CN117448636A - Preparation and processing method of high heat-resistant dispersion strengthening Al-Mg-Mn-Zr-Cr-Mo alloy - Google Patents
Preparation and processing method of high heat-resistant dispersion strengthening Al-Mg-Mn-Zr-Cr-Mo alloy Download PDFInfo
- Publication number
- CN117448636A CN117448636A CN202311440248.5A CN202311440248A CN117448636A CN 117448636 A CN117448636 A CN 117448636A CN 202311440248 A CN202311440248 A CN 202311440248A CN 117448636 A CN117448636 A CN 117448636A
- Authority
- CN
- China
- Prior art keywords
- alloy
- percent
- temperature
- treatment
- room temperature
- 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.)
- Pending
Links
- 229910001182 Mo alloy Inorganic materials 0.000 title claims abstract description 32
- 239000006185 dispersion Substances 0.000 title claims abstract description 19
- 238000005728 strengthening Methods 0.000 title claims abstract description 16
- 238000002360 preparation method Methods 0.000 title abstract description 12
- 238000003672 processing method Methods 0.000 title abstract description 11
- 239000000956 alloy Substances 0.000 claims abstract description 87
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 86
- 230000032683 aging Effects 0.000 claims abstract description 56
- 238000011282 treatment Methods 0.000 claims abstract description 50
- 239000012535 impurity Substances 0.000 claims abstract description 31
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 11
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 11
- 238000005098 hot rolling Methods 0.000 claims abstract description 4
- 238000001816 cooling Methods 0.000 claims abstract 4
- 230000009467 reduction Effects 0.000 claims description 32
- 238000000034 method Methods 0.000 claims description 25
- 239000002994 raw material Substances 0.000 claims description 24
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 20
- 238000005096 rolling process Methods 0.000 claims description 16
- 230000008569 process Effects 0.000 claims description 15
- 230000008018 melting Effects 0.000 claims description 12
- 238000002844 melting Methods 0.000 claims description 12
- 229910052786 argon Inorganic materials 0.000 claims description 10
- 238000007872 degassing Methods 0.000 claims description 10
- 239000002893 slag Substances 0.000 claims description 10
- 229910052725 zinc Inorganic materials 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000010791 quenching Methods 0.000 claims 1
- 230000000171 quenching effect Effects 0.000 claims 1
- 229910000838 Al alloy Inorganic materials 0.000 abstract description 11
- 230000000694 effects Effects 0.000 abstract description 10
- 238000012545 processing Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 229910000714 At alloy Inorganic materials 0.000 abstract 1
- 238000003723 Smelting Methods 0.000 abstract 1
- 230000000052 comparative effect Effects 0.000 description 18
- 229910052802 copper Inorganic materials 0.000 description 17
- 239000010949 copper Substances 0.000 description 17
- 238000012360 testing method Methods 0.000 description 17
- 229910052726 zirconium Inorganic materials 0.000 description 12
- 229910052804 chromium Inorganic materials 0.000 description 11
- 229910052750 molybdenum Inorganic materials 0.000 description 11
- 229910052748 manganese Inorganic materials 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- 238000001556 precipitation Methods 0.000 description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 8
- 229910000831 Steel Inorganic materials 0.000 description 8
- 229910002804 graphite Inorganic materials 0.000 description 8
- 239000010439 graphite Substances 0.000 description 8
- 238000000227 grinding Methods 0.000 description 8
- 239000000155 melt Substances 0.000 description 8
- 239000010959 steel Substances 0.000 description 8
- 238000003756 stirring Methods 0.000 description 8
- 239000004575 stone Substances 0.000 description 8
- 238000009826 distribution Methods 0.000 description 7
- 238000005275 alloying Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 238000005097 cold rolling Methods 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000011160 research Methods 0.000 description 4
- 230000002195 synergetic effect Effects 0.000 description 4
- 229910000599 Cr alloy Inorganic materials 0.000 description 3
- 229910000914 Mn alloy Inorganic materials 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 210000001787 dendrite Anatomy 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 229910018134 Al-Mg Inorganic materials 0.000 description 1
- 229910018467 Al—Mg Inorganic materials 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000006911 nucleation Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 238000002203 pretreatment Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- 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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
-
- 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
- C22F1/002—Changing 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
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)
- Heat Treatment Of Steel (AREA)
Abstract
Description
技术领域Technical field
本发明涉及一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,属于铝合金加工制造领域。The invention relates to a preparation and processing method of a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy, belonging to the field of aluminum alloy processing and manufacturing.
背景技术Background technique
5000系Al-Mg基合金因其高比强度、高刚度、耐蚀性和可焊性的良好结合,在海洋轮船、汽车零部件和焊接结构件等领域中得到广泛应用。传统5xxx系铝合金属于不可时效强化型铝合金,其主要通过溶质Mg原子的固溶强化和加工硬化获得中等强度。5000 series Al-Mg-based alloys are widely used in fields such as marine ships, automotive parts and welded structural parts due to their good combination of high specific strength, high stiffness, corrosion resistance and weldability. Traditional 5xxx series aluminum alloys are non-age-strengthenable aluminum alloys, which obtain medium strength mainly through solid solution strengthening and work hardening of solute Mg atoms.
