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CN115874088A - A kind of high-strength heat-resistant and damage-resistant aluminum alloy powder, preparation method and application - Google Patents

A kind of high-strength heat-resistant and damage-resistant aluminum alloy powder, preparation method and application Download PDF

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CN115874088A
CN115874088A CN202211454436.9A CN202211454436A CN115874088A CN 115874088 A CN115874088 A CN 115874088A CN 202211454436 A CN202211454436 A CN 202211454436A CN 115874088 A CN115874088 A CN 115874088A
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alloy powder
aluminum alloy
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张莎莎
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Nanjing University of Aeronautics and Astronautics
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Abstract

本发明公开一种高强耐热耐损伤铝合金粉末、制备方法及应用,所述铝合金粉末的组成按照质量百分比计算包括以下组分:Mg:4.0~12%,Ca:0.50~3.0%,Sc:0.10~0.90%,Mn:0.20~1.5%,Zr:0.1~0.5%,其余为Al和不可避免引入的杂质元素。通过合金元素Ca的添加,显著抑制了合金在3D打印成形过程中的热裂倾向,本发明中所涉及的高强耐热Al‑Mg‑Ca‑Sc合金粉末3D打印成形性良好,经过3D打印,零件不产生裂纹,致密度高。通过构建多尺度结构,发挥多级强化机制,3D打印后样件具有优良的室温力学性能和高温稳定性。

Figure 202211454436

The invention discloses a high-strength, heat-resistant and damage-resistant aluminum alloy powder, a preparation method and an application thereof. The composition of the aluminum alloy powder includes the following components calculated according to mass percentage: Mg: 4.0-12%, Ca: 0.50-3.0%, Sc : 0.10-0.90%, Mn: 0.20-1.5%, Zr: 0.1-0.5%, and the rest are Al and inevitably introduced impurity elements. The addition of the alloying element Ca significantly suppresses the thermal cracking tendency of the alloy during the 3D printing forming process. The high-strength heat-resistant Al-Mg-Ca-Sc alloy powder involved in the present invention has good 3D printing formability. After 3D printing, Parts do not produce cracks, high density. By building a multi-scale structure and exerting a multi-level strengthening mechanism, the 3D printed sample has excellent room temperature mechanical properties and high temperature stability.

Figure 202211454436

Description

一种高强耐热耐损伤铝合金粉末、制备方法及应用A kind of high-strength heat-resistant and damage-resistant aluminum alloy powder, preparation method and application

技术领域technical field

本发明属于增材制造材料技术领域,具体涉及一种高强耐热耐损伤铝合金粉末、制备方法及应用。The invention belongs to the technical field of additive manufacturing materials, and in particular relates to a high-strength heat-resistant and damage-resistant aluminum alloy powder, a preparation method and an application thereof.

背景技术Background technique

增材制造技术由于具有易于复杂结构成形、制造周期短、节能减材等优点,在航空航天、轨道交通、生物医疗等方面获得了广泛的应用。其中,基于粉末床的选区激光熔化(SelectiveLaserMelting,SLM)成形是最先发展起来的代表性增材制造技术之一。铝合金作为应用最广泛的结构材料之一,其激光增材制造在轻量化、高性能铝基复杂零件制造领域变得越来越重要。Additive manufacturing technology has been widely used in aerospace, rail transit, biomedical and other fields due to its advantages of easy forming of complex structures, short manufacturing cycle, energy saving and material reduction. Among them, powder bed-based selective laser melting (Selective Laser Melting, SLM) forming is one of the first representative additive manufacturing technologies developed. Aluminum alloy is one of the most widely used structural materials, and its laser additive manufacturing is becoming more and more important in the field of lightweight, high-performance aluminum-based complex parts manufacturing.

当前激光增材制造铝合金主要以传统铸造牌号合金为主,存在以下问题:At present, laser additive manufacturing of aluminum alloys is mainly based on traditional casting grade alloys, and there are the following problems:

(1)以AlSi10Mg和AlSi12为代表的Al-Si基近共晶合金,共晶组织较为粗大,强度和延展率有限;SLM制造的AlSi10Mg合金的机械性能通常在214至358MPa的拉伸强度范围内,热处理后的延伸率为4至15%。(2)2xxx系铝合金和7xxx系铝合金等常规中高强铝合金在增材制造过程中容易发生热裂,这是制约其进一步发展的关键瓶颈;(3)另一种选择是与Sc和/或Zr合金化的5xxx系列铝合金,具有代表性的是被称为Scalmalloy的Al-Mg-Sc-Zr合金,由于细小的Al3(Sc,Zr)颗粒的强化和Mg的固溶强化,表现出良好的室温强度和塑性。然而,对于Scalmalloy和具有相似成分的合金,避免热裂倾向和改善力学性能在很大程度上取决于高水平的稀有元素Sc(>0.66wt%)。此外,高温下较差的热稳定性和力学性能的急剧下降限制了它们的应用。(4)为了扩大增材制造铝合金在高温下的应用,新的耐热铝合金被设计用于增材制造,例如Al-Ce基和Al-Ni基铝合金。然而,上述合金的室温强度低且延展性差。(1) Al-Si-based near-eutectic alloys represented by AlSi10Mg and AlSi12 have relatively coarse eutectic structures and limited strength and elongation; the mechanical properties of AlSi10Mg alloys produced by SLM are usually within the tensile strength range of 214 to 358MPa , the elongation after heat treatment is 4 to 15%. (2) Conventional medium-high-strength aluminum alloys such as 2xxx series aluminum alloys and 7xxx series aluminum alloys are prone to thermal cracking during the additive manufacturing process, which is a key bottleneck restricting their further development; (3) Another option is to combine with Sc and /or Zr alloyed 5xxx series aluminum alloys, the representative Al-Mg-Sc-Zr alloy called Scalmalloy, due to the strengthening of fine Al3(Sc,Zr) particles and the solid solution strengthening of Mg, the performance Good room temperature strength and plasticity. However, for Scalmalloy and alloys with similar compositions, avoiding hot cracking tendency and improving mechanical properties largely depend on high levels of rare element Sc (>0.66 wt%). In addition, poor thermal stability and sharp drop in mechanical properties at high temperature limit their applications. (4) In order to expand the application of additively manufactured aluminum alloys at high temperatures, new heat-resistant aluminum alloys are designed for additive manufacturing, such as Al-Ce-based and Al-Ni-based aluminum alloys. However, the above alloys have low room temperature strength and poor ductility.

现有技术中也有对增材制造的材料进行改进,如专利CN111922331A提供一种纳米颗粒增强铝合金粉末及其制备方法,包括以下步骤:(1)将纳米粉末A和纳米粉末B在有机溶剂中分散均匀,得到混合体系C,所述纳米粉末A为纳米Ti粉、纳米Ta粉、纳米Nb粉和纳米Zr粉的至少一种,所述纳米粉末B为纳米硼粉;(2)将粘结剂分散在所述混合体系C中,得到混合体系D;(3)向搅拌状态下的铝合金粉末中加入所述混合体系D至铝合金粉末形成团聚颗粒并继续搅拌至有机溶剂挥发得到固体颗粒E;(4)筛分固体颗粒E去除粒径大于270目的颗粒,该专利所制备铝合金粉末进行应用均具备良好的力学性能,选区激光熔化制备得到的铝合金材料无裂纹缺陷,但是耐热性较差,室温强度较低。In the prior art, the materials for additive manufacturing are also improved. For example, the patent CN111922331A provides a nanoparticle-reinforced aluminum alloy powder and a preparation method thereof, including the following steps: (1) dissolving nanopowder A and nanopowder B in an organic solvent Disperse evenly, obtain mixing system C, described nano-powder A is at least one of nano-Ti powder, nano-Ta powder, nano-Nb powder and nano-Zr powder, and described nano-powder B is nano-boron powder; (2) bonding (3) Add the mixed system D to the aluminum alloy powder under stirring until the aluminum alloy powder forms agglomerated particles and continue to stir until the organic solvent volatilizes to obtain solid particles E; (4) Screening solid particles E to remove particles with a particle size greater than 270 meshes, the aluminum alloy powder prepared by this patent has good mechanical properties for application, and the aluminum alloy material prepared by selective laser melting has no crack defects, but is heat-resistant Poor resistance, low strength at room temperature.

专利CN110791686A公开一种用于增材制造的铝合金粉末材料、制备方法。该铝合金粉末材料的表达式为:Al-X-Y,X组分为Fe、Co、Ni的一种或多种,Y组分为Sc、Ti、Zr的一种或多种,其中,X组分的原子百分比为0.1~10%、Y组分的原子百分比为0.1~5%,其余的组分为Al。所述制备方法为:按照铝合金粉末的表达式进行配料,采用加热方法熔炼制备母合金铸锭,然后将母合金铸锭进行雾化制粉,从而获得铝合金粉末材料。该专利所制得的铝合金粉末增材制造成形后的零件具有力学性能相比于前述专利更好、也有较好的热稳定性、高温强度也得到提升,但是延展性较差,致密度较差。Patent CN110791686A discloses an aluminum alloy powder material and a preparation method for additive manufacturing. The expression of the aluminum alloy powder material is: Al-X-Y, X component is one or more of Fe, Co, Ni, Y component is one or more of Sc, Ti, Zr, wherein, X group The atomic percentage of the Y component is 0.1-10%, the atomic percentage of the Y component is 0.1-5%, and the rest of the components are Al. The preparation method is as follows: batching according to the expression of aluminum alloy powder, adopting heating method to melt and prepare master alloy ingot, and then atomizing the master alloy ingot to make powder, so as to obtain aluminum alloy powder material. Compared with the previous patent, the aluminum alloy powder additive manufacturing formed parts produced by this patent have better mechanical properties, better thermal stability, and improved high-temperature strength, but poor ductility and low density. Difference.

因此,开发兼具室温高强高韧和良好高温热稳定性,能有效抑制3D打印过程中热裂纹损伤、具有良好致密度的铝合金仍然是亟需解决的。Therefore, it is still urgent to develop an aluminum alloy with high strength and toughness at room temperature and good thermal stability at high temperature, which can effectively inhibit thermal crack damage during 3D printing and has good density.

