CN104313423B - The manufacture method of magnesium base composite material wallboard section bar - Google Patents
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- 239000011777 magnesium Substances 0.000 title claims abstract description 99
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 title claims abstract description 95
- 229910052749 magnesium Inorganic materials 0.000 title claims abstract description 95
- 239000002131 composite material Substances 0.000 title claims abstract description 88
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 26
- 238000000034 method Methods 0.000 title claims abstract description 21
- 238000001125 extrusion Methods 0.000 claims abstract description 22
- 238000000137 annealing Methods 0.000 claims abstract description 21
- 238000005266 casting Methods 0.000 claims abstract description 16
- 239000002994 raw material Substances 0.000 claims abstract description 11
- 238000003723 Smelting Methods 0.000 claims abstract description 7
- 238000002844 melting Methods 0.000 claims abstract 2
- 230000008018 melting Effects 0.000 claims abstract 2
- 229910045601 alloy Inorganic materials 0.000 claims description 21
- 239000000956 alloy Substances 0.000 claims description 21
- 239000002245 particle Substances 0.000 claims description 19
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 14
- 239000000498 cooling water Substances 0.000 claims description 8
- 229910052802 copper Inorganic materials 0.000 claims description 8
- 239000010949 copper Substances 0.000 claims description 8
- 229910052725 zinc Inorganic materials 0.000 claims description 8
- 239000011701 zinc Substances 0.000 claims description 8
- 238000005520 cutting process Methods 0.000 claims description 7
- 238000000265 homogenisation Methods 0.000 claims description 7
- 239000011159 matrix material Substances 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 claims description 5
- 229910052684 Cerium Inorganic materials 0.000 claims description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 4
- MKPXGEVFQSIKGE-UHFFFAOYSA-N [Mg].[Si] Chemical compound [Mg].[Si] MKPXGEVFQSIKGE-UHFFFAOYSA-N 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- RRTQFNGJENAXJJ-UHFFFAOYSA-N cerium magnesium Chemical compound [Mg].[Ce] RRTQFNGJENAXJJ-UHFFFAOYSA-N 0.000 claims description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- MHKWSJBPFXBFMX-UHFFFAOYSA-N iron magnesium Chemical compound [Mg].[Fe] MHKWSJBPFXBFMX-UHFFFAOYSA-N 0.000 claims description 4
- KBMLJKBBKGNETC-UHFFFAOYSA-N magnesium manganese Chemical compound [Mg].[Mn] KBMLJKBBKGNETC-UHFFFAOYSA-N 0.000 claims description 4
- ATTFYOXEMHAYAX-UHFFFAOYSA-N magnesium nickel Chemical compound [Mg].[Ni] ATTFYOXEMHAYAX-UHFFFAOYSA-N 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 4
- 239000011572 manganese Substances 0.000 claims description 4
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 238000003756 stirring Methods 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000005452 bending Methods 0.000 description 2
- 206010003549 asthenia Diseases 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 235000012438 extruded product Nutrition 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
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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
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
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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
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
- C22C1/1047—Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites
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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
- C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
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- 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)
- Composite Materials (AREA)
- Extrusion Of Metal (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
技术领域technical field
本发明涉及一种制造镁基复合材料壁板型材的方法。The invention relates to a method for manufacturing a magnesium-based composite material wall board profile.