为了提高不可时效强化型铝合金的力学性能,人们通过添加微合金化元素来实现弥散强化。因此,我们通过向5000系铝合金中添加Mn元素,在热处理过程中实现过饱和固溶体的分解,从而产生含有复杂晶体结构的Mn弥散相。这些含Mn的弥散相有可能在传统的不可时效强化型铝合金中获得额外的弥散强化效果。一般来说,这些弥散相的弥散强化效果主要取决于它们的类型、形貌、尺寸以及在基体中的数密度,而所有这些都随着不同微合金化和加工工艺的不同而显著变化。In order to improve the mechanical properties of non-age-hardenable aluminum alloys, dispersion strengthening is achieved by adding micro-alloying elements. Therefore, by adding Mn element to the 5000 series aluminum alloy, we achieve the decomposition of the supersaturated solid solution during the heat treatment process, thereby producing a Mn dispersed phase containing a complex crystal structure. These Mn-containing dispersed phases may obtain additional dispersion strengthening effects in traditional non-age-strengthenable aluminum alloys. Generally speaking, the dispersion strengthening effect of these dispersed phases mainly depends on their type, morphology, size and number density in the matrix, all of which vary significantly with different microalloying and processing processes.
目前,主要采用不同的单级和多级时效处理来促进Al-Mg-Mn合金中含Mn弥散相析出,然而仅依靠现有的热处理工艺并不能达到明显的弥散强化效果。另一方面,含Mn弥散相的不均匀分布是含Mn铝合金时效处理后的普遍现象。由于凝固过程的微观偏析,在枝晶中心处会形成无弥散析出带会进一步削弱其弥散强化效果。而传统的时效处理很难减少或消除枝晶中心处的无弥散析出带。因此,迫切需要开发其他解决方案,以实现5000合金中含Mn弥散相更好的弥散强化效果。除此之外,为保证合金材料在高温服役状态下的热稳定性,进一步提升富Mn弥散相的高温热稳定性势在必行。At present, different single-stage and multi-stage aging treatments are mainly used to promote the precipitation of Mn-containing dispersed phases in Al-Mg-Mn alloys. However, the existing heat treatment process alone cannot achieve obvious dispersion strengthening effects. On the other hand, the uneven distribution of Mn-containing dispersed phases is a common phenomenon after aging treatment of Mn-containing aluminum alloys. Due to microsegregation during the solidification process, a non-dispersed precipitation zone will be formed at the center of the dendrites, which will further weaken its dispersion strengthening effect. However, traditional aging treatment is difficult to reduce or eliminate the non-dispersed precipitation zone in the center of dendrites. Therefore, there is an urgent need to develop other solutions to achieve better dispersion strengthening effects of Mn-containing dispersed phases in 5000 alloy. In addition, in order to ensure the thermal stability of alloy materials under high-temperature service conditions, it is imperative to further improve the high-temperature thermal stability of the Mn-rich dispersed phase.
发明内容Contents of the invention
本发明的目的在于提供一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,旨在提高耐热弥散强化型铝合金时效响应能力和强度。The purpose of the present invention is to provide a preparation and processing method of a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy, aiming to improve the aging response capability and strength of the heat-resistant dispersion-strengthened aluminum alloy.
为了实现上述目的,本发明采取以下技术方案:In order to achieve the above objects, the present invention adopts the following technical solutions:
本发明提供一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金,按照质量百分比计:Mg:2.0~6.0%,Mn:0.5~1.5%,Zr:0.1~0.5%,Cr:0.1~0.5%,Mo:0.1~0.5%,余量为铝及不可避免的杂质;其中杂质来源于原料,其不可避免,杂质含量为:Si:0.1-0.5%,Fe:0.1-0.5%,Cu≤0.05%,Zn≤0.05%。The invention provides a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy. In terms of mass percentage: Mg: 2.0-6.0%, Mn: 0.5-1.5%, Zr: 0.1-0.5%. Cr: 0.1~0.5%, Mo: 0.1~0.5%, the balance is aluminum and unavoidable impurities; the impurities are derived from raw materials and are unavoidable. The impurity content is: Si: 0.1-0.5%, Fe: 0.1-0.5 %, Cu≤0.05%, Zn≤0.05%.
本发明还提供了所述的Al-Mg-Mn-Zr-Cr-Mo合金的制备及加工方法,包括以下步骤:The invention also provides a preparation and processing method of the Al-Mg-Mn-Zr-Cr-Mo alloy, which includes the following steps:
按照成分配比配料,得到混合原料;Mix ingredients according to the ingredient ratio to obtain mixed raw materials;
将所述混合原料加热熔融后浇筑,得到铸锭;The mixed raw materials are heated and melted and then poured to obtain an ingot;
将所述铸锭合金高温预时效处理,随后冷却;将预时效处理后的样品进行预变形,随后进行人工时效硬化处理,最后进行热轧处理,得到轧板。The ingot alloy is pre-aged at high temperature and then cooled; the pre-aged sample is pre-deformed, then artificially aged and hardened, and finally hot-rolled to obtain a rolled plate.
优选的,所述得到铸锭的过程具体为:Preferably, the process of obtaining the ingot is specifically:
将所述混合原料加热至850~900℃,熔化后保温30~50min,降温至740~760℃进行流氩除气,将得到的熔体静置扒渣后于730~750℃浇注于预热至200~250℃的模具中,得到铸锭。Heat the mixed raw materials to 850-900°C, keep the temperature for 30-50 minutes after melting, cool to 740-760°C for argon degassing, and let the resulting melt stand for slag removal before pouring it into the preheated oven at 730-750°C. to a mold at 200-250°C to obtain an ingot.
优选的,所述预时效温度在200-300℃之间,保温时间为0.5-36h,随后空冷或淬火至室温。Preferably, the pre-aging temperature is between 200-300°C, the holding time is 0.5-36h, and then air-cooled or quenched to room temperature.
