CN103949639B - The method that a kind of selective laser smelting technology prepares Nb-Si based ultra-high temperature alloy - Google Patents
The method that a kind of selective laser smelting technology prepares Nb-Si based ultra-high temperature alloy Download PDFInfo
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Abstract
本发明属于高温合金制备技术领域,特别涉及一种激光选区熔化技术(Selective Laser Melting,SLM)制备NbSi超高温合金的方法,利用激光选区熔化设备,通过合理的工艺参数设置,直接由CAD模型一步完成NbSi合金成形件的制备,制备的NbSi合金致密度高,缺陷少,主要由Nbss固溶体和Nb5Si3强化相组成,相尺寸细小且分布均匀。本方法制备NbSi合金无需模具,避免界面反应,减少合金污染,降低夹杂含量,材料利用率高,可以提高NbSi合金的综合性能和生产效率。
The invention belongs to the technical field of high-temperature alloy preparation, and in particular relates to a method for preparing NbSi ultra-high-temperature alloy by selective laser melting technology (Selective Laser Melting, SLM). Using laser selective melting equipment, through reasonable process parameter settings, the CAD model can be directly processed in one step. The preparation of NbSi alloy formed parts is completed. The prepared NbSi alloy has high density and few defects. It is mainly composed of Nbss solid solution and Nb 5 Si 3 strengthening phase, and the phase size is fine and evenly distributed. The method prepares the NbSi alloy without mold, avoids interface reaction, reduces alloy pollution, reduces inclusion content, has high material utilization rate, and can improve the comprehensive performance and production efficiency of the NbSi alloy.
Description
技术领域technical field
本发明属于高温合金制备技术领域,特别涉及一种利用激光选区熔化技术制备NbSi超高温合金的方法。The invention belongs to the technical field of high-temperature alloy preparation, and in particular relates to a method for preparing NbSi super high-temperature alloy by using laser selective melting technology.
背景技术Background technique
随着高性能航空发动机、燃气涡轮机向着高流量比、高推重比、高进口温度方向发展,涡轮叶片等热端部件的工作温度不断提高,涡轮进口温度也在不断提升。目前,喷气发动机中使用的第三代镍基单晶高温合金的最高使用温度已经达到了1100~1150℃,接近该合金熔点的85%,再提升的潜力不大,因此迫切需要开发新型的结构材料。目前,难熔硅化物因其优异的综合性能,成为超高温结构材料研究领域的热点方向,而其中Nb-Si基超高温合金具有高熔点(>1750℃)、低密度(6.6-7.2g/cm3),良好的高温强度及一定的断裂韧性、疲劳性能和可加工性等优点,成为极具竞争力的新型高温金属结构材料之一。Nb-Si基合金由NbSS固溶体和金属间化合物Nb5Si3构成的,依靠高韧性的NbSS固溶体承受塑性变形,提高室温断裂韧性,依靠硬脆的硅化物相Nb5Si3承受高温下的机械载荷,提高高温强度。With the development of high-performance aero-engines and gas turbines in the direction of high flow ratio, high thrust-to-weight ratio, and high inlet temperature, the operating temperature of hot-end components such as turbine blades continues to increase, and the turbine inlet temperature also continues to increase. At present, the maximum service temperature of the third-generation nickel-based single crystal superalloy used in jet engines has reached 1100-1150 °C, which is close to 85% of the melting point of the alloy, and there is little potential for further improvement. Therefore, it is urgent to develop new structures. Material. At present, refractory silicides have become a hot spot in the research field of ultra-high temperature structural materials due to their excellent comprehensive properties, and among them, Nb-Si-based ultra-high temperature alloys have high melting point (>1750°C), low density (6.6-7.2g/ cm 3 ), good high-temperature strength, certain fracture toughness, fatigue performance and machinability, etc., has become one of the highly competitive new high-temperature metal structural materials. Nb-Si-based alloys are composed of Nb SS solid solution and intermetallic compound Nb 5 Si 3 , relying on high toughness Nb SS solid solution to withstand plastic deformation, improve room temperature fracture toughness, and rely on hard and brittle silicide phase Nb 5 Si 3 to withstand high temperature Mechanical load, improve high temperature strength.