发明内容Contents of the invention

为实现上述目的,本发明一个方面,提出一种高强耐热耐损伤铝合金粉末,所述铝合金粉末的组成按照质量百分比计算:Mg:4.0~12%,Ca:0.50~3.0%,Sc:0.10~0.90%,Mn:0.20~1.5%,Zr:0.1~0.5%,其余为Al和不可避免引入的杂质元素。In order to achieve the above object, one aspect of the present invention proposes a high-strength, heat-resistant and damage-resistant aluminum alloy powder. The composition of the aluminum alloy powder is calculated according to mass percentage: Mg: 4.0-12%, Ca: 0.50-3.0%, Sc: 0.10-0.90%, Mn: 0.20-1.5%, Zr: 0.1-0.5%, and the rest are Al and unavoidable impurity elements.

本发明的另一个方面,提供一种高强耐热耐损伤铝合金粉末的制备方法,包括以下步骤:Another aspect of the present invention provides a method for preparing a high-strength heat-resistant and damage-resistant aluminum alloy powder, comprising the following steps:

步骤1、配制元素组分:所述铝合金粉末的组成组分包括Mg、Ca、Sc、Mn、Zr,其余的组分为Al;Step 1, preparing elemental components: the compositional components of the aluminum alloy powder include Mg, Ca, Sc, Mn, Zr, and the remaining components are Al;

步骤2、真空熔炼-雾化制粉:将经过步骤1中配制的高强耐热铝合金粉末进行真空熔炼;经过所述真空熔炼后进行雾化制粉,即得到所述高强耐热耐损伤铝合金粉末。Step 2. Vacuum smelting-atomization pulverization: the high-strength heat-resistant aluminum alloy powder prepared in step 1 is vacuum smelted; after the vacuum smelting, atomization pulverization is carried out to obtain the high-strength heat-resistant and damage-resistant aluminum alloy powder alloy powder.

优选地,所述步骤2中,所述真空熔炼的熔炼温度为750~850℃,真空度≤0.1Pa。Preferably, in the step 2, the smelting temperature of the vacuum smelting is 750-850° C., and the vacuum degree is ≤0.1 Pa.

优选地,所述步骤2中,所述真空气雾化的工艺为通入Ar、He或者混合气体保护并气雾化,雾化压力为0.3~10MPa。Preferably, in the step 2, the vacuum atomization process is to pass through Ar, He or a mixed gas protection and gas atomization, and the atomization pressure is 0.3-10 MPa.

本发明的另一个方面,提供了一种高强耐热耐损伤铝合金粉末材料在选区激光熔化成型3D打印技术中的应用。Another aspect of the present invention provides an application of a high-strength heat-resistant and damage-resistant aluminum alloy powder material in the selective laser melting forming 3D printing technology.

优选地,将制备所得的铝合金粉末应用在3D打印中,包括如下步骤:Preferably, applying the prepared aluminum alloy powder in 3D printing includes the following steps:

步骤一、将所述铝合金粉末在惰性气体中保温处理,温度为300~400℃,时间为3~6h;Step 1. heat-preserve the aluminum alloy powder in an inert gas at a temperature of 300-400° C. for 3-6 hours;

步骤二、将经过所述预处理后的粉末进行3D打印。Step 2, 3D printing the pretreated powder.

优选地,将所述铝合金粉末进行选取激光融化成型处理,其中,激光功率为200~400W,扫描速度为500~2000mm/s,扫描间距为50~120μm,层间厚度为20~50μm。Preferably, the aluminum alloy powder is subjected to selective laser melting molding treatment, wherein the laser power is 200-400W, the scanning speed is 500-2000mm/s, the scanning distance is 50-120μm, and the interlayer thickness is 20-50μm.

优选地,在步骤二之后,对3D打印出的合金进行热处理,所述热处理温度为300~420℃,时间为3~36h。Preferably, after step 2, the 3D printed alloy is subjected to heat treatment, the heat treatment temperature is 300-420° C., and the time is 3-36 hours.

与现有技术相比,本发明的有益效果:Compared with prior art, the beneficial effect of the present invention:

(1)本发明公开的高强耐热Al-Mg-Ca-Sc合金粉末通过合金元素Ca的添加,显著抑制了合金在3D打印成形过程中的热裂倾向,本发明中所涉及的高强耐热Al-Mg-Ca-Sc合金粉末3D打印成形性良好,经过3D打印,零件不产生裂纹,致密度高。通过构建多尺度结构,发挥多级强化机制,3D打印后样件具有优良的室温力学性能和高温稳定性。(1) The high-strength heat-resistant Al-Mg-Ca-Sc alloy powder disclosed in the present invention significantly suppresses the thermal cracking tendency of the alloy during the 3D printing forming process through the addition of the alloying element Ca. Al-Mg-Ca-Sc alloy powder has good 3D printing formability. After 3D printing, the parts do not produce cracks and have high density. By building a multi-scale structure and exerting a multi-level strengthening mechanism, the 3D printed sample has excellent room temperature mechanical properties and high temperature stability.