优选的,所述预变形工艺为室温冷轧制变形,道次压下量为1~3%,总压下量为5~15%;或预变形工艺为室温预拉伸,拉伸速率为1×10-3s-1,应变量为2~6%;Preferably, the pre-deformation process is room temperature cold rolling deformation, the pass reduction is 1 to 3%, and the total reduction is 5 to 15%; or the pre-deformation process is room temperature pre-stretching, and the stretching rate is 1×10 -3 s -1 , the strain is 2~6%;
优选的,所述人工时效硬化处理其温度为400~425℃,时间为4~24h。Preferably, the artificial aging hardening treatment is performed at a temperature of 400 to 425°C and a time of 4 to 24 hours.
优选的,所述热轧的温度为280~320℃,道次压下量为5~10%,总压下量为65%~75%。Preferably, the hot rolling temperature is 280-320°C, the pass reduction is 5-10%, and the total reduction is 65%-75%.
有益效果:Beneficial effects:
1、本发明公开了一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金,利用Zr、Cr、Mo多元协同的微合金化促进纳米级α相和Al3Zr弥散粒子的析出,而有利于提高合金的室温和高温强度。1. The present invention discloses a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy, which utilizes multi-component synergistic micro-alloying of Zr, Cr, and Mo to promote nanoscale α phase and Al 3 Zr dispersed particles. The precipitation will help improve the room temperature and high temperature strength of the alloy.
2、本发明还公开了Al-Mg-Mn-Zr-Cr-Mo合金的制备及加工方法,通过对铸态合金进行预时效+预应变协同作用,以抑制合金中的无弥散粒子析出带的形成,并提高弥散相的析出密度和细化弥散相的尺寸,从而提高合金的强度,2. The present invention also discloses a preparation and processing method of Al-Mg-Mn-Zr-Cr-Mo alloy, which uses the synergistic effect of pre-aging + pre-straining on the as-cast alloy to suppress the formation of non-dispersed particle precipitation zones in the alloy. Form, and increase the precipitation density of the dispersed phase and refine the size of the dispersed phase, thereby improving the strength of the alloy,
附图说明Description of the drawings
图1为在经过不同的预处理方法后的实施例1、参考例1和参考例2合金在400℃时效处理过程中的硬度变化。Figure 1 shows the hardness changes of the alloys of Example 1, Reference Example 1 and Reference Example 2 after different pretreatment methods during the aging treatment at 400°C.
图2是实施例1合金在400℃时效处理12h后的TEM明场像。Figure 2 is a TEM bright field image of the alloy of Example 1 after aging treatment at 400°C for 12 hours.
图3是参考例1合金在400℃时效处理12h后的TEM明场像。Figure 3 is a TEM bright field image of the alloy of Reference Example 1 after aging treatment at 400°C for 12 hours.
图4是参考例2合金在400℃时效处理12h后的TEM明场像。Figure 4 is the TEM bright field image of the alloy in Reference Example 2 after aging treatment at 400°C for 12 hours.
具体实施方法Specific implementation methods
下面结合具体实例对本发明进行详细说明,以下实施例将有助于本领域的研究人员进一步理解本发明,但不以任何形式限制本发明。应当指出的是,在不脱离本发明构思的前提下,仍可以做出若干改进,这些都属于本发明的保护范围。The present invention will be described in detail below with reference to specific examples. The following examples will help researchers in the field further understand the present invention, but do not limit the present invention in any form. It should be noted that, without departing from the concept of the present invention, several improvements can still be made, and these all belong to the protection scope of the present invention.
实施例1Example 1
本实施例中的一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,包括以下步骤:The preparation and processing method of a highly heat-resistant dispersion strengthened Al-Mg-Mn-Zr-Cr-Mo alloy in this embodiment includes the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.2%,Mo:0.2%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, in which the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.2%, Mo: 0.2%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对步骤1所得铸态Al-Mg-Mn-Zr-Cr-Mo合金在300℃进行预时效处理。预时效处理时间为8h,空冷至室温;Step 2: Pre-age the as-cast Al-Mg-Mn-Zr-Cr-Mo alloy obtained in Step 1 at 300°C. The pre-aging treatment time is 8 hours, and air-cooled to room temperature;
步骤3、对经过步骤2所得的合金板材开展室温冷轧,道次压下量为2%,轧制速度0.1ms-1,总压下量10%;Step 3. Carry out room temperature cold rolling on the alloy sheet obtained in step 2, with a pass reduction of 2%, a rolling speed of 0.1ms -1 and a total reduction of 10%;
步骤4、对经过步骤3所得的合金在400℃进行等温时效处理。Step 4: Perform isothermal aging treatment on the alloy obtained in Step 3 at 400°C.
步骤5、对经过步骤4在400℃下时效处理12h后所得的合金开展热轧处理,轧制温度为320℃,道次压下量为10%,总压下量为70%。Step 5: Hot-roll the alloy obtained after aging treatment at 400°C for 12 hours in Step 4. The rolling temperature is 320°C, the pass reduction is 10%, and the total reduction is 70%.
