[go: up one dir, main page]

CN108359852A - A kind of high silica/aluminum-based composite material and preparation method of graphene enhancing - Google Patents

A kind of high silica/aluminum-based composite material and preparation method of graphene enhancing Download PDF

Info

Publication number
CN108359852A
CN108359852A CN201810239677.9A CN201810239677A CN108359852A CN 108359852 A CN108359852 A CN 108359852A CN 201810239677 A CN201810239677 A CN 201810239677A CN 108359852 A CN108359852 A CN 108359852A
Authority
CN
China
Prior art keywords
aluminum
composite material
graphene
based composite
silicon
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
Application number
CN201810239677.9A
Other languages
Chinese (zh)
Other versions
CN108359852B (en
Inventor
姘翠附
水丽
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang Ligong University
Original Assignee
Shenyang Ligong University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shenyang Ligong University filed Critical Shenyang Ligong University
Priority to CN201810239677.9A priority Critical patent/CN108359852B/en
Publication of CN108359852A publication Critical patent/CN108359852A/en
Application granted granted Critical
Publication of CN108359852B publication Critical patent/CN108359852B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/05Mixtures of metal powder with non-metallic powder
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/002Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps

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)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Conductive Materials (AREA)

Abstract

A kind of high silica/aluminum-based composite material and preparation method of graphene enhancing, composite material contain ingredient by mass percentage:Silicon:15.0~20.0%, copper:2.0~4.0%, magnesium:0.5~1.0%, titanium:0.05~0.07%, boron:0.02~0.05%, graphene:0.3~0.6%, surplus is aluminium;Preparation method:1) by each ingredient of raw material, under gas shield, batch mixing obtains alloy powder;2) after alloy powder being pressed into blocky sintered blank material, vacuum-sintering obtains sintered blank;3) it is directed to the content of different silicon, quenching treatment+temper or multiway forging+annealing are carried out to it, the high silica/aluminum-based composite material of graphene enhancing is made;The method of the present invention makes reinforced phase distribution of particles evenly, and generates a large amount of dislocations in material internal, and dislocation born of the same parents are broken into subgrain or fine grain, reach refined crystalline strengthening;Its tensile strength is increased to 400MPa or more;The yield strength of material is increased to 236MPa or more simultaneously.

Description

一种石墨烯增强的高硅铝基复合材料及其制备方法A kind of graphene-reinforced high-silicon-aluminum matrix composite material and preparation method thereof

技术领域technical field

本发明涉及石墨烯应用技术的领域,特别涉及一种石墨烯增强的高硅铝基复合材料及其制备方法。The invention relates to the field of graphene application technology, in particular to a graphene-reinforced high-silicon-aluminum matrix composite material and a preparation method thereof.

背景技术Background technique

铝硅复合材料的比强度和比刚度高,热膨胀系数低,耐磨性及体积稳定性较好,并具有足够高的高温强度等优点在航空航天及汽车制造业中得到广泛应用。当硅含量超过铝硅共晶点成分12.6%后,虽然强度得到进一步提高,但由于镶嵌在基体中的硅颗粒尺寸增大且形状不规则,使其基体严重割裂,在硅相尖端处形成应力集中,降低了材料的抗拉强度,并且恶化材料的切削加工性能。目前常用铝硅基复合材料的硅含量基本低于共晶成分,铝硅基复合材料的增强体主要分为颗粒增强和纤维增强体,但其生产成本较高,且利用颗粒增强和纤维增强等进一步增强铝基复合材料的潜力越来越小。Aluminum-silicon composite materials have the advantages of high specific strength and specific stiffness, low thermal expansion coefficient, good wear resistance and volume stability, and high enough high temperature strength, and are widely used in aerospace and automobile manufacturing industries. When the silicon content exceeds 12.6% of the Al-Si eutectic point, although the strength is further improved, due to the increased size and irregular shape of the silicon particles embedded in the matrix, the matrix is severely split, and stress is formed at the tip of the silicon phase. Concentration reduces the tensile strength of the material and deteriorates the machinability of the material. At present, the silicon content of commonly used aluminum-silicon-based composite materials is basically lower than that of eutectic components. The reinforcements of aluminum-silicon-based composite materials are mainly divided into particle reinforcement and fiber reinforcement, but their production costs are high, and particle reinforcement and fiber reinforcement are used. The potential for further reinforcement of aluminum matrix composites is diminishing.

发明内容Contents of the invention

针对现有技术的不足,本发明提供一种石墨烯增强的高硅铝基复合材料及其制备方法。Aiming at the deficiencies of the prior art, the invention provides a graphene-reinforced high-silicon-aluminum matrix composite material and a preparation method thereof.

本发明的石墨烯增强的高硅铝基复合材料,含有成分按质量百分比为:硅:15.0~20.0%,铜:2.0~4.0%,镁:0.5~1.0%,钛:0.05~0.07%,硼:0.02~0.05%,石墨烯:0.3~0.6%,余量为铝。The graphene-enhanced high-silicon aluminum-based composite material of the present invention contains the following components by mass percentage: silicon: 15.0-20.0%, copper: 2.0-4.0%, magnesium: 0.5-1.0%, titanium: 0.05-0.07%, boron : 0.02 to 0.05%, graphene: 0.3 to 0.6%, and the balance is aluminum.

上述的石墨烯增强的高硅铝基复合材料,含有成分按质量百分比第一优选方案为:硅:15.0~18.0%,铜:3.0~4.0%,镁::0.5~1.0%,钛:0.05~0.06%,硼:0.02~0.03%,石墨烯:0.3~0.6%,余量为铝。The above-mentioned graphene-enhanced high-silicon-aluminum-based composite material contains the first preferred solution in terms of mass percentage: silicon: 15.0-18.0%, copper: 3.0-4.0%, magnesium: 0.5-1.0%, titanium: 0.05- 0.06%, boron: 0.02-0.03%, graphene: 0.3-0.6%, and the balance is aluminum.