(2)本发明的另一有益效果是铝合金粉末的特定组合发挥固溶强化、晶界强化和纳米析出相强化等多重强化的协同作用,具有高的室温强度和塑性。其中,金元素Mg固溶在铝合金基体中,起到固溶强化的作用;合金元素Ca在晶界形成网状/半网状共晶组织,发挥晶界强化和第二相强化效应;Sc和Zr形成Al3(Sc,Zr)纳米相,一方面作为凝固过程中的异质形核点,细化晶粒,另一方面经过热处理后,在基体内弥散析出共格/半共格的纳米析出相,发挥弥散强化效应。(2) Another beneficial effect of the present invention is that the specific combination of aluminum alloy powder exerts the synergistic effect of multiple strengthening such as solid solution strengthening, grain boundary strengthening and nano-precipitated phase strengthening, and has high room temperature strength and plasticity. Among them, the gold element Mg is solid-dissolved in the aluminum alloy matrix, which plays a role of solid solution strengthening; the alloy element Ca forms a network/semi-network eutectic structure at the grain boundary, and exerts the effects of grain boundary strengthening and second phase strengthening; Sc Al3(Sc, Zr) nanophase is formed with Zr, on the one hand, it acts as a heterogeneous nucleation point in the solidification process, and refines the grains; The precipitated phase exerts the dispersion strengthening effect.

(3)本发明公开的铝合金粉末的特定组合,具有优良的热稳定性,在高温条件下力学性能损失较小。这主要归因于:一方面,合金元素Ca在晶界上形成的网状/半网状共晶组织对晶界具有明显的钉扎效果,抑制晶粒的长大;另一方面,晶内的共格/半共格Al3(Sc,Zr)纳米相热稳定性好,弥散强化效应削弱不明显。(3) The specific combination of aluminum alloy powder disclosed in the present invention has excellent thermal stability, and the loss of mechanical properties is small under high temperature conditions. This is mainly due to: on the one hand, the network/semi-network eutectic structure formed by the alloying element Ca on the grain boundary has an obvious pinning effect on the grain boundary and inhibits the growth of the grain; on the other hand, the intragranular The coherent/semi-coherent Al3(Sc,Zr) nanophase has good thermal stability, and the dispersion strengthening effect is not significantly weakened.

上述说明仅是本申请技术方案的概述,为了能够更清楚了解本申请的技术手段,从而可依照说明书的内容予以实施,并且为了让本申请的上述和其他目的、特征和优点能够更明显易懂,以下以本申请的较佳实施例并配合附图详细说明如后。The above description is only an overview of the technical solution of the present application. In order to understand the technical means of the present application more clearly, it can be implemented according to the contents of the description, and in order to make the above and other purposes, features and advantages of the present application more obvious and understandable , the preferred embodiments of the application and accompanying drawings are described in detail below.

根据下文结合附图对本申请具体实施例的详细描述,本领域技术人员将会更加明了本申请的上述及其他目的、优点和特征。According to the following detailed description of specific embodiments of the application in conjunction with the accompanying drawings, those skilled in the art will be more aware of the above and other objectives, advantages and features of the application.

附图说明Description of drawings

为了更清楚地说明本申请实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图是本申请的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。在所有附图中,类似的元件或部分一般由类似的附图标记标识。附图中,各元件或部分并不一定按照实际的比例绘制。In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are For some embodiments of the present application, those of ordinary skill in the art can also obtain other drawings based on these drawings without creative effort. Throughout the drawings, similar elements or parts are generally identified by similar reference numerals. In the drawings, elements or parts are not necessarily drawn in actual scale.

图1为本发明所述高强耐热耐损伤铝合金粉末的形貌图;Fig. 1 is the morphology figure of high-strength, heat-resistant and damage-resistant aluminum alloy powder of the present invention;

图2为本发明所述高强耐热耐损伤铝合金粉末的粒度分布图;Fig. 2 is a particle size distribution diagram of the high-strength, heat-resistant and damage-resistant aluminum alloy powder of the present invention;

图3为本发明所述铝合金粉末进行选区激光熔化成型工艺处理下铝合金的光镜图,图3a-3c是所述铝合金粉末进行选区激光熔化成型工艺不同处理参数下铝合金的光镜图;Fig. 3 is the optical mirror image of the aluminum alloy powder under the selected area laser melting molding process of the present invention, and Fig. 3a-3c is the optical mirror image of the aluminum alloy powder under the selected area laser melting forming process with different processing parameters picture;

图4为本发明所述高强耐热耐损伤铝合金粉末经过3D打印后的透射电镜HADDF图及对应Ca元素的分布;Fig. 4 is the transmission electron microscope HADDF diagram of the high-strength heat-resistant and damage-resistant aluminum alloy powder of the present invention after 3D printing and the distribution of corresponding Ca elements;

图5为本发明所述高强耐热耐损伤铝合金粉末经过3D打印后的高分辨透射电镜图显示纳米弥散第二相粒子;Fig. 5 is a high-resolution transmission electron microscope image of the high-strength heat-resistant and damage-resistant aluminum alloy powder of the present invention after 3D printing, showing nano-dispersed second phase particles;

图6为本发明所述3D打印铝合金不同温度条件下的力学性能图;Fig. 6 is a diagram of the mechanical properties of the 3D printed aluminum alloy according to the present invention under different temperature conditions;

图7为本发明所述3D打印铝合金与其他合金在不同温度条件下的力学性能对比图;Fig. 7 is a comparison diagram of the mechanical properties of the 3D printed aluminum alloy of the present invention and other alloys under different temperature conditions;

图8为本发明所述3D打印铝合金的热裂纹敏感因子随着Ca含量的变化图。Fig. 8 is a graph showing the variation of the thermal crack sensitivity factor of the 3D printed aluminum alloy according to the present invention with the Ca content.