图1为步骤4中合金在时效过程中的硬度变化曲线。图2为步骤4中合金在400℃下时效处理12h后的TEM明场像。表2为步骤4中合金在400℃下时效处理12h后的析出相统计分布。对步骤4中合金在400℃下时效处理12h后进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为178.5±2.5MPa,抗拉强度为291.9±10.8MPa,延伸率为7.1±0.5%。对步骤5所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为310.5±1.3MPa,抗拉强度为395.6±8.7MPa,延伸率为11.1±0.6%。对步骤5所得到的合金进行300℃高温拉伸力学性能测试。拉伸性能见表3,最终屈服强度为119.2±2.8MPa,抗拉强度为119.2±2.8MPa,延伸率为45.5±5.6%。Figure 1 shows the hardness change curve of the alloy during the aging process in step 4. Figure 2 is the TEM bright field image of the alloy after aging treatment at 400°C for 12 hours in step 4. Table 2 shows the statistical distribution of precipitated phases after the alloy was aged at 400°C for 12 hours in step 4. After the alloy in step 4 is aged at 400°C for 12 hours, the tensile mechanical properties at room temperature are tested. The tensile properties are shown in Table 1. The final yield strength is 178.5±2.5MPa, the tensile strength is 291.9±10.8MPa, and the elongation is 7.1±0.5%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 5. The tensile properties are shown in Table 1. The final yield strength is 310.5±1.3MPa, the tensile strength is 395.6±8.7MPa, and the elongation is 11.1±0.6%. The alloy obtained in step 5 was subjected to a high temperature tensile mechanical property test at 300°C. The tensile properties are shown in Table 3. The final yield strength is 119.2±2.8MPa, the tensile strength is 119.2±2.8MPa, and the elongation is 45.5±5.6%.
实施例2Example 2
本实施例中的一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,包括以下步骤:The preparation and processing method of a highly heat-resistant dispersion strengthened Al-Mg-Mn-Zr-Cr-Mo alloy in this embodiment includes the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.2%,Mo:0.1%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, where the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.2%, Mo: 0.1%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对步骤1所得铸态Al-Mg-Mn-Zr-Cr-Mo合金在200℃下进行预时效处理。预时效处理时间为36h,淬火至室温;Step 2: Pre-age the as-cast Al-Mg-Mn-Zr-Cr-Mo alloy obtained in Step 1 at 200°C. The pre-aging treatment time is 36 hours and quenched to room temperature;
步骤3、对经过步骤2所得的合金开展室温冷轧,道次压下量为3%,轧制速度0.1ms-1,总压下量15%;Step 3. Carry out room temperature cold rolling on the alloy obtained in step 2, with a pass reduction of 3%, a rolling speed of 0.1ms -1 and a total reduction of 15%;
步骤4、对经过步骤3所得的合金在425℃下进行时效处理,时效处理时间为12h。Step 4. Aging treatment is performed on the alloy obtained in Step 3 at 425°C, and the aging treatment time is 12 hours.
步骤5、对经过步骤4所得的合金开展热轧处理,轧制温度为300℃,道次压下量为10%,总压下量为75%。Step 5: Hot-roll the alloy obtained in Step 4. The rolling temperature is 300°C, the pass reduction is 10%, and the total reduction is 75%.
对步骤4所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为175.5±3.6MPa,抗拉强度为286.9±8.7MPa,延伸率为6.2±1.3%。对步骤5所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为304.6±2.6MPa,抗拉强度为393.8±6.2MPa,延伸率为10.2±0.7%。Conduct room temperature tensile mechanical properties test on the alloy obtained in step 4. The tensile properties are shown in Table 1. The final yield strength is 175.5±3.6MPa, the tensile strength is 286.9±8.7MPa, and the elongation is 6.2±1.3%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 5. The tensile properties are shown in Table 1. The final yield strength is 304.6±2.6MPa, the tensile strength is 393.8±6.2MPa, and the elongation is 10.2±0.7%.
实施例3Example 3
本实施例中的一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,包括以下步骤:The preparation and processing method of a highly heat-resistant dispersion strengthened Al-Mg-Mn-Zr-Cr-Mo alloy in this embodiment includes the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.1%,Mo:0.1%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, in which the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.1%, Mo: 0.1%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对步骤1所得铸态Al-Mg-Mn-Zr-Cr-Mo合金在300℃下进行预时效处理。预时效处理时间为30min,淬火至室温;Step 2: Pre-age the as-cast Al-Mg-Mn-Zr-Cr-Mo alloy obtained in Step 1 at 300°C. The pre-aging treatment time is 30 minutes and quenched to room temperature;
步骤3、对经过步骤2所得的合金开展室温拉伸,应变速率1×10-3s-1,应变量6%;Step 3. Tensile the alloy obtained in Step 2 at room temperature, with a strain rate of 1×10 -3 s -1 and a strain of 6%;
步骤4、对经过步骤3所得的合金在400℃下进行时效处理,时效处理时间为24h。Step 4. Perform aging treatment on the alloy obtained in step 3 at 400°C, and the aging treatment time is 24 hours.
步骤5、对经过步骤4所得的合金开展热轧处理,轧制温度为300℃,道次压下量为10%,总压下量为70%。Step 5: Hot-roll the alloy obtained in Step 4. The rolling temperature is 300°C, the pass reduction is 10%, and the total reduction is 70%.
对步骤4所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为176.3±2.4MPa,抗拉强度为289.3±5.5MPa,延伸率为6.7±0.8%。对步骤5所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为305.7±3.8MPa,抗拉强度为393.7±4.2MPa,延伸率为9.6±1.1%。Conduct room temperature tensile mechanical properties test on the alloy obtained in step 4. The tensile properties are shown in Table 1. The final yield strength is 176.3±2.4MPa, the tensile strength is 289.3±5.5MPa, and the elongation is 6.7±0.8%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 5. The tensile properties are shown in Table 1. The final yield strength is 305.7±3.8MPa, the tensile strength is 393.7±4.2MPa, and the elongation is 9.6±1.1%.
