CN113373388B - A method for improving the ductility and toughness of boron-containing eutectic alloys by using dual structure - Google Patents

A method for improving the ductility and toughness of boron-containing eutectic alloys by using dual structure Download PDF

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CN113373388B
CN113373388B CN202110471441.XA CN202110471441A CN113373388B CN 113373388 B CN113373388 B CN 113373388B CN 202110471441 A CN202110471441 A CN 202110471441A CN 113373388 B CN113373388 B CN 113373388B
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张柯
张凤辉
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Baoji University of Arts and Sciences
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Abstract

The invention discloses a method for improving the plasticity and toughness of a boron-containing eutectic alloy by utilizing a double-structure, which is characterized in that the double-structure is obtained by means of an integrated regulation and control means of non-equilibrium solidification and subsequent isothermal annealing heat treatment, so that the plasticity and toughness of the boron-containing eutectic alloy are improved; and (3) carrying out subsequent isothermal annealing heat treatment on the non-equilibrium solidification structure of the eutectic alloy, so that a surface single-phase recrystallization tissue layer is obtained, the interior of the surface single-phase recrystallization tissue layer is a double-structure with two irregular phases, and the strength and the ductility and the toughness of the alloy are improved. The method combines the non-equilibrium solidification structure acquisition and the subsequent structure transformation of the boron-containing eutectic alloy by combining the non-equilibrium solidification method with the subsequent isothermal annealing heat treatment to obtain an alloy double-structure, thereby realizing the improvement of the comprehensive mechanical property of the alloy, greatly enriching and promoting the existing eutectic alloy structure property regulation and control method, and being used for regulating and controlling the mechanical property of boron-containing eutectic and similar alloy materials.

Description

一种利用双组织结构提升含硼共晶合金塑韧性的方法A method for improving the ductility and toughness of boron-containing eutectic alloys by using dual structure

技术领域technical field

本发明属于金属材料加工技术领域,特别是涉及一种利用双组织结构提升含硼共晶合金塑韧性的方法。The invention belongs to the technical field of metal material processing, and in particular relates to a method for improving the plasticity and toughness of a boron-containing eutectic alloy by utilizing a dual structure.

背景技术Background technique

因其丰富的组织花样及优异的综合性能,共晶合金一直是工业应用最广泛的合金之一,而通过调控共晶合金的组织改进合金性能也一直为人们所关注。(Fe,Ni)-B共晶合金因具有优异的软磁性能,良好的力学性能以及冶金性能而被人们研究并应用,决定合金服役性能的合金组织往往受控于其凝固及后续冷/热加工过程,而其中的一个关键问题就是合金凝固组织的演化及其后续转变组织调控。通过非平衡凝固技术获取平衡条件下无法实现的非平衡组织,也一直是凝固科学和技术研究的重要内容。非平衡凝固组织不仅具有平衡态组织所不具备的力学、物理性能,而且基于非平衡凝固组织的亚稳特性,结合热处理手段诱发后续固态转变,可实现合金终态组织进一步调控。Due to its rich microstructure and excellent comprehensive properties, eutectic alloys have always been one of the most widely used alloys in industry, and people's attention has been paid to improving the properties of eutectic alloys by regulating the microstructure of eutectic alloys. (Fe, Ni)-B eutectic alloys have been studied and applied because of their excellent soft magnetic properties, good mechanical properties and metallurgical properties. The alloy structure that determines the service performance of the alloy is often controlled by its solidification and subsequent cooling/heating. One of the key issues is the evolution of the solidification structure of the alloy and its subsequent transformation and control of the structure. Obtaining non-equilibrium structures that cannot be achieved under equilibrium conditions by non-equilibrium solidification technology has always been an important part of solidification science and technology research. The non-equilibrium solidified structure not only has mechanical and physical properties that the equilibrium structure does not have, but also based on the metastable characteristics of the non-equilibrium solidified structure, combined with heat treatment to induce subsequent solid state transformation, the final state structure of the alloy can be further regulated.

合金材料理想的服役性能是高强度兼具良好塑性,而以位错理论为基础的传统强化方法导致合金强度提升必然以牺牲材料部分塑性为代价。大量研究发现,通过施加组织非平衡性结合后续热处理固态转变,可以实现材料强度和塑性同时改善。在传统意义上,依靠后续静态再结晶转变实现金属组织性能改善,只能够在具有冷变形金属材料中通过后续再结晶退火实现。而非平衡凝固作为合金组织非平衡性产生的有效手段,如与后续热处理结合,则可实现合金组织性能一体化调控。The ideal service performance of alloy materials is high strength and good plasticity, and the traditional strengthening method based on dislocation theory leads to the increase of alloy strength at the expense of partial plasticity of the material. Numerous studies have found that the simultaneous improvement of material strength and plasticity can be achieved by applying structural nonequilibrium combined with subsequent heat treatment for solid-state transformation. In the traditional sense, the improvement of metal structure and properties by subsequent static recrystallization transformation can only be achieved by subsequent recrystallization annealing in metallic materials with cold deformation. Non-equilibrium solidification is an effective means to generate the non-equilibrium of the alloy structure. If combined with the subsequent heat treatment, the integrated control of the alloy structure and properties can be realized.