具体实施方式Detailed ways

为使本申请实施例的目的、技术方案和优点更加清楚,下面将结合本申请实施例中的附图,对本申请实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本申请一部分实施例,而不是全部的实施例。在下面的描述中,提供诸如具体的配置和组件的特定细节仅仅是为了帮助全面理解本申请的实施例。因此,本领域技术人员应该清楚,可以对这里描述的实施例进行各种改变和修改而不脱离本申请的范围和精神。另外,为了清楚和简洁,实施例中省略了对已知功能和构造的描述。In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments It is a part of the embodiments of this application, not all of them. In the following description, specific details, such as specific configurations and components, are provided merely to help a comprehensive understanding of the embodiments of the present application. Accordingly, those of ordinary skill in the art should recognize that various changes and modifications of the embodiments described herein can be made without departing from the scope and spirit of the application. Also, descriptions of well-known functions and constructions are omitted in the embodiments for clarity and conciseness.

本文中术语“和/或”,仅仅是一种描述关联对象的关联关系,表示可以存在三种关系,例如,A和/或B,可以表示:单独存在A,单独存在B,同时存在A和B三种情况,本文中术语“/和”是描述另一种关联对象关系,表示可以存在两种关系,例如,A/和B,可以表示:单独存在A,单独存在A和B两种情况,另外,本文中字符“/”,一般表示前后关联对象是一种“或”关系。The term "and/or" in this article is just an association relationship describing associated objects, which means that there may be three relationships, for example, A and/or B, which can mean: A exists alone, B exists alone, and A and B exist simultaneously. In the three cases of B, the term "/and" in this article is to describe another associated object relationship, which means that there can be two relationships, for example, A/ and B, which can mean: there is A alone, and there are two cases of A and B alone , In addition, the character "/" in this article generally indicates that the contextual objects are an "or" relationship.

还需要说明的是,在本文中,诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来,而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且,术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含。It should also be noted that in this article, relational terms such as first and second etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply that these entities or operations Any such actual relationship or order exists between. Moreover, the terms "comprises", "comprises" or any other variation thereof are intended to cover a non-exclusive inclusion.

实施例1Example 1

本实施例制备一种高强耐热耐损伤铝合金粉末。In this embodiment, a high-strength heat-resistant and damage-resistant aluminum alloy powder is prepared.

步骤1、配制元素组分:该铝合金粉末的成分各元素按质量百分比包括,Mg:5%,Ca:1%,Sc:0.6%;Zr:0.3%;Mn:0.6%,不可避免引入的杂质元素小于0.25%,其余为Al。Step 1. Prepare elemental components: the components of the aluminum alloy powder include, by mass percentage, Mg: 5%, Ca: 1%, Sc: 0.6%; Zr: 0.3%; Mn: 0.6%, which are inevitably introduced The impurity element is less than 0.25%, and the rest is Al.

步骤2、真空熔炼-雾化制粉:以上合金粉末的制备方法为按照质量配比混合后,经过所述真空熔炼后进行雾化制粉,得到该高强耐热耐损伤铝合金粉末。Step 2. Vacuum smelting-atomization pulverization: the preparation method of the above alloy powder is to mix according to the mass ratio, and then conduct atomization pulverization after the vacuum smelting to obtain the high-strength heat-resistant and damage-resistant aluminum alloy powder.

步骤2中的真空熔炼温度为820℃,真空度0.01Pa。然后采用氩气作为介质对金属熔滴进行雾化,雾化气压为5MPa。将所述铝合金粉末在氩气氛围中进行350℃,4小时保温处理。The vacuum melting temperature in step 2 is 820° C., and the vacuum degree is 0.01 Pa. Then, argon gas is used as the medium to atomize the metal droplet, and the atomization pressure is 5 MPa. The aluminum alloy powder was subjected to heat preservation treatment at 350° C. for 4 hours in an argon atmosphere.