实施例4Example 4
本实施例中的一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,包括以下步骤:The preparation and processing method of a highly heat-resistant dispersion strengthened Al-Mg-Mn-Zr-Cr-Mo alloy in this embodiment includes the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.1%,Mo:0.2%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, where the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.1%, Mo: 0.2%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对步骤1所得铸态Al-Mg-Mn-Zr-Cr-Mo合金在300℃下进行预时效处理。预时效处理时间为12h,空冷至室温;Step 2: Pre-age the as-cast Al-Mg-Mn-Zr-Cr-Mo alloy obtained in Step 1 at 300°C. The pre-aging treatment time is 12 hours, and air-cooled to room temperature;
步骤3、对经过步骤2所得的合金开展室温拉伸,应变速率1×10-3s-1,应变量6%;Step 3. Tensile the alloy obtained in Step 2 at room temperature, with a strain rate of 1×10 -3 s -1 and a strain of 6%;
步骤4、对经过步骤3所得的合金在425℃下进行时效处理,时效处理时间为24h。Step 4. Aging treatment is performed on the alloy obtained in step 3 at 425°C, and the aging treatment time is 24 hours.
步骤5、对经过步骤4所得的合金开展热轧处理,轧制温度为300℃,道次压下量为10%,总压下量为70%。Step 5: Hot-roll the alloy obtained in Step 4. The rolling temperature is 300°C, the pass reduction is 10%, and the total reduction is 70%.
对步骤4所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为175.8±1.9MPa,抗拉强度为288.9±6.3MPa,延伸率为6.3±0.7%。对步骤5所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为301.8±5.1MPa,抗拉强度为388.4±6.1MPa,延伸率为9.3±0.8%。Conduct room temperature tensile mechanical properties test on the alloy obtained in step 4. The tensile properties are shown in Table 1. The final yield strength is 175.8±1.9MPa, the tensile strength is 288.9±6.3MPa, and the elongation is 6.3±0.7%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 5. The tensile properties are shown in Table 1. The final yield strength is 301.8±5.1MPa, the tensile strength is 388.4±6.1MPa, and the elongation is 9.3±0.8%.
对比例1Comparative example 1
本对比例采用一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金作为研究实例,包括以下步骤:This comparative example uses a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy as a research example, including the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.2%,Mo:0.2%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, in which the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.2%, Mo: 0.2%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对经过步骤1所得的合金在室温下冷轧,道次压下量为2%,轧制速度0.1ms-1,总压下量10%;Step 2. Cold-roll the alloy obtained in Step 1 at room temperature with a pass reduction of 2%, a rolling speed of 0.1ms -1 and a total reduction of 10%;
步骤3、对经过步骤2所得的合金在400℃下进行时效处理。Step 3: Aging treatment is performed on the alloy obtained in Step 2 at 400°C.
步骤4、对经过步骤3在400℃下时效处理12h后所得的合金开展热轧处理,轧制温度为320℃,道次压下量为10%,总压下量为70%。Step 4: Hot-roll the alloy obtained after aging treatment at 400°C for 12 hours in step 3. The rolling temperature is 320°C, the pass reduction is 10%, and the total reduction is 70%.
图1为步骤3中合金在时效过程中的硬度变化曲线。图3为步骤3中合金在400℃下时效处理12h后的TEM明场像。表2为步骤3中合金在400℃下时效处理12h后的析出相统计分布。对步骤3中合金在400℃下时效处理12h后进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为173.9±1.1MPa,抗拉强度为251.0±8.5MPa,延伸率为5.4±0.6%。对步骤4所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为290.4±2.6MPa,抗拉强度为361.5±5.4MPa,延伸率为12.5±0.7%。Figure 1 shows the hardness change curve of the alloy during the aging process in step 3. Figure 3 is the TEM bright field image of the alloy after aging treatment at 400°C for 12 hours in step 3. Table 2 shows the statistical distribution of precipitated phases after the alloy was aged at 400°C for 12 hours in step 3. After the alloy in step 3 is aged at 400°C for 12 hours, the tensile mechanical properties at room temperature are tested. The tensile properties are shown in Table 1. The final yield strength is 173.9±1.1MPa, the tensile strength is 251.0±8.5MPa, and the elongation is 5.4±0.6%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 4. The tensile properties are shown in Table 1. The final yield strength is 290.4±2.6MPa, the tensile strength is 361.5±5.4MPa, and the elongation is 12.5±0.7%.
对比例2Comparative example 2
本对比例采用一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金作为研究实例,包括以下步骤:This comparative example uses a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy as a research example, including the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.2%,Mo:0.2%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, in which the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.2%, Mo: 0.2%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对经过步骤1所得的合金在400℃下进行时效处理。Step 2: Aging treatment is performed on the alloy obtained in Step 1 at 400°C.
步骤3、对经过步骤2在400℃下时效处理12h后所得的合金开展热轧处理,轧制温度为320℃,道次压下量为10%,总压下量为70%。Step 3: Hot-roll the alloy obtained after aging treatment at 400°C for 12 hours in step 2. The rolling temperature is 320°C, the pass reduction is 10%, and the total reduction is 70%.