背景技术Background technique
镁基复合材料具有重量轻、比强度高、比刚度高和耐磨性好的优点,在航空航天、军事领域及汽车等行业越来越得到广泛的应用。其中颗粒增强镁基复合材料具有成本低,制备工艺简单等特点,已逐渐成为镁基复合材料领域的研究重点。现有的壁板型材材质为镁合金,采用圆挤压筒挤压获得,挤压变形程度大,挤压过程闷车,型材外形尺寸、直线度超出标准要求的范围,弯曲度每米为2.5mm~3.5mm,型材任何部位的每米长度上绕纵轴的扭转度为2.0°~3.0°,波浪高度为1.0mm~2.0mm,无法满足用户的要求。Magnesium-based composites have the advantages of light weight, high specific strength, high specific stiffness and good wear resistance, and are increasingly used in aerospace, military and automotive industries. Particle-reinforced magnesium-based composites have the characteristics of low cost and simple preparation process, and have gradually become the focus of research in the field of magnesium-based composites. Existing siding profiles are made of magnesium alloy, which are obtained by extruding a circular extrusion cylinder. The degree of extrusion deformation is large, and the extrusion process is stuffy. The profile dimensions and straightness exceed the range required by the standard, and the curvature per meter is 2.5 mm to 3.5mm, the torsion around the longitudinal axis per meter of any part of the profile is 2.0° to 3.0°, and the wave height is 1.0mm to 2.0mm, which cannot meet the requirements of users.
发明内容Contents of the invention
本发明是为了解决现有制造壁板型材中挤压过程易闷车,型材的弯曲度和扭转度较高的问题,而提供的一种镁基复合材料壁板型材的制造方法。The present invention provides a method for manufacturing a magnesium-based composite wall plate profile in order to solve the problems that the extrusion process is easy to be stuffy and the profile has a high degree of curvature and torsion in the existing wall plate profile production.
本发明镁基复合材料壁板型材的制造方法按下列步骤实现:The manufacture method of the magnesium-based composite material wall plate profile of the present invention is realized by the following steps:
一、按元素的质量百分比为Al:0.2%、Mn:1.3%~2.2%、Zn:0.3%、Ce:0.15%~0.35%、Fe:≤0.05%、Si:≤0.1%、Cu:≤0.05%、Ni:≤0.007%,余量为Mg分别称取铝锭、镁锰中间合金、锌锭、镁铈中间合金、镁铁中间合金、镁硅中间合金、铜锭、镁镍中间合金和镁锭作为原料,将原料加入到干燥的熔炼炉中,在温度为760℃~780℃下熔炼3.5h~5h,得到镁合金熔液;1. According to the mass percentage of elements, Al: 0.2%, Mn: 1.3%-2.2%, Zn: 0.3%, Ce: 0.15%-0.35%, Fe: ≤0.05%, Si: ≤0.1%, Cu: ≤0.05 %, Ni: ≤0.007%, and the balance is Mg. Weigh aluminum ingots, magnesium-manganese master alloys, zinc ingots, magnesium-cerium master alloys, magnesium-iron master alloys, magnesium-silicon master alloys, copper ingots, magnesium-nickel master alloys and magnesium Ingots are used as raw materials, and the raw materials are added to a dry smelting furnace, and smelted at a temperature of 760°C to 780°C for 3.5h to 5h to obtain a magnesium alloy melt;
二、对SiC颗粒进行预热,预热温度为490℃~510℃,保温时间为1.5h~2.5h,将预热后的SiC颗粒加入到步骤一得到的镁合金熔液中,搅拌10min~15min,得到镁基复合材料熔液;2. Preheat the SiC particles, the preheating temperature is 490℃~510℃, the holding time is 1.5h~2.5h, add the preheated SiC particles into the magnesium alloy melt obtained in step 1, and stir for 10min~ 15min, obtain magnesium-based composite material melt;