上述的石墨烯增强的高硅铝基复合材料,含有成分按质量百分比第二优选方案:硅:18.0~20.0%,铜:2.0~3.0%,镁:0.5~1.0%,钛:0.06~0.07%,硼:0.03~0.05%,石墨烯:0.3~0.6%,余量为铝。The above-mentioned graphene-enhanced high-silicon aluminum-based composite material contains the second preferred solution in terms of mass percentage: silicon: 18.0-20.0%, copper: 2.0-3.0%, magnesium: 0.5-1.0%, titanium: 0.06-0.07% , boron: 0.03-0.05%, graphene: 0.3-0.6%, and the balance is aluminum.

本发明的石墨烯增强的高硅铝基复合材料的制备方法,具体包括如下步骤:The preparation method of the high-silicon-aluminum-based composite material reinforced by graphene of the present invention specifically comprises the following steps:

步骤1,混料:Step 1, mixing ingredients:

按石墨烯增强的高硅铝基复合材料的成分百分比配料后,在惰性气体或氮气保护下,装入混料罐,以30~50r/min的转速混料24~36h,静置1~2h后,再以30~40r/min的转速混料24~36h,静置散热至常温,得到混合均匀的合金粉末;After batching according to the composition percentage of the graphene-reinforced high-silicon-aluminum matrix composite material, under the protection of inert gas or nitrogen, put it into a mixing tank, mix at a speed of 30-50r/min for 24-36 hours, and let it stand for 1-2 hours Finally, mix the materials at a speed of 30-40r/min for 24-36 hours, let it cool down to room temperature, and obtain a uniformly mixed alloy powder;

步骤2,模压烧结:Step 2, molding and sintering:

(1)将混合均匀的合金粉末,在惰性气体保护下倒入压制模具,在220~250MPa保压5~8min,脱模得到块状烧结坯料;(1) Pour the uniformly mixed alloy powder into a pressing mold under the protection of an inert gas, hold the pressure at 220-250MPa for 5-8min, and demould to obtain a block-shaped sintered billet;

(2)对块状烧结坯料进行真空烧结,烧结温度560~575℃,烧结时间1.5~2h后,随炉冷却至室温,得烧结后的坯料;(2) Carry out vacuum sintering on the bulk sintered billet, the sintering temperature is 560-575°C, and the sintering time is 1.5-2 hours, then cool to room temperature with the furnace to obtain the sintered billet;

步骤3,后续热处理:Step 3, subsequent heat treatment:

针对步骤1中石墨烯增强的高硅铝基复合材料的成分配比,当15.0%≤硅的质量百分含量<18%时,采用如下处理(a)和(b):For the composition ratio of the graphene-enhanced high-silicon-aluminum matrix composite material in step 1, when 15.0%≤silicon mass percentage content<18%, the following treatments (a) and (b) are adopted:

(a)对烧结后的坯料,进行淬火处理,淬火温度为500℃,保温时间1~3h后水冷;(a) Quenching treatment is carried out on the sintered blank, the quenching temperature is 500°C, water cooling after holding time for 1 to 3 hours;

(b)将淬火后的坯料,进行回火处理,回火温度为150~200℃,保温时间1~3h后空冷,制得石墨烯增强的高硅铝基复合材料;(b) Tempering the quenched billet, the tempering temperature is 150-200°C, the holding time is 1-3h, and then air-cooled to obtain a graphene-enhanced high-silicon-aluminum matrix composite material;

针对步骤1中石墨烯增强的高硅铝基复合材料的成分配比,当18.0%≤硅的质量百分含量≤20.0%%时,采用如下处理(c)和(d):For the composition ratio of the graphene-enhanced high-silicon-aluminum-based composite material in step 1, when the mass percentage of 18.0%≤silicon≤20.0%%, the following treatments (c) and (d) are adopted:

(c)对烧结后的坯料进行多向锻造,锻造温度为480~500℃,变形速度为2~4mm/s,每道次锻造均改变锻造变形方向;(c) Multi-directional forging is carried out on the sintered blank, the forging temperature is 480-500°C, the deformation speed is 2-4mm/s, and the forging deformation direction is changed for each forging pass;

(d)将锻造后的坯料,进行退火处理,退火温度180~200℃,退火时间1~3h,制得石墨烯增强的高硅铝基复合材料。(d) performing annealing treatment on the forged billet at an annealing temperature of 180-200° C. and an annealing time of 1-3 hours to obtain a graphene-reinforced high-silicon-aluminum matrix composite material.

上述的石墨烯增强的高硅铝基复合材料的制备方法,其中:The preparation method of the above-mentioned graphene-reinforced high-silicon-aluminum-based composite material, wherein:

所述步骤1中,装入混料罐是在气体保护手套隔离箱中进行。In said step 1, loading into the mixing tank is carried out in a gas protection glove isolation box.

所述步骤1中,惰性气体为氩气。In the step 1, the inert gas is argon.

所述步骤1中,混料在三维空间运动混料球磨机中进行。In the step 1, the mixing is carried out in a three-dimensional space motion mixing ball mill.

所述步骤1中,以30~40r/min的转速混料24~36h后静置1~2h,目的是防止长时间连续旋转导致混料罐温度升高,引起罐内粉末出现冷焊现象,故停顿1~2h。In the step 1, the mixture is mixed at a speed of 30-40r/min for 24-36 hours and then left to stand for 1-2 hours. The purpose is to prevent the temperature of the mixing tank from rising due to continuous rotation for a long time, causing cold welding of the powder in the tank. Therefore, stop for 1 ~ 2h.