制备所得的铝合金粉末如图1、图2所示,图1为本发明方法高强耐热耐损伤铝合金粉末的形貌图,图2为本发明所述高强耐热耐损伤铝合金粉末的粒度分布图。其粒径小于55.4μm的颗粒占90%,粒径小于25.4μm的颗粒占50%。通过在要制备的铝合金粉末中添加合金元素Ca,显著的抑制了合金在3D打印成形过程中的热裂倾向。其中,金元素Mg固溶在铝合金基体中,起到固溶强化的作用;合金元素Ca在晶界形成网状/半网状共晶组织,发挥晶界强化和第二相强化效应;Sc和Zr形成Al3(Sc,Zr)纳米相,一方面作为凝固过程中的异质形核点,细化晶粒,另一方面经过热处理后,在基体内弥散析出共格/半共格的纳米析出相,发挥弥散强化效应。The prepared aluminum alloy powder is shown in Fig. 1 and Fig. 2. Fig. 1 is a topography diagram of the high-strength heat-resistant and damage-resistant aluminum alloy powder according to the method of the present invention, and Fig. 2 is a profile of the high-strength heat-resistant and damage-resistant aluminum alloy powder according to the present invention. Particle size distribution diagram. The particles whose particle size is less than 55.4 μm account for 90%, and the particles whose particle size is less than 25.4 μm account for 50%. By adding the alloying element Ca to the aluminum alloy powder to be prepared, the thermal cracking tendency of the alloy during the 3D printing forming process is significantly suppressed. Among them, the gold element Mg is solid-dissolved in the aluminum alloy matrix, which plays a role of solid solution strengthening; the alloy element Ca forms a network/semi-network eutectic structure at the grain boundary, and exerts the effects of grain boundary strengthening and second phase strengthening; Sc Al3(Sc, Zr) nanophase is formed with Zr, on the one hand, it acts as a heterogeneous nucleation point in the solidification process, and refines the grains; The precipitated phase exerts the dispersion strengthening effect.

进一步的,将制备所得的铝合金粉末材料在选区激光熔化成型3D打印技术中进行应用。如图3a所示,图3a是所述铝合金粉末进行选区激光熔化成型工艺处理下铝合金的光镜图。将以上制备的铝合金粉末进行选区激光熔化成型(SLM)工艺处理,在本实施例中工艺处理参数:激光功率为350W,扫描速度为800mm/s,扫描间距为80μm,层间厚度为30μm。通过上述3D打印工艺制备了成形质量良好,致密度高的样件,样件内部没有观察到明显的孔洞、裂纹等缺陷。Further, the prepared aluminum alloy powder material is applied in the selective laser melting forming 3D printing technology. As shown in Fig. 3a, Fig. 3a is an optical microscope image of the aluminum alloy powder processed by the selective laser melting molding process. The above-prepared aluminum alloy powder was subjected to selective laser melting (SLM) process, and the process parameters in this embodiment were: laser power 350W, scanning speed 800mm/s, scanning distance 80μm, interlayer thickness 30μm. A sample with good forming quality and high density was prepared through the above-mentioned 3D printing process, and no obvious defects such as holes and cracks were observed inside the sample.

实施例2Example 2

本实施例与实施例1不同的是,实施例1的合金为打印态,未经过热处理,而本实施例中的铝合金是由实施例1合金经过325℃,9h热处理获得的。如图5所示,图5为本发明所述高强耐热耐损伤铝合金粉末经过3D打印后的高分辨透射电镜图显示纳米弥散第二相粒子。通过上述热处理,样件内部析出弥散分布的Al3(Sc,Zr)纳米相,发挥弥散强化的作用,显著提升合金的强度。The difference between this example and Example 1 is that the alloy in Example 1 is in a printed state without heat treatment, while the aluminum alloy in this example is obtained from the alloy in Example 1 after heat treatment at 325° C. for 9 hours. As shown in Figure 5, Figure 5 is a high-resolution transmission electron microscope image of the high-strength heat-resistant and damage-resistant aluminum alloy powder of the present invention after 3D printing, showing nano-dispersed second-phase particles. Through the above heat treatment, dispersed Al3(Sc, Zr) nano phases are precipitated inside the sample, which exerts the effect of dispersion strengthening and significantly improves the strength of the alloy.

实施例3Example 3

本实施例与实施例1不同的是,如图3b所示,图3b是所述铝合金粉末进行选区激光熔化成型工艺处理下铝合金的光镜图。将制备的所述铝合金粉末进行选区激光熔化成型(SLM)工艺处理,在本实施例中工艺处理参数:激光功率为350W,扫描速度为700mm/s,扫描间距为80μm,层间厚度为30μm。经过上述处理后,在低扫描速度下,能量密度大,会导致粉体熔化后形成的金属液体发生气化,形成金属蒸汽,在试样中形成气孔。The difference between this embodiment and embodiment 1 is that, as shown in Fig. 3b, Fig. 3b is an optical microscope image of the aluminum alloy powder processed by the selective laser melting molding process. The prepared aluminum alloy powder was subjected to a selective laser melting molding (SLM) process. In this embodiment, the process parameters were: laser power 350W, scanning speed 700 mm/s, scanning distance 80 μm, interlayer thickness 30 μm . After the above treatment, at low scanning speed, the energy density is high, which will lead to the gasification of the metal liquid formed after the powder is melted, forming metal vapor, and forming pores in the sample.