三、将步骤二制得的镁基复合材料熔液在铸造温度为710℃~740℃、铸造速度为2.0m/h~2.4m/h、冷却水强度为0.05MPa~0.10MPa和冷却水温度为10℃~20℃的条件下铸造成横截面的宽高比为3.2~3.6的镁基复合材料扁铸棒;3. The magnesium-based composite material melt obtained in step 2 is cast at a casting temperature of 710°C-740°C, a casting speed of 2.0m/h-2.4m/h, a cooling water strength of 0.05MPa-0.10MPa and a cooling water temperature of 0.05MPa-0.10MPa. A magnesium-based composite material flat cast rod with a cross-sectional aspect ratio of 3.2 to 3.6 is cast under the condition of 10°C to 20°C;
四、将步骤三得到的镁基复合材料扁铸棒切断,得到切断后的扁铸棒;Four, the magnesium-based composite material flat cast rod that step 3 is obtained is cut off, obtains the flat cast rod after cutting;
五、车去切断后的扁铸棒表面的铸造氧化皮,得到去氧化皮的镁基复合材料扁铸锭;5. Remove the casting scale on the surface of the cut-off flat cast rod by car to obtain a magnesium-based composite material flat cast ingot that has been descaled;
六、将去氧化皮的镁基复合材料扁铸锭在退火温度为380℃~400℃的退火炉中进行均匀化退火10h~15h,随炉冷却得到退火后的镁基复合材料扁铸锭;6. Perform homogenization annealing of the descaled magnesium-based composite flat ingot in an annealing furnace with an annealing temperature of 380°C to 400°C for 10h to 15h, and cool down with the furnace to obtain the annealed magnesium-based composite flat ingot;
七、将退火后的镁基复合材料扁铸锭放入加热炉中加热至360℃~430℃,然后放入到挤压机的扁挤压筒中,在压力为500MPa~550MPa、温度为360℃~430℃的条件下以流出速度为0.3m/min~0.7m/min进行挤压,制得镁基复合材料壁板型材;7. Put the annealed flat cast ingot of magnesium-based composite material into a heating furnace and heat it to 360°C-430°C, and then put it into the flat extrusion barrel of the extruder. Under the condition of ~430°C, extrude at an outflow speed of 0.3m/min~0.7m/min to obtain magnesium-based composite wall panel profiles;
八、将镁基复合材料壁板型材加热到150℃~180℃,然后进行张力矫直拉伸,并依次进行辊式矫直和人工矫直,得到矫直后的镁基复合材料壁板型材;8. Heat the magnesium-based composite wallboard profile to 150°C to 180°C, then perform tension straightening and stretching, and perform roller straightening and manual straightening in turn to obtain the straightened magnesium-based composite wallboard profile ;
九、切去矫直后的镁基复合材料壁板型材的头端和尾端,完成镁基复合材料壁板型材的制造;Nine, cut off the head end and tail end of the magnesium-based composite material wall panel profile after straightening, and complete the manufacture of the magnesium-based composite material wall panel profile;
其中步骤二SiC颗粒的加入量占镁合金熔液体积分数的3%~6%。Wherein the addition amount of the SiC particles in the second step accounts for 3%-6% of the integral fraction of the magnesium alloy melt.
本发明镁基复合材料壁板型材的制造方法通过合金成分的合理配比,采用均匀化退火消除晶内偏析和铸造应力,合理控制铸锭成分配比,保证了铸锭的成分稳定,组织均匀,使得镁基复合材料具有良好的塑性加工变形能力。The manufacturing method of the magnesium-based composite material wall plate profile of the present invention adopts a reasonable ratio of alloy components, adopts homogenization annealing to eliminate intragranular segregation and casting stress, and reasonably controls the distribution ratio of ingot components to ensure stable composition and uniform structure of the ingot. , so that the magnesium matrix composites have good plastic deformation ability.