所述步骤2中,模压采用0.5MN双柱手动液压机。In the step 2, a 0.5MN double-column manual hydraulic press is used for molding.

所述步骤2中,真空烧结采用真空热压烧结炉。In the step 2, a vacuum hot-press sintering furnace is used for vacuum sintering.

所述步骤2中,烧结时间视合金粉末量确定。In the step 2, the sintering time is determined depending on the amount of alloy powder.

所述步骤3中,淬火处理采用电阻炉。淬火保温时间根据零件尺寸确定。In the step 3, a resistance furnace is used for the quenching treatment. The quenching and holding time is determined according to the size of the part.

所述步骤3中,多向锻造采用双柱手动液压机。In the step 3, a double-column manual hydraulic press is used for multi-directional forging.

所述步骤3中,共进行5~10道次锻造。In the step 3, a total of 5 to 10 passes of forging are carried out.

石墨烯本身是新型高性能纳米材料,强度高,柔韧性好,导电导热性能及光学性能优异,因其独特的结构而具有狄拉克-费米特性、奇异的量子霍尔效应和最小量子电导率等性质。与传统增强体相比,具有更大的比强度、比表面积和更低的生产成本,成为代替陶瓷纤维、碳纳米管和硬质颗粒的最理想的增强体材料。目前国内外常见的A390、ZL117、KS282等硅含量大约在15%~22%的高硅铝合金,其比强度更高、热膨胀系数更低,尤其适用于航模和摩托车活塞材料,但随着硅含量的提高,出现粗大多角形块状或板状硅颗粒,力学性能特别是伸长率显著降低。改善硅颗粒在铝基体中的形态及分布,使硅颗粒细化弥散分布对提高高硅铝基材料的机械性能至关重要。石墨烯的添加,明显改善了高硅铝基复合材料中硅颗粒的形态,对硅颗粒有细化效果,提高了铝硅复合材料的综合力学性能。Graphene itself is a new type of high-performance nanomaterial with high strength, good flexibility, excellent electrical and thermal conductivity and optical properties. Because of its unique structure, it has Dirac-Fermi characteristics, singular quantum Hall effect and minimum quantum conductivity. and other properties. Compared with traditional reinforcements, it has larger specific strength, specific surface area and lower production cost, making it the most ideal reinforcement material to replace ceramic fibers, carbon nanotubes and hard particles. At present, high-silicon aluminum alloys such as A390, ZL117, and KS282, which are common at home and abroad, have a silicon content of about 15% to 22%, which has higher specific strength and lower thermal expansion coefficient, and is especially suitable for aircraft model and motorcycle piston materials. As the silicon content increases, coarse polygonal block or plate silicon particles appear, and the mechanical properties, especially the elongation, decrease significantly. Improving the morphology and distribution of silicon particles in the aluminum matrix and making the silicon particles fine and dispersed is crucial to improving the mechanical properties of high-silicon-aluminum-based materials. The addition of graphene significantly improves the morphology of silicon particles in the high-silicon-aluminum matrix composite material, has a refinement effect on silicon particles, and improves the comprehensive mechanical properties of the aluminum-silicon composite material.

本发明的石墨烯增强的高硅铝基复合材料及其制备方法,与现有技术相比,有益效果为:Compared with the prior art, the graphene-reinforced high-silicon aluminum-based composite material and the preparation method thereof of the present invention have the beneficial effects of:

本发明通过选择特定的配方制备出一种具有较高强度和硬度的高性能石墨烯增强高硅铝基复合材料,同时具有轻量、耐磨损、导热系数高、低热膨胀系数、良好切削加工性能的优点,并且还具有优异的导热性,可广泛应用于航空航天、精密仪器和汽车制造领域。The invention prepares a high-performance graphene-reinforced high-silicon-aluminum matrix composite material with high strength and hardness by selecting a specific formula, and also has light weight, wear resistance, high thermal conductivity, low thermal expansion coefficient, and good cutting process Performance advantages, and also has excellent thermal conductivity, can be widely used in aerospace, precision instruments and automobile manufacturing fields.

添加石墨烯纳米材料提高了高硅铝基复合材料的拉伸强度和屈服强度,且其延伸率也有提高。石墨烯纳米片的加入,使高硅铝基复合材料组织中的硅颗粒细化并弥散分布,材料的抗拉强度从328MPa提高到400MPa以上,增加了20%以上;同时材料的屈服强度从202MPa以上提高到236MPa以上。其改善的效果明显优于其他材料增强高硅铝基复合材料的强化效果。石墨烯的添加改善了硅颗粒的形态和分布,使其屈服强度和塑性均获得改善。The addition of graphene nanomaterials improves the tensile strength and yield strength of the high-silicon-aluminum matrix composites, and its elongation also increases. The addition of graphene nanosheets makes the silicon particles in the high-silicon-aluminum matrix composite structure fine and dispersed, and the tensile strength of the material increases from 328MPa to over 400MPa, an increase of more than 20%; at the same time, the yield strength of the material increases from 202MPa The above increases to above 236MPa. Its improved effect is obviously better than that of other materials reinforced high-silicon-aluminum matrix composites. The addition of graphene improved the morphology and distribution of silicon particles, resulting in improved yield strength and plasticity.

随着Si含量的提高,复合材料抗热裂能力提高,为使石墨烯铝硅基多元复合材料的强度得到最大的释放,针对Si含量接近20%的石墨烯增强高硅铝基复合材料采用多向锻造工艺,可以使增强相颗粒分布更均匀,并且在材料内部产生大量位错,位错胞破碎成亚晶或细晶,达到细晶强化的效果。With the increase of Si content, the thermal cracking resistance of the composite material is improved. In order to maximize the strength of the graphene-aluminum-silicon-based multi-component composite material, for graphene-reinforced high-silicon-aluminum-based composite materials with a Si content close to 20%, multiple The forging process can make the distribution of reinforcement phase particles more uniform, and generate a large number of dislocations inside the material, and the dislocation cells are broken into sub-grains or fine grains to achieve the effect of fine-grain strengthening.

