CN110218913A - A kind of aluminum matrix composite and preparation method thereof with excellent high deformability - Google Patents
A kind of aluminum matrix composite and preparation method thereof with excellent high deformability Download PDFInfo
- Publication number
- CN110218913A CN110218913A CN201910589036.0A CN201910589036A CN110218913A CN 110218913 A CN110218913 A CN 110218913A CN 201910589036 A CN201910589036 A CN 201910589036A CN 110218913 A CN110218913 A CN 110218913A
- Authority
- CN
- China
- Prior art keywords
- composite material
- phase
- nanocrystalline
- aluminum matrix
- excellent high
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/20—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by extruding
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0408—Light metal alloys
- C22C1/0416—Aluminium-based alloys
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/20—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by extruding
- B22F2003/208—Warm or hot extruding
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Description
技术领域technical field
本发明属于铝基复合材料技术领域,具体涉及一种具有优良高温变形能力的纳米晶非晶双相颗粒增强铝基复合材料及其制备方法。The invention belongs to the technical field of aluminum-based composite materials, and in particular relates to a nanocrystalline amorphous dual-phase particle-reinforced aluminum-based composite material with excellent high-temperature deformability and a preparation method thereof.
背景技术Background technique
颗粒增强铝基复合材料具有高比强度、高耐磨性和尺寸稳定性好等优异的性能,在航空航天、汽车、军事和电子等领域具有广泛应用前景。高强度、高弹性模量和高耐磨性的陶瓷颗粒如Al2O3、SiC和B4C等是最常见的增强体颗粒。然而,陶瓷颗粒密度大、硬度高、脆性大、易团聚、以及与基体易发生化学反应形成脆性界面相等导致铝基复合材料的热加工性能严重恶化,极大限制了铝基复合材料的工程应用。高温变形阻力小可以使得产品加工省力、节能、设备加工能力要求较低和易于成型形状复杂的整体部件,可以避免铝基复合材料焊接困难的问题。因此,如何提升铝基复合材料的高温变形能力是促进铝基复合材料大规模应用的关键。Particle-reinforced aluminum matrix composites have excellent properties such as high specific strength, high wear resistance, and good dimensional stability, and have broad application prospects in aerospace, automotive, military, and electronics fields. Ceramic particles with high strength, high elastic modulus and high wear resistance such as Al 2 O 3 , SiC and B 4 C are the most common reinforcement particles. However, the high density of ceramic particles, high hardness, high brittleness, easy agglomeration, and easy chemical reaction with the matrix to form a brittle interface lead to serious deterioration of the thermal processing performance of aluminum matrix composites, which greatly limits the engineering application of aluminum matrix composites. . Small high temperature deformation resistance can save labor and energy in product processing, lower equipment processing capacity requirements and easy to form integral parts with complex shapes, and can avoid the problem of difficult welding of aluminum matrix composite materials. Therefore, how to improve the high-temperature deformation ability of aluminum matrix composites is the key to promote the large-scale application of aluminum matrix composites.
发明内容Contents of the invention
为了在提高铝基复合材料强度的同时解决铝基复合材料热加工难的技术问题,本发明的目的在于提供一种具有优良高温变形能力的纳米晶非晶双相颗粒增强铝基复合材料及其制备方法。In order to solve the technical problem of difficult thermal processing of aluminum matrix composite materials while improving the strength of aluminum matrix composite materials, the purpose of the present invention is to provide a nanocrystalline amorphous dual-phase particle reinforced aluminum matrix composite material with excellent high temperature deformation ability and its Preparation.
本发明的目的由以下技术方案来实现:The purpose of the present invention is achieved by the following technical solutions:
一种具有优良高温变形能力的纳米晶非晶双相颗粒增强铝基复合材料,由体积分数为2%~20%的增强颗粒与80%~98%的铝合金制备而成。A nanocrystalline amorphous dual-phase particle-reinforced aluminum-based composite material with excellent high-temperature deformability is prepared from reinforced particles with a volume fraction of 2% to 20% and aluminum alloys with a volume fraction of 80% to 98%.
所述增强颗粒为纳米晶非晶双相颗粒。The reinforcing particles are nanocrystalline amorphous dual-phase particles.