非平衡凝固组织后续热处理转变研究伴随着Fe-,Ni-基合金的应用已开展多年,但大都集中于单相组织或单相合金,而共晶合金非平衡凝固组织后续转变研究甚少,这主要归因于单相组织后续转变单一,便于从实验和理论上对转变驱动力来源、过程及最终组织进行表征。近年共晶合金凝固组织的后续固态转变研究伴随综合性能优异的高熵合金成为材料研究及应用热点也有开展,但其研究对象主要针对常规平衡或近平衡凝固组织,此类组织后续再结晶转变发生的先决条件是人为引入非平衡性,即试样经受较大塑性变形。这归因于共晶合金非平衡凝固组织往往非单一转变过程产生,共晶合金非平衡凝固过程包含共晶团组织的初生凝固及团间残余液相的后续凝固,甚至亚稳相组织的形成,使得凝固过程非平衡效应耗散方式多样,组织非平衡性在凝固及后续冷却过程可通过多种方式释放,平衡及近平衡凝固条件下,合金组织中的非平衡性较少累积和存储。The research on the subsequent heat treatment transformation of non-equilibrium solidification structure has been carried out for many years along with the application of Fe- and Ni-based alloys, but most of them focus on single-phase structure or single-phase alloy, while the follow-up transformation of non-equilibrium solidification structure of eutectic alloys is rarely studied. It is mainly attributed to the single subsequent transformation of the single-phase organization, which is convenient to characterize the source, process and final organization of the transformation driving force experimentally and theoretically. In recent years, the follow-up solid-state transformation research on the solidification structure of eutectic alloys has been carried out with the high-entropy alloys with excellent comprehensive properties becoming a material research and application hotspot. The prerequisite is the artificial introduction of non-equilibrium, that is, the specimen undergoes large plastic deformation. This is attributed to the fact that the non-equilibrium solidification structure of eutectic alloys is often not produced by a single transformation process. The non-equilibrium solidification process of eutectic alloys includes the primary solidification of the eutectic cluster structure and the subsequent solidification of the residual liquid phase between the clusters, and even the formation of the metastable phase structure. , so that the non-equilibrium effect of the solidification process is dissipated in various ways, and the structure non-equilibrium can be released in various ways during the solidification and subsequent cooling process. Under the conditions of equilibrium and near-equilibrium solidification, the non-equilibrium in the alloy structure is less accumulated and stored.

发明内容SUMMARY OF THE INVENTION

本发明解决了现有工艺方法中的不足,提供一种利用双组织结构提升含硼共晶合金塑韧性的方法,借助非平衡凝固获得合金组织非平衡性,而无需借助人为塑性变形,与后续热处理一体化调控技术结合形成双组织结构,提升含硼共晶合金塑韧性。The invention solves the deficiencies in the existing process methods, provides a method for improving the plastic toughness of a boron-containing eutectic alloy by using a double structure, and obtains the non-equilibrium of the alloy structure by means of non-equilibrium solidification, without artificial plastic deformation, and is compatible with subsequent The integrated control technology of heat treatment is combined to form a dual structure, which improves the plasticity and toughness of boron-containing eutectic alloys.

本发明所采用的技术方案:一种利用双组织结构提升含硼共晶合金塑韧性的方法,其特征在于,具有以下步骤:The technical scheme adopted in the present invention: a method for improving the plastic toughness of a boron-containing eutectic alloy by utilizing a dual structure, which is characterized in that it has the following steps:

S1:选择含硼二元或三元共晶合金,采用高频电磁感应熔炼炉对所述共晶合金进行熔炼,利用熔融玻璃净化结合循环过热方法获得过冷合金熔体,对过冷合金熔体进行自然冷却或激冷获得共晶合金非平衡凝固组织;S1: Select a boron-containing binary or ternary eutectic alloy, use a high-frequency electromagnetic induction melting furnace to smelt the eutectic alloy, use molten glass purification combined with a cyclic superheating method to obtain a supercooled alloy melt, and melt the supercooled alloy The body is naturally cooled or chilled to obtain a non-equilibrium solidification structure of the eutectic alloy;

S2:对共晶合金非平衡凝固组织进行等温退火热处理,以共晶合金非平衡凝固组织中累积的非平衡性为驱动力,在等温退火热处理的诱导下,其表层组织脱硼的同时发生再结晶转变,形成单相组织层,与其内部非规则共晶组织构成双组织结构。S2: Perform isothermal annealing heat treatment on the non-equilibrium solidification structure of the eutectic alloy. The non-equilibrium accumulated in the non-equilibrium solidification structure of the eutectic alloy is used as the driving force. Crystallization transforms to form a single-phase structure layer, which forms a dual structure with its internal irregular eutectic structure.