壁板型材作为一种宽而薄并带有许多加强筋条的特殊型材。采用扁挤压筒挤压壁板型材,由于扁挤压筒的断面积小,形状和壁板外形相似,因此与现有圆挤压筒相比,扁挤压筒的挤压系数小、比压高,金属流动均匀,不闷车;它所挤出的壁板型材尺寸精确,易于矫直。镁基体具有密排六方晶体结构,对称性低,其轴比(c/a)值为1.623,接近理想的密排值1.633,室温滑移系少,冷加工成形困难。镁基复合材料壁板型材的加工温度如果低于150℃时,多晶镁的塑性变形仅限于基面{0001}滑移和锥面 孪生,变形时只有3个几何滑移系和2个独立滑移系,易在晶界处产生大的应力集中。而本发明步骤八将镁基复合材料壁板型材加热到150℃~180℃,高于150℃时温度升高增加了原子振动的振幅,最密排面和次密排面的差别减小,使附加角锥滑移面 启动,此时塑性大大提高;同时由于发生回复、再结晶而造成的软化,也会使镁基体具有较高的塑性,所以后续采用预热矫直拉伸工艺,达到了壁板型材的表面质量要求,使壁板型材的弯曲度每米小于1.5mm,型材任何部位的每米长度上绕纵轴的扭转度不超过1.5°,波浪高度低于0.5mm。The siding profile is a special profile that is wide and thin with many ribs. The flat extrusion cylinder is used to extrude the panel profile. Since the cross-sectional area of the flat extrusion cylinder is small and its shape is similar to that of the wall panel, compared with the existing round extrusion cylinder, the extrusion coefficient of the flat extrusion cylinder is small and relatively High pressure, uniform metal flow, no stuffiness; the extruded wallboard profiles are accurate in size and easy to straighten. The magnesium matrix has a close-packed hexagonal crystal structure with low symmetry, and its axial ratio (c/a) value is 1.623, which is close to the ideal close-packed value of 1.633. There are few slip systems at room temperature and it is difficult to form by cold working. If the processing temperature of magnesium-based composite wall panel profiles is lower than 150 °C, the plastic deformation of polycrystalline magnesium is limited to the base surface {0001} Slip and Cone Twins, there are only 3 geometric slip systems and 2 independent slip systems during deformation, and it is easy to generate large stress concentration at the grain boundary. However, step 8 of the present invention heats the magnesium-based composite wall plate profile to 150°C to 180°C. When the temperature is higher than 150°C, the amplitude of atomic vibration is increased, and the difference between the closest-packed surface and the second-closed-packed surface is reduced. make the additional pyramid slip surface At this time, the plasticity is greatly improved; at the same time, the softening caused by recovery and recrystallization will also make the magnesium matrix have higher plasticity, so the preheating straightening and stretching process is adopted subsequently to achieve the surface quality of the wall panel profile It is required that the bending degree of the panel profile be less than 1.5mm per meter, the twisting degree of any part of the profile around the longitudinal axis per meter length is not more than 1.5°, and the wave height is less than 0.5mm.
附图说明Description of drawings
图1为本发明步骤三得到的镁基复合材料扁铸棒的横截面结构示意图,其中b代表横截面的宽度,h代表横截面的高度,R代表圆弧的半径。Fig. 1 is the schematic diagram of the cross-sectional structure of the magnesium-based composite flat cast rod obtained in Step 3 of the present invention, wherein b represents the width of the cross-section, h represents the height of the cross-section, and R represents the radius of the arc.
具体实施方式detailed description
具体实施方式一:本实施方式镁基复合材料壁板型材的制造方法按下列步骤实施:Specific implementation mode one: the manufacturing method of the magnesium-based composite material wall plate profile of this implementation mode is implemented according to the following steps:
一、按元素的质量百分比为Al:0.2%、Mn:1.3%~2.2%、Zn:0.3%、Ce:0.15%~0.35%、Fe:≤0.05%、Si:≤0.1%、Cu:≤0.05%、Ni:≤0.007%,余量为Mg分别称取铝锭、镁锰中间合金、锌锭、镁铈中间合金、镁铁中间合金、镁硅中间合金、铜锭、镁镍中间合金和镁锭作为原料,将原料加入到干燥的熔炼炉中,在温度为760℃~780℃下熔炼3.5h~5h,得到镁合金熔液;1. According to the mass percentage of elements, Al: 0.2%, Mn: 1.3%-2.2%, Zn: 0.3%, Ce: 0.15%-0.35%, Fe: ≤0.05%, Si: ≤0.1%, Cu: ≤0.05 %, Ni: ≤0.007%, and the balance is Mg. Weigh aluminum ingots, magnesium-manganese master alloys, zinc ingots, magnesium-cerium master alloys, magnesium-iron master alloys, magnesium-silicon master alloys, copper ingots, magnesium-nickel master alloys and magnesium Ingots are used as raw materials, and the raw materials are added to a dry smelting furnace, and smelted at a temperature of 760°C to 780°C for 3.5h to 5h to obtain a magnesium alloy melt;
二、对SiC颗粒进行预热,预热温度为490℃~510℃,保温时间为1.5h~2.5h,将预热后的SiC颗粒加入到步骤一得到的镁合金熔液中,搅拌10min~15min,得到镁基复合材料熔液;2. Preheat the SiC particles, the preheating temperature is 490℃~510℃, the holding time is 1.5h~2.5h, add the preheated SiC particles into the magnesium alloy melt obtained in step 1, and stir for 10min~ 15min, obtain magnesium-based composite material melt;
三、将步骤二制得的镁基复合材料熔液在铸造温度为710℃~740℃、铸造速度为2.0m/h~2.4m/h、冷却水强度为0.05MPa~0.10MPa和冷却水温度为10℃~20℃的条件下铸造成横截面的宽高比为3.2~3.6的镁基复合材料扁铸棒;3. The magnesium-based composite material melt obtained in step 2 is cast at a casting temperature of 710°C-740°C, a casting speed of 2.0m/h-2.4m/h, a cooling water strength of 0.05MPa-0.10MPa and a cooling water temperature of 0.05MPa-0.10MPa. A magnesium-based composite material flat cast rod with a cross-sectional aspect ratio of 3.2 to 3.6 is cast under the condition of 10°C to 20°C;
四、将步骤三得到的镁基复合材料扁铸棒切断,得到切断后的扁铸棒;Four, the magnesium-based composite material flat cast rod that step 3 is obtained is cut off, obtains the flat cast rod after cutting;
五、车去切断后的扁铸棒表面的铸造氧化皮,得到去氧化皮的镁基复合材料扁铸锭;5. Remove the casting scale on the surface of the cut-off flat cast rod by car to obtain a magnesium-based composite material flat cast ingot that has been descaled;
六、将去氧化皮的镁基复合材料扁铸锭在退火温度为380℃~400℃的退火炉中进行均匀化退火10h~15h,随炉冷却得到退火后的镁基复合材料扁铸锭;6. Perform homogenization annealing of the descaled magnesium-based composite flat ingot in an annealing furnace with an annealing temperature of 380°C to 400°C for 10h to 15h, and cool down with the furnace to obtain the annealed magnesium-based composite flat ingot;
七、将退火后的镁基复合材料扁铸锭放入加热炉中加热至360℃~430℃,然后放入到挤压机的扁挤压筒中,在压力为500MPa~550MPa、温度为360℃~430℃的条件下以流出速度为0.3m/min~0.7m/min进行挤压,制得镁基复合材料壁板型材;7. Put the annealed flat cast ingot of magnesium-based composite material into a heating furnace and heat it to 360°C-430°C, and then put it into the flat extrusion barrel of the extruder. Under the condition of ~430°C, extrude at an outflow speed of 0.3m/min~0.7m/min to obtain magnesium-based composite wall panel profiles;
八、将镁基复合材料壁板型材加热到150℃~180℃,然后进行张力矫直拉伸,并依次进行辊式矫直和人工矫直,得到矫直后的镁基复合材料壁板型材;8. Heat the magnesium-based composite wallboard profile to 150°C to 180°C, then perform tension straightening and stretching, and perform roller straightening and manual straightening in turn to obtain the straightened magnesium-based composite wallboard profile ;
九、切去矫直后的镁基复合材料壁板型材的头端和尾端,完成镁基复合材料壁板型材的制造;Nine, cut off the head end and tail end of the magnesium-based composite material wall panel profile after straightening, and complete the manufacture of the magnesium-based composite material wall panel profile;
其中步骤二SiC颗粒的加入量占镁合金熔液体积分数的3%~6%。Wherein the addition amount of the SiC particles in the second step accounts for 3%-6% of the integral fraction of the magnesium alloy melt.