所述的铝合金优选7xxx系铝合金和/或2xxx系铝合金中的一种以上。The aluminum alloy is preferably one or more of 7xxx series aluminum alloys and/or 2xxx series aluminum alloys.
所述增强颗粒优选Ti-Cu-Zr系合金,其微观组织为10-90vol.%的纳米晶相和10-90vol.%的非晶相;其中,非晶相在50vol.%及其以上时,复合材料具有更好的高温变形能力。增强颗粒中纳米晶直径为2-15nm,增强颗粒的粒度<20μm。The reinforcing particles are preferably Ti-Cu-Zr alloys, whose microstructure is 10-90vol.% nanocrystalline phase and 10-90vol.% amorphous phase; wherein, when the amorphous phase is 50vol.% or above , the composite material has better high temperature deformation ability. The diameter of the nanocrystals in the reinforced particles is 2-15nm, and the particle size of the reinforced particles is <20μm.
优选地,增强颗粒成分为Ti45Cu45Zr5Ni5;所述纳米晶非晶双相颗粒采用球磨制备,具体为:按Ti45Cu45Zr5Ni5的化学计量比称量出相应的各纯金属粉末,在行星式球磨机上进行机械合金化,制备出纳米晶非晶双相颗粒(通过筛粉,过滤得到20μm以下的粉末)。优选地,混粉时间为5h,球料比为15:1,球磨转速为200rpm,球磨时间为5h~100h,纳米晶非晶双相颗粒中非晶相随球磨时间增加而增加,纳米晶相随球磨时间增加而减少。Preferably, the reinforcing particle composition is Ti 45 Cu 45 Zr 5 Ni 5 ; the nanocrystalline amorphous dual-phase particles are prepared by ball milling, specifically: the corresponding stoichiometric ratio of Ti 45 Cu 45 Zr 5 Ni 5 is weighed Each pure metal powder is mechanically alloyed on a planetary ball mill to prepare nanocrystalline amorphous dual-phase particles (by sieving and filtering to obtain a powder below 20 μm). Preferably, the powder mixing time is 5 hours, the ball-to-material ratio is 15:1, the ball milling speed is 200rpm, and the ball milling time is 5h to 100h. The amorphous phase in the nanocrystalline amorphous dual-phase particles increases with the ball milling time, and the nanocrystalline phase Decreases with increasing milling time.
上述具有优良高温变形能力的纳米晶非晶双相颗粒增强铝基复合材料的制备方法,包括以下步骤:The preparation method of the above-mentioned nanocrystalline amorphous dual-phase particle-reinforced aluminum-based composite material with excellent high-temperature deformability comprises the following steps:
(1)混粉:将体积分数为2%~20%的增强颗粒和80%~98%的铝合金粉末进行球磨,获得复合材料粉末;球磨的时间为10-30h;(1) Powder mixing: ball mill the reinforcing particles with a volume fraction of 2% to 20% and the aluminum alloy powder of 80% to 98% to obtain composite material powder; the time of ball milling is 10-30h;
(2)复合材料粉末包套热挤压:将步骤(1)所得复合材料粉末进行热挤压,获得纳米晶非晶双相颗粒增强铝基复合材料。所述热挤压是指将粉末装进挤压套,装进热挤压设备的预热模具中进行挤压。热挤压的条件:挤压温度为300℃~550℃,升温速率为30℃~150℃/min,挤压时间为1min~20min,挤压压力为50~200MPa。(2) Composite material powder-coated hot extrusion: the composite material powder obtained in step (1) is subjected to hot extrusion to obtain a nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material. The hot extrusion refers to putting the powder into an extrusion sleeve and putting it into a preheated mold of a hot extrusion equipment for extrusion. Hot extrusion conditions: extrusion temperature is 300°C-550°C, heating rate is 30°C-150°C/min, extrusion time is 1min-20min, extrusion pressure is 50-200MPa.
本发明的原理:本发明的增强体为纳米晶非晶双相颗粒,具有强度高、润湿性好等优点,提高了复合材料的室温强度;同时利用了非晶相在过冷液相区间粘度低的特点,提高了复合材料的高温变形能力,使该纳米晶非晶双相颗粒增强铝基复合材料具有优良的高温变形能力;纳米晶非晶双相的比例可以通过球磨过程中的球磨时间和热挤压过程中的温度来调控。The principle of the present invention: the reinforcing body of the present invention is a nanocrystalline amorphous dual-phase particle, which has the advantages of high strength and good wettability, and improves the room temperature strength of the composite material; at the same time, the amorphous phase is used in the supercooled liquid phase interval The characteristics of low viscosity improve the high-temperature deformation ability of the composite material, so that the nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material has excellent high-temperature deformation ability; Time and temperature during hot extrusion are regulated.