近年来,NbSi超高温合金研究重点在合金设计和制备工艺方面。合金化设计主要是添加Ti、Al、Hf、Cr、铂系金属(Re,Ru等)、Wo、Ta、Mo、稀土元素(Ho、Dy、Y)、B、C、Ge、Zr、V、Sn、N、Fe、In。合金元素的加入可以显著改善其室温断裂韧性、高温蠕变强度以及高温抗氧化能力等性能之间的匹配。在制备工艺方面,Nb-Si基合金由于其熔点高,易氧化、含有脆性相以及大量的Ti和Hf等高活性元素,制备工艺受到很大的限制,目前主要有真空非自耗/自耗电弧熔炼、真空感应熔炼、定向凝固、粉末冶金和熔模铸造等。真空电弧熔炼得到的NbSi合金组织中往往存在成分偏析现象,容易出现粗大初生相、Nb3Si亚稳相以及裂纹等,氧含量和其它杂质含量较高,不利于高温结构材料的直接应用。粉末冶金NbSi合金时,在烧结及冷却产生的应力容易导致裂纹产生,从而影响合金的综合性能,烧结温度对合金组织的影响很大,烧结温度不同,所得产物的组织组成也不同,晶粒大小不同,组成相也可能不同(如Nb3Si相的出现);真空感应熔炼能保持合金成分均匀和高纯度,缺点是熔体温度不均匀,过热度低,容易形成浇铸不足等缺陷。定向凝固能消除大部分横向晶界,有效控制合金的微观组织和化学成分,并获得低缺陷的铸件,正逐渐成为制备铌硅超高温合金的主要工艺手段。但是传统的定向凝固缺点主要有:凝固过程冷却速率低,导致合金组织粗化并长大,限制了合金性能的提高,另外由于NbSi超高温合金中含有Hf、Ti等高温下化学活性很强的元素,因此在高温下非常容易与接触的坩埚发生界面反应,造成合金污染,含氧量增加,铸件夹杂增加,机械性能下降。熔模铸造Nb-Si基合金,其型壳承温能力将超过2000℃,然而目前用于高温结构材料熔模铸造的型壳承温能力多不超过1700℃,且在高温下与Nb-Si基合金发生反应,难以满足Nb-Si基合金熔模铸造成型要求。In recent years, the research of NbSi super high temperature alloy has focused on alloy design and preparation process. The alloying design is mainly to add Ti, Al, Hf, Cr, platinum group metals (Re, Ru, etc.), Wo, Ta, Mo, rare earth elements (Ho, Dy, Y), B, C, Ge, Zr, V, Sn, N, Fe, In. The addition of alloying elements can significantly improve the matching among properties such as room temperature fracture toughness, high temperature creep strength and high temperature oxidation resistance. In terms of preparation technology, due to its high melting point, easy oxidation, brittle phase, and a large amount of highly active elements such as Ti and Hf, the preparation technology of Nb-Si-based alloys is greatly limited. At present, there are mainly vacuum non-consumable/consumable Arc melting, vacuum induction melting, directional solidification, powder metallurgy and investment casting, etc. The structure of NbSi alloy obtained by vacuum arc melting often has composition segregation phenomenon, which is prone to coarse primary phase, Nb 3 Si metastable phase and cracks, etc., and the content of oxygen and other impurities is high, which is not conducive to the direct application of high temperature structural materials. When powder metallurgy NbSi alloy, the stress generated during sintering and cooling can easily lead to cracks, which will affect the overall performance of the alloy. Different, the composition phase may also be different (such as the appearance of Nb 3 Si phase); vacuum induction melting can maintain uniform composition and high purity of the alloy, but the disadvantages are uneven melt temperature, low superheat, and defects such as insufficient casting. Directional solidification can eliminate most of the transverse grain boundaries, effectively control the microstructure and chemical composition of the alloy, and obtain low-defect castings. It is gradually becoming the main process for preparing niobium-silicon superalloys. However, the disadvantages of traditional directional solidification mainly include: the low cooling rate during the solidification process, which leads to the coarsening and growth of the alloy structure, which limits the improvement of the alloy performance. Elements, so it is very easy to have interface reaction with the contacting crucible at high temperature, causing alloy pollution, increased oxygen content, increased casting inclusions, and decreased mechanical properties. For investment casting of Nb-Si based alloys, the shell temperature capacity will exceed 2000°C. However, the shell temperature capacity currently used for investment casting of high-temperature structural materials does not exceed 1700°C. It is difficult to meet the requirements of Nb-Si based alloy investment casting.