优选的,所述共晶合金为Fe40Ni40B20(at.%)合金,共晶转变温度为1323K。Preferably, the eutectic alloy is Fe40Ni40B20 (at.%) alloy, and the eutectic transformation temperature is 1323K.

优选的,在S1中,共晶合金非平衡凝固组织累积一定的非平衡性,其共晶合金非平衡凝固组织初始过冷度大于等于170K时进行自然冷却,或其共晶合金非平衡凝固组织初始过冷度小于100K进行激冷处理。Preferably, in S1, the non-equilibrium solidification structure of the eutectic alloy accumulates a certain degree of non-equilibrium, and the non-equilibrium solidification structure of the eutectic alloy is naturally cooled when the initial undercooling degree is greater than or equal to 170K, or the non-equilibrium solidification structure of the eutectic alloy is The initial subcooling degree is less than 100K for chilling treatment.

优选的,在S1中,所述激冷处理借助红外测温仪监测采集过冷合金熔体的冷却过程温度数据,过冷度小于100K时,将过冷合金熔体倾入Ga-In液态合金或铜金属模具中进行激冷处理。Preferably, in S1, in the chilling treatment, the temperature data of the cooling process of the supercooled alloy melt is monitored and collected by means of an infrared thermometer, and when the degree of subcooling is less than 100K, the supercooled alloy melt is poured into the Ga-In liquid alloy or Chilled in a copper metal mold.

优选的,在S2中,在真空或保护氛围下进行等温退火热处理,退火温度873K至1273K,退火时间1.5h至60h。Preferably, in S2, isothermal annealing heat treatment is performed in a vacuum or a protective atmosphere, the annealing temperature is 873K to 1273K, and the annealing time is 1.5h to 60h.

与现有技术相比,本发明具有如下有益效果:Compared with the prior art, the present invention has the following beneficial effects:

1、本发明将非平衡凝固与后续热处理技术相结合,利用快速凝固方法自发实现合金微观组织中非平衡累积,结合后续热处理转变,获得双组织结构,实现合金塑韧性的提升。具体的,由于深过冷非平衡凝固,可以实现合金组织非平衡亚稳定组织,其中包含大量微观缺陷,微观应力应变等组织非平衡性;进一步结合激冷更大程度保留组织非平衡性,形成后续再结晶转变驱动力,后续热处理过程表层组织脱硼同时发生再结晶转变,形成表层单相再结晶塑性组织层而内部为非规则两相组织的双组织结构,提升合金的塑韧性和综合力学性能。1. The present invention combines non-equilibrium solidification with subsequent heat treatment technology, utilizes the rapid solidification method to spontaneously realize non-equilibrium accumulation in the microstructure of the alloy, and combines the subsequent heat treatment transformation to obtain a dual-structure structure, thereby improving the plasticity and toughness of the alloy. Specifically, due to the non-equilibrium solidification of deep undercooling, the non-equilibrium metastable structure of the alloy structure can be realized, which contains a large number of microscopic defects, microscopic stress and strain and other microstructure non-equilibrium; further combined with chilling, the microstructure non-equilibrium can be preserved to a greater extent, forming The driving force of the subsequent recrystallization transformation, the deboronization of the surface layer and the recrystallization transformation occur at the same time during the subsequent heat treatment, forming a single-phase recrystallized plastic structure layer on the surface layer and a dual-structure structure with irregular two-phase structure inside, which improves the plastic toughness and comprehensive mechanics of the alloy. performance.

2、本发明提供的无需人为引入非平衡性(塑性变形)实现组织一体化调控的方法,一方面简化了含硼共晶合金组织性能一体化工序和工艺;另一方面获得合金组织塑性和韧性可显著提升,这极大的丰富和推进了已有共晶合金组织调控和性能改进的方法,该方法也可被推广于其他类似合金材料组织性能一体化调控,因而具有重要的生产实践意义。通过深过冷以及激冷凝固等非平衡凝固技术,实现合金远离平衡状态凝固,产生组织非平衡性(如大量微观缺陷、应力引起的晶格畸变等),并迅速保留,累积下的组织非平衡性可作为后续转变的驱动力,在合金后续组织热处理过程推动组织进一步转变。已有铝合金激冷亚快速凝固,结合后续低温退火实验可以获得多级析出相的组织,同时提升合金强度和塑性。合金激光快速成型过程,金属同样经历非平衡快速凝固,凝固非平衡效应不仅影响凝固组织的形成演化,同时也影响后续热处理转变,凝固和热处理共同决定材料终态性能。2. The method provided by the present invention does not require artificially introducing non-equilibrium (plastic deformation) to realize the integrated control of the structure. On the one hand, it simplifies the process and process of integrating the structure and properties of the boron-containing eutectic alloy; on the other hand, the plasticity and toughness of the alloy structure are obtained. It can be significantly improved, which greatly enriches and promotes the existing methods of eutectic alloy structure control and performance improvement, and this method can also be extended to other similar alloy materials. Through non-equilibrium solidification technologies such as deep undercooling and chilling solidification, the alloy is solidified away from the equilibrium state, resulting in structural non-equilibrium (such as a large number of microscopic defects, lattice distortion caused by stress, etc.), and quickly retained, and the accumulated structural non-equilibrium Equilibrium can be used as the driving force for subsequent transformation, and promote further transformation of the structure during the subsequent heat treatment of the alloy. Existing aluminum alloys have been sub-rapidly solidified by quenching. Combined with the subsequent low-temperature annealing experiments, the structure of multi-stage precipitation can be obtained, and the strength and plasticity of the alloy can be improved at the same time. In the process of alloy laser rapid prototyping, the metal also undergoes non-equilibrium rapid solidification. The non-equilibrium effect of solidification not only affects the formation and evolution of the solidified structure, but also affects the subsequent heat treatment transformation. Solidification and heat treatment jointly determine the final properties of the material.