附图说明Description of drawings

图1本发明实施例1制备的石墨烯增强的高硅铝基复合材料的微观组织形貌;The microstructure morphology of the high-silicon-aluminum matrix composite material prepared by Fig. 1 embodiment 1 of the present invention reinforced by graphene;

图2本发明实施例2制备的石墨烯增强的高硅铝基复合材料的微观组织形貌;The microstructure morphology of the high-silicon-aluminum-based composite material reinforced by graphene reinforced by Fig. 2 of the present invention embodiment 2;

图3本发明实施例3制备的石墨烯增强的高硅铝基复合材料的微观组织形貌;The microstructure morphology of the high-silicon-aluminum matrix composite material prepared by Fig. 3 embodiment 3 of the present invention reinforced by graphene;

图4本发明实施例4制备的石墨烯增强的高硅铝基复合材料的微观组织形貌。Fig. 4 is the microstructure morphology of the graphene-reinforced high-silicon-aluminum matrix composite material prepared in Example 4 of the present invention.

具体实施方式Detailed ways

实施例1Example 1

一种石墨烯增强的高硅铝基复合材料,含有成分按质量百分比为:硅:15.0%,铜:4.0%,镁:1.0%,钛:0.06%,硼:0.03%,石墨烯:0.5%,铝为余量。A graphene-reinforced high-silicon-aluminum matrix composite material, containing components by mass percentage: silicon: 15.0%, copper: 4.0%, magnesium: 1.0%, titanium: 0.06%, boron: 0.03%, graphene: 0.5% , with aluminum as the balance.

上述的石墨烯增强的高硅铝基复合材料的制备方法,具体包括如下步骤:The preparation method of the above-mentioned graphene-enhanced high-silicon-aluminum-based composite material specifically comprises the following steps:

步骤1,混料:Step 1, mixing ingredients:

石墨烯增强的高硅铝基复合材料的成分按质量百分比计,硅 15.0%,铜 4.0%,镁 1.0%,钛 0.06%,硼 0.03%,石墨烯 0.5%,铝为余量。The composition of the graphene-reinforced high-silicon-aluminum matrix composite is 15.0% silicon, 4.0% copper, 1.0% magnesium, 0.06% titanium, 0.03% boron, 0.5% graphene, and aluminum as the balance.

在氩气保护下的手套隔离箱中按上述质量百分比将700目的各种原材料粉末进行配料并装入混料罐,再将混料罐装配在球磨机上,然后在三维空间运动混料球磨机中,以40r/min的转速混料30h,静置1h后,目的是防止长时间连续旋转导致混料罐温度升高,引起罐内粉末出现冷焊现象,再次重复连续旋转混料30h,静置散热至常温后从球磨机卸下,得到混合均匀的合金粉末;In the glove isolation box under the protection of argon, the 700-mesh various raw material powders are batched according to the above mass percentages and put into the mixing tank, and then the mixing tank is assembled on the ball mill, and then in the three-dimensional space motion mixing ball mill , mixed at a speed of 40r/min for 30 hours, and after standing for 1 hour, the purpose is to prevent the temperature of the mixing tank from rising due to continuous rotation for a long time, causing cold welding of the powder in the tank, repeat the continuous rotation and mixing for 30 hours, and let it stand After dissipating heat to normal temperature, it is unloaded from the ball mill to obtain evenly mixed alloy powder;

步骤2,模压烧结:Step 2, molding and sintering:

(1)将混合均匀的合金粉末在氩气保护下倒入压制模具,采用0.5MN双柱手动液压机,在240MPa保压5min,脱模得到块状烧结坯料;(1) Pour the uniformly mixed alloy powder into a pressing mold under the protection of argon, adopt a 0.5MN double-column manual hydraulic press, hold the pressure at 240MPa for 5min, and demould to obtain a block-shaped sintered blank;

(2)采用真空热压烧结炉对块状烧结坯料进行真空烧结,烧结温度560℃,烧结时间2h后,随炉冷却至室温,得烧结后的坯料;(2) Carry out vacuum sintering to block-shaped sintered blanks in a vacuum hot-pressing sintering furnace at a sintering temperature of 560° C. and after sintering for 2 hours, cool to room temperature with the furnace to obtain a sintered blank;

步骤3,后续热处理:Step 3, subsequent heat treatment:

(1)对烧结后的坯料,采用电阻炉进行淬火处理,淬火温度为500℃,保温时间2h(可根据烧结零件尺寸确定)后水冷;(1) For the sintered billet, use a resistance furnace for quenching treatment, the quenching temperature is 500 ° C, the holding time is 2 hours (can be determined according to the size of the sintered part), and then water cooling;

(2)将淬火后的坯料,进行回火处理,回火温度为180℃,保温时间2h后空冷,制得石墨烯增强的高硅铝基复合材料;其微观组织见附图1,图中深色粒状物是Si颗粒,灰白色区域多为Al2Cu相。(2) Tempering the quenched billet, the tempering temperature is 180°C, air cooling after 2 hours of holding time, and a graphene-enhanced high-silicon-aluminum matrix composite material is obtained; its microstructure is shown in Figure 1, in the figure The dark particles are Si particles, and the off-white area is mostly Al 2 Cu phase.

实施例2Example 2

一种石墨烯增强的高硅铝基复合材料,含有成分按质量百分比为:硅:16.0%,铜:3.5%,镁:1.0%,钛:0.06%,硼:0.03%,石墨烯:0.3%,铝为余量。A graphene-reinforced high-silicon-aluminum matrix composite material, containing components by mass percentage: silicon: 16.0%, copper: 3.5%, magnesium: 1.0%, titanium: 0.06%, boron: 0.03%, graphene: 0.3% , with aluminum as the balance.