不仅如此,上述几种方法制备NbSi合金均需要坩埚或模具,很难直接制备具有特定尺寸和复杂结构(变截面、内腔或者冷却通道)的合金件,往往需要较多的机加工和后处理,工艺繁琐,生产效率低同时容易造成合金材料的浪费。因此,开发一种更加高效的制备Nb-Si基超高温合金的方法无疑是至关重要的。Not only that, the preparation of NbSi alloys by the above methods requires crucibles or molds, and it is difficult to directly prepare alloy parts with specific dimensions and complex structures (variable cross-sections, inner cavities or cooling channels), often requiring more machining and post-processing , the process is cumbersome, the production efficiency is low, and it is easy to cause waste of alloy materials. Therefore, it is undoubtedly crucial to develop a more efficient method for preparing Nb-Si-based superalloys.
发明内容Contents of the invention
本发明正是针对传统方法制备NbSi基超高温合金存在的问题,提供了一种激光选区熔化技术(Selective Laser Melting,SLM)快速制备NbSi基超高温合金的方法。The present invention is aimed at the problems existing in the preparation of NbSi-based super high-temperature alloys by traditional methods, and provides a method for rapidly preparing NbSi-based super high-temperature alloys by selective laser melting technology (Selective Laser Melting, SLM).
激光选区熔化(SLM)技术是将激光熔覆与快速原型(rapid prototyping)技术结合起来的一种最新的先进制造技术。SLM能够实现三维复杂结构零部件的无模具、高性能的快速制备。其过程主要为:利用计算机得到零部件的三维CAD实体模型,然后利用分层软件在部件高度方向进行分层切片,并将部件的三维轮廓信息转化为二维轮廓信息,并生成扫描路径。激光束按照指定的扫描路径逐层熔化沉积金属或合金粉末,堆积形成三维实体零件。经过材料及工艺优化,一次成形的致密度可高于95%,成形合金可直接满足工业需求。SLM技术适用于难加工、高性能难熔金属和合金的制备。Selective laser melting (SLM) technology is the latest advanced manufacturing technology that combines laser cladding and rapid prototyping (rapid prototyping) technology. SLM can realize the mold-free and high-performance rapid preparation of three-dimensional complex structural parts. The main process is: use the computer to obtain the three-dimensional CAD solid model of the part, and then use the layering software to slice in the height direction of the part, convert the three-dimensional contour information of the part into two-dimensional contour information, and generate a scanning path. The laser beam melts and deposits metal or alloy powder layer by layer according to the specified scanning path, and accumulates to form a three-dimensional solid part. After material and process optimization, the density of one-time forming can be higher than 95%, and the formed alloy can directly meet the industrial needs. SLM technology is suitable for the preparation of difficult-to-machine, high-performance refractory metals and alloys.