本发明的制备方法及所得复合材料具有如下优点及有益效果:The preparation method of the present invention and the resulting composite material have the following advantages and beneficial effects:
(1)本发明所采用纳米晶非晶双相颗粒不仅可以提升复合材料的室温强度,而且可以提升复合材料的高温变形能力,有利于热加工和温变形,突破了传统铝基复合材料高温变形难的瓶颈。(1) The nanocrystalline amorphous dual-phase particles used in the present invention can not only improve the room temperature strength of the composite material, but also improve the high-temperature deformation capacity of the composite material, which is beneficial to thermal processing and temperature deformation, and breaks through the high-temperature deformation of traditional aluminum-based composite materials difficult bottleneck.
(2)本发明所采用纳米晶非晶双相颗粒本身包含了纳米晶相,因而对非晶相的纳米晶化行为可以兼容。(2) The nanocrystalline amorphous dual-phase particles used in the present invention itself contain a nanocrystalline phase, so they are compatible with the nanocrystallization behavior of the amorphous phase.
(3)本发明制备的纳米晶非晶双相颗粒增强铝基复合材料具备室温强度高、比强度高、高温变形能力优良,基本满足作为轻量化结构材料的应用要求,在航空航天、交通运输、军工等领域具有广泛的推广应用前景。(3) The nanocrystalline amorphous dual-phase particle-reinforced aluminum-based composite material prepared by the present invention has high room temperature strength, high specific strength, and excellent high-temperature deformation ability, and basically meets the application requirements as a lightweight structural material. , military industry and other fields have a wide range of promotion and application prospects.
附图说明Description of drawings
图1为实施例1制备的纳米晶非晶双相颗粒增强铝基复合材料的扫描电镜图;a,b分别表示不同放大倍数图;Fig. 1 is the scanning electron micrograph of the nanocrystalline amorphous dual-phase particle reinforced aluminum-based composite material prepared in Example 1; a and b respectively represent different magnification figures;
图2为实施例1、2制备的纳米晶非晶双相颗粒增强铝基复合材料和纯7075铝合金在250℃压缩时的真应力-真应变曲线对比图;7075Al+2%增强体对应实施例1,7075Al+6%增强体对应实施例2,7075Al对应纯7075铝合金;Figure 2 is a comparison of the true stress-true strain curves of the nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material prepared in Examples 1 and 2 and pure 7075 aluminum alloy when compressed at 250°C; 7075Al+2% reinforcement corresponds to the implementation Example 1, 7075Al+6% reinforcement corresponds to Example 2, 7075Al corresponds to pure 7075 aluminum alloy;
图3为实施例1、2制备的纳米晶非晶双相颗粒增强铝基复合材料和纯7075铝合金在400℃压缩时的真应力-真应变曲线对比图;7075Al+2%增强体对应实施例1,7075Al+6%增强体对应实施例2,7075Al对应纯7075铝合金;Figure 3 is a comparison of the true stress-true strain curves of the nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material prepared in Examples 1 and 2 and pure 7075 aluminum alloy when compressed at 400°C; 7075Al+2% reinforcement corresponds to the implementation Example 1, 7075Al+6% reinforcement corresponds to Example 2, 7075Al corresponds to pure 7075 aluminum alloy;
图4为实施例1、2制备的纳米晶非晶双相颗粒增强铝基复合材料和纯7075铝合金在450℃压缩时的真应力-真应变曲线对比图;7075Al+2%增强体对应实施例1,7075Al+6%增强体对应实施例2,7075Al对应纯7075铝合金。Figure 4 is a comparison of the true stress-true strain curves of the nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite prepared in Examples 1 and 2 and pure 7075 aluminum alloy when compressed at 450°C; 7075Al+2% reinforcement corresponds to the implementation Example 1, 7075Al+6% reinforcement corresponds to Example 2, 7075Al corresponds to pure 7075 aluminum alloy.