实施例4Example 4

本实施例与实施例1、3的不同的是,如图3c所示,图3c是所述铝合金粉末进行选区激光熔化成型工艺处理下铝合金的光镜图。将制备的所述铝合金粉末进行选区激光熔化成型(SLM)工艺处理,在本实施例中工艺处理参数激光功率为300W,扫描速度为1000mm/s,扫描间距为80μm,层间厚度为30μm。通过上述3D打印工艺制备成形的样件,质量良好,致密度高,样件内部没有观察到明显的孔洞、裂纹等缺陷。The difference between this embodiment and Embodiments 1 and 3 is that, as shown in FIG. 3c, FIG. 3c is an optical microscope image of the aluminum alloy powder subjected to selective laser melting molding process. The prepared aluminum alloy powder was subjected to a selective laser melting (SLM) process. In this embodiment, the process parameters were 300 W laser power, 1000 mm/s scanning speed, 80 μm scanning distance, and 30 μm interlayer thickness. The sample prepared by the above 3D printing process has good quality and high density, and no obvious holes, cracks and other defects are observed inside the sample.

实施例5Example 5

基于上述实施例,将制备获得的该高强耐热耐损伤铝合金粉末材料通过3D打印,3D打印的样件经过铣面、清洗,通过线切割加工方式切割成室温/高温拉伸试样尺寸;进一步的,拉伸试样经过打磨处理并用酒精清洗。Based on the above examples, the prepared high-strength, heat-resistant and damage-resistant aluminum alloy powder material was 3D printed, and the 3D printed sample was milled, cleaned, and cut into room temperature/high temperature tensile sample size by wire cutting; Further, the tensile specimens were ground and cleaned with alcohol.

其中,室温、高温拉伸试样分别在CMT5205和CMT5808试验机上完成。如图6所示,图6为本发明所述3D打印铝合金不同温度条件下的力学性能图。分别选取实施例1中经过处理的样件和实施例2经过处理的样件,并观察不同温度下的应力应变曲线的变化。包括:温度在25℃下的实施例1样件的应力应变曲线变化,以及温度分别在25℃、150℃、250℃下的实施例2样件的应力应变曲线变化。其中,实施例2中样件在不同温度条件下的力学性能试验数据如下表1所示。Among them, the room temperature and high temperature tensile samples were completed on CMT5205 and CMT5808 testing machines respectively. As shown in Fig. 6, Fig. 6 is a diagram of the mechanical properties of the 3D printed aluminum alloy according to the present invention under different temperature conditions. Select the treated sample in embodiment 1 and the processed sample in embodiment 2 respectively, and observe the changes of the stress-strain curves at different temperatures. Including: the change of the stress-strain curve of the sample of Example 1 at a temperature of 25°C, and the change of the stress-strain curve of the sample of Example 2 at a temperature of 25°C, 150°C, and 250°C. Wherein, the mechanical performance test data of the samples in Example 2 under different temperature conditions are shown in Table 1 below.

表1实施例2在不同温度条件下的力学性能结果The mechanical property result of table 1 embodiment 2 under different temperature conditions

Figure BDA0003952784640000061
Figure BDA0003952784640000061

实施例2与已经报道的3D打印铝合金(Scalmalloy合金,AlSi10Mg)和铸造态合金相比,样件具有优良的综合力学性能,如图7所示,图7为本发明所述3D打印铝合金与其他合金在不同温度条件下的力学性能对比图。包括在室温下具有高强度和延展性,并在高温下热稳定性优良,强度损失小。Embodiment 2 Compared with the reported 3D printing aluminum alloy (Scalmalloy alloy, AlSi10Mg) and cast alloy, the sample has excellent comprehensive mechanical properties, as shown in Figure 7, Figure 7 is the 3D printing aluminum alloy of the present invention Comparison of mechanical properties with other alloys at different temperatures. Including high strength and ductility at room temperature, and excellent thermal stability at high temperature with little loss of strength.

一种高强耐热耐损伤铝合金优异的力学性能源于固溶强化、纳米颗粒有序强化和晶界强化的协同作用。如图4所示,图4为本发明所述高强耐热耐损伤铝合金粉末经过3D打印后的透射电镜HADDF图及对应Ca元素的分布。沿晶界的半网络Al4Ca抑制了高温下的晶粒生长,保持了较高的强度。The excellent mechanical properties of a high-strength heat-resistant and damage-resistant aluminum alloy are derived from the synergistic effect of solid solution strengthening, ordered strengthening of nanoparticles and grain boundary strengthening. As shown in Figure 4, Figure 4 is the HADDF diagram of the transmission electron microscope and the distribution of the corresponding Ca element after the high-strength, heat-resistant and damage-resistant aluminum alloy powder of the present invention has been 3D printed. The semi-network Al4Ca along the grain boundary suppresses the grain growth at high temperature and maintains high strength.

与铸造合金相比,强度的增加主要是由于增材制造过程中快速凝固导致晶粒和Al3(Sc,Zr)纳米粒子尺寸减小,如图5所示,图5为本发明所述高强耐热耐损伤铝合金粉末经过3D打印后的高分辨透射电镜图显示纳米弥散第二相粒子。Compared with cast alloys, the increase in strength is mainly due to the rapid solidification during the additive manufacturing process, which leads to the reduction in the size of grains and Al 3 (Sc, Zr) nanoparticles, as shown in Figure 5, which is a high-strength alloy according to the present invention. The high-resolution transmission electron microscope image of heat-resistant and damage-resistant aluminum alloy powder after 3D printing shows nano-dispersed second phase particles.