上述的石墨烯增强的高硅铝基复合材料的制备方法,具体包括如下步骤:The preparation method of the above-mentioned graphene-enhanced high-silicon-aluminum-based composite material specifically comprises the following steps:

步骤1,混料:Step 1, mixing ingredients:

石墨烯增强的高硅铝基复合材料的成分按质量百分比计,硅 16.0%,铜 3.5%,镁 1.0%,钛 0.06%,硼 0.03%,石墨烯 0.3%,铝为余量。The composition of the graphene-reinforced high-silicon-aluminum matrix composite is 16.0% silicon, 3.5% copper, 1.0% magnesium, 0.06% titanium, 0.03% boron, 0.3% graphene, and aluminum as the balance.

在氩气保护下的手套隔离箱中按上述质量百分比将700目的各种原材料粉末进行配料并装入混料罐,再将混料罐装配在球磨机上,然后在三维空间运动混料球磨机中,以40r/min的转速混料30h,静置1h后,目的是防止长时间连续旋转导致混料罐温度升高,引起罐内粉末出现冷焊现象,再次重复连续旋转混料30h,静置散热至常温后从球磨机卸下,得到混合均匀的合金粉末;In the glove isolation box under the protection of argon, the 700-mesh various raw material powders are batched according to the above mass percentages and put into the mixing tank, and then the mixing tank is assembled on the ball mill, and then in the three-dimensional space motion mixing ball mill , mixed at a speed of 40r/min for 30 hours, and after standing for 1 hour, the purpose is to prevent the temperature of the mixing tank from rising due to continuous rotation for a long time, causing cold welding of the powder in the tank, repeat the continuous rotation and mixing for 30 hours, and let it stand After dissipating heat to normal temperature, it is unloaded from the ball mill to obtain evenly mixed alloy powder;

步骤2,模压烧结:Step 2, molding and sintering:

(1)将混合均匀的合金粉末在氩气保护下倒入压制模具,采用0.5MN双柱手动液压机,在240MPa保压5min,脱模得到块状烧结坯料;(1) Pour the uniformly mixed alloy powder into a pressing mold under the protection of argon, adopt a 0.5MN double-column manual hydraulic press, hold the pressure at 240MPa for 5min, and demould to obtain a block-shaped sintered blank;

(2)采用真空热压烧结炉对块状烧结坯料进行真空烧结,烧结温度575℃,烧结时间1.52h后,随炉冷却至室温,得烧结后的坯料;(2) Carry out vacuum sintering to block-shaped sintered billets in a vacuum hot-pressing sintering furnace, the sintering temperature is 575°C, and the sintering time is 1.52 hours, and then cooled to room temperature with the furnace to obtain a sintered billet;

步骤3,后续热处理:Step 3, subsequent heat treatment:

(1)对烧结后的坯料,采用电阻炉进行淬火处理,淬火温度为500℃,保温时间2h(可根据烧结零件尺寸确定)后水冷;(1) For the sintered billet, use a resistance furnace for quenching treatment, the quenching temperature is 500 ° C, the holding time is 2 hours (can be determined according to the size of the sintered part), and then water cooling;

(2)将淬火后的坯料,进行回火处理,回火温度为180℃,保温时间2h后空冷,制得石墨烯增强的高硅铝基复合材料;其微观组织见附图2。(2) Tempering the quenched blank, the tempering temperature is 180°C, air cooling after 2 hours of holding time, and a graphene-reinforced high-silicon-aluminum matrix composite material is obtained; its microstructure is shown in Figure 2.

实施例3Example 3

一种石墨烯增强的高硅铝基复合材料,含有成分按质量百分比为:硅:20.0%,铜:2.0%,镁:1.0%,钛:0.07%,硼:0.04%,石墨烯:0.6%,铝为余量。A graphene-reinforced high-silicon-aluminum matrix composite material, containing components by mass percentage: silicon: 20.0%, copper: 2.0%, magnesium: 1.0%, titanium: 0.07%, boron: 0.04%, graphene: 0.6% , with aluminum as the balance.

上述的石墨烯增强的高硅铝基复合材料的制备方法,具体包括如下步骤:The preparation method of the above-mentioned graphene-enhanced high-silicon-aluminum-based composite material specifically comprises the following steps:

步骤1,混料:Step 1, mixing ingredients:

石墨烯增强的高硅铝基复合材料的成分按质量百分比计,硅 20.0%,铜 2.0%,镁 1.0%,钛 0.07%,硼 0.04%,石墨烯 0.6%,铝为余量。The composition of the graphene-reinforced high-silicon-aluminum matrix composite is 20.0% silicon, 2.0% copper, 1.0% magnesium, 0.07% titanium, 0.04% boron, 0.6% graphene, and aluminum as the balance.