附图说明Description of drawings

图1为本发明实施例1-实施例2中合金熔体再辉-冷却温度曲线,其中,图1(a)为实施例1的初始过冷度70K和250K的Fe40Ni40B20(at.%)共晶合金熔体再辉-冷却温度曲线,图1(b)为Fe40Ni40B20(at.%)合金力学性能测试试样加工尺寸试样图;Fig. 1 is the re-brightening-cooling temperature curve of the alloy melt in Example 1-Example 2 of the present invention, wherein, Fig. 1(a) is the Fe40Ni40B20 (at.%) of the initial undercooling degree of 70K and 250K in Example 1. The re-glow-cooling temperature curve of the crystalline alloy melt, Figure 1(b) is the processing size of the Fe40Ni40B20 (at.%) alloy mechanical property test sample;

图2为本发明实施例1制备的Fe40Ni40B20(at.%)共晶合金深过冷非平衡凝固组织及显微结构示意图;其中,图2(a)为光学显微镜下合金组织,图2(b)为透射电镜下组织中的位错、层错等非平衡结构,图2(c)为合金非平衡组织相组成XRD衍射结果;Figure 2 is a schematic diagram of the deep undercooling non-equilibrium solidification structure and microstructure of the Fe40Ni40B20 (at.%) eutectic alloy prepared in Example 1 of the present invention; wherein, Figure 2 (a) is the alloy structure under an optical microscope, Figure 2 (b) ) are the non-equilibrium structures such as dislocations and stacking faults in the microstructure under the transmission electron microscope, and Fig. 2(c) is the XRD diffraction result of the phase composition of the non-equilibrium microstructure of the alloy;

图3为本发明实施例1深过冷非平衡凝固Fe40Ni40B20(at.%)共晶合金试样等温退火热处理后表层及横截面组织及相组成;其中图3(a)为表层组织及相组成XRD结果,图3(b)为试样横截面组织;Fig. 3 is the surface layer and cross-sectional structure and phase composition of the deep undercooling non-equilibrium solidification Fe40Ni40B20 (at.%) eutectic alloy sample after isothermal annealing heat treatment in Example 1 of the present invention; wherein Fig. 3(a) is the surface layer structure and phase composition XRD results, Figure 3(b) is the cross-sectional structure of the sample;

图4为本发明实施例2制备的Fe40Ni40B20(at.%)共晶合金小过冷凝固组织及其等温退火后组织;其中图4(a)为小过冷度下共晶合金凝固组织及显微结构透射电镜示意图,图4(b)为小过冷凝固试样等温退火处理后表层组织形貌及XRD衍射结果示意图;Fig. 4 is the micro-undercooling solidification structure of Fe40Ni40B20 (at.%) eutectic alloy prepared in Example 2 of the present invention and the microstructure after isothermal annealing; Fig. 4(a) is the solidification structure and the apparent microstructure of the eutectic alloy under small undercooling degree. Schematic diagram of microstructure transmission electron microscope, Figure 4(b) is a schematic diagram of the surface microstructure and XRD diffraction results of the undercooled solidified sample after isothermal annealing;

图5为本发明实施例3中大过冷凝固试样,不同热处理时长下表层及表层附近组织金相照片;其中图5(a)-5(e)对应等温退火时长分别为0.5h,4h,12h,40h,60h;Figure 5 is a metallographic photograph of the undercooled solidification sample in Example 3 of the present invention, with different heat treatment durations of the lower surface layer and the microstructure near the surface layer; wherein the corresponding isothermal annealing durations of Figures 5(a)-5(e) are 0.5h and 4h respectively , 12h, 40h, 60h;

图6为本发明实施例3中大过冷凝固试样,较低等温退火温度下热处理表层组织X射线衍射结果;其中图6(a)为873K处理1.5h结果,图6(b)为1073K处理1h结果;Figure 6 is the X-ray diffraction result of the surface layer structure of the large undercooled solidification sample in Example 3 of the present invention, heat-treated at a lower isothermal annealing temperature; Figure 6(a) is the result of 873K treatment for 1.5h, and Figure 6(b) is 1073K Process 1h result;