本发明利用SLM技术制备NbSi超高温合金的技术方案是:The technical scheme that the present invention utilizes SLM technology to prepare NbSi super high temperature alloy is:
采用氩气雾化法制备的预合金化NbSi超高温合金粉末,NbSi粉末呈球形或近球形,直径在10~60μm之间。随后利用选区激光熔化(selective laser melting,SLM)工艺对Nb-Si合金粉末进行快速成形制备。设定合理的激光成形参数(激光功率、激光束扫描速度、扫描间距和铺粉厚度),利用高能激光束使NbSi合金粉末熔化。此外,在选区激光熔化工艺中,粉末熔化/凝固极快,冷却速度极高(105~106K/s),因此可以制备得到细小、均匀、稳定的快速凝固合金组织,从而获得力学性能优异的NbSi超高温合金零件。Pre-alloyed NbSi super high temperature alloy powder prepared by argon atomization method, the NbSi powder is spherical or nearly spherical, and the diameter is between 10 and 60 μm. Then, the Nb-Si alloy powder was prepared by rapid prototyping by selective laser melting (SLM) process. Set reasonable laser forming parameters (laser power, laser beam scanning speed, scanning distance and powder coating thickness), and use high-energy laser beam to melt NbSi alloy powder. In addition, in the selective laser melting process, the powder melts/solidifies extremely fast and the cooling rate is extremely high (10 5 ~ 10 6 K/s), so a fine, uniform and stable rapid solidification alloy structure can be prepared to obtain mechanical properties Excellent NbSi superalloy parts.
本发明利用SLM技术制备NbSi超高温合金的方法,制备过程具体包括以下步骤:The present invention utilizes SLM technology to prepare the method for NbSi super high temperature alloy, and the preparation process specifically comprises the following steps:
(1)利用电脑设计出零件的三维CAD模型,并用切片软件对模型在高度方向上进行分层切片离散化处理,切片厚度均匀(0.03~0.1mm),且包含零件的横截面轮廓信息和激光加工路径,将多层切片信息并保存为STL文件,并传输到SLM激光选区熔化系统;(1) Use the computer to design the 3D CAD model of the part, and use the slicing software to discretize the model in the height direction. Processing path, save multi-layer slicing information as an STL file, and transmit it to the SLM laser melting system;
(2)将成形基板固定在可升降的工作台上,密封装置抽真空后充入高纯氩气(99.99%)进行气氛保护,送粉系统在基板上均匀铺一层厚度为0.03~0.1mm的待加工NbSi超高温合金粉末;(2) Fix the forming substrate on the liftable workbench, vacuumize the sealing device and fill it with high-purity argon (99.99%) for atmosphere protection. The powder feeding system evenly spreads a layer with a thickness of 0.03-0.1mm on the substrate NbSi ultra-high temperature alloy powder to be processed;
(3)激光束按照预先设定的扫描路径,选择性的对基板上的粉末进行扫描,粉末熔化并凝固,形成熔覆层;具体的制备参数:激光器功率350~500W,扫描速度200~400mm/s,扫描间距0.05~0.15mm;(3) The laser beam selectively scans the powder on the substrate according to the preset scanning path, and the powder melts and solidifies to form a cladding layer; specific preparation parameters: laser power 350-500W, scanning speed 200-400mm /s, scanning distance 0.05~0.15mm;
(4)完成一个层面扫描后,基板下降一个层厚的距离,并在先熔覆层上再均匀铺上一层厚度为0.03~0.1mm的NbSi合金粉末;(4) After completing a layer scan, the substrate is lowered by a layer thickness, and a layer of NbSi alloy powder with a thickness of 0.03-0.1mm is evenly spread on the first cladding layer;
(5)重复上述(3)-(4)步骤,直至NbSi基超高温合金加工完成;(5) Repeat the above steps (3)-(4) until the processing of the NbSi-based ultra-high temperature alloy is completed;
本发明中,制备NbSi超高温合金采用Ti6Al4V成形基板,基板厚度为10mm;In the present invention, the Ti6Al4V forming substrate is used to prepare the NbSi super high temperature alloy, and the thickness of the substrate is 10mm;