在氩气保护下的手套隔离箱中按上述质量百分比将700目的各种原材料粉末进行配料并装入混料罐,再将混料罐装配在球磨机上,然后在三维空间运动混料球磨机中,以40r/min的转速混料30h,静置1h后,目的是防止长时间连续旋转导致混料罐温度升高,引起罐内粉末出现冷焊现象,再次重复连续旋转混料30h,静置散热至常温后从球磨机卸下,得到混合均匀的合金粉末;In the glove isolation box under the protection of argon, the 700-mesh various raw material powders are batched according to the above mass percentages and put into the mixing tank, and then the mixing tank is assembled on the ball mill, and then in the three-dimensional space motion mixing ball mill , mixed at a speed of 40r/min for 30 hours, and after standing for 1 hour, the purpose is to prevent the temperature of the mixing tank from rising due to continuous rotation for a long time, causing cold welding of the powder in the tank, repeat the continuous rotation and mixing for 30 hours, and let it stand After dissipating heat to normal temperature, it is unloaded from the ball mill to obtain evenly mixed alloy powder;

步骤2,模压烧结:Step 2, molding and sintering:

(1)将混合均匀的合金粉末在氩气保护下倒入压制模具,采用0.5MN双柱手动液压机,在240MPa保压5min,脱模得到块状烧结坯料;(1) Pour the uniformly mixed alloy powder into a pressing mold under the protection of argon, adopt a 0.5MN double-column manual hydraulic press, hold the pressure at 240MPa for 5min, and demould to obtain a block-shaped sintered blank;

(2)采用真空热压烧结炉对块状烧结坯料进行真空烧结,烧结温度565℃,烧结时间1.8h后,随炉冷却至室温,得烧结后的坯料;(2) Carry out vacuum sintering to block-shaped sintered billets in a vacuum hot-pressing sintering furnace, the sintering temperature is 565°C, and the sintering time is 1.8 hours, and then cooled to room temperature with the furnace to obtain a sintered billet;

步骤3,后续热处理:Step 3, subsequent heat treatment:

(1)采用双柱手动液压机,对烧结后的坯料进行多向锻造,共进行5道次锻造,锻造温度为490℃,变形速度为3mm/s,每道次锻造均改变锻造变形方向;(1) Using a double-column manual hydraulic press, multi-directional forging is carried out on the sintered billet, and a total of 5 forging passes are carried out. The forging temperature is 490°C, and the deformation speed is 3mm/s. The forging deformation direction is changed for each forging pass;

(2)将锻造后的坯料,进行退火处理,退火温度200℃,退火时间2h,制得石墨烯增强的高硅铝基复合材料。其微观组织见附图3。(2) Annealing the forged billet with an annealing temperature of 200° C. and an annealing time of 2 hours to prepare a graphene-reinforced high-silicon-aluminum matrix composite material. Its microstructure is shown in Figure 3.

实施例4Example 4

一种石墨烯增强的高硅铝基复合材料,含有成分按质量百分比为:硅:19.0%,铜:2.5%,镁:1.0%,钛:0.06%,硼:0.04%,石墨烯:0.5%,铝为余量。A graphene-reinforced high-silicon-aluminum matrix composite material, containing components by mass percentage: silicon: 19.0%, copper: 2.5%, magnesium: 1.0%, titanium: 0.06%, boron: 0.04%, graphene: 0.5% , with aluminum as the balance.

上述的石墨烯增强的高硅铝基复合材料的制备方法,具体包括如下步骤:The preparation method of the above-mentioned graphene-enhanced high-silicon-aluminum-based composite material specifically comprises the following steps:

步骤1,混料:Step 1, mixing ingredients:

石墨烯增强的高硅铝基复合材料的成分按质量百分比计,硅 19.0%,铜 2.5%,镁 1.0%,钛 0.06%,硼 0.04%,石墨烯 0.5%,铝为余量。The composition of the graphene-reinforced high-silicon-aluminum matrix composite is 19.0% silicon, 2.5% copper, 1.0% magnesium, 0.06% titanium, 0.04% boron, 0.5% graphene, and aluminum as the balance.

在氩气保护下的手套隔离箱中按上述质量百分比将700目的各种原材料粉末进行配料并装入混料罐,再将混料罐装配在球磨机上,然后在三维空间运动混料球磨机中,以40r/min的转速混料30h,静置1h后,目的是防止长时间连续旋转导致混料罐温度升高,引起罐内粉末出现冷焊现象,再次重复连续旋转混料30h,静置散热至常温后从球磨机卸下,得到混合均匀的合金粉末;In the glove isolation box under the protection of argon, the 700-mesh various raw material powders are batched according to the above mass percentages and put into the mixing tank, and then the mixing tank is assembled on the ball mill, and then in the three-dimensional space motion mixing ball mill , mixed at a speed of 40r/min for 30 hours, and after standing for 1 hour, the purpose is to prevent the temperature of the mixing tank from rising due to continuous rotation for a long time, causing cold welding of the powder in the tank, repeat the continuous rotation and mixing for 30 hours, and let it stand After dissipating heat to normal temperature, it is unloaded from the ball mill to obtain evenly mixed alloy powder;

步骤2,模压烧结:Step 2, molding and sintering:

(1)将混合均匀的合金粉末在氩气保护下倒入压制模具,采用0.5MN双柱手动液压机,在240MPa保压5min,脱模得到块状烧结坯料;(1) Pour the uniformly mixed alloy powder into a pressing mold under the protection of argon, adopt a 0.5MN double-column manual hydraulic press, hold the pressure at 240MPa for 5min, and demould to obtain a block-shaped sintered billet;

(2)采用真空热压烧结炉对块状烧结坯料进行真空烧结,烧结温度570℃,烧结时间1.5~2h后,随炉冷却至室温,得烧结后的坯料;(2) Carry out vacuum sintering of block-shaped sintered blanks in a vacuum hot-pressing sintering furnace, the sintering temperature is 570°C, and the sintering time is 1.5 to 2 hours, and then cooled to room temperature with the furnace to obtain a sintered blank;

步骤3,后续热处理:Step 3, subsequent heat treatment:

(1)采用双柱手动液压机,对烧结后的坯料进行多向锻造,共进行10道次锻造,锻造温度为490℃,变形速度为3mm/s,每道次锻造均改变锻造变形方向;(1) Using a double-column manual hydraulic press, multi-directional forging is carried out on the sintered billet, and a total of 10 forging passes are carried out. The forging temperature is 490°C and the deformation speed is 3mm/s. The forging deformation direction is changed for each forging pass;

(2)将锻造后的坯料,进行退火处理,退火温度200℃,退火时间2h,制得石墨烯增强的高硅铝基复合材料。其微观组织见附图4。(2) Annealing the forged billet with an annealing temperature of 200° C. and an annealing time of 2 hours to prepare a graphene-reinforced high-silicon-aluminum matrix composite material. Its microstructure is shown in Figure 4.

