the content of iron.
铬、锰、钒、钛(锰、铬、钒、钛):这几种元素均为合金中的杂质元素,对铝合金的导电性能影响较大。铝导体中的钛、钒、锰、铬杂质元素在固溶态存在时,很容易吸收导体材料内的自由电子而填充它们不完整的电子层。这种传导电子数目的减少导致了铝导体导电性的降低。研究表明,每1%(铬+钛+锰+钒)的有害作用为每1%硅对铝导电性有害作用的5倍。由此能看出严格控制这几种元素的含量对保证铝导体的质量具有重要的实际应用意义。Chromium, manganese, vanadium, titanium (manganese, chromium, vanadium, titanium): these elements are impurity elements in the alloy, which have a great influence on the electrical conductivity of the aluminum alloy. When the titanium, vanadium, manganese, and chromium impurity elements in aluminum conductors exist in solid solution state, they can easily absorb free electrons in the conductor material and fill their incomplete electron layers. This reduction in the number of conduction electrons results in a reduction in the conductivity of the aluminum conductor. Research has shown that every 1% (chromium + titanium + manganese + vanadium) is 5 times more detrimental than every 1% silicon is to aluminum conductivity. It can be seen that strictly controlling the content of these elements has important practical significance for ensuring the quality of aluminum conductors.
实施例1Example 1
一种架空导线用耐热铝合金单丝材料,组分及其质量分数为:A heat-resistant aluminum alloy monofilament material for overhead conductors, the composition and mass fraction thereof are:
纯度为99.7%的纯铝锭,加入铝-硼中间合金、铝-铒中间合金和纯铟锭,使合金元素的最终含量如上所示。经过熔炼、精炼、铸造、轧制或挤压得到圆铝杆,经过10道次拉拔后得到铝合金单丝,单丝在120℃保温0.5小时后室温冷却。所制备出的耐热铝合金单丝导电率为61.8%IACS(20℃),抗拉强度为168MPa,延伸率为2.0%,230℃保温1小时后的室温强度残存率为92%,满足长期运行温度为150℃的要求。A pure aluminum ingot with a purity of 99.7% was added with aluminum-boron master alloy, aluminum-erbium master alloy and pure indium ingot, so that the final content of alloying elements was as shown above. After smelting, refining, casting, rolling or extrusion, the round aluminum rod is obtained, and it is obtained after 10 times of drawing. Aluminum alloy monofilament, the monofilament is kept at 120°C for 0.5 hours and then cooled at room temperature. The prepared heat-resistant aluminum alloy monofilament has a conductivity of 61.8% IACS (20°C), a tensile strength of 168MPa, an elongation of 2.0%, and a room temperature strength residual rate of 92% after being kept at 230°C for 1 hour. Operating temperature of 150°C is required.
实施例2Example 2
一种架空导线用耐热铝合金单丝材料,组分及其质量分数为:A heat-resistant aluminum alloy monofilament material for overhead conductors, the composition and mass fraction thereof are:
纯度为99.7%的纯铝锭,加入铝-硼中间合金、铝-铒中间合金和纯铟锭,使合金元素的最终含量如上所示。经过熔炼、精炼、铸造、轧制或挤压得到圆铝杆,经过15道次拉拔后得到铝合金单丝,单丝在90℃保温2小时后室温冷却。所制备出的耐热铝合金单丝导电率为61.92%IACS(20℃),抗拉强度为160MPa,延伸率为2.3%,230℃保温1小时后的室温强度残存率为90%,满足长期运行温度为150℃的要求。A pure aluminum ingot with a purity of 99.7% was added with aluminum-boron master alloy, aluminum-erbium master alloy and pure indium ingot, so that the final content of alloying elements was as shown above. After smelting, refining, casting, rolling or extrusion, the round aluminum rod is obtained, which is obtained after 15 times of drawing. Aluminum alloy monofilament, the monofilament is kept at 90°C for 2 hours and then cooled at room temperature. The prepared heat-resistant aluminum alloy monofilament has a conductivity of 61.92% IACS (20°C), a tensile strength of 160MPa, an elongation of 2.3%, and a room temperature strength residual rate of 90% after being kept at 230°C for 1 hour. Operating temperature of 150°C is required.
实施例3Example 3
一种架空导线用耐热铝合金单丝材料,组分及其质量分数为:A heat-resistant aluminum alloy monofilament material for overhead conductors, the composition and mass fraction thereof are:
纯度为99.7%的纯铝锭,加入铝-硼中间合金、铝-铒中间合金和纯铟锭,使合金元素的最终含量如上所示。经过熔炼、精炼、铸造、轧制或挤压得到圆铝杆,经过12道次拉拔后得到铝合金单丝,单丝在100℃保温1.5小时后室温冷却。所制备出的耐热铝合金单丝导电率为61.85%IACS(20℃),抗拉强度为166MPa,延伸率为2.1%,230℃保温1小时后的室温强度残存率为91%,满足长期运行温度为150℃的要求。A pure aluminum ingot with a purity of 99.7% was added with aluminum-boron master alloy, aluminum-erbium master alloy and pure indium ingot, so that the final content of alloying elements was as shown above. After smelting, refining, casting, rolling or extrusion, the round aluminum rod is obtained, which is obtained after 12 times of drawing. Aluminum alloy monofilament, the monofilament is kept at 100°C for 1.5 hours and then cooled at room temperature. The prepared heat-resistant aluminum alloy monofilament has a conductivity of 61.85% IACS (20°C), a tensile strength of 166MPa, an elongation of 2.1%, and a room temperature strength residual rate of 91% after 1 hour at 230°C. Operating temperature of 150°C is required.