图7为本发明实施例3中不同大过冷度试样1173K等温退火热处理再结晶组织层厚度随处理时间变化关系及计算结果;Fig. 7 is the variation relation and the calculation result of the thickness of the recrystallized microstructure layer of the samples with different large undercooling degree 1173K isothermal annealing heat treatment with the treatment time in Example 3 of the present invention;

图8为本发明实施例4制备的共晶合金铜模激冷非平衡凝固组织及其热处理后组织;其中,图8(a)为合金非平衡组织,图8(b)为铜模激冷非平衡凝固试样热处理后1173K等温退火40h后试样表层及附近组织;Fig. 8 is the non-equilibrium solidification structure of the eutectic alloy copper mold prepared in Example 4 of the present invention and the structure after heat treatment; wherein, Fig. 8(a) is the non-equilibrium structure of the alloy, and Fig. 8(b) is the cooling of the copper mold. Non-equilibrium solidification sample after heat treatment at 1173K isothermal annealing for 40h, the surface layer and nearby microstructure of the sample;

图9为本发明实施例5中不同处理状态下合金试样拉伸力性能曲线,图中As-s代表非平衡凝固试样,HT代表等温退火热处理试样。FIG. 9 is the tensile force performance curve of the alloy sample under different treatment states in Example 5 of the present invention. In the figure, As-s represents the non-equilibrium solidification sample, and HT represents the isothermal annealing heat treatment sample.

具体实施方式Detailed ways

为使本领域技术人员更好地理解本发明的技术方案,并能予以实施,下面结合具体实施例对本发明作进一步说明,但所举实施例不作为对本发明的限定。In order for those skilled in the art to better understand the technical solutions of the present invention and implement them, the present invention will be further described below with reference to specific embodiments, but the embodiments are not intended to limit the present invention.

实施例1Example 1

本实施例选择含硼三元共晶Fe40Ni40B20(at.%)合金为实验合金系,其共晶转变温度为1323K,利用电弧熔炼方法获得该成分合金的母合金,进一步取质量20g母合金,利用高频电磁感应熔炼炉结合熔融玻璃净化与循环过热方法,获得过冷合金熔体。对过冷合金熔体进行自然冷却获得共晶合金非平衡凝固组织;过冷合金熔体初始过冷度大于等于170K时进行自然冷却(此例中过冷度为250K)的Fe40Ni40B20(at.%),对共晶合金非平衡凝固组织取合金试样,采用测温仪激冷合金熔体凝固过程冷却曲线,如图1(a)所示。随后依据力学性能试样加工标准中非标试样尺寸参考要求,将合金试样加工成拉伸及弯曲样品,尺寸示意如图1(b),将试样用熔融玻璃包覆密封于石英坩埚,置于真空或普通热处理炉中进行等温退火热处理,退火温度为1173K,处理时长60h。In this example, boron-containing ternary eutectic Fe40Ni40B20 (at.%) alloy is selected as the experimental alloy system, and its eutectic transformation temperature is 1323K. The master alloy of this component alloy is obtained by the arc melting method. The high-frequency electromagnetic induction melting furnace combines molten glass purification and circulating superheating methods to obtain supercooled alloy melt. The non-equilibrium solidification structure of the eutectic alloy is obtained by natural cooling of the supercooled alloy melt; Fe40Ni40B20 (at.%) of Fe40Ni40B20 (at. ), take the alloy sample for the non-equilibrium solidification structure of the eutectic alloy, and use a thermometer to chill the cooling curve of the solidification process of the alloy melt, as shown in Figure 1(a). Then, according to the non-standard sample size reference requirements in the mechanical property sample processing standard, the alloy sample is processed into tensile and bending samples, the size of which is shown in Figure 1(b), and the sample is covered with molten glass and sealed in a quartz crucible. , placed in a vacuum or ordinary heat treatment furnace for isothermal annealing heat treatment, the annealing temperature is 1173K, and the treatment time is 60h.

我们对实施例1方法获得的合金试样进行样品制备,测试分析其共晶合金非平衡凝固组织相组成及微观结构,如图2所示。对等温退火热处理后合金组织进行观测分析,温退火热处理后合金组织横截面及表层组织微观结构及相组成如图3所示。由图3可以看出,合金非平衡深过冷凝固组织为(FeNi)3B和γ-FeNi构成的两相非规则共晶,合金相内部包含大量非平衡效应累积所产生的位错网络,堆垛层错等;等温退火热处理后,合金试样表层组织发生脱硼和再结晶转变,形成表层单相γ-FeNi固溶体而内部依然为非规则两相的双组织结构。We prepared samples of the alloy samples obtained by the method in Example 1, and tested and analyzed the phase composition and microstructure of the non-equilibrium solidification structure of the eutectic alloy, as shown in Figure 2. The microstructure of the alloy after isothermal annealing and heat treatment was observed and analyzed. It can be seen from Figure 3 that the non-equilibrium deep undercooling solidification structure of the alloy is a two-phase irregular eutectic composed of (FeNi) 3 B and γ-FeNi, and the alloy phase contains a large number of dislocation networks generated by the accumulation of non-equilibrium effects. Stacking faults, etc.; after isothermal annealing and heat treatment, the surface structure of the alloy sample undergoes deboronization and recrystallization transformation, forming a single-phase γ-FeNi solid solution on the surface and a dual structure with irregular two-phase inside.