Claims (7)

1. a kind of high silica/aluminum-based composite material of graphene enhancing, which is characterized in that be by mass percentage containing ingredient:Silicon: 15.0~20.0%, copper:2.0~4.0%, magnesium:0.5~1.0%, titanium:0.05~0.07%, boron:0.02~0.05%, graphite Alkene:0.3~0.6%, surplus is aluminium.
2. the high silica/aluminum-based composite material of graphene enhancing according to claim 1, which is characterized in that press matter containing ingredient Measuring percentage is:Silicon:15.0~18.0%, copper:3.0~4.0%, magnesium::0.5~1.0%, titanium:0.05~0.06%, boron: 0.02~0.03%, graphene:0.3~0.6%, surplus is aluminium.
3. the high silica/aluminum-based composite material of graphene enhancing according to claim 1, which is characterized in that press matter containing ingredient Measuring percentage is:Silicon:18.0~20.0%, copper:2.0~3.0%, magnesium:0.5~1.0%, titanium:0.06~0.07%, boron: 0.03~0.05%, graphene:0.3~0.6%, surplus is aluminium.
4. the preparation method of the high silica/aluminum-based composite material of graphene enhancing described in claim 1, which is characterized in that specific packet Include following steps:
Step 1, batch mixing:
After percentage composition dispensing by the high silica/aluminum-based composite material of graphene enhancing, under inert gas or nitrogen protection, It is packed into mixing tank, with rotating speed 24~36h of batch mixing of 30~50r/min, after standing 1~2h, then it is mixed with the rotating speed of 30~40r/min Expect 24~36h, stands heat dissipation to room temperature, obtain uniformly mixed alloy powder;
Step 2, molding sintering:
(1) alloy powder that will be uniformly mixed, pours into compacting tool set under inert gas protection, 220~250MPa pressurizes 5~ 8min, demoulding obtain blocky sintering blank;
(2) vacuum-sintering, 560~575 DEG C of sintering temperature, after 1.5~2h of sintering time, with furnace cooling are carried out to bulk sintering blank But to room temperature, sintered blank is obtained;
Step 3, subsequent heat treatment:
For the composition proportion for the high silica/aluminum-based composite material that graphene in step 1 enhances, when the quality percentage of 15.0%≤silicon When content < 18%, using following processing (a) and (b):
(a) to sintered blank, quenching treatment is carried out, hardening heat is 500 DEG C, water cooling after 1~3h of soaking time;
(b) by quenched blank, temper is carried out, temperature is 150~200 DEG C, air-cooled after 1~3h of soaking time, The high silica/aluminum-based composite material of graphene enhancing is made;
For the composition proportion for the high silica/aluminum-based composite material that graphene in step 1 enhances, when the quality percentage of 18.0%≤silicon When content≤20.0%%, using following processing (c) and (d):
(c) multiway forging is carried out to sintered blank, forging temperature is 480~500 DEG C, and deformation velocity is 2~4mm/s, often Passage forging changes forging deformation direction;
(d) it by the blank after forging, is made annealing treatment, 180~200 DEG C, 1~3h of annealing time of annealing temperature, graphite is made The high silica/aluminum-based composite material of alkene enhancing.
5. the preparation method of the high silica/aluminum-based composite material of graphene enhancing described in claim 1, which is characterized in that the step In rapid 1, being fitted into mixing tank is carried out in gas shield gloves shielded box;Batch mixing in three-dimensional space motion batch mixing ball mill into Row;In the step 2, molding uses 0.5MN double-column hand-operated hydraulic press, vacuum-sintering to use vacuum sintering funace;The step In rapid 3, quenching treatment uses resistance furnace, multiway forging to use double-column hand-operated hydraulic press.
6. the preparation method of the high silica/aluminum-based composite material of graphene enhancing described in claim 1, which is characterized in that the step In rapid 1, inert gas is argon gas.
7. the preparation method of the high silica/aluminum-based composite material of graphene enhancing described in claim 1, which is characterized in that the step In rapid 3, the forging of 5~10 passages is carried out altogether.
CN201810239677.9A 2018-03-22 2018-03-22 A kind of graphene-enhanced high-silicon aluminum-based composite material and preparation method thereof Expired - Fee Related CN108359852B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810239677.9A CN108359852B (en) 2018-03-22 2018-03-22 A kind of graphene-enhanced high-silicon aluminum-based composite material and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810239677.9A CN108359852B (en) 2018-03-22 2018-03-22 A kind of graphene-enhanced high-silicon aluminum-based composite material and preparation method thereof

Publications (2)

Publication Number Publication Date
CN108359852A true CN108359852A (en) 2018-08-03
CN108359852B CN108359852B (en) 2020-06-16

Family

ID=63000732

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810239677.9A Expired - Fee Related CN108359852B (en) 2018-03-22 2018-03-22 A kind of graphene-enhanced high-silicon aluminum-based composite material and preparation method thereof

Country Status (1)