具体实施方式Detailed ways
下面结合实施例及附图对本发明作进一步详细的描述,但本发明的实施方式不限于此。The present invention will be further described in detail below in conjunction with the embodiments and the accompanying drawings, but the embodiments of the present invention are not limited thereto.
实施例中纳米晶非晶双相颗粒的成分为Ti45Cu45Zr5Ni5;所述纳米晶非晶双相颗粒采用球磨制备,具体为:按Ti45Cu45Zr5Ni5的化学计量比称量出相应的各纯金属粉末,在行星式球磨机上进行机械合金化,通过筛粉,过滤得到20μm以下的粉末,制备出纳米晶非晶双相颗粒。优选地,混粉时间为5h,球料比为15:1,球磨转速为200rpm,球磨时间为5h~100h,纳米晶非晶双相颗粒中非晶相随球磨时间增加而增加,纳米晶相随球磨时间增加而减少。The composition of the nanocrystalline amorphous dual-phase particles in the examples is Ti 45 Cu 45 Zr 5 Ni 5 ; the nanocrystalline amorphous dual-phase particles are prepared by ball milling, specifically: according to the stoichiometric ratio of Ti 45 Cu 45 Zr 5 Ni 5 The corresponding pure metal powders are weighed out, mechanically alloyed on a planetary ball mill, sieved and filtered to obtain powders below 20 μm, and nanocrystalline amorphous dual-phase particles are prepared. Preferably, the powder mixing time is 5 hours, the ball-to-material ratio is 15:1, the ball milling speed is 200rpm, and the ball milling time is 5h to 100h. The amorphous phase in the nanocrystalline amorphous dual-phase particles increases with the ball milling time, and the nanocrystalline phase Decreases with increasing milling time.
实施例1Example 1
(1)混粉:将体积分数为2%的增强颗粒和98%的铝合金粉末(7075铝合金)装进球磨罐中,在球磨机上球磨20h(球磨转速为200rpm),得到复合材料粉末;(1) Powder mixing: put 2% reinforced particles and 98% aluminum alloy powder (7075 aluminum alloy) into a ball mill jar, and ball mill on a ball mill for 20 hours (the ball milling speed is 200rpm) to obtain a composite material powder;
(2)复合材料粉末包套热挤压:将步骤(1)所得复合材料粉末装进挤压套,装进热挤压设备的预热模具中,挤压温度为350℃,升温速率为100℃/min,挤压时间为~5min,挤压压力为~100MPa,得到块体纳米晶非晶双相颗粒增强铝基复合材料。其中,增强颗粒含有约20vol.%的纳米晶相和约80vol.%的非晶相。图1为实施例1制备的纳米晶非晶双相颗粒增强铝基复合材料的扫描电镜图。(2) Composite material powder-coated hot extrusion: put the composite material powder obtained in step (1) into the extrusion sleeve, and put it into the preheated mold of the hot extrusion equipment, the extrusion temperature is 350 °C, and the heating rate is 100 °C/min, the extrusion time is ~5min, and the extrusion pressure is ~100MPa to obtain a bulk nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material. Wherein, the reinforcing particles contain about 20vol.% nanocrystalline phase and about 80vol.% amorphous phase. FIG. 1 is a scanning electron microscope image of the nanocrystalline amorphous dual-phase particle-reinforced aluminum-based composite material prepared in Example 1.
经测试,在室温压缩变形过程中,应变速率为1×10-3s-1时,复合材料的屈服强度和抗压强度分别为520MPa和596MPa,相比于同等条件下纯7075Al铝合金的480MPa和553MPa,分别提高了40MPa和43MPa。在高温压缩变形过程中,应变速率为1×10-3s-1,热压缩温度为250℃,400℃和450℃时,复合材料的变形抗力分别为257MPa,54MPa和36MPa,相比于纯7075Al铝合金的272MPa,62MPa和43MPa,变形抗力分别降低了5.5%,13.0%和16.3%。本实施例的复合材料高温压缩获得的真应力-真应变曲线如图2,3,4所示。After testing, in the process of compression deformation at room temperature, when the strain rate is 1×10 -3 s -1 , the yield strength and compressive strength of the composite material are 520MPa and 596MPa, respectively, compared with 480MPa of pure 7075Al aluminum alloy under the same conditions and 553MPa, increased by 40MPa and 43MPa respectively. During high temperature compression deformation, when the strain rate is 1×10 -3 s -1 and the thermal compression temperature is 250°C, 400°C and 450°C, the deformation resistance of the composite is 257MPa, 54MPa and 36MPa, respectively, compared with pure 272MPa, 62MPa and 43MPa of 7075Al aluminum alloy, the deformation resistance is reduced by 5.5%, 13.0% and 16.3%, respectively. The true stress-true strain curves obtained by high temperature compression of the composite material in this embodiment are shown in Figures 2, 3 and 4.