实施例2Example 2

本实施例的具体过程和实施例1相同,不同之处仅在于,过冷合金熔体过冷度小于100K。主要是为了考察小过冷度自然凝固组织(近平衡凝固组织)后续转变能否发生,以验证组织非平衡性对后续转变的驱动作用。合金试样过冷凝固组织光镜及透射电镜照片如图4(a),1173K等温热处理60h后组织及相组成XRD结果如图4(b)所示。The specific process of this example is the same as that of Example 1, the difference is only that the undercooling degree of the undercooled alloy melt is less than 100K. The main purpose is to investigate whether the subsequent transformation of the naturally solidified structure (near-equilibrium solidified structure) with small undercooling degree can occur, so as to verify the driving effect of the structure non-equilibrium on the subsequent transformation. The light microscope and transmission electron microscope photos of the supercooled solidification of the alloy sample are shown in Figure 4(a), and the XRD results of the microstructure and phase composition after isothermal heat treatment at 1173K for 60 h are shown in Figure 4(b).

可以看出,合金试样的组织包含部分规则共晶,为近平衡凝固组织,组织中非平衡效应累积较弱,对应组织中位错等缺陷较少;合金试样等温退火热处理后表层组织亦未发生显著固态转变,依然为非规则两相组织。It can be seen that the structure of the alloy sample contains part of regular eutectic, which is a near-equilibrium solidification structure, the accumulation of non-equilibrium effects in the structure is weak, and there are fewer defects such as dislocations in the corresponding structure; the surface structure of the alloy sample after isothermal annealing heat treatment also changes. No significant solid-state transformation has occurred, and it is still an irregular two-phase structure.

实施例3Example 3

本实施例的具体过程和实施例1相同,不同之处仅在于,共晶合金非平衡凝固组织后续等温退火热处理温度为1173K,等温时长分别为0.5h,4h,12h,40h,60h,主要是为了考察不同热处理时长对共晶合金非平衡凝固组织后续转变影响,不同等温退火时长对应合金表层及附近组织如图5;同时在873K和1073K分别对共晶合金非平衡凝固组织进行1.5h和1h等温退火热处理,主要为了确定非平衡凝固组织后续转变可发生的等温温度,由于合金试样表层组织单相层很薄,金相组织制取需要磨、抛光及腐蚀,无法获得,因此对应等温温度下合金试样表层组织采用XRD衍射方法分析其相组成,结果如图6,可依据以上实验结果制定合金热处理工艺。The specific process of this example is the same as that of Example 1, the only difference is that the subsequent isothermal annealing heat treatment temperature of the non-equilibrium solidification structure of the eutectic alloy is 1173K, and the isothermal time durations are 0.5h, 4h, 12h, 40h, 60h respectively. In order to investigate the effect of different heat treatment time on the subsequent transformation of the non-equilibrium solidification structure of the eutectic alloy, the surface layer and nearby microstructure of the alloy corresponding to different isothermal annealing time are shown in Figure 5; at the same time, the non-equilibrium solidification structure of the eutectic alloy was subjected to 1.5h and 1h at 873K and 1073K, respectively. Isothermal annealing heat treatment is mainly to determine the isothermal temperature at which the subsequent transformation of the non-equilibrium solidified structure can occur. Since the single-phase layer of the surface structure of the alloy sample is very thin, the preparation of the metallographic structure requires grinding, polishing and corrosion, which cannot be obtained. Therefore, the corresponding isothermal temperature The surface structure of the lower alloy sample was analyzed by XRD diffraction method. The results are shown in Figure 6. The alloy heat treatment process can be formulated according to the above experimental results.