在一定的变形程度范围内,挤压系数越大,壁板型材的强度、硬度越高。当减少挤压系数时,壁板型材的强度受到损失。因此,本实施方式采用SiC颗粒增强镁基复合材料。SiC颗粒作为镁合金基体的增强相,主要分布于晶界间,能够阻止晶界和位错的运动,导致强度大幅度提高,以弥补由挤压变形程度减少而造成壁板型材的强度损失。Within a certain range of deformation, the greater the extrusion coefficient, the higher the strength and hardness of the panel profile. When reducing the extrusion factor, the strength of the siding profile suffers. Therefore, this embodiment adopts SiC particles to reinforce the magnesium-based composite material. As the reinforcing phase of the magnesium alloy matrix, SiC particles are mainly distributed between the grain boundaries, which can prevent the movement of grain boundaries and dislocations, resulting in a significant increase in strength to compensate for the strength loss of the wall plate profile caused by the reduction in extrusion deformation.
本实施方式步骤九由于挤压制品的前端保留铸造组织,机械性能偏低,应该切除;在尾端由于金属填充不满所形成的挤压缩尾等破坏金属连续性的缺陷亦应切除。In Step 9 of this embodiment, since the front end of the extruded product retains the casting structure, the mechanical properties are relatively low, so it should be removed; at the tail end, defects that destroy the continuity of the metal, such as the extruded tail formed by insufficient metal filling, should also be removed.
具体实施方式二:本实施方式与具体实施方式一不同的是步骤一将原料加入到干燥的熔炼炉中,在温度为770℃下熔炼4h。其它步骤及参数与具体实施方式一相同。Specific embodiment 2: The difference between this embodiment and specific embodiment 1 is that in step 1, raw materials are added into a dry smelting furnace and smelted at a temperature of 770° C. for 4 hours. Other steps and parameters are the same as those in Embodiment 1.
具体实施方式三:本实施方式与具体实施方式一或二不同的是步骤二所述的SiC颗粒的粒度为5μm~8μm。其它步骤及参数与具体实施方式一或二相同。Embodiment 3: This embodiment differs from Embodiment 1 or Embodiment 2 in that the particle size of the SiC particles described in Step 2 is 5 μm˜8 μm. Other steps and parameters are the same as those in Embodiment 1 or Embodiment 2.
具体实施方式四:本实施方式与具体实施方式一至三之一不同的是步骤三铸造成横截面的两侧为圆弧形,横截面的宽度b为545~565mm,高度h为150~170mm的镁基复合材料扁铸棒。其它步骤及参数与具体实施方式一至三之一相同。Embodiment 4: The difference between this embodiment and Embodiments 1 to 3 is that in step 3, the two sides of the cross-section are arc-shaped, the width b of the cross-section is 545-565 mm, and the height h is 150-170 mm. Magnesium matrix composite flat cast rod. Other steps and parameters are the same as those in Embodiments 1 to 3.
本实施方式所述的镁基复合材料扁铸棒的横截面的中部为矩形,在矩形的短边侧为半圆形,半圆的半径R为h/2。The middle part of the cross-section of the magnesium-based composite flat cast rod described in this embodiment is a rectangle, and the short side of the rectangle is a semicircle, and the radius R of the semicircle is h/2.
具体实施方式五:本实施方式与具体实施方式一至四之一不同的是步骤四切断后的扁铸棒的长度为900mm~950mm。其它步骤及参数与具体实施方式一至四之一相同。Embodiment 5: This embodiment is different from Embodiment 1 to Embodiment 4 in that the length of the flat cast rod after cutting in Step 4 is 900mm-950mm. Other steps and parameters are the same as in one of the specific embodiments 1 to 4.