图1为步骤2中合金在时效过程中的硬度变化曲线。图4为步骤2中合金在400℃下时效处理12h后的TEM明场像。表2为步骤2中合金在400℃下时效处理12h后的析出相统计分布。对步骤2中合金在400℃下时效处理12h后进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为133.4±5.1MPa,抗拉强度为208.5±15.7MPa,延伸率为5.8±0.8%。对步骤3所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为252.8±3.4MPa,抗拉强度为321.8±6.7MPa,延伸率为9.8±2.1%。Figure 1 shows the hardness change curve of the alloy during the aging process in step 2. Figure 4 is the TEM bright field image of the alloy after aging treatment at 400°C for 12 hours in step 2. Table 2 shows the statistical distribution of precipitated phases after the alloy was aged at 400°C for 12 hours in step 2. After the alloy in step 2 is aged at 400°C for 12 hours, the tensile mechanical properties at room temperature are tested. The tensile properties are shown in Table 1. The final yield strength is 133.4±5.1MPa, the tensile strength is 208.5±15.7MPa, and the elongation is 5.8±0.8%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 3. The tensile properties are shown in Table 1. The final yield strength is 252.8±3.4MPa, the tensile strength is 321.8±6.7MPa, and the elongation is 9.8±2.1%.
对比例3Comparative example 3
本对比例采用一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金作为研究实例,包括以下步骤:This comparative example uses a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy as a research example, including the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr-Mo合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.2%,Mo:0.1%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至875℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr-Mo alloy, where the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.2%, Mo: 0.1%, and the balance is Aluminum and unavoidable impurities, of which the impurities originate from raw materials and are unavoidable, the impurity content is: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, Zn: 0.05%. After batching, heat the raw materials to 875°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is left to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对步骤1所得铸态Al-Mg-Mn-Zr-Cr-Mo合金在200℃下进行预时效处理。预时效处理时间为24h,淬火至室温;Step 2: Pre-age the as-cast Al-Mg-Mn-Zr-Cr-Mo alloy obtained in Step 1 at 200°C. The pre-aging treatment time is 24h and quenched to room temperature;
步骤3、对经过步骤2所得的合金在400℃下进行时效处理,时效处理时间为20h。Step 3. Aging treatment is performed on the alloy obtained in Step 2 at 400°C, and the aging treatment time is 20 hours.
步骤4、对经过步骤3所得的合金开展热轧处理,轧制温度为300℃,道次压下量为10%,总压下量为70%。Step 4: Hot-roll the alloy obtained in Step 3. The rolling temperature is 300°C, the pass reduction is 10%, and the total reduction is 70%.
对步骤3所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为151.4±3.1MPa,抗拉强度为220.4±8.6MPa,延伸率为5.6±0.7%。对步骤4所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为252.8±3.4MPa,抗拉强度为321.8±6.7MPa,延伸率为9.8±2.1%。Conduct room temperature tensile mechanical properties test on the alloy obtained in step 3. The tensile properties are shown in Table 1. The final yield strength is 151.4±3.1MPa, the tensile strength is 220.4±8.6MPa, and the elongation is 5.6±0.7%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 4. The tensile properties are shown in Table 1. The final yield strength is 252.8±3.4MPa, the tensile strength is 321.8±6.7MPa, and the elongation is 9.8±2.1%.
对比例4Comparative example 4
本对比例采用一种Al-Mg-Mn-Zr-Cr合金作为研究实例,包括以下步骤:This comparative example uses an Al-Mg-Mn-Zr-Cr alloy as a research example, including the following steps:
步骤1、准备Al-Mg-Mn-Zr-Cr合金,其中合金成分为:Mg:4.0%,Mn:1.0%,Zr:0.2%,Cr:0.1%,余量为铝及不可避免的杂质,其中杂质来源于原料,其不可避免,杂质含量为:Fe:0.3%,Si:0.2%,Cu:0.05%,Zn:0.05%。配料后将原料加热至780℃,完全熔化后保温40min并多次用石磨棒进行搅拌,随后降温至750℃进行流氩除气3~5min,熔体静置、扒渣后,于730~750℃浇注于预热至200℃的模具(钢模、铜模、石墨模均可)中,得到铸锭;Step 1. Prepare Al-Mg-Mn-Zr-Cr alloy, in which the alloy composition is: Mg: 4.0%, Mn: 1.0%, Zr: 0.2%, Cr: 0.1%, and the balance is aluminum and inevitable impurities. The impurities originate from the raw materials and are unavoidable. The impurity contents are: Fe: 0.3%, Si: 0.2%, Cu: 0.05%, and Zn: 0.05%. After batching, heat the raw materials to 780°C. After complete melting, keep the temperature for 40 minutes and stir with a stone grinding rod several times. Then cool to 750°C and perform argon degassing for 3 to 5 minutes. After the melt is allowed to stand and the slag is removed, it is heated to 730 to 730°C. Pour at 750°C into a mold preheated to 200°C (steel mold, copper mold, graphite mold can be used) to obtain an ingot;
步骤2、对步骤1所得铸态Al-Mg-Mn-Zr-Cr合金在300℃进行预时效处理。预时效处理时间为8h,空冷至室温;Step 2: Pre-age the as-cast Al-Mg-Mn-Zr-Cr alloy obtained in Step 1 at 300°C. The pre-aging treatment time is 8 hours, and air-cooled to room temperature;
步骤3、对经过步骤2所得的合金板材开展室温冷轧,道次压下量为2%,轧制速度0.1ms-1,总压下量10%;Step 3. Carry out room temperature cold rolling on the alloy sheet obtained in step 2, with a pass reduction of 2%, a rolling speed of 0.1ms -1 and a total reduction of 10%;
步骤4、对经过步骤3所得的合金在400℃进行时效处理,时效处理时间为12h。Step 4: Aging treatment is performed on the alloy obtained in step 3 at 400°C, and the aging treatment time is 12 hours.