可以看出,合金试样热处理0.5h表层即已开始发生脱硼及再结晶固态转变,对各合金试样不同等温退火时长表层再结晶单相组织层厚度进行测量,以退火时间为横坐标,单相层厚度为纵坐标绘图,同时采用扩散控制固态转变方程Zener方程进行简单计算,如图7所示,可见表层单相固溶体层随着等温处理时间增加而增厚,共晶合金非平衡凝固组织表层固态转变过程符合扩散及热激活控制的固态相转变规律。图6中XRD衍射结果显示873K热处理1.5h和1073K热处理1h深过冷合金试样表层即已开始发生转变,表明退火温度高于873K,转变均可发生。It can be seen that the surface layer of the alloy sample has begun to undergo deboronization and recrystallization solid state transformation after heat treatment for 0.5h. The thickness of the single-phase layer is plotted on the ordinate, and the Zener equation of the diffusion-controlled solid-state transformation equation is used for simple calculation. As shown in Figure 7, it can be seen that the surface single-phase solid solution layer increases with the increase of the isothermal treatment time, and the eutectic alloy solidifies non-equilibrium. The solid-state transformation process of the tissue surface conforms to the solid-state phase transformation law controlled by diffusion and thermal activation. The XRD diffraction results in Figure 6 show that the surface layer of the deep undercooled alloy samples after heat treatment at 873K for 1.5h and heat treatment at 1073K for 1h has begun to transform, indicating that the transformation can occur when the annealing temperature is higher than 873K.

实施例4Example 4

本实施例的具体过程和实施例1相同,不同之处仅在于,过冷合金熔体过冷度小于100K,同时结合过冷合金熔体激冷非平衡凝固手段。通过红外测温仪监测过冷合金熔体温度曲线,在过冷合金熔体冷却过程中,将过冷度小于100K的过冷合金熔体快速淬入Ga-In合金熔体或铜模型槽中,实现过冷合金熔体的激冷快速凝固。此例中过冷合金熔体过冷度约为40K时,快速淬入铜模型槽,激冷凝固组织如图8(a),采用同例1中等温退火热处理方法对共晶合金非平衡凝固组织进行热处理,等温退火温度1173K,保温时长40h,热处理后合金表层及附近组织如图8(b)。The specific process of this example is the same as that of Example 1, the only difference is that the degree of undercooling of the undercooled alloy melt is less than 100K, and the unbalanced solidification method of chilling the undercooled alloy melt is combined. The temperature curve of the supercooled alloy melt is monitored by an infrared thermometer. During the cooling process of the supercooled alloy melt, the supercooled alloy melt with a subcooling degree of less than 100K is quickly quenched into the Ga-In alloy melt or the copper model tank. , to achieve the rapid solidification of the supercooled alloy melt. In this example, when the undercooling degree of the supercooled alloy melt is about 40K, it is rapidly quenched into the copper mold groove, and the chilled solidification structure is shown in Figure 8(a). The structure was heat treated, the isothermal annealing temperature was 1173K, and the holding time was 40h. After heat treatment, the surface layer and nearby structures of the alloy were shown in Figure 8(b).

可以看出,通过小过冷结合激冷获得的共晶合金非平衡凝固合金组织为非规则两相组织,类似于大过冷凝固组织,合金试样中因激冷而被快速保留下的组织非平衡性会驱动合金后续固态转变的发生,最终合金试样由表层再结晶单相,而内部依然为非规则两相的双组织结构构成。It can be seen that the non-equilibrium solidified alloy structure of the eutectic alloy obtained by the combination of small undercooling and chilling is an irregular two-phase structure, which is similar to the solidification structure of large undercooling. The non-equilibrium will drive the subsequent solid-state transformation of the alloy, and the final alloy sample is composed of a single-phase recrystallized surface layer, while the interior is still composed of a dual structure of irregular two-phase.

实施例5Example 5

对实施例1和2中试样,以及未进行后续等温退火热处理的小过冷及大过冷非平衡凝固试样,采用微小力学性能试验机对合金试样进行拉伸和弯曲性能测试(力学性能测试试样尺寸如图1(b)所示),拉伸性能测试结果(应力-应变曲线)如图9所示;试样预置缺口三点弯曲断裂韧性计算结果如表1所示。For the samples in Examples 1 and 2, as well as the small undercooling and large undercooling non-equilibrium solidification samples without subsequent isothermal annealing heat treatment, the tensile and bending properties of the alloy samples were tested by a micro mechanical property testing machine (mechanics). The size of the performance test sample is shown in Figure 1(b)), and the tensile performance test results (stress-strain curve) are shown in Figure 9;

可以看出,相较于非平衡凝固试样,以及小过冷非平衡凝固结合后续等温退火热处理获得合金试样,大过冷凝固结合后续等温退火热处理形成的双组织结构合金试样的拉伸塑性和弯曲韧性显著提升。表1为该实施例5中不同过冷度(70K、250K)凝固试样热处理前后试样三点弯曲断裂韧性计算结果。It can be seen that, compared with the non-equilibrium solidification sample, and the alloy sample obtained by small undercooling non-equilibrium solidification combined with subsequent isothermal annealing heat treatment, the tensile strength of the double-structured alloy sample formed by large undercooling solidification combined with subsequent isothermal annealing heat treatment The plasticity and flexural toughness are significantly improved. Table 1 shows the calculation results of the three-point bending fracture toughness of the solidified samples with different undercooling degrees (70K, 250K) in Example 5 before and after heat treatment.