本发明中采用氩气雾化制备粉末和SLM工艺相结合的方法制备NbSi超高温合金,粉末与激光束的相互作用不同于其它传统的粉末冶金工艺过程,其熔化/凝固行为区别于传统方法。此技术方案主要优点在于:In the present invention, the combination of argon atomization powder preparation and SLM process is used to prepare NbSi super high temperature alloy. The interaction between powder and laser beam is different from other traditional powder metallurgy processes, and its melting/solidification behavior is different from traditional methods. The main advantages of this technical solution are:
(1)SLM技术利用激光束逐层沉积NbSi超高温合金粉末,直接由CAD模型一步完成NbSi合金的制备。制备过程无需准备坩埚、模具或粉末包套等,减少尺寸误差;SLM技术可以有效的避免高温合金与坩埚、模具等的界面反应,减少合金污染,降低夹杂含量;SLM过程有氩气气氛保护,对高温状态的NbSi合金具有保护效果,有效避免合金的氧化,提高合金的综合性能。(1) SLM technology uses laser beams to deposit NbSi ultra-high temperature alloy powder layer by layer, and directly completes the preparation of NbSi alloy in one step from the CAD model. The preparation process does not need to prepare crucibles, molds or powder jackets, etc., reducing dimensional errors; SLM technology can effectively avoid interface reactions between superalloys and crucibles, molds, etc., reduce alloy pollution, and reduce inclusion content; the SLM process is protected by argon atmosphere, It has a protective effect on the NbSi alloy in high temperature state, effectively avoids the oxidation of the alloy, and improves the comprehensive performance of the alloy.
(2)SLM技术制备超高温NbSi合金过程中,粉末熔化时液相熔池温度极高、尺寸很小、凝固时间极短,因此冷却速度极高(105~106K/s),为高度非平衡凝固,凝固时间极短,能有效减少NbSi超高温合金的微观偏析,而且合金致密度较传统粉末冶金工艺更高,具有细小、均匀、稳定的快速凝固组织,从而获得力学性能优异的NbSi超高温合金零件;(2) During the preparation of ultra-high temperature NbSi alloys by SLM technology, when the powder is melted, the temperature of the liquid phase molten pool is extremely high, the size is small, and the solidification time is extremely short, so the cooling rate is extremely high (10 5 ~ 10 6 K/s), which is High non-equilibrium solidification, extremely short solidification time, can effectively reduce the micro-segregation of NbSi ultra-high temperature alloy, and the alloy density is higher than the traditional powder metallurgy process, with a small, uniform and stable rapid solidification structure, so as to obtain excellent mechanical properties NbSi ultra-high temperature alloy parts;
(3)SLM适用于制备各种复杂结构的NbSi的合金部件,尤其是内部具有复杂异型结构(空腔、冷却通道),传统方法无法制造的合金部件;制备NbSi合金工艺简单快速、免去了设计与制造模具过程,避免了传统的机加工和后处理,节省人力物力;同时未加工、多余的NbSi预合金粉末可以回收重复利用,材料利用率高;(3) SLM is suitable for the preparation of NbSi alloy parts with various complex structures, especially alloy parts with complex special-shaped structures (cavity, cooling channel) inside, which cannot be manufactured by traditional methods; the preparation process of NbSi alloy is simple and fast, eliminating the need for The process of designing and manufacturing molds avoids traditional machining and post-processing, saving manpower and material resources; at the same time, unprocessed and redundant NbSi pre-alloyed powders can be recycled and reused, and the material utilization rate is high;
(4)利用SLM技术成形的NbSi超高温合金致密度高,合金主要由Nbss固溶体和Nb5Si3强化相组成,分布均匀,相尺寸极其细小(小于1μm),达到纳米尺度,远小于传统方法制备得到相尺寸。SLM得到的这种组织特征可以提高NbSi合金的综合力学性能。(4) The NbSi ultra-high temperature alloy formed by SLM technology has high density. The alloy is mainly composed of Nbss solid solution and Nb 5 Si 3 strengthening phase, which is evenly distributed, and the phase size is extremely small (less than 1 μm), reaching the nanometer scale, which is much smaller than the traditional method Prepare the phase size. The microstructure characteristics obtained by SLM can improve the comprehensive mechanical properties of NbSi alloy.