在本申请所提出的这一种3D打印用铝合金粉末中合金元素Ca的添加,显著的抑制了合金的热裂纹倾向性。如图8所示,图8为本发明所述3D打印铝合金的热裂纹敏感因子随着Ca含量的变化图。Ca的添加使合金的裂纹敏感性显著降低,同时3D打印后的样件在较宽的打印工艺窗口内都没有发现明显的热裂现象,证明了本申请所公开的这一种高强耐热耐损伤铝合金粉末在3D打印制备过程中具有明显的抑制损伤的优势。The addition of alloying element Ca in the aluminum alloy powder for 3D printing proposed in this application significantly suppresses the hot cracking tendency of the alloy. As shown in FIG. 8 , FIG. 8 is a graph showing the variation of the thermal crack sensitivity factor of the 3D printed aluminum alloy according to the present invention with the Ca content. The addition of Ca significantly reduces the crack sensitivity of the alloy. At the same time, no obvious hot cracking phenomenon was found in the 3D printed samples in a wide printing process window, which proves that the high-strength, heat-resistant and resistant alloy disclosed in this application Damage Aluminum alloy powder has the obvious advantage of inhibiting damage during the preparation process of 3D printing.

以上所述仅为本申请的优选实施例而已,其并非因此限制本申请的保护范围,对于本领域的技术人员来说,本申请可以有各种更改和变化。凡在本申请的精神和原则之内,通过常规的替代或者能够实现相同的功能在不脱离本申请的原理和精神的情况下对这些实施例进行变化、修改、替换、整合和参数变更均落入本申请的保护范围内。The above descriptions are only preferred embodiments of the present application, which are not intended to limit the scope of protection of the present application. For those skilled in the art, various modifications and changes can be made to the present application. Within the spirit and principles of the application, changes, modifications, replacements, integrations and parameter changes of these embodiments can be achieved through conventional substitutions or can achieve the same function without departing from the principles and spirit of the application. Into the scope of protection of this application.

Claims (8)

1. The high-strength heat-resistant damage-resistant aluminum alloy powder is characterized by comprising the following components in percentage by mass: mg:4.0 to 12%, ca: 0.50-3.0%, sc:0.10 to 0.90%, mn:0.20 to 1.5%, zr:0.1 to 0.5 percent, and the balance of Al and inevitable introduced impurity elements.
2. A method of making a high strength, heat resistant, damage tolerant aluminum alloy powder as recited in claim 1 comprising the steps of:
step 1, preparing element components: the aluminum alloy powder comprises the following components of Mg, ca, sc, mn and Zr, and the balance of Al;
step 2, vacuum melting-atomization powder preparation: vacuum smelting is carried out on the high-strength heat-resistant aluminum alloy powder prepared in the step 1; and atomizing to prepare powder after vacuum melting, thus obtaining the high-strength heat-resistant damage-resistant aluminum alloy powder.
3. The method for preparing high-strength heat-resistant damage-resistant aluminum alloy powder according to claim 2, wherein in the step 2, the melting temperature of vacuum melting is 750-850 ℃, and the vacuum degree is less than or equal to 0.1Pa.
4. The method for preparing high-strength heat-resistant damage-resistant aluminum alloy powder according to any one of claims 2 or 3, wherein in the step 2, the vacuum atomization process is performed by introducing Ar, he or mixed gas for protection and atomizing, and the atomization pressure is 0.3-10 MPa.
5. Use of the high strength, heat and damage resistant aluminium alloy powder according to claim 1 in 3D printing technology.
6. The application of the high-strength heat-resistant damage-resistant aluminum alloy powder in 3D printing according to claim 5, wherein the prepared aluminum alloy powder is applied in 3D printing, and the method comprises the following steps:
firstly, heat-preserving the aluminum alloy powder in inert gas at the temperature of 300-400 ℃ for 3-6 h;
and step two, performing 3D printing on the powder subjected to heat preservation treatment.
7. The use of a high strength heat and damage resistant aluminum alloy powder in 3D printing as claimed in claim 6, wherein the aluminum alloy powder is subjected to selective laser melting forming treatment, wherein the laser power is 200-400W, the scanning speed is 500-2000 mm/s, the scanning pitch is 50-120 μm, and the interlayer thickness is 20-50 μm.
8. Use of a high strength heat resistant damage tolerant aluminium alloy powder in 3D printing according to any one of claims 6 or 7 wherein after step two the 3D printed alloy is heat treated at a temperature of 300 to 420 ℃ for a period of 3 to 36 hours.
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CN119162494A (en) * 2024-11-22 2024-12-20 中国航发北京航空材料研究院 A heat-resistant high-strength aluminum alloy material for additive manufacturing and a preparation method thereof
CN119162494B (en) * 2024-11-22 2025-02-11 中国航发北京航空材料研究院 Heat-resistant high-strength aluminum alloy material for additive manufacturing and preparation method thereof

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