具体实施方式六:本实施方式与具体实施方式一至五之一不同的是步骤六在退火温度为390℃的退火炉中进行均匀化退火12h。其它步骤及参数与具体实施方式一至五之一相同。Embodiment 6: The difference between this embodiment and one of Embodiments 1 to 5 is that in step 6, homogenization annealing is performed in an annealing furnace with an annealing temperature of 390° C. for 12 hours. Other steps and parameters are the same as one of the specific embodiments 1 to 5.
具体实施方式七:本实施方式与具体实施方式一至六之一不同的是步骤七在压力为530MPa、温度为390℃的条件下以流出速度为0.5m/min进行挤压。其它步骤及参数与具体实施方式一至六之一相同。Embodiment 7: This embodiment differs from Embodiment 1 to Embodiment 6 in that step 7 is extruded at a pressure of 530 MPa and a temperature of 390° C. at an outflow velocity of 0.5 m/min. Other steps and parameters are the same as one of the specific embodiments 1 to 6.
具体实施方式八:本实施方式与具体实施方式一至七之一不同的是步骤八镁基复合材料壁板型材加热到160℃。其它步骤及参数与具体实施方式一至七之一相同。Embodiment 8: This embodiment is different from Embodiment 1 to Embodiment 7 in that Step 8 heats the magnesium-based composite wall plate profile to 160°C. Other steps and parameters are the same as one of the specific embodiments 1 to 7.
具体实施方式九:本实施方式与具体实施方式一至八之一不同的是步骤八张力矫直拉伸的拉伸变形率为1%~3%。其它步骤及参数与具体实施方式一至八之一相同。Embodiment 9: The difference between this embodiment and Embodiment 1 to Embodiment 8 is that the tensile deformation rate of step 8 is 1% to 3% in tension straightening and stretching. Other steps and parameters are the same as those in Embodiments 1 to 8.
实施例一:本实施例镁基复合材料壁板型材的制造方法按下列步骤实施:Embodiment 1: The manufacturing method of the magnesium-based composite wall plate profile of this embodiment is implemented according to the following steps:
一、按元素的质量百分比为Al:0.2%、Mn:1.8%、Zn:0.3%、Ce:0.2%、Fe:0.03%、Si:0.02%、Cu:0.02%、Ni:0.003%,余量为Mg分别称取铝锭、镁锰中间合金、锌锭、镁铈中间合金、镁铁中间合金、镁硅中间合金、铜锭、镁镍中间合金和镁锭作为原料,将原料加入到干燥的熔炼炉中,在温度为770℃下熔炼4h,得到镁合金熔液;1. According to the mass percentage of elements, Al: 0.2%, Mn: 1.8%, Zn: 0.3%, Ce: 0.2%, Fe: 0.03%, Si: 0.02%, Cu: 0.02%, Ni: 0.003%, and the balance Weigh aluminum ingots, magnesium-manganese master alloys, zinc ingots, magnesium-cerium master alloys, magnesium-iron master alloys, magnesium-silicon master alloys, copper ingots, magnesium-nickel master alloys and magnesium ingots as raw materials for Mg, and add the raw materials to the dry In the smelting furnace, smelting at a temperature of 770°C for 4 hours to obtain a magnesium alloy melt;
二、将粒度为6μm的SiC颗粒进行预热,预热温度为500℃,保温时间为2.0h,将预热后的SiC颗粒迅速加入到步骤一制得的镁合金熔液中,搅拌13min,SiC颗粒的加入量为镁合金熔液体积分数的4%,得到镁基复合材料熔液;2. Preheat the SiC particles with a particle size of 6 μm. The preheating temperature is 500°C, and the holding time is 2.0h. The preheated SiC particles are quickly added to the magnesium alloy melt prepared in step 1, and stirred for 13 minutes. The amount of SiC particles added is 4% of the integral fraction of the magnesium alloy melt to obtain a magnesium-based composite material melt;