附图说明:Description of drawings:
附图1 SLM技术成形Nb-18Si-24Ti-2Cr-2Al-2Hf合金XRD图谱;Figure 1 XRD pattern of Nb-18Si-24Ti-2Cr-2Al-2Hf alloy formed by SLM technology;
附图2 SLM技术成形Nb-18Si-24Ti-2Cr-2Al-2Hf合金扫描电镜图片;Accompanying drawing 2 is the SEM image of Nb-18Si-24Ti-2Cr-2Al-2Hf alloy formed by SLM technology;
附图3 SLM技术成形Nb-16Si-22Ti-4Cr-2Al-2Hf合金XRD图谱;Figure 3 is the XRD pattern of Nb-16Si-22Ti-4Cr-2Al-2Hf alloy formed by SLM technology;
附图4 SLM技术成形Nb-16Si-22Ti-4Cr-2Al-2Hf合金扫描电镜图片。Accompanying drawing 4 SLM technology forming Nb-16Si-22Ti-4Cr-2Al-2Hf alloy scanning electron microscope pictures.
具体实施方式detailed description
以下结合实例对本发明做进一步阐述,但本发明并不局限于具体实施例。The present invention is described further below in conjunction with example, but the present invention is not limited to specific embodiment.
实施例1Example 1
利用SLM技术制备Nb-18Si-24Ti-2Cr-2Al-2Hf(at.%,原子百分比)超高温合金:使用的SLM激光选区熔化系统主要包括:Nd-YAG激光器、用于成形控制的计算机系统、送粉系统和氩气气氛保护装置;Using SLM technology to prepare Nb-18Si-24Ti-2Cr-2Al-2Hf (at.%, atomic percentage) super high temperature alloy: the SLM laser selective melting system used mainly includes: Nd-YAG laser, computer system for forming control, Powder feeding system and argon atmosphere protection device;
1.选用利用氩气雾化法制备的Nb-18Si-24Ti-2Cr-2Al-2Hf预合金化粉末,粉末成球形或近球形,直径在10~60μm之间;1. Select Nb-18Si-24Ti-2Cr-2Al-2Hf pre-alloyed powder prepared by argon atomization method, the powder is spherical or nearly spherical, and the diameter is between 10 and 60 μm;
2.根据待加工合金零件形状,利用电脑建立三维CAD模型,并用切片软件在模型高度方向上进行分层切片离散化处理,切片厚度均匀(厚度均为0.05mm),且包含待加工零件的横截面轮廓信息和扫描加工路径,将多层切片信息并保存为STL文件,并传输到SLM激光选区熔化系统中;2. According to the shape of the alloy parts to be processed, use the computer to establish a three-dimensional CAD model, and use the slicing software to perform layered slice discretization in the height direction of the model. Section profile information and scanning processing path, save multi-layer slice information as STL file, and transfer to SLM laser melting system;
3.将粉末装入成形腔中,将厚度为10mm的Ti6Al4V成形基板固定在可升降的工作台上;密封的成形腔首先抽真空,然后冲入高纯氩气(99.99%)进行保护。利用送粉系统在基板上均匀铺一层厚度为0.05mm的Nb-18Si-24Ti-2Cr-2Al-2Hf超高温合金粉末;3. Put the powder into the forming cavity, and fix the Ti6Al4V forming substrate with a thickness of 10mm on the liftable workbench; the sealed forming cavity is first evacuated, and then flushed with high-purity argon (99.99%) for protection. Use the powder feeding system to evenly spread a layer of Nb-18Si-24Ti-2Cr-2Al-2Hf ultra-high temperature alloy powder with a thickness of 0.05mm on the substrate;
4.激光束按照预先设定的扫描路径和制备参数,对基板上的预置好的粉末进行扫描,粉末熔化并凝固,形成熔覆层;具体的制备参数:激光器功率400W,扫描速度250mm/s,扫描间距0.10mm;4. The laser beam scans the preset powder on the substrate according to the preset scanning path and preparation parameters, and the powder melts and solidifies to form a cladding layer; specific preparation parameters: laser power 400W, scanning speed 250mm/ s, scanning distance 0.10mm;