实施例2Example 2
(1)混粉:将体积分数为6%的增强颗粒和94%的铝合金粉末装进球磨罐中,在球磨机上球磨20h(球磨转速为200rpm),得到复合材料粉末;(1) Powder mixing: put the reinforced particles with a volume fraction of 6% and the aluminum alloy powder of 94% into a ball mill jar, and ball mill on a ball mill for 20 hours (the ball milling speed is 200rpm) to obtain a composite material powder;
(2)复合材料粉末包套热挤压:将步骤(1)所得复合材料粉末装进挤压套,装进热挤压设备的预热模具中,挤压温度为350℃,升温速率为100℃/min,挤压时间为~5min,挤压压力为~100MPa,得到块体纳米晶非晶双相颗粒增强铝基复合材料。其中,增强颗粒含有约25vol.%的纳米晶相和约75vol.%的非晶相。(2) Composite material powder-coated hot extrusion: put the composite material powder obtained in step (1) into the extrusion sleeve, and put it into the preheated mold of the hot extrusion equipment, the extrusion temperature is 350 °C, and the heating rate is 100 °C/min, the extrusion time is ~5min, and the extrusion pressure is ~100MPa to obtain a bulk nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material. Wherein, the reinforcing particles contain about 25vol.% nanocrystalline phase and about 75vol.% amorphous phase.
经测试,在室温压缩变形过程中,应变速率为1×10-3s-1时,复合材料的屈服强度和抗压强度分别为557MPa和618MPa,相比于同等条件下纯7075Al铝合金分别提高了77MPa和65MPa。在高温压缩变形过程中,应变速率为1×10-3s-1,热压缩温度为250℃,400℃和450℃时,复合材料的变形抗力分别为214MPa,38MPa和30MPa,相比于纯7075Al铝合金变形抗力分别降低了21.3%,38.7%和30.2%。本实施例的复合材料高温压缩获得的真应力-真应变曲线如图2,3,4所示。After testing, in the process of compression deformation at room temperature, when the strain rate is 1×10 -3 s -1 , the yield strength and compressive strength of the composite material are 557MPa and 618MPa respectively, which are higher than those of pure 7075Al aluminum alloy under the same conditions. 77MPa and 65MPa. During high temperature compression deformation, when the strain rate is 1×10 -3 s -1 , and the thermal compression temperature is 250°C, 400°C and 450°C, the deformation resistance of the composite is 214MPa, 38MPa and 30MPa, respectively. The deformation resistance of 7075Al aluminum alloy decreased by 21.3%, 38.7% and 30.2%, respectively. The true stress-true strain curves obtained by high temperature compression of the composite material in this embodiment are shown in Figures 2, 3 and 4.
实施例3Example 3
(1)混粉:将体积分数为17%的纳米晶非晶双相颗粒和83%的铝合金粉末装进球磨罐中,在球磨机上球磨20h(球磨转速为200rpm),得到复合材料粉末;(1) Powder mixing: the nanocrystalline amorphous dual-phase particles with a volume fraction of 17% and the aluminum alloy powder of 83% are loaded into a ball mill jar, and ball milled on a ball mill for 20 hours (the ball milling speed is 200rpm) to obtain a composite material powder;
(2)复合材料粉末包套热挤压:将步骤(1)所得复合材料粉末装进挤压套,装进热挤压设备的预热模具中,挤压温度为350℃,升温速率为100℃/min,挤压时间为~5min,挤压压力为~100MPa,得到块体纳米晶非晶双相颗粒增强铝基复合材料。其中,增强颗粒含有约30vol.%的纳米晶相和约70vol.%的非晶相。(2) Composite material powder-coated hot extrusion: put the composite material powder obtained in step (1) into the extrusion sleeve, and put it into the preheated mold of the hot extrusion equipment, the extrusion temperature is 350 °C, and the heating rate is 100 °C/min, the extrusion time is ~5min, and the extrusion pressure is ~100MPa to obtain a bulk nanocrystalline amorphous dual-phase particle-reinforced aluminum matrix composite material. Wherein, the reinforcing particles contain about 30vol.% nanocrystalline phase and about 70vol.% amorphous phase.