三、将步骤二制得的镁基复合材料熔液在铸造温度为730℃、铸造速度为2.2m/h、冷却水强度为0.08MPa和冷却水温度为15℃的条件下铸造成横截面的宽为555mm、高为160mm的镁基复合材料扁铸棒;3. Cast the molten magnesium-based composite material obtained in step 2 into a cross-section at a casting temperature of 730°C, a casting speed of 2.2m/h, a cooling water strength of 0.08MPa, and a cooling water temperature of 15°C. Magnesium-based composite material flat cast rod with a width of 555mm and a height of 160mm;
四、将步骤二得到的镁基复合材料扁铸棒切断,得到切断后长度为930mm扁铸棒;Four, the magnesium-based composite material flat cast rod that step 2 is obtained is cut off, and the length obtained after cutting is a 930mm flat cast rod;
五、车去切断后的扁铸棒表面的铸造氧化皮,得到宽为545mm、高为150mm的去氧化皮的镁基复合材料扁铸锭;Five, car removes the casting scale on the surface of the flat cast rod after cutting, and obtains a magnesium-based composite material flat cast ingot that is 545mm wide and 150mm high in scale;
六、将去氧化皮的镁基复合材料扁铸锭在退火温度为390℃的退火炉中进行均匀化退火12h,随炉冷却,得到退火后的镁基复合材料扁铸锭;6. Perform homogenization annealing on the descaled magnesium-based composite flat ingot in an annealing furnace with an annealing temperature of 390° C. for 12 hours, and cool with the furnace to obtain an annealed magnesium-based composite flat ingot;
七、将退火后的镁基复合材料扁铸锭放入加热炉中加热至400℃,然后放入到挤压机的扁挤压筒中,在压力为530MPa、温度为390℃的条件下以流出速度为0.5m/min进行挤压,制得镁基复合材料壁板型材;7. Put the annealed magnesium-based composite flat ingot into a heating furnace and heat it to 400°C, then put it into the flat extrusion barrel of the extruder, and flow it out under the conditions of a pressure of 530MPa and a temperature of 390°C Extruding at a speed of 0.5m/min to obtain a magnesium-based composite wall plate profile;
八、将镁基复合材料壁板型材加热到160℃,然后进行张力矫直拉伸,拉伸变形率为2%,并依次进行辊式矫直和人工矫直,得到矫直后的镁基复合材料壁板型材;8. Heating the magnesium-based composite wall plate profile to 160°C, then performing tension straightening and stretching, the tensile deformation rate is 2%, and performing roller straightening and manual straightening in turn to obtain the straightened magnesium-based Composite siding profiles;
九、切去矫直后的镁基复合材料壁板型材的150mm头端和300mm尾端,完成镁基复合材料壁板型材的制造。9. Cut off the 150mm head end and the 300mm tail end of the straightened magnesium-based composite material wall plate profile to complete the manufacture of the magnesium-based composite material wall plate profile.
本实施例得到的镁基复合材料壁板型材的弯曲度每米为1.2mm,型材任何部位的每米长度上绕纵轴的扭转度为1°,波浪高度为0.3mm。本实施例中弯曲度、扭拧度、波浪高度按GB/T14846-2008标准测试。型材表面质量好,尺寸精度高,成品率为80%,力学性能稳定,其抗拉强度为350MPa,延伸率为6.5%。挤压过程由于挤压系数小、比压高,所需挤压力小,金属流动均匀,因此,没发生闷车现象。The degree of curvature of the magnesium-based composite panel profile obtained in this embodiment is 1.2 mm per meter, the twist degree of any part of the profile around the longitudinal axis is 1° per meter, and the wave height is 0.3 mm. In this embodiment, the bending degree, twisting degree and wave height are tested according to GB/T14846-2008 standard. The profile has good surface quality, high dimensional accuracy, yield rate of 80%, stable mechanical properties, tensile strength of 350MPa, and elongation of 6.5%. In the extrusion process, due to the small extrusion coefficient and high specific pressure, the required extrusion force is small, and the metal flow is uniform, so there is no stuffy phenomenon.
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