5.完成一个层面扫描后,基板下降一个层厚的距离,并在先熔覆层上再均匀铺上一层厚度为0.05mm的Nb-18Si-24Ti-2Cr-2Al-2Hf合金粉末;5. After completing a layer scan, the substrate is lowered by a layer thickness, and a layer of Nb-18Si-24Ti-2Cr-2Al-2Hf alloy powder with a thickness of 0.05mm is evenly spread on the first cladding layer;
6.重复上述(5)、(6)步骤,直至Nb-18Si-24Ti-2Cr-2Al-2Hf超高温合金件加工完成,然后关闭系统,待部件冷却至室温时取出;整个制备过程是在氩气保护气氛中进行的;6. Repeat the above steps (5) and (6) until the Nb-18Si-24Ti-2Cr-2Al-2Hf ultra-high temperature alloy parts are processed, then shut down the system, and take them out when the parts are cooled to room temperature; the whole preparation process is carried out under argon Carried out in a protective atmosphere;
由附图1可以看出,SLM成形Nb-18Si-24Ti-2Cr-2Al-2Hf合金组织主要由NbSS固溶体和Nb5Si3两相组成。浅色相为Nbss固溶体,深色相为Nb5Si3相。It can be seen from Figure 1 that the structure of the Nb-18Si-24Ti-2Cr-2Al-2Hf alloy formed by SLM is mainly composed of Nb SS solid solution and Nb 5 Si 3 phases. The light phase is Nbss solid solution, and the dark phase is Nb 5 Si 3 phase.
由附图2可以看出,SLM成形Nb-18Si-24Ti-2Cr-2Al-2Hf合金致密度高,没有裂纹产生。Nbss相和Nb5Si3相的尺寸极其细小(<1μm),达到纳米相程度,而且两相分布均匀,呈现明显的快速凝固组织特征,可以提高NbSi超高温合金的综合性能。It can be seen from Figure 2 that the SLM formed Nb-18Si-24Ti-2Cr-2Al-2Hf alloy has high density and no cracks. The size of Nbss phase and Nb 5 Si 3 phase is extremely small (<1 μm), reaching the level of nano phase, and the two phases are evenly distributed, showing obvious characteristics of rapid solidification structure, which can improve the comprehensive performance of NbSi super high temperature alloy.
实施例2Example 2
利用SLM技术制备Nb-16Si-22Ti-4Cr-2Al-2Hf(at.%,原子百分比)超高温合金:使用的SLM激光选区熔化系统主要包括:Nd-YAG激光器、用于成形控制的计算机系统、送粉系统和氩气气氛保护装置;Using SLM technology to prepare Nb-16Si-22Ti-4Cr-2Al-2Hf (at.%, atomic percentage) super high temperature alloy: the SLM laser selective melting system used mainly includes: Nd-YAG laser, computer system for forming control, Powder feeding system and argon atmosphere protection device;
1.选用利用氩气雾化法制备的Nb-16Si-22Ti-4Cr-2Al-2Hf预合金化粉末,粉末成球形或近球形,直径在10~60μm之间;1. Select Nb-16Si-22Ti-4Cr-2Al-2Hf pre-alloyed powder prepared by argon atomization method, the powder is spherical or nearly spherical, and the diameter is between 10 and 60 μm;
2.根据待加工合金零件形状,利用电脑建立三维CAD模型,并用切片软件在模型高度方向上进行分层切片离散化处理,切片厚度均匀(厚度均为0.08mm),且包含待加工零件的横截面轮廓信息和扫描加工路径,将多层切片信息并保存为STL文件,并传输到SLM激光选区熔化系统中;2. According to the shape of the alloy parts to be processed, use the computer to establish a three-dimensional CAD model, and use the slicing software to perform layered slice discretization in the height direction of the model. Section profile information and scanning processing path, save multi-layer slice information as STL file, and transfer to SLM laser melting system;