实施例4Example 4
一种架空导线用耐热铝合金单丝材料,组分及其质量分数为:A heat-resistant aluminum alloy monofilament material for overhead conductors, the composition and mass fraction thereof are:
纯度为99.7%的纯铝锭,加入铝-硼中间合金、铝-铒中间合金和纯铟锭,使合金元素的最终含量如上所示。经过熔炼、精炼、铸造、轧制或挤压得到圆铝杆,经过13道次拉拔后得到铝合金单丝,单丝在110℃保温1小时后室温冷却。所制备出的耐热铝合金单丝导电率为61.82%IACS(20℃),抗拉强度为168MPa,延伸率为2.2%,230℃保温1小时后的室温强度残存率为92%,满足长期运行温度为150℃的要求。A pure aluminum ingot with a purity of 99.7% was added with aluminum-boron master alloy, aluminum-erbium master alloy and pure indium ingot, so that the final content of alloying elements was as shown above. After smelting, refining, casting, rolling or extrusion, the round aluminum rod is obtained, and it is obtained after 13 passes of drawing. Aluminum alloy monofilament, the monofilament is kept at 110°C for 1 hour and then cooled at room temperature. The prepared heat-resistant aluminum alloy monofilament has a conductivity of 61.82% IACS (20°C), a tensile strength of 168MPa, an elongation of 2.2%, and a room temperature strength residual rate of 92% after being kept at 230°C for 1 hour. Operating temperature of 150°C is required.
实施例5Example 5
一种架空导线用耐热铝合金单丝材料,组分及其质量分数为:A heat-resistant aluminum alloy monofilament material for overhead conductors, the composition and mass fraction thereof are:
纯度为99.7%的纯铝锭,加入铝-硼中间合金、铝-铒中间合金和纯铟锭,使合金元素的最终含量如上所示。经过熔炼、精炼、铸造、轧制或挤压得到圆铝杆,经过14道次拉拔后得到铝合金单丝,单丝在105℃保温1小时后室温冷却。所制备出的耐热铝合金单丝导电率为61.87%IACS(20℃),抗拉强度为163MPa,延伸率为2.2%,230℃保温1小时后的室温强度残存率为91%,满足长期运行温度为150℃的要求。A pure aluminum ingot with a purity of 99.7% was added with aluminum-boron master alloy, aluminum-erbium master alloy and pure indium ingot, so that the final content of alloying elements was as shown above. After smelting, refining, casting, rolling or extrusion, the round aluminum rod is obtained, which is obtained after 14 times of drawing. Aluminum alloy monofilament, the monofilament is kept at 105°C for 1 hour and then cooled at room temperature. The prepared heat-resistant aluminum alloy monofilament has a conductivity of 61.87% IACS (20°C), a tensile strength of 163MPa, an elongation of 2.2%, and a room temperature strength residual rate of 91% after 1 hour at 230°C. Operating temperature of 150°C is required.
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104946936A (en) * | 2015-05-29 | 2015-09-30 | 国网智能电网研究院 | High-conductivity rare earth duralumin monofilament material for overhead conductors |
CN107699755A (en) * | 2017-09-28 | 2018-02-16 | 山东南山铝业股份有限公司 | A kind of aluminium alloys for auto body and preparation method thereof |
CN109338166A (en) * | 2018-09-25 | 2019-02-15 | 全球能源互联网研究院有限公司 | A kind of Al-Er-B heat-resistant alloy monofilament and preparation method thereof |
US20190096538A1 (en) * | 2016-03-25 | 2019-03-28 | Central South University | Lightweight, high-conductivity, heat-resistant, and iron-containing aluminum wire, and preparation process thereof |
RU2749073C1 (en) * | 2020-10-30 | 2021-06-03 | Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский технологический университет "МИСиС" | Heat-resistant cast deformable aluminum alloys based on al-cu-y and al-cu-er systems (options) |
CN113674890A (en) * | 2021-07-14 | 2021-11-19 | 国网辽宁省电力有限公司营口供电公司 | A kind of high-conductivity heat-resistant aluminum alloy monofilament and preparation method thereof |
-
2022
- 2022-01-07 CN CN202210016836.5A patent/CN114480921A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104946936A (en) * | 2015-05-29 | 2015-09-30 | 国网智能电网研究院 | High-conductivity rare earth duralumin monofilament material for overhead conductors |
US20190096538A1 (en) * | 2016-03-25 | 2019-03-28 | Central South University | Lightweight, high-conductivity, heat-resistant, and iron-containing aluminum wire, and preparation process thereof |
CN107699755A (en) * | 2017-09-28 | 2018-02-16 | 山东南山铝业股份有限公司 | A kind of aluminium alloys for auto body and preparation method thereof |
CN109338166A (en) * | 2018-09-25 | 2019-02-15 | 全球能源互联网研究院有限公司 | A kind of Al-Er-B heat-resistant alloy monofilament and preparation method thereof |
RU2749073C1 (en) * | 2020-10-30 | 2021-06-03 | Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский технологический университет "МИСиС" | Heat-resistant cast deformable aluminum alloys based on al-cu-y and al-cu-er systems (options) |
CN113674890A (en) * | 2021-07-14 | 2021-11-19 | 国网辽宁省电力有限公司营口供电公司 | A kind of high-conductivity heat-resistant aluminum alloy monofilament and preparation method thereof |
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