表1Table 1

Figure BDA0003045561360000081
Figure BDA0003045561360000081

试样状态:AS-S,原始凝固组织;HT,热处理试样Specimen state: AS-S, original solidified structure; HT, heat-treated specimen

综上,本发明利用深过冷及激冷非平衡凝固技术,获得累积大量非平衡性的FeNiB共晶合金凝固组织,例如合金微观组织塑性变形引发的位错网络。进一步,对合金非平衡凝固组织进行后续等温退火热处理,合金试样表层组织发生了显著的脱硼及再结晶转变,形成了表层为γ-FeNi单相固溶体,而内部为(FeNi)3B和γ-FeNi非规则两相的双组织结构;力学性能测试结果表明,双组织结构的形成大大提升了合金的塑性和韧性。而对小过冷自然冷却组织进行相同条件下的等温退火热处理实验,合金表层及内部组织几乎没有发生变化,合金性能亦未改变。显然,此些研究结果揭示了含硼共晶合金大过冷凝固组织非平衡累积的,以及可能手段,同时揭示了共晶合金凝固组织非平衡性驱动后续转变发生进一步调控合金组织性能的可行性。因此,该方法大大的丰富和推动了已有共晶合金组织及性能调控技术,可用于调控共晶合金材料的各种物理性能。To sum up, the present invention utilizes deep undercooling and chilling non-equilibrium solidification technology to obtain a solidified structure of FeNiB eutectic alloy that accumulates a large amount of non-equilibrium, such as dislocation network caused by plastic deformation of alloy microstructure. Further, the non-equilibrium solidification structure of the alloy was subjected to subsequent isothermal annealing heat treatment, and the surface structure of the alloy sample underwent significant deboronization and recrystallization transformation, forming a single-phase solid solution of γ-FeNi on the surface and (FeNi) 3 B and The dual structure of γ-FeNi irregular two-phase; the mechanical properties test results show that the formation of the dual structure greatly improves the plasticity and toughness of the alloy. However, in the isothermal annealing heat treatment experiment under the same conditions for the small undercooled natural cooling structure, the surface layer and internal structure of the alloy hardly changed, and the properties of the alloy did not change. Obviously, these research results reveal the possible means of non-equilibrium accumulation of boron-containing eutectic alloys under large undercooling solidification structure, and also reveal the feasibility of eutectic alloy solidification structure non-equilibrium to drive subsequent transformations to further control the alloy's microstructure and properties. . Therefore, this method greatly enriches and promotes the existing eutectic alloy structure and property control technology, which can be used to control various physical properties of eutectic alloy materials.

以上所述实施例仅是为充分说明本发明而所举的较佳的实施例,其保护范围不限于此。本技术领域的技术人员在本发明基础上所作的等同替代或变换,均在本发明的保护范围之内,本发明的保护范围以权利要求书为准。The above-mentioned embodiments are only preferred embodiments for fully illustrating the present invention, and the protection scope thereof is not limited thereto. Equivalent substitutions or transformations made by those skilled in the art on the basis of the present invention are all within the protection scope of the present invention, and the protection scope of the present invention is subject to the claims.

Claims (1)

1. A method for improving the ductility and toughness of a boron-containing eutectic alloy by using a double-structure is characterized by comprising the following steps of:
s1: selecting a boron-containing eutectic alloy, smelting the eutectic alloy by adopting a high-frequency electromagnetic induction smelting furnace, obtaining a supercooled alloy melt by utilizing a molten glass purification combined cycle overheating method, and naturally cooling or chilling the supercooled alloy melt to obtain an unbalanced solidification structure of the eutectic alloy;
the eutectic alloy is Fe40Ni40B20 (at.%) alloy, and the eutectic transformation temperature is 1323K;
certain non-equilibrium is accumulated in the non-equilibrium solidification structure of the eutectic alloy, the initial supercooling degree of the non-equilibrium solidification structure of the eutectic alloy is naturally cooled when the initial supercooling degree is more than or equal to 170K, or the initial supercooling degree of the non-equilibrium solidification structure of the eutectic alloy is less than 100K for chilling;
in the chilling treatment process, an infrared thermometer is used for monitoring and acquiring temperature data of the supercooled alloy melt In the cooling process, and when the supercooling degree is less than 100K, the supercooled alloy melt is poured into a Ga-In liquid alloy or copper metal mold for chilling treatment;
s2: carrying out isothermal annealing heat treatment on the eutectic alloy non-equilibrium solidification structure, taking the non-equilibrium accumulated in the eutectic alloy non-equilibrium solidification structure as a driving force, and carrying out recrystallization transformation while carrying out boron removal on a surface layer structure under the induction of the isothermal annealing heat treatment to form a single-phase tissue layer which forms a double-structure with an irregular eutectic structure in the single-phase tissue layer;
and carrying out isothermal annealing heat treatment under vacuum or protective atmosphere, wherein the annealing temperature is 873K to 1273K, and the annealing time is 1.5h to 60 h.
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