步骤5、对经过步骤4所得的合金开展热轧处理,轧制温度为320℃,道次压下量为10%,总压下量为70%。Step 5: Hot-roll the alloy obtained in Step 4. The rolling temperature is 320°C, the pass reduction is 10%, and the total reduction is 70%.
对步骤4所得到合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为165.5±2.6MPa,抗拉强度为282.4±5.7MPa,延伸率为6.4±1.3%。对步骤5所得到的合金进行室温拉伸力学性能测试。拉伸性能见表1,最终屈服强度为281.8±2.5MPa,抗拉强度为375.7±8.7MPa,延伸率为9.7±2.4%。对步骤5所得到的合金进行300℃高温拉伸力学性能测试。拉伸性能见表3,最终屈服强度为91.3±3.7MPa,抗拉强度为91.3±3.7MPa,延伸率为37.2±4.9%。Conduct room temperature tensile mechanical properties test on the alloy obtained in step 4. The tensile properties are shown in Table 1. The final yield strength is 165.5±2.6MPa, the tensile strength is 282.4±5.7MPa, and the elongation is 6.4±1.3%. Conduct room temperature tensile mechanical properties test on the alloy obtained in step 5. The tensile properties are shown in Table 1. The final yield strength is 281.8±2.5MPa, the tensile strength is 375.7±8.7MPa, and the elongation is 9.7±2.4%. The alloy obtained in step 5 was subjected to a high temperature tensile mechanical property test at 300°C. The tensile properties are shown in Table 3. The final yield strength is 91.3±3.7MPa, the tensile strength is 91.3±3.7MPa, and the elongation is 37.2±4.9%.
表1、各实施例和对比例相应状态室温拉伸性能测试对比。Table 1. Comparison of room temperature tensile properties test in corresponding states of each example and comparative example.
表2、各实施例和对比例相应状态的析出相统计分布。Table 2. Statistical distribution of precipitated phases in corresponding states of each example and comparative example.
表3、各实施例和对比例相应状态300℃高温拉伸性能测试对比。Table 3. Comparison of 300°C high-temperature tensile properties test in corresponding states of each example and comparative example.
从表1和表3可以看出,相比与对比例4而言,实施例1表现出较强的耐热性能,这主要是由于Zr、Cr、Mo等多元协同微合金化,促进析出高密度的纳米级α相和Al3Zr弥散粒子,直接提供了可观的强度;在后续的轧制退火过程中,其抑制再结晶间接强化的作用仍然得以保留,故而使最终成品强度大幅度提高。It can be seen from Table 1 and Table 3 that compared with Comparative Example 4, Example 1 shows stronger heat resistance. This is mainly due to the synergistic micro-alloying of Zr, Cr, Mo, etc., which promotes high precipitation. The dense nanoscale α phase and Al 3 Zr dispersed particles directly provide considerable strength; during the subsequent rolling and annealing process, their indirect strengthening effect of inhibiting recrystallization is still retained, so the strength of the final product is greatly improved.
从图1中可以看出实施例1合金经过预时效+预变形处理后,与对比例2铸态合金相比,其硬度得到明显提高并且达到峰值硬度的时间实现明显减短。而与仅经过预变形的对比例1合金相比,在各时效阶段处的硬度均有一定提升。同时我们可以看出,在长时间高温时效处理后,可以看出实例1合金硬度仍然能保持较高的水平。这说明预时效+预变形处理工艺能加快Al-Mg-Mn-Zr-Cr-Mo合金的时效响应过程,同时可以进一步提高合金的弥散强化效果并保持较高的耐热性。It can be seen from Figure 1 that after the alloy of Example 1 undergoes pre-aging + pre-deformation treatment, compared with the as-cast alloy of Comparative Example 2, its hardness is significantly improved and the time to reach peak hardness is significantly shortened. Compared with the alloy of Comparative Example 1 that has only undergone pre-deformation, the hardness at each aging stage has been improved to a certain extent. At the same time, we can see that after long-term high-temperature aging treatment, the hardness of the alloy in Example 1 can still maintain a high level. This shows that the pre-aging + pre-deformation treatment process can accelerate the aging response process of Al-Mg-Mn-Zr-Cr-Mo alloy, while further improving the dispersion strengthening effect of the alloy and maintaining high heat resistance.
从图2-4中可以看出,合金经过预时效+预变形处理工艺后,析出相的分布明显细化且数量得到明显提升。在两种包含预变形处理工艺的合金中,可以观测到析出相沿位错线分布,这说明预变形工艺可以通过引入位错来增加α相的形核位点,提高合金的弥散强化效果。从表2种可以看出实施例1相对于比对例1和对比例2,析出相明显具有更高的数密度和更小的尺寸,说明预时效+预变形处理工艺能够有效的促进α相的析出,这与图1中的硬度变化相一致。It can be seen from Figure 2-4 that after the alloy undergoes pre-aging + pre-deformation treatment process, the distribution of precipitated phases is significantly refined and the quantity is significantly increased. In the two alloys containing the predeformation treatment process, the distribution of precipitated phases along the dislocation lines can be observed, which shows that the predeformation process can increase the nucleation sites of α phase by introducing dislocations and improve the dispersion strengthening effect of the alloy. It can be seen from Table 2 that compared to Comparative Example 1 and Comparative Example 2, the precipitated phase in Example 1 has a significantly higher number density and smaller size, indicating that the pre-aging + pre-deformation treatment process can effectively promote the α phase. precipitation, which is consistent with the hardness change in Figure 1.