经测试,在室温压缩变形过程中,应变速率为1×10-3s-1时,复合材料的屈服强度和抗压强度分别为902MPa和953MPa,相比于同等条件下纯7075Al铝合金分别提高了422MPa和400MPa。在高温压缩变形过程中,应变速率为1×10-3s-1,热压缩温度为250℃,400℃和450℃时,复合材料的变形抗力分别为180MPa,29MPa和25MPa,相比于纯7075Al铝合金变形抗力分别降低了34%,23%和15%。After testing, in the process of compression deformation at room temperature, when the strain rate is 1×10 -3 s -1 , the yield strength and compressive strength of the composite material are 902MPa and 953MPa respectively, which are higher than those of pure 7075Al aluminum alloy under the same conditions. 422MPa and 400MPa. In the process of high temperature compression deformation, when the strain rate is 1×10 -3 s -1 and the hot compression temperature is 250℃, 400℃ and 450℃, the deformation resistance of the composite material is 180MPa, 29MPa and 25MPa, respectively, compared with pure The deformation resistance of 7075Al aluminum alloy was reduced by 34%, 23% and 15%, respectively.
上述实施例为本发明较佳的实施方式,但本发明的实施方式并不受上述实施例的限制,其它的任何未背离本发明的精神实质与原理下所作的改变、修饰、替代、组合、简化,均应为等效的置换方式,都包含在本发明的保护范围之内。The above-mentioned embodiment is a preferred embodiment of the present invention, but the embodiment of the present invention is not limited by the above-mentioned embodiment, and any other changes, modifications, substitutions, combinations, Simplifications should be equivalent replacement methods, and all are included in the protection scope of the present invention.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910589036.0A CN110218913B (en) | 2019-07-02 | 2019-07-02 | Aluminum-based composite material with excellent high-temperature deformation capacity and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910589036.0A CN110218913B (en) | 2019-07-02 | 2019-07-02 | Aluminum-based composite material with excellent high-temperature deformation capacity and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN110218913A true CN110218913A (en) | 2019-09-10 |
CN110218913B CN110218913B (en) | 2021-08-10 |
Family
ID=67815829
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201910589036.0A Expired - Fee Related CN110218913B (en) | 2019-07-02 | 2019-07-02 | Aluminum-based composite material with excellent high-temperature deformation capacity and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110218913B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111575542A (en) * | 2020-05-03 | 2020-08-25 | 上海工程技术大学 | Amorphous reinforced aluminum alloy composite material and preparation method thereof |
CN115612880A (en) * | 2022-10-28 | 2023-01-17 | 上海交通大学 | A kind of nano-amorphous alloy particle reinforced aluminum matrix composite material and preparation method thereof |
CN115961251A (en) * | 2022-12-19 | 2023-04-14 | 广东省科学院中乌焊接研究所 | Titanium alloy part with nano double-phase structure coating and preparation method thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070020521A1 (en) * | 2005-07-25 | 2007-01-25 | 3M Innovative Properties Company | Alloy compositions for lithium ion batteries |
CN104294064A (en) * | 2014-09-12 | 2015-01-21 | 重庆科技学院 | Preparation method of Cu-based bulky non-crystalline-nanocrystalline alloy composite material |
CN106967900A (en) * | 2017-04-26 | 2017-07-21 | 华南理工大学 | A kind of titanium-based metal glass particle reinforced aluminum matrix composites and preparation method thereof |
-
2019
- 2019-07-02 CN CN201910589036.0A patent/CN110218913B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070020521A1 (en) * | 2005-07-25 | 2007-01-25 | 3M Innovative Properties Company | Alloy compositions for lithium ion batteries |
CN104294064A (en) * | 2014-09-12 | 2015-01-21 | 重庆科技学院 | Preparation method of Cu-based bulky non-crystalline-nanocrystalline alloy composite material |
CN106967900A (en) * | 2017-04-26 | 2017-07-21 | 华南理工大学 | A kind of titanium-based metal glass particle reinforced aluminum matrix composites and preparation method thereof |
Non-Patent Citations (2)
Title |
---|
X. D. LIU ET AL: "Amorphization Tendency of Ti34Zr11Cu47Ni8 and Ti37Zr17Cu42Ni4 during Mechanical Alloying", 《MATERIALS TRANSACTIONS,JIM》 * |