3.将粉末装入成形腔中,将厚度为10mm的Ti6Al4V成形基板固定在可升降的工作台上,密封的成形腔首先抽真空,然后冲入高纯氩气(99.99%)进行保护。利用送粉系统在基板上均匀铺一层厚度为0.08mm的Nb-16Si-22Ti-4Cr-2Al-2Hf超高温合金粉末;3. Put the powder into the forming cavity, and fix the Ti6Al4V forming substrate with a thickness of 10mm on the liftable workbench. The sealed forming cavity is first evacuated, and then flushed with high-purity argon (99.99%) for protection. Use the powder feeding system to evenly spread a layer of Nb-16Si-22Ti-4Cr-2Al-2Hf ultra-high temperature alloy powder with a thickness of 0.08mm on the substrate;
4.激光束按照预先设定的扫描路径和制备参数,对基板上的预置好的粉末进行扫描,粉末熔化并凝固,形成熔覆层;具体的制备参数:激光器功率400W,扫描速度300mm/s,扫描间距0.06mm;4. The laser beam scans the preset powder on the substrate according to the preset scanning path and preparation parameters, and the powder melts and solidifies to form a cladding layer; specific preparation parameters: laser power 400W, scanning speed 300mm/ s, scanning distance 0.06mm;
5.完成一个层面扫描后,基板下降一个层厚的距离,并在先熔覆层上再均匀铺上一层厚度为0.08mm的Nb-16Si-22Ti-4Cr-2Al-2Hf合金粉末;5. After completing a layer scan, the substrate is lowered by a layer thickness, and a layer of Nb-16Si-22Ti-4Cr-2Al-2Hf alloy powder with a thickness of 0.08mm is evenly spread on the first cladding layer;
6.重复上述(5)、(6)步骤,直至Nb-16Si-22Ti-4Cr-2Al-2Hf超高温合金件加工完成,然后关闭系统,待部件冷却至室温时取出;整个制备过程是在氩气保护气氛中进行的;6. Repeat the above steps (5) and (6) until the Nb-16Si-22Ti-4Cr-2Al-2Hf ultra-high temperature alloy parts are processed, then shut down the system and take them out when the parts are cooled to room temperature; the whole preparation process is carried out under argon Carried out in a protective atmosphere;
由附图3和附图4可以看出,SLM成形Nb-16Si-22Ti-4Cr-2Al-2Hf合金致密度高,存在少量气孔(尺寸<1μm),没有空隙和热裂纹等缺陷。成形合金由纳米尺度Nbss相和Nb5Si3相组成(浅色相为Nbss固溶体,深色相为Nb5Si3相),尺寸极其细小(<1μm),而且两相分布均匀,呈现明显的快速凝固组织特征,可以提高NbSi超高温合金的综合性能。It can be seen from Figure 3 and Figure 4 that the SLM formed Nb-16Si-22Ti-4Cr-2Al-2Hf alloy has high density, a small amount of pores (size <1μm), and no defects such as voids and hot cracks. The formed alloy is composed of nanoscale Nb ss phase and Nb 5 Si 3 phase (the light-colored phase is Nbss solid solution, and the dark-colored phase is Nb 5 Si 3 phase), the size is extremely small (<1 μm), and the two phases are evenly distributed, showing obvious The characteristics of rapid solidification structure can improve the comprehensive performance of NbSi super high temperature alloy.
以上所述仅为本发明的优选实施例,并非因此限制本发明的专利范围,凡是利用本发明说明书内容所作的等效结构或等效流程变换,或直接或间接运用在其他相关的技术领域,均同理包括在本发明的专利保护范围内。The above is only a preferred embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process conversion made by using the content of the description of the present invention, or directly or indirectly used in other related technical fields, All are included in the scope of patent protection of the present invention in the same way.
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