综上所述,本发明公开了一种高耐热弥散强化型Al-Mg-Mn-Zr-Cr-Mo合金制备及加工方法,首先利用Zr、Cr、Mo多元协同的微合金化促进纳米级α相和Al3Zr弥散粒子的析出,而有利于提高合金的室温和高温强度。其次预变形和预时效相结合一方面可以能够有效缩短合金达到峰值强度的时间,另一方面能够有效提高合金的弥散强化效果,使得机械性能远超目前常规Al-Mg-Mn合金,扩展了Al-Mg-Mn合金的应用范围。In summary, the present invention discloses a preparation and processing method of a highly heat-resistant dispersion-strengthened Al-Mg-Mn-Zr-Cr-Mo alloy. First, the synergistic micro-alloying of Zr, Cr, and Mo is used to promote nanoscale The precipitation of α phase and Al 3 Zr dispersed particles is beneficial to improving the room temperature and high temperature strength of the alloy. Secondly, the combination of pre-deformation and pre-aging can effectively shorten the time for the alloy to reach peak strength on the one hand, and on the other hand can effectively improve the dispersion strengthening effect of the alloy, making the mechanical properties far exceed the current conventional Al-Mg-Mn alloy, expanding the Al -Application range of Mg-Mn alloy.
以上所述的具体描述,对发明的目的、技术方案和有益效果进行了进一步详细说明,所应理解的是,以上所述仅为本发明的具体实施例而已,并不用于限定本发明的保护范围,凡在本发明的精神和原则之内,所做的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above-mentioned specific description further explains the purpose, technical solutions and beneficial effects of the invention in detail. It should be understood that the above-mentioned are only specific embodiments of the invention and are not intended to limit the protection of the invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention shall be included in the protection scope of the present invention.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202311440248.5A CN117448636A (en) | 2023-11-01 | 2023-11-01 | Preparation and processing method of high heat-resistant dispersion strengthening Al-Mg-Mn-Zr-Cr-Mo alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202311440248.5A CN117448636A (en) | 2023-11-01 | 2023-11-01 | Preparation and processing method of high heat-resistant dispersion strengthening Al-Mg-Mn-Zr-Cr-Mo alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
CN117448636A true CN117448636A (en) | 2024-01-26 |
Family
ID=89587077
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202311440248.5A Pending CN117448636A (en) | 2023-11-01 | 2023-11-01 | Preparation and processing method of high heat-resistant dispersion strengthening Al-Mg-Mn-Zr-Cr-Mo alloy |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN117448636A (en) |
-
2023
- 2023-11-01 CN CN202311440248.5A patent/CN117448636A/en active Pending
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103031473B (en) | Processing method of high-toughness Al-Si system die-casting aluminum alloy | |
CN110983131B (en) | 7-series aluminum alloy section and manufacturing method thereof | |
CN102978497B (en) | Casting magnesium alloy with high strength and toughness and preparation method thereof | |
TW201925489A (en) | Aluminum alloy sheet for battery lids for molding integrated explosion-prevention valve, and method for producing same | |
EP1882753A1 (en) | Aluminium alloy | |
CN115125420A (en) | A kind of cast aluminum alloy for high-performance structural parts without heat treatment and preparation method thereof | |
CN107488823A (en) | Method that is a kind of while improving intensity of aluminum alloy and elongation percentage | |
CN102965553A (en) | Aluminum alloy cast ingot for automotive bumper and production process thereof | |
CN113355565A (en) | High-temperature-resistant welded aluminum alloy suitable for extrusion casting and preparation method thereof | |
CN103981408B (en) | A kind of preparation method of high strength weldable Al-Zn-Mg-Mn-Sc alloy | |
CN110218917B (en) | Alloy aluminum bar containing rare earth elements and preparation process thereof | |
CN107675053A (en) | A kind of preparation method of high strength magnesium lithium alloy and its deep cooling intensive treatment | |
CN115109974A (en) | Al-Cu-Li-Zr-Ce-Sc alloy plate with ultrahigh strength and good plasticity and preparation method thereof | |
CN115011846A (en) | High-strength and high-stability Al-Mg-Si-Cu-Sc aluminum alloy and preparation method thereof | |
CN108913956A (en) | A kind of Al-Mg-Si-Cu-Mn-Sr alloy and preparation method thereof with excellent anticorrosive performance | |
CN110791688B (en) | High-strength high-fracture-toughness aluminum alloy bar and preparation method thereof | |
TWI696706B (en) | Aluminum alloy plate for battery cover used for forming integrated explosion-proof valve and manufacturing method thereof | |
CN104805322B (en) | Non-heat-treated self-strengthening aluminum and magnesium alloy and preparation technology thereof | |
CN114107757B (en) | Cast aluminum alloy for automobile metal casting and processing technology thereof | |
CN108193101B (en) | Er, Zr, Si microalloyed Al-Mg-Cu alloy and its deformation heat treatment process | |
CN117448636A (en) | Preparation and processing method of high heat-resistant dispersion strengthening Al-Mg-Mn-Zr-Cr-Mo alloy | |
CN114561575A (en) | A kind of preparation method of high-strength and tough aluminum alloy with compound addition of Er and Zr | |
CN115537621A (en) | High-temperature-resistant high-strength Mg-Gd-Y-Zn-Mn alloy and preparation method thereof | |
KR102277133B1 (en) | Method for manufacturing high strength aluminum alloy forged plate | |
CN112126830B (en) | Preparation and heat treatment process of a high-strength and high-plasticity Al-Mg-Si-Sc aluminum alloy plate |
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 |