Country Link
CN (1) CN108359852B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111636006A (en) * 2020-05-29 2020-09-08 香港生产力促进局 A kind of aluminum silicon alloy graphite composite thermal conductive material and its preparation and application
CN112143944A (en) * 2020-08-17 2020-12-29 福建祥鑫股份有限公司 Graphene-modified silicon-aluminum composite material and preparation method thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105112732A (en) * 2015-06-25 2015-12-02 中国航空工业集团公司北京航空材料研究院 Graphene/aluminium alloy composite
CN105112699A (en) * 2015-06-25 2015-12-02 中国航空工业集团公司北京航空材料研究院 Preparation method of graphene/aluminum alloy composite material
CN105734360A (en) * 2016-03-31 2016-07-06 山东正凯机械科技有限公司 Preparation method of Si-Al alloy material for automobile brake disc
CN106521220A (en) * 2016-10-11 2017-03-22 常州大学 Novel graphene Al-Cu intermediate alloy preparation method
CN106567785A (en) * 2016-11-10 2017-04-19 无锡市明盛强力风机有限公司 Graphene-doped aluminum alloy air cylinder cover
CN107299257A (en) * 2017-05-16 2017-10-27 苏州莱特复合材料有限公司 A kind of modified graphene reinforced aluminum matrix composites and preparation method thereof

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105112732A (en) * 2015-06-25 2015-12-02 中国航空工业集团公司北京航空材料研究院 Graphene/aluminium alloy composite
CN105112699A (en) * 2015-06-25 2015-12-02 中国航空工业集团公司北京航空材料研究院 Preparation method of graphene/aluminum alloy composite material
CN105734360A (en) * 2016-03-31 2016-07-06 山东正凯机械科技有限公司 Preparation method of Si-Al alloy material for automobile brake disc
CN106521220A (en) * 2016-10-11 2017-03-22 常州大学 Novel graphene Al-Cu intermediate alloy preparation method
CN106567785A (en) * 2016-11-10 2017-04-19 无锡市明盛强力风机有限公司 Graphene-doped aluminum alloy air cylinder cover
CN107299257A (en) * 2017-05-16 2017-10-27 苏州莱特复合材料有限公司 A kind of modified graphene reinforced aluminum matrix composites and preparation method thereof

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
PRASHANTHA KUMAR H.G ET AL: "EFFECT OF GRAPHENE ADDITION ON FLEXURAL PROPERTIES OF Al 6061 NANOCOMPOSITES", 《MATERIALS TODAY:PROCEEDINGS》 *
WENSHU YANG ET AL: "Graphene nanoflakes reinforced Al-20Si matrix composites prepared by pressure infiltration method", 《MATERIALS SCIENCE & ENGINEERING A》 *
肖瑞: "石墨烯及其Al-20Si基复合材料的制备与性能研究", 《中国优秀硕士学位论文全文数据库》 *
闫庆斌: "《铸造合金熔炼及控制》", 31 March 2011, 中南大学出版社 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111636006A (en) * 2020-05-29 2020-09-08 香港生产力促进局 A kind of aluminum silicon alloy graphite composite thermal conductive material and its preparation and application
CN111636006B (en) * 2020-05-29 2021-09-28 香港生产力促进局 Aluminum-silicon alloy graphite composite heat conduction material and preparation and application thereof
CN112143944A (en) * 2020-08-17 2020-12-29 福建祥鑫股份有限公司 Graphene-modified silicon-aluminum composite material and preparation method thereof

Also Published As

Publication number Publication date
CN108359852B (en) 2020-06-16

Similar Documents

Publication Publication Date Title
CN109182854B (en) A kind of 1GPa high-strength aluminum-based light medium-entropy alloy and preparation method thereof
CN101463440B (en) A kind of aluminum-based composite material for piston and preparation method thereof
CN105328186B (en) A kind of aluminum-based in-situ composite materials formed based on laser 3D printing and preparation method thereof
CN110273092B (en) CoCrNi particle reinforced magnesium-based composite material and preparation method thereof
CN110724860B (en) High-thermal-conductivity particle reinforced aluminum-based composite material and preparation method thereof
CN108251710B (en) High-strength and high-toughness high-silicon aluminum alloy suitable for extrusion casting and preparation process thereof
CN108203780B (en) A kind of liquid forging high-strength abrasion-proof aluminum alloy and preparation method thereof
CN101538667B (en) High-strength and wear-resistant cocrystallized Al-Si alloy forging stock material and preparation method thereof
CN107034372B (en) A kind of preparation method of High Strength Cast Aluminum Alloy
CN103866165A (en) Isotropical high-strength high-toughness particle reinforced aluminium-based composite material and preparation method thereof
CN108642332A (en) A kind of high-performance beryllium alumin(i)um alloy and preparation method thereof
CN110284032A (en) A kind of high-entropy alloy particle reinforced magnesium base compound material preparation method
CN108265207B (en) High-thermal-conductivity aluminum alloy, preparation method thereof and heat radiation body
CN106756302A (en) A kind of high-strength aluminium piston alloy composite of high-temperature wearable and preparation method thereof
CN111690840B (en) Amorphous phase silicate particle and SiC particle reinforced aluminum matrix composite material and preparation
CN113186418A (en) Preparation method of aluminum-based composite material
CN108359852A (en) A kind of high silica/aluminum-based composite material and preparation method of graphene enhancing
CN109778019B (en) Hypereutectic aluminum-silicon alloy composite modifier and preparation method thereof
CN118166244A (en) Aluminum-based composite material and preparation method thereof
CN112375946A (en) High Mg2Si-aluminum alloy, design and rapid solidification preparation method and application thereof
CN1065921C (en) Iron-carbon-boron composite refining agent for aluminium and aluminium alloy
CN106555068B (en) A kind of aluminium silicon composite material and preparation method thereof
CN113528915B (en) An impact-resistant high-strength heat-resistant magnesium rare earth alloy material
CN114934206A (en) A kind of multi-component aluminide reinforced aluminum matrix composite material and its preparation method and application
CN114686735A (en) Wrought aluminum alloy with gradient structure and preparation method thereof

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20200616

CF01 Termination of patent right due to non-payment of annual fee