张冠群等: "高能球磨Ti55.5Cu18.5Ni17.5Al8.5合金非晶化研究", 《稀有金属材料与工程》 * |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111575542A (en) * | 2020-05-03 | 2020-08-25 | 上海工程技术大学 | Amorphous reinforced aluminum alloy composite material and preparation method thereof |
CN111575542B (en) * | 2020-05-03 | 2021-04-06 | 上海工程技术大学 | Amorphous reinforced aluminum alloy composite material and preparation method thereof |
CN115612880A (en) * | 2022-10-28 | 2023-01-17 | 上海交通大学 | A kind of nano-amorphous alloy particle reinforced aluminum matrix composite material and preparation method thereof |
CN115961251A (en) * | 2022-12-19 | 2023-04-14 | 广东省科学院中乌焊接研究所 | Titanium alloy part with nano double-phase structure coating and preparation method thereof |
CN115961251B (en) * | 2022-12-19 | 2023-08-08 | 广东省科学院中乌焊接研究所 | Titanium alloy part with nano diphase structure coating and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
CN110218913B (en) | 2021-08-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Dey et al. | Magnesium metal matrix composites-a review | |
CN101492781B (en) | High-ductility titanium based ultra-fine crystal composite material and method for producing the same | |
CN104372230B (en) | High-strength high-toughness ultrafine-grained high-entropy alloy and preparation method thereof | |
CN109097657B (en) | A kind of Mo nanoparticle reinforced CoCrNi medium entropy alloy composite material and preparation method thereof | |
CN108796265B (en) | Preparation method of TiB nano-reinforced titanium-based composite material | |
CN102747240B (en) | Preparation method of carbon-nanotube-enhanced magnesium-based composite material | |
CN103572087B (en) | The preparation method of boron carbide particles reinforced aluminum matrix composites | |
CN102618774B (en) | Manufacturing method of metal matrix nanocomposites with high toughness | |
CN110592412B (en) | Nano-AlN particle reinforced mixed crystal heat-resistant aluminum matrix composite material and preparation method | |
CN112391556A (en) | High-strength high-conductivity Cu-Cr-Nb alloy reinforced by double-peak grain size and double-scale nanophase | |
CN108723371A (en) | A kind of high-entropy alloy reinforced aluminum matrix composites and preparation method | |
CN108796264A (en) | A kind of preparation method of oriented alignment TiB whisker-reinforced titanium-based composite materials | |
CN109554565A (en) | A kind of interface optimization method of carbon nanotube enhanced aluminium-based composite material | |
CN110218913A (en) | A kind of aluminum matrix composite and preparation method thereof with excellent high deformability | |
CN106967900A (en) | A kind of titanium-based metal glass particle reinforced aluminum matrix composites and preparation method thereof | |
CN105695781B (en) | A kind of preparation method of high-performance in-situ nano particle reinforced magnesium base compound material | |
CN105238954A (en) | Multi-scale and double-state structure titanium alloy based on eutectic transformation, preparation and application | |
CN102925737B (en) | A kind of nano TiB2 particle reinforced metal matrix composite material and preparation method thereof | |
CN109338168B (en) | Preparation method of complex-phase reinforced aluminum-based composite material | |
CN108326302A (en) | A kind of graphene enhancing aluminum alloy materials and preparation method thereof | |
CN101935777A (en) | Titanium-based ultrafine-grain or fine-grain composite material with high compressive strength and preparation method thereof | |
CN112593123A (en) | Zirconium-based amorphous particle reinforced aluminum-based composite material and preparation method thereof | |
CN109136611A (en) | A kind of metal-base composites and its preparation method and application | |
CN116463523A (en) | In-situ self-generated nano oxide carbide synergistic toughening fine-grain molybdenum alloy and preparation method thereof | |
CN110484839B (en) | Preparation method of carbon fiber reinforced aluminum composite material with high interlayer strength |
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